A lever balance mode structure energy storage endogenous force and load force interaction dynamic system

Abstract

The application discloses a rod scale mode structure energy storage endogenous force and load force interaction power system, which is a kind of device that is physically symmetrical to link endogenous force components in the left / right point of the rod scale mode scale rod fulcrum area and link load force components in the right / left point of the fulcrum area, and is configured as a structure energy storage mode endogenous force interaction device formed by the action force in the left / right point of the fulcrum area and the reaction force formed by the load force in the right / left point of the fulcrum area. The endogenous force with specific properties is configured as a structure energy storage mode in a specific scenario, the rod scale fulcrum is formed by linking the specific point of the scale rod with the rod scale, and the bearing endogenous force component is fixed in the left / right point of the scale rod fulcrum area. The left and right fixed bearing points respectively form the force arm value, and the balance of the action force and the reaction force is realized by respectively regulating the bearing force point or the single-side action force of the left / right side of the scale rod fulcrum in the static and unbalanced dynamic transition process of the scale rod, and there is no material, gas emission and scattering characteristics.

Description

Technical Field

[0001] This invention relates to a lever scale mechanism in the field of physics and mechanics, which involves the interaction and correlation of the forces of the left / right assisting forces and the structural energy storage endogenous forces of the lever fulcrum, and the reaction forces of the loads on the right / left sides of the fulcrum, to provide a rotary dynamic system that drives the load components to perform work. Background Technology

[0002] In their daily lives and activities, humans have discovered many regular and reproducible phenomena in nature. Through continuous exploration, they have summarized numerous patterns that can be learned from, developed tools to easily resolve and solve difficulties and problems that cannot be overcome by their own abilities in daily life and activities, and created instruments to realize their aspirations. The steelyard balance is a landmark instrument invented by humans in civilized society by applying the principles of physical symmetry.

[0003] The lever is connected to the horizontal axis through a specific part of the weighing beam. Utilizing the principle and formula of the physical symmetry and interaction of gravity on both sides of the axis, the lever scale can achieve movement according to the user-designed stroke and trajectory by setting or modifying the specific gravity value of an object in the weighing pan on one side of the horizontal axis, or by modifying the gravity value of the weighing hammer set on the other side; or by using the horizontal axis of the weighing beam as the center of convergence of gravity on both sides, the lever scale can achieve movement according to the user-designed stroke and trajectory by moving the part of the weighing pan connected to the weighing beam or the part of the weighing hammer distributed on the weighing beam. The weighing beam connecting axis can also show synchronous, same rotation direction and same rotation angle as the weighing beam.

[0004] Accordingly, the horizontal axis connecting the weighing beam is defined as the fulcrum axis of the weighing beam's movement. If the weighing pan and load-bearing frame on one side of the fulcrum axis are designed as a symmetrical structure with a quantified weight weight connected to the fulcrum axis, by changing the weight value of the weight weight on the other side or moving the weight weight's position on the weighing beam, the load force connected to the fulcrum axis and the weight weight of the weight weight become physically symmetrical, and the left and right sides of the fulcrum axis of the weighing beam enter an interactive state. Similarly, if the input external force is added to the weight weight of the weight weight positioned on the left or right side of the fulcrum axis as a force, it can also affect or change the trajectory and angle of the weighing beam's rotational motion. Thus, a relatively small input assistance can be used to drive the movement of a relatively large load-bearing component connected to the fulcrum axis. Summary of the Invention

[0005] The purpose of this invention is to provide a dynamic system for the interaction between the endogenous energy storage force and the load force in a lever balance structure, so as to solve the problems mentioned in the background art.

[0006] To solve the above-mentioned technical problems, the present invention provides the following technical solutions:

[0007] I. System Overview

[0008] The structural unit of the dynamic system in this lever scale mode is attached, showing the physical symmetric interaction between the intrinsic force and the load force.Figure 1 The unit DY is a reciprocating rotary motion unit that interacts with the force variables at specific node points on both sides of the fulcrum of the scale beam; the dual-unit DY output mechanism intermittently reciprocates and alternates counterclockwise and clockwise rotational dynamics to shape, converge and relay force, and drive the load mechanism to perform work.

[0009] The unit DY structure has space to configure endogenous force NS“F” type modules adapted to specific operating scenarios. The endogenous force NS“F” modules are assigned values ​​at specific points on the left and right sides of the three support axes of the scale lever through the link interface, and can be driven by the input cooperative force to reverse symmetrically.

[0010] The force XL, which is synthesized from the input controllable assist and the endogenous force NS "F" value side of the fulcrum bearing a large proportion, forms a physical symmetry and interacts with the load reaction force. When the force XL is greater than the load reaction force, the weighing rod 3 and the meshing fulcrum shaft 18 rotate. The rotating fulcrum shaft 18 presents and outputs intermittent reciprocating alternating counterclockwise and clockwise rotational dynamic driving force to drive the load mechanism.

[0011] ① Unit DY structure attachment Figure 2 The left and right ends of the weighing rod 3 on both sides of the fulcrum shaft 18, which serves as the fulcrum, are respectively equipped with ratchet gears 14 and 13 or chain guide wheels J11 that are subjected to counterclockwise and clockwise forces.

[0012] ①-1. The two ends of the screw component 4 are connected to the bearing inner rings configured in the positioning components J7z and J7y.

[0013] 4. The threads engage with the internal threads of the reversing motion components 10z and 10y, which are located to the left and right of the positioning component J7(0) of the positioning reversing gear J5; (see Appendix) Figure 19 )

[0014] ①-2. The internal force "F" bearing components 10z and 10y are respectively connected and fixed to the left (front, rear) column J8-(2, 1) and the right (front, rear) column J8-(3, 4). (See appendix) Figure 20 )

[0015] ② The endogenous force NS“F” generated within the J2-1-4 frame of the endogenous force module compartment of unit DY is suspended or pulled by the power bearing wheel J11(y0) of the connecting structure via zipper 29. It is then assigned to the physically symmetrical bearing components 12z and 12y at specific node positions of the weighing beam 3 via chain J16, forming an interconnected and interactive body with specific dynamic dynamics. (See appendix) Figure 30 )

[0016] ③ By combining, matching, and arranging specific types of components, a component or module structure with controllable motion direction, trajectory, and stroke can be formed to achieve specific functions and performance. This enables the controllable assistance of the interface component 39wk-1 in a specific scenario domain to be combined with the controllable time-sequence intermittent mode or gapless endogenous force NS“F” to form force XL. This force is then applied in a physically symmetrical mode to the load-bearing components 12z and 12y connected to the 1 / 3 node position at the center of the scale bar, and their values ​​are assigned and their direction is reversed.

[0017] ④ Through the transformation of the variables of the force XL in the physical symmetry within the domain, the variables interact and correlate according to the physical and mechanical laws of the relevant fields. The multi-faceted fulcrum shaft 18 of the center multi-faceted inner hole 1 / 3 of the lever arm 3 of the lever assembly randomly outputs the unit DY dynamic shape of reciprocating alternating counterclockwise and clockwise intermittent rotation.

[0018] ⑤ A dual-unit dynamic system with interaction between the left / right force XL of the lever 3 and the load in a physically symmetrical mode. (See appendix) Figure 2 )

[0019] ⑥ The two units DY-(1,2) are each converted to the same rotation angle as the controllable assist input by the interface component 39wk-1 through the power dynamic conversion component Dxzh-(1,2), and the clockwise and counterclockwise rotation power dynamics are output by the interface component 18ds-(1,2).

[0020] ⑦ The dual-unit rotating power dynamic interface 18ds-(1,2) outputs converge and relay, and the interface components 39jh-(1,2) synchronously output clockwise and counterclockwise continuous power dynamics.

[0021] ⑧. Based on the power dynamic requirements of the load components, in the dual-unit convergence system of the lever scale power symmetry mode, select the clockwise and counterclockwise continuously rotating power dynamic output interface component 39jh-(1 or 2) that matches the load interface to connect the power load interface component 39qd.

[0022] II. The timing sequence of the transition process of the counterclockwise-clockwise intermittent rotational motion within the power unit domain, which is influenced by the interaction between the input controllable assistance and the endogenous force NS“F” acting on the lever 3 of the lever scale through the link and the physically symmetrical load reaction force.

[0023] 2.1 The endogenous force NS "F" of the physical symmetric interaction dynamic unit in the lever balance mode is assigned to parts 12z and 12y respectively according to the distances from the bearing parts 12z and 12y to the vertical center of the fulcrum axis.

[0024] ① The physical symmetry mechanism of the lever scale in unit DY involves the engagement of the inner hole 1 / 3 of the polyhedral core at the center of the lever 3 with the polyhedral fulcrum axis 18. The lever 18 serves as the left-right physical fulcrum, forming an interactive mechanism where the lever 3 and the fulcrum axis 18 rotate synchronously in the same direction. (See appendix) Figure 3 )

[0025] ② The connecting power bearing components 12y and 12z of the weighing beam 3 are subject to J2-1-22 (see appendix). Figure 68 The externally controlled micro-force drive, via the link input, drives the bearing component 12y to approach ya|45|° from the origin, or the bearing component 12z to approach za|45|° from the stationary point. The internal force NS“F” ratio x0% borne by the symmetrical components 12y…12z on the left and right sides of the scale bar 3 will randomly increase, decrease, or even be converted. That is, if the internal force NS“F” borne by 12z is XX%, while the internal force NS“F borne by the symmetrical 12y is “1-XX%” (i.e., xx%), after conversion, the internal force NS“F borne by 12z is “1-XX%” (i.e., xx%), while the internal force NS“F borne by the symmetrical 12y is XX%.

[0026] ③ Stroke a: The intrinsic force NS "F" value XX% acts on the load-bearing component 12z on the left side of the center of the fulcrum shaft 18, which approaches the static point za|45|°. The intrinsic force NS "F" value XX% of 12z is less than the weak force formed by the load force of the load-bearing component NS "F" value xx% of 12y plus the input controllable assist. When the combined force XL of the intrinsic force NS "F" value XX% of 12z plus the input controllable assist is greater than or equal to the load force of the load-bearing component 12y on the right side of the center of the fulcrum shaft 18 plus the input controllable assist, the load-bearing component 12z of the scale lever 3 rotates counterclockwise by approximately 90° towards the static point zb|45|°, and the input controllable assist is "0".

[0027] ④ Stroke b: The bearing component 12z reaches the left horizontal stationary point zb|45|° of the center of the fulcrum shaft 18. When the external control micro force drives the screw component 4 to rotate, it drives the bearing component 12z connected to the weighing beam 3 to move linearly from the stationary point zb|45|° to the stationary point ya|45|°. The bearing component 12y on the right side approaches the stationary point ya|45|°.

[0028] ⑤ Stroke c: The intrinsic force NS "F" value XX% acts on the load-bearing component 12y on the right side of the center of the fulcrum shaft 18, approaching the static point ya|45|°. The intrinsic force NS "F" value XX% of 12y is less than the weak force formed by the load force of the load-bearing component NS "F" value xx% of 12z plus the input controllable assist. When the combined force XL of the intrinsic force NS "F" value XX% of 12y plus the input controllable assist is greater than or equal to the load force of the load-bearing component 12z on the left side of the center of the fulcrum shaft 18 plus the input controllable assist value xx%, the load-bearing component 12y of the scale lever 3 related body rotates clockwise approximately 90° towards the static point yb|45|°. The input controllable assist is "0".

[0029] ⑥ Stroke d: The bearing component 12y reaches the horizontal right static point yb|45|° of the center of the fulcrum shaft 18. When the external control micro force drives the screw component 4 to rotate in the opposite direction, it drives the bearing component 12y connected to the weighing beam 3 to move linearly from the static point yb|45|° to the static point za|45|°. The bearing component 12z on the left side approaches the static point za|45|°.

[0030] ⑦ The ratio of rotational to lateral motion time in the unit DY lever scale mode is: 10

t(a, c): 0...10)

t(b, d): (0...6)

[0031] II.2 Physical Symmetrical Lever Scale Mode: The endogenous force NS "F" is assigned symmetrically on the left and right sides, and the combined force XL of the external control assist drives the lever 3 of the lever scale to rotate, load change direction... the static point - moving point trajectory - motion stroke - static point reciprocating motion power unit DY-1 running sequence and stroke (a) state. (See Appendix) Figure 4 )

[0032] The lever 3 and associated components of a unit DY-1 lever scale are symmetrically supported by the fulcrum axis 18. The associated load-bearing components 12z are configured to move or be controlled to approach the za|45|° static point.

[0033] Another unit, the DY-2 lever scale, has a lever 3 and associated components with fulcrum axis 18 as the left and right symmetrical fulcrums. The associated load-bearing components 12y are configured to move or be controlled to approach the ya|45|° static point.

[0034] Unit DY-1 carries component 12z, which forms the intersection of the associated interactive body J11||13z and the chain J16; and carries component 12y, which forms the intersection of the associated interactive body J11||14y and the chain J16.

[0035] ① When the endogenous force "F" carried by unit DY-1{12z and J11||13z is input by component 39wk-1 and acts on the external control assist domain of the fulcrum shaft 18 - The force XL of the intrinsic force "F" of bearing 12y and J11||14y is greater than the load force of the fulcrum shaft 18, and DY-1 enters the transition process. Transitional journey within the domain The weighing beam 3 and its associated components rotate counterclockwise synchronously with the fulcrum shaft 18. The load-bearing component 12z approaches the static point zb|45|°.

[0036] ②, in Intra-domain transition journey When the endogenous force "F"+ borne by another unit DY-2{12y and J11||14y is input by the 39wk-1 component and acts on the external control assist domain of the fulcrum shaft 18 - The force XL of the intrinsic force "F" carried by 12z and J11||13z is greater than the load force of the fulcrum shaft 18, and DY-2 enters the transition process. Transitional journey within the domain The weighing beam 3 and its associated components rotate clockwise synchronously with the fulcrum shaft 18. The load-bearing component 12y approaches the static point zb|45|°.

[0037] II. 3. The intrinsic force NS "F" of the physical symmetrical lever scale mode is symmetrically assigned on the left and right sides, and the force XL, which is combined with the external control assist, drives the lever scale 3 to rotate, load change direction... the static point - moving point trajectory - motion stroke - static point reciprocating motion power unit DY-1 running sequence and stroke (b) state. (See appendix) Figure 5 ).

[0038] The beam 3 of the DY-1 lever scale rotates counterclockwise, and the associated connecting bearing component 12z rotates counterclockwise as well. Arrive at the near point zb|45|°.

[0039] ① In another unit, the DY-2 scale bar 3 and the load-bearing mechanism 12y rotate clockwise with the fulcrum shaft 18. Transitional travel within the region The DY-1 unit is subjected to a slight external force 12wk-1 from the J2-1-22 component. domain.

[0040] ② The load-bearing component 12z, which is connected to the weighing beam 3 of the DY-1 dynamic symmetrical mechanism, moves linearly from the stationary point zb|45|° to the stationary point ya|45|° under the drive of the external control micro-force 12wk-1 of the mechanism at the J2-1-22 location, following the synchronous rotation of the follower gear 30, gear 1 / 5, and screw 4. The load-bearing component 12y also transitions through another unit-2. Transitional travel within the region Unit DY-1 Transition Stroke Arrive at the point of rest at approximately 45°.

[0041] II. 4. The intrinsic force NS "F" of the physical symmetrical lever scale mode is symmetrically assigned left and right, and the force XL, which is combined with the external control assist, drives the lever scale 3 to rotate, load change direction... the static point - moving point trajectory - motion stroke - static point reciprocating motion power unit DY-1 running sequence and stroke (c) state. (See appendix) Figure 6 )

[0042] The DY-1 lever scale's lever J3 and associated components are symmetrically supported by pivot axis 18. The associated link bearing component 12y is configured to move in a controlled linear motion to reach the near point ya|45|° of the stationary point.

[0043] ① During the transition process of unit DY-2 Transitional journey within the domain When the internal force "F" at the intersection point of unit DY-1 {bearing component 12y forming the interconnected interactive body J11||14y and chain J16 is input by component 39wk-1 and acts on the external control assist domain of the fulcrum axis 18, - The internal force XL at the intersection point of J11||13z and chain J16, which forms an interactive mechanism with the load-bearing component 12z, is greater than the load force of the fulcrum shaft 18. The load-bearing component 12y transitions from the static point ya|45|° near point into the domain. Transitional travel Synchronous clockwise rotation 12 years in the transition period Approaching the static point yb|45|°.

[0044] ② In unit DY-1 Transitional journey within the domain Another unit, DY-2, has a physically symmetrical lever scale whose lever 3 is linked to a load-bearing component 12y. This component 12wk-1 at its J2-1-22 location is driven by an externally controlled micro-force and enters the unit. Within the domain, Transition process within the domain The motion begins with the synchronous counter-rotation of gear 30, gear 1 / 5, and screw 4, moving linearly from the stationary point yb|45|° to the stationary point za|45|°. Meanwhile, another unit, DY-2, carries component 12z during the transition process of unit DY-1. Transitional journey within the domain Approaching the quiescent point at za|45|°.

[0045] ③ During the DY-1 transition process Transitional journey within the domain Another unit, DY-2, has a physically symmetrical lever scale whose lever 3 is linked to a load-bearing component 12z. This component, under the external control and assistance of its 39wk-1 input, enters the transition process driven by the force XL of the fulcrum shaft 18. Transitional journey within the domain

[0046] II. The intrinsic force NS "F" of the 5-physical symmetrical lever scale mode is symmetrically assigned left and right, and the combined force XL of the external control assist drives the lever scale 3 to rotate, load reversing... the static point - moving point trajectory - motion stroke - static point reciprocating motion power unit DY-1 running sequence and stroke (d) state. (See appendix) Figure 7 )

[0047] The DY-1 lever scale unit's lever 3 and associated mechanisms are symmetrically positioned around fulcrum axis 18, with associated link bearing mechanism 12y controlled during the transition process. Transitional journey within the domain The rotational motion reaches the near point yb|45|° of the stationary point.

[0048] ① Transition process in another unit DY-2 Transitional journey within the domain The unit DY-1 dynamic symmetrical component weighing bar 3 and the associated load-bearing component 12y enter the transition process. Transitional journey within the domain

[0049] ② Transition process in another unit DY-2 Transitional journey within the domain The load-bearing component 12y of the DY-1 dynamic symmetrical lever scale, connected to the lever 3, is driven by the external micro-force 12wk-1 of the component at position J2-1-22. The DY-1 load-bearing component 12y begins to rotate synchronously in the opposite direction to gears 30, 1 / 5, and screw 4, moving linearly from the stationary point yb|45|° to the stationary point za|45|°. This movement occurs during the transition stroke of the DY-2 unit. Unit DY-1 Transition Process Transitional journey within the domain The load-bearing component 12z of unit DY-1 reaches the near point of static point za|45|°.

[0050] ③ In another DY-2 transition process Transitional journey within the domain The physical symmetry of the lever scale in unit DY-1, the lever 3 of the scale, the associated linking component 12z, and the load-bearing capacity of its 39wk-1 component input external control assist, under the force XL driven by the fulcrum shaft 18, unit DY-1 enters the transition process. Transitional journey within the domain

[0051] II. The endogenous force NS "F" of the 6-physical symmetrical lever scale mode is symmetrically assigned left and right, and the force XL, which is combined with the external control assist, drives the lever scale 3 to rotate, and the micro-force drives the reversal... The static-moving point trajectory-motion stroke-static reciprocating motion of the power unit DY-1 and unit DY-2 is shown in the appendix. Figure 8 .

[0052] The advantages of this invention compared to the prior art are as follows: the mechanism with endogenous force is linked to specific points on the left / right of the fulcrum area of ​​the lever scale mode, and is physically symmetrical with the mechanism with load force linked on the right / left of the fulcrum area, thus constructing a device in which the action force formed by the endogenous force in the structural energy storage form on the left / right of the fulcrum area interacts with the reaction force formed by the load force on the right / left of the fulcrum area.

[0053] To realize the construction of the endogenous force of natural force attributes into a structural energy storage mode in a specific scenario, the lifting rope of a lever scale is used to connect the lever to specific points to form the lever fulcrum. The mechanism that bears the endogenous force is fixed at the left / right points of the lever fulcrum domain: the left and right fixed bearing points respectively form a certain lever arm value, and each bears the corresponding proportion of the endogenous force value according to the lever arm value ratio. Moreover, by adjusting the bearing points respectively, the static and unbalanced dynamic states of the lever scale can be achieved by balancing the action and reaction forces.

[0054] At specific points on the left or right of the lever fulcrum of the lever assembly, where a large proportion of the endogenous force is borne, the structure is a body whose action force of the structural energy storage endogenous force is less than or equal to the reaction force of the small proportion of the endogenous force borne at the specific points on the right or left of the lever fulcrum plus the connecting load force. When a controllable assist is input to the fulcrum axis of the connecting load component in the same direction as the large proportion of the structural energy storage endogenous force, the endogenous force module and the load module can be linked and interact. The lever, following the controllable assist, moves around the fulcrum, driving the connected load interface component into a rotational motion stroke and trajectory.

[0055] A controllable micro-force drive component is configured in the lever scale module to reverse the proportional internal force values ​​of the fulcrum, enabling the reversal of the large-proportion structural energy storage internal force at the fulcrum's left and right assignment points. When the controllable micro-force drive reverses the large-proportion structural energy storage internal force NS "F" by 180°, it assigns a value at the new point and forms a corresponding force. The load components also synchronously form a reaction force symmetrical to the internal force on the fulcrum axis. The external control assist for the reverse rotational motion, the combined force XL of the structural energy storage internal force at the assignment point, and the reaction force of the load on the other side of the fulcrum interact and correlate with each other on the fulcrum axis components, becoming a unit for the lever scale module to control intermittently reverse and output clockwise and counterclockwise rotational motion.

[0056] Each of the above operating stages has the characteristics of no material, gas, or heat emission, and no noise or vibration scattering. Attached Figure Description

[0057] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings listed below are only some structural schematic diagrams of the present invention, and not all of them.

[0058] Figure 1 This is a system diagram of the present invention.

[0059] Figure 2 This is a structural diagram of the dual-unit DY output power dynamic shape of the present invention, with dynamic shapes of the same rotation direction converging and connecting the load.

[0060] Figure 3 This is a schematic diagram of the stationary point-moving point trajectory-motion stroke-stationary point of the present invention.

[0061] Figures 4 to 7 This is a schematic diagram of the running sequence and process (a, b, c, d) states of unit DY-1 of the present invention.

[0062] Figure 8 This is a schematic diagram of the runtime sequence of unit DY-1 and unit DY-2 of the present invention and the in-domain process t(a, b, c, d).

[0063] Figure 9 This is a structural diagram of the dual-unit DY-(1,2) output power dynamic shaping, convergence relay, system output drive power dynamic shaping module power dynamic convergence drive structure.

[0064] Figure 10 Unit pivot shaft 18-minute clockwise and counterclockwise rotation conversion component synchronous output clockwise and counterclockwise structural diagram

[0065] Figure 11 Unit-to-conversion component synchronous output clockwise and counterclockwise interface structure diagram

[0066] Figure 12 Diagram of the synchronous output clockwise and counterclockwise interface junction of the dual-unit conversion component.

[0067] Figure 13 Dual-unit conversion component synchronous output clockwise and counterclockwise interface convergence output link load diagram

[0068] Figure 14 It is a dynamic timing diagram of dual-unit dynamic shaping and convergence relay in a physically symmetrical lever balance mode.

[0069] Figure 15Rotary wheel J11 p(y0) physical coordinate longitudinal dynamic variable automatically approaches → "0" module structure diagram

[0070] Figure 16 Physical symmetric lever balance mode left and right endogenous forces NS "F" link assignment module structure diagram

[0071] Figure 17 Front view of component 3 of the weighing beam

[0072] Figure 18 Top view of the three components of the weighing beam

[0073] Figure 19 Front view of the weighing beam 3 and the reversing connection component

[0074] Figure 20 This is a diagram of the interconnected and interactive components and parts in part 3 of the left-right physically symmetrical lever scale assembly.

[0075] Figure 21 Left and right pictures: attached Figure 20 Left sectional view of part 01 / g-01 / g

[0076] Figure 22 Left and right pictures: attached Figure 20 Right sectional view of the 02 / g-02 / g component

[0077] Figure 23 Front view of lever scale left and right force reversing gear J5

[0078] Figure 24 Front view of the lever scale's left and right force reversing assembly

[0079] Figure 25 Appendix Figure 20 Right side view of the 03 / g-03 / g fuselage

[0080] Figure 26 Left view of the spiral body 10z body graphic

[0081] Figure 27 Left view of commutation component J5

[0082] Figure 28 It is a diagram showing the travel and trajectory of the left and right endpoints of the clockwise and counterclockwise rotation of the scale beam.

[0083] Figure 29 Front view of the automatic adjustment module for lateral physical variables

[0084] Figure 30 Endogenous Force NS“F”-Lx Type Module Front View

[0085] Figure 31 Front view of the NS(1-1) [f(1)...(m·g)] type module for high-density objects

[0086] Figure 32 Front view of the large volume liquid gravity type NS(1-2) [m·g(1-2)] type module

[0087] Figure 33 yes Figure 35 Front view of section 00 / ns-00 / ns, state 1.

[0088] Figure 34 yes Figure 35 Front view of section 00 / ns-00 / ns, state 2.

[0089] Figure 35 It is a top-view cross-section diagram of 01 / ns-01 / ns.

[0090] Figure 36 It is a top-view cross-section diagram of 02 / ns-02 / ns.

[0091] Figure 37 It is a top-view cross-section diagram (03 / ns-03 / ns).

[0092] Figure 38 It is a top-view cross-section diagram (04 / ns-04 / ns).

[0093] Figure 39 yes Figure 35 Enlarged front view of section 00 / ns-00 / ns.

[0094] Figure 40 It is a top-view cross-section diagram (05 / ns-05 / ns).

[0095] Figure 41 It is a top-view cross-section 06 / ns - 06 / ns graph.

[0096] Figure 42 Unit DY Intrinsic Force NS“F”-Lx [Object Gravity Type NS (G=m·g) + Mechanical Contraction Force (N)] Series Synthesis of Intrinsic Force “F” Module Diagram

[0097] Figure 43 Unit DY Intrinsic Force NS“F”-Lx [Magnetic force f(N) of magnet terminal pair (nn) or f(Ss) + gravity of object of specific material f(m·g) + magnetic force f(N) of magnet terminal pair (ns)] Series synthesis of the intrinsic force NS“F module structure diagram of the "tension" value

[0098] Figure 44 This is the front view of the top plate 25-1.

[0099] Figure 45 This is a top view of the top plate 25-1.

[0100] Figure 46 It is a front sectional view of 0 / J24-0 / J24. Figure 47 It is a top view of 0 / J24-0 / J24. Figure 48 It is a bottom view of the connection between 25-1 and J24-1. Figure 49 These are top views of the magnetic pole of magnet terminal J20 and top views of the magnetic pole code hole of magnet terminal J(20). Figure 50 This is the front view of the connecting component 27. Figure 51 This is a top view of the connecting component 27. Figure 52 This is a top view of the magnetic pole of magnet terminal J21. Figure 53 This is a top view of the magnetic pole of magnet terminal J22. Figure 54 This is a top view of the magnetic pole of magnet terminal J23. Figure 55 It is attached Figure 49 52, 53, and 54, the magnet terminals are symmetrical about the N / S poles in the J20-J23 domain, the magnet terminals rotate symmetrically and interact, and the attraction / repulsion relationship is combined and sorted in a top view. Figure 56 The attached figures (49), (52), (53), and (54) show the magnetic terminals in the J(20)-J(23) domain with the magnetic pole hole codes “1” / “0” symmetrical. The magnetic terminals rotate symmetrically and interact with each other, and the attraction / repulsion relationship is combined and sorted in the front section view. Figure 57 Front view of the intrinsic force NS“F”-Lx module, which combines the series synthesis of the "tension" force value of the magnet terminal (nn) or (ss)f (N) + the gravity of the object of specific material f (m·g) + the mechanical force of the spring f (N). Figure 58 Front view of the intrinsic force NS“F”-Lx [spring mechanical force f(N)] series synthesis of the "tension" force value. Figure 59 Front view of the intrinsic force NS“F”-Lx module, which combines the array of spring mechanical thrust f(N·x) + gravity of a specific material object f(m·g) + spring mechanical tension f(N) to form the "tension" force. Figure 60 Front view of the NS“F”-Lx module, which combines the mechanical elastic force f(N·x) array of springs, the gravity f(m·g) of a specific material object, and the magnetic force f(N) of a magnet pair (ns) to synthesize an endogenous force NS“F” with a specific tensile value. Figure 61 This is a front view of the internal rear body layout of the unit box frame. Figure 62 It is a top view showing the symmetrical structure of the left, right, front, and back sides inside the box. Figure 63 This is the front view of the rear side of the inner frame of unit 1 and 2, and the configuration positioning holes of the connecting functional modules. Figure 64 This is the adjustment module connection panel. Figure 65 It is a conductive shaft positioning link panel. Figure 66 The endogenous force horizontal and vertical coordinate values ​​|→0| are the adjustment module connection panel. Figure 67 This is a diagram of the connection panel for the endogenous force generation module. Figure 68 It is the external control interface for reversing the symmetrical force of the weighing beam. Figure 69 It is an interface for the generation, regulation, and external control of endogenous forces. Figure 70 This is a composite front view showing the installation and positioning of the rear functional panel inside the module housing. Figure 71 This is a front view of the installation and positioning of the rear functional panel device inside the module box. Detailed Implementation

[0101] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0102] In the description of the embodiments of the present invention, it should be noted that if terms such as "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" appear, the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship in which the product of the invention is usually placed when in use. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on the present invention.

[0103] Furthermore, the terms "first," "second," and "third" are used only for distinguishing descriptions and should not be interpreted as indicating or implying relative importance. The use of terms such as "horizontal," "vertical," and "suspended" does not imply that the component must be absolutely horizontal or suspended, but rather that it can be slightly tilted. For example, "horizontal" simply means that its direction is more horizontal than "vertical," not that the structure must be perfectly horizontal, but can be slightly tilted.

[0104] In the description of the embodiments of the present invention, the terms "multiple" or "several" refer to at least two.

[0105] In the description of the embodiments of the present invention, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in the present invention according to the specific circumstances.

[0106] This embodiment is illustrated in conjunction with the accompanying drawings. 10 to Figure 60 This paper provides a detailed description of a dynamic system based on the interaction between the endogenous energy storage force and the load force in a lever balance structure.

[0107] This embodiment presents a dynamic system based on the interaction between the energy storage endogenous force and the load force in a lever balance structure.

[0108] 1. Unit 1 DY Output Power Dynamic Shaping Component

[0109] ① Appendix Figure 10 The unit DY fulcrum component 18 outputs counterclockwise-clockwise intermittent rotational power shaping, the shaping output component 18ds-1 outputs clockwise-clockwise intermittent rotational power shaping, and the 18ds-2 outputs counterclockwise-counterclockwise intermittent rotational power shaping component.

[0110] ② Unit DY output power dynamic shaping component structure attached Figure 11 The unit output pivot shaft 18 polyhedron meshes with the inner bore of the transmission gears 36, 37 and 39wk-1 polyhedron. The external force controllable assist mechanism meshes with the teeth of gear 39wk-1. The force XL carried by the transmission gears 36 and 37 meshes with the teeth of the transmission gears 38-1 and 38-2. The polyhedron transmission shafts 18ds-1 and 18ds-2 output clockwise and counterclockwise rotational power respectively.

[0111] I. 2. Appendix Figure 12The output components of the dual-unit DY-(1,2) power dynamic shaping Dxzx-(1,2)) output mechanism have the same dynamic output interface. The multi-faceted transmission shafts 18ds-1 and 18ds-2 are respectively meshed with the inner hole of the transmission gear 39jh-(1,2) multi-faceted structure to realize the dual-unit DY-(1,2) dynamic convergence relay component structure.

[0112] 1.3 System output link load loader component fz-(1, 2)

[0113] Appendix Figure 13 According to the power movement required by the load component fz-(1,2), the teeth of the transmission gear 39cd mesh with the teeth of the transmission gear 39jh-(1 or / 2), and the rotational power output by the unit pivot shaft 18 drives the load component to move and work the component structure.

[0114] I. Physical architecture of 4 dual-unit DY-(1,2) dynamic convergence relay components, system output link load components, and component interconnection and interaction.

[0115] In the attached figures (12, 13), the fulcrum shaft 18 of the dual-unit DY-(1, 2) outputs the power dynamic shaping component Dxzx, the power dynamic convergence relay component, and the system link drive load component combination module. Each positioning component J7(0) is fixed at a specific point on the chassis frame. The components of each associated interactive body are respectively connected by the multifaceted bearing inner ring of their respective component J7(0) and the multifaceted body of the gear 39(...).

[0116] The polyhedral pivot shaft 18 of unit DY-(1,2) is connected to the bearing polyhedral inner ring of the associated interactive body through the channel J2-1-21 of the chassis frame, and is respectively engaged with the ratchet gears 36 and 37 of the dynamic shaping component Dxzx(...).

[0117] ① When the polyhedral pivot shaft 18 rotates counterclockwise, it drives the ratchet gear 36 to rotate counterclockwise synchronously. The teeth of the ratchet gear 36 interact with the teeth of gears 38-1, 38-2, and 37 through meshing. Gears 38-1 rotates clockwise, 38-2 rotates counterclockwise, and 37 rotates clockwise intermittently by 90°. The polyhedral moving shaft 18ds-1, which is embedded in the inner hole of the polyhedral shaft of gear 38-1, rotates clockwise synchronously, and the polyhedral moving shaft 18ds-2, which is embedded in the inner hole of the polyhedral shaft of gear 38-2, rotates counterclockwise synchronously.

[0118] Thus, the time-division counterclockwise rotation of the polyhedron pivot axis 18 is approximately 90° – clockwise rotation is approximately 90° – the outputs of the dynamic motion on the polyhedron motion axis 18ds-1 and the polyhedron motion axis 18ds-2 are respectively shaped into dynamic motions with single counterclockwise and clockwise rotation directions (approximately 90° – approximately 90° –).

[0119] ②, Dual-unit dynamic dynamic convergence relay gear 39Jh-(1, 2).

[0120] The front view of one unit DY-(1 / 2) physical structure and the rear view of another unit DY-(2 / 1) physical structure are considered as an intersecting planar structure.

[0121] ②-1. The two clockwise and counterclockwise rotating (≈90°——≈90°——) dynamic polyhedral transmission shafts 18ds-(1 / 2) output by one unit DY-(1 / 2) and the two clockwise or counterclockwise rotating (≈90°——≈90°——) dynamic polyhedral transmission shafts 18ds-(2 / 1) output by another unit DY-(2 / 1) on the same physical plane enter the bearing inner ring of the converging relay gear 39jh-(1,2) and mesh with its polyhedral inner ring respectively.

[0122] ②-2, The two interconnected interactive bodies converge and relay the gear 39jh-(1,2) respectively output a backlash-free clockwise or counterclockwise rotation ≈90°... dynamic dynamic shape.

[0123] ③ The transmission speed change and connection load drive component selects the associated interactive body interlocking gear 39jh-(1 / 2) that meshes with the teeth of the transmission gear 39cd according to the rotation direction of the load;

[0124] ③-1. Based on the load speed requirements, set the speed ratio coefficient and other related component parameters of the converging relay gear 39jh-(1 / 2) and the connected transmission gear 39cd;

[0125] ③-2. The teeth of the transmission gear 39cd can mesh with several system load drive gears 39qd that match the type and speed ratio parameters.

[0126] ③-3. The multi-faceted inner hole of the drive gear 39qd is connected to multiple load fz interfaces and other multi-faceted inner holes of the transmission shaft 18qd through meshing, so as to realize the force control of the intersection of two (multi) units and drive the operation of the load.

[0127] 1. The intrinsic force NS "F" of the 5-physical symmetrical lever scale mode is assigned symmetrically on the left and right sides, and the force XL combined with the external control assist drives the lever 3 to rotate, carry the load reversal... static point-moving point trajectory-motion stroke-static point reciprocating motion power unit DY-1 motion sequence stroke-(1,2)t(a,b,c,d) state shaping, and unit DY-1 and unit DY-2 converge and relay force.

[0128] ① The motion sequence of the force XL, which is the result of the controllable assist and endogenous force NS“F”-Lx of the counterclockwise intermittent rotational dynamics combined with the dynamics of the unit DY-(1,2) fulcrum axis 18, in the state of -(1,2)t(a,b,c,d); and the motion sequence of the force XL, which is the result of the counterclockwise intermittent rotational dynamics and the dynamics of the unit DY-(1,2) in the state of -(1,2)t(a,b,c,d) after shaping, in the state of -(1,2)t(a,b,c,d) of the unit DY-(1,2) 18ds-1 of the physical symmetry lever scale mode domain.

[0129] ② The clockwise intermittent rotational dynamic motion and motion timing stroke -(1,2)t(a,b,c,d) states acting on the 18ds-1 physical symmetric lever scale mode domain of unit DY-(1,2) respectively are output by the seamless relay continuous rotational dynamic motion and motion timing stroke state through the relay device Jh-(1 / 2)39.

[0130] II. The energy storage endogenous force and load force interact in the lever scale mode structure. The power system unit consists of 4 functional modules linked by chain J16.

[0131] II.1. Appendix Figure 15 The internal force NS“F” module links the wheel J11(y0) physical coordinate longitudinal dynamic variable automatically approaches →”0” (\″0\f(y)) module structure.

[0132] During the force-driven motion of chain J16, the longitudinal pulsation amplitude of the endogenous force NS“F”-Lx link wheel J11(y0) generated by the counter-rotation trajectory of the weighing bar J3 and its associated interactive body is reduced.

[0133] ① Each eccentric bearing gear 15-(1, 2, 3, 4 or more) and the inner ring of the pivot wheel J11p are respectively connected and fixed to the machine part positioning link plate J2-1-1 through the connecting shaft.

[0134] ② The teeth of each eccentric bearing gear 15-(1, 2, 3, 4 or more) and the outer ring groove of the pivot wheel J11p mesh with the chain link of the chain J16-(1-n) that carries the internal force NS“F”-Lx.

[0135] ③ When the chain J16-(1-n) is subjected to force, within the specific left or right motion range, each eccentric bearing gear 15 and the pivot wheel J11p rotate in sequence.

[0136] ④ Based on the longitudinal motion trend of the physical coordinate of the wheel J11(y0) of the endogenous force NS“F”-Lx link within the intermittent clockwise-counterclockwise (90°) motion domain of the weighing beam 3, set the eccentric amplitude value of each eccentric bearing gear and the tooth and chain link matching parameters.

[0137] ⑤ Within the specific left or right motion range of chain J16-(1-n) under force, the chain length between teeth Cy-1 and Cy-2 is automatically and randomly changed to counteract the amplitude of the longitudinal f(y) point of the physical coordinate of the connecting wheel J11(y0) within the clockwise-reverse rotation (90°) motion range of the weighing lever J3, and to weaken the fluctuation of the endogenous power NS“F”-Lx of the bearing components 12z, 12y and the chain J16-(1-n) connection point.

[0138] II.2, Appendix Figure 16 The physical symmetrical lever scale mode features left and right internal forces NS "F" linked and assigned, symmetrical about the fulcrum axis 18, reversing direction, and force driving the lever 3 to intermittently rotate counterclockwise and clockwise (≈90°) in a lever scale module structure.

[0139] Appendix Figure 17 ...27. The lever scale module uses the fulcrum axis 18 as the symmetrical fulcrum of the lever scale 3, and is composed of specific functional components, related interactive bodies, and parts... in a combined, proportioned, sorted, connected, and linked structure.

[0140] ① Appendix Figure 17 , 18 The lever scale module is based on a specific type of component 3. The polyhedral hole 1 / 3 in the middle of the left and right sides of the lever 3 engages with the polyhedral fulcrum shaft 18, serving as the physical symmetrical fulcrum of the lever scale. The power dynamics converge, interact, and correlate on the polyhedral fulcrum shaft 18.

[0141] ② Appendix Figure 19 The bearing brackets J7z and J7y, which are fixed on the left and right sides of the upper plane of the weighing beam 3, have their multifaceted inner rings meshing with the ends of the left and right multifaceted parts of the reversing screw 4, respectively.

[0142] ③ The middle 3 / 4 of the screw 4 is a multi-faceted part for power reversal transmission. The left and right sides of the weighing rod 3 bear the symmetrical reversal motion of the internal force NS“F”-Lx. The inner threads of the spiral components 10z and 10y respectively mesh with the threads of the screw 4. As the middle 3 / 4 of the screw 4 is driven by the force, the screw 4 rotates clockwise or counterclockwise and moves synchronously to the left or right.

[0143] ④ The left and right polyhedral holes 2 / 3, 3 / 3 and 4 / 3, 5 / 3 of part 3 respectively mesh with the ratchet gears 13z and 14y through the left and right polyhedral shafts 12z and 12y, or the multi-faceted inner ring of the chain guide wheel J11 at the same point.

[0144] ⑤ The front and rear force reversing mechanism J9-(1,2) with physical symmetry at the fulcrum is embedded in the front and rear triangular concave guide rails 7 / 3 of the mechanism 3 respectively.

[0145] ⑥ Appendix Figure 16 , 21 Left sectional view 01 / g-01 / g, and appendix Figure 25 The weighing beam component 3 has two physically symmetrical forces (the physically symmetrical forces mentioned in this chapter refer to the endogenous force NS“F”-Lx) distributed on the left rear and front to convert the frame column J8-(1-2). The frame column J8-(1-2) is connected and fixed through the connecting holes 1 / 8 to the connecting holes 3 / 10 and 4 / 10 of the physically symmetrical force reversing motion screw component 10z.

[0146] Appendix Figure 16 , 22 Right sectional view 02 / g-02 / g, and appendix Figure 25 The weighing beam component 3 has two physically symmetrical force conversion frame columns J8-(3-4) distributed on the right front and rear. The frame columns J8-(3-4) are connected and fixed through the connecting holes 1 / 8 to the physically symmetrical force reversing motion spiral component 10y via the connecting components 4 / 10 and 3 / 10 respectively.

[0147] ⑦、 Figure 16 , 21 Left sectional view 01 / g-01 / g, weighing beam component 3 has two physically symmetrical force conversion frame columns J8-(1-2) distributed at the rear and front. Frame column J8-1 connection holes 2 / 8 are respectively connected and fixed to the rear reversing mechanism J9-2 of the physically symmetrical force conversion component through the connecting mechanism and the connection hole J9h. Frame column J8-2 connection holes 2 / 8 are respectively connected and fixed to the front reversing mechanism J9-1 of the physically symmetrical force conversion component through the connecting mechanism and the connection hole J9q.

[0148] Appendix Figure 16 , 22 Right sectional view 02 / g-02 / g, weighing beam component 3 has two physically symmetrical force conversion frame columns J8-(3-4) distributed at the front and rear. Frame column J8-3 is connected and fixed to the front reversing mechanism J9-1 via connecting holes 2 / 8 through connecting components, and to the front reversing mechanism J9-1 via connecting holes J9q through connecting components. Frame column J8-4 is connected and fixed to the front reversing mechanism J9-1 via connecting holes 2 / 8 through connecting components, and to the front reversing mechanism J9-1 via connecting holes J9h.

[0149] ⑧. Appendix Figure 16 , and attached figure (21 / (21)) left sectional view 01 / g-01 / g, the weighing beam component 3 left view rear and front distribution two physically symmetrical force conversion frame columns J8-(1-2). The frame column J8-(1-2) connection holes 3 / 8 are respectively connected and fixed to the physically symmetrical endogenous force NS“F”-Lx left polyhedral bearing shaft 12z through the connection component.

[0150] Appendix Figure 16And the right sectional view of the attached figure (22 / (22)) 02 / g-02 / g, the weighing beam component 3 has two physically symmetrical force conversion frame columns J8-(3-4) distributed in front and back on the right. The frame column J8-(3-4) connection holes 3 / 8 are respectively connected and fixed to the right polyhedral bearing axis 12y of the physically symmetrical endogenous force NS“F”-Lx through the connection components.

[0151] ⑨ In the lever balance mode, the internal force NS "F"-Lx specific gravity "%" value of the left and right fulcrum is physically symmetrically reversed.

[0152] Appendix Figure 16 , 23 24, and appendix Figure 25 Right sectional view 03 / g-03 / g, bearing components 12z and 12y respectively bear xx% and xx% ("1-xx%) of the intrinsic force NS"F"-Lx value;

[0153] Front view of shift gear J5, screw 4 and associated interactive components 10z, 10y and J5.

[0154] ⑨-1. Channel J2-2-22 is configured with connecting component 12wk-1 externally controlled micro-force, which is connected to the transmission shaft 12 through the configured special power dynamic adapter component. The multifaceted body 3 / 4 of the reversing screw 4 meshes with the multifaceted inner hole 4 / 5 of the force shifting gear J5. When the multifaceted inner hole 1 / 30 of the transmission gear 30 and the meshing multifaceted transmission shaft 12 are subjected to force and rotate clockwise or counterclockwise, the multifaceted body 3 / 4 of the reversing screw 4, which meshes with the multifaceted inner hole 4 / 5 of the shifting gear J5 through the teeth of the transmission gear 30, rotates clockwise or counterclockwise in the same direction.

[0155] ⑨-2, Appendix Figure 20 , 24 and appendices Figure 26 Left sectional view 04 / g-04 / g, Figure 27 Right sectional view 05 / g-05 / g. The left extension polyhedron 3 / 5 of the physically symmetrical force reversing gear J5, the left and right gears 1 / 5 and 2 / 5 are integrated through 0 / 5, and the inner hole 4 / 5 of the polyhedron meshes with the polyhedron 3 / 4 of the reversing screw 4 to form a coaxially related interactive body with the force reversing screw 4.

[0156] The left extension of the reversing gear J5, the multifaceted body 3 / 5, is connected to the middle of the upper end face of the weighing rod 3. The bearing multifaceted inner ring of the bracket J7(0) meshes with the left and right multifaceted ends of the reversing screw 4 and the bearing multifaceted inner rings of the left and right brackets J7z and J7y, ensuring the straight state of the reversing screw 4 during the force-driven rotational motion of the reversing gear J5.

[0157] ⑨-3, Appendix Figure 16Within the clockwise and counterclockwise rotation micro-force drive domain of component 12wk-1 at part J2-1-22, the multi-faceted transmission shaft 12 and transmission gear 30 are driven to rotate clockwise and counterclockwise through the (speed-related matching ratio adapter component).

[0158] ⑨-4, Appendix Figure 16 , 24 When the physical symmetry endogenous force NS“F”-Lx bearing component 12y moves linearly from the static point yb|45|° to the static point za|45|°, and the endogenous force NS“F”-Lx bearing component 12a approaches the static point za|45|° throughout the entire process, the teeth of the transmission gear 30 mesh with the teeth of the force reversing gear J5 by 1 / 5.

[0159] During the linear motion of the bearing component 12y from the static point zb|45|° to the static point ya|45|°, and during the entire process of the bearing component 12y approaching the static point ya|45|°, the teeth of the transmission gear 30 mesh with 2 / 5 of the teeth of the force reversing gear J5.

[0160] The screw component 10 (z, y) with its internal thread meshes with the screw 4, and moves synchronously to the left or right as the screw 4 rotates.

[0161] ⑨-5. The clockwise and counterclockwise rotational micro-force of the driving component 12wk-1 is transmitted to the polyhedral transmission shaft 12, which meshes with the inner hole of the multi-faceted gear 30, through the configured adapter connection device. The teeth of the gear 30 mesh with 2 / 5 and 1 / 5 of the teeth of the force reversing gear J5 in a time-sharing or continuous manner.

[0162] ⑨-6. The inner hole of the polyhedral gear J5 meshes with the polyhedral 3 / 4 of the middle of the transposition screw 4. When the transposition gear J5 is subjected to force and rotates clockwise or counterclockwise, it drives the internally powered transposition screw 4 to rotate clockwise or counterclockwise. The thread of the transposition screw 4 meshes with the inner thread of the physically symmetrical reversing motion spiral component 10 (z, y), driving the spiral component 10 (z, y) to move synchronously to the left or right in a linear motion.

[0163] ⑨-7, Appendix Figure 20 The physical symmetry of the lever scale module structure is that the left and right center polyhedral inner hole 1 / 3 of the lever 3 is connected to the polyhedral central pivot 18, and the center point of the left and right center polyhedral inner hole 1 / 3 of the lever 3, the center point of the pivot axis 18, and the center points of the endogenous force NS“F”-Lx bearing components 12z and 12y are on the same parallel line.

[0164] ⑨-8. The weighing beam 3 and related components take the fulcrum axis 18 as the fulcrum. When the internal force NS "F"-Lx on the left side of the weighing beam 3 of a unit DY-1 is the load-bearing component 12z, the initial position of the component 12z is near the static point za|45|° or the initial position of the component 12y on the right side is near the static point ya|45|°.

[0165] The initial position of the load-bearing component 12z on the left side of the weighing bar 3, which is the physical symmetry of another unit DY-2, can also be near the static point za|45|° or the initial position of the right side 12y can be near the static point ya|45|°.

[0166] ⑨-9. The length “x” from the center point of the left or right force-bearing components 12z and 12y of the weighing beam 3 to the center point of the polyhedral fulcrum axis 18 is r. The rotational stroke of the left and right internal force NS “F”-Lx bearing components 12z and 12y in counterclockwise and clockwise rotation of the weighing beam 3 is 2π “x” / 4.

[0167] ⑨-10. Bearing capacity of the moving points of the left and right bearing components 12z and 12y in the counterclockwise and clockwise rotational motion trajectories of the weighing beam 3: The endogenous force NS "F" - Lx bearing variable of the moving point in the rotational motion domain of the bearing components 12z and 12y → "0".

[0168] II. The structure of the 3-unit DY endogenous force NS“F” module for the vertical and pulling connection of the power bearing wheel J11(y0) with the lateral coordinate motion trajectory of the moving point physical variable automatic adjustment module.

[0169] ① Appendix Figure 29 Each eccentric bearing gear 15-(5, 6 or more) and the inner ring of the power bearing wheel J11(x0) that is vertically suspended or pulled by the transverse internal force NS“F”-Lx are each connected and fixed to the machine part positioning link plate J2-1-3 through the connecting shaft.

[0170] ② The centers of the auxiliary wheel J11(x0) and the power bearing wheel J11(y0) are aligned with the center of the fulcrum axis 18 in a longitudinal straight line.

[0171] ③ The meshing of the outer ring grooves of each eccentric bearing gear 15-(5, 6 or more) and auxiliary wheel J11(x0), power bearing wheel J11(y0) with the chain links of the internal force NS“F”-Lx transmission chain J16-1(x) to J16-n(x).

[0172] ④ Based on the intermittent clockwise-counterclockwise (90°) rotation of the weighing beam 3, the chain 16-1(x) to J16-n(x) is subjected to force reversal within a specific motion stroke range, and the outer rings of each eccentric bearing gear 15-(5, 6) and auxiliary wheel J11(x0) and power bearing wheel J11(y0) are subjected to force and rotate in sequence.

[0173] ⑤ By setting the eccentricity of the meshing shaft of the inner ring of the eccentric bearing gear 15-(5,6) and the tooth and chain link matching parameters, and randomly modifying the physical lateral coordinate of the power bearing wheel J11(y0) of the connection, the force ratio of the endogenous force NS“F”-Lx on the connecting parts 12z and 12y of the weighing bar 3 can be realized.

[0174] II.4 Appendix Figure 30 , the endogenous force of unit DY endogenous force “F” is the endogenous force NS “F”-Lx type module, component.

[0175] The endogenous force module compartment J2-1-4 of unit DY is equipped with a hanging and pulled on the inner ring of the power bearing wheel J11(y0). The different material components of the hanging are connected by zipper 29. The module and component model of the endogenous force NS“F”-Lx〖f(1)…(n)〗 type structure.

[0176] The unit DY endogenous force NS“F”-Lx type is configured within the J2-1-4 frame of the endogenous force module chamber, which features the combination, proportion, and sorting of natural force elements.

[0177] 4-1. Gravity (G = m·g) "Hanging" type;

[0178] 4-2. Gravity (G=m·g) + Mechanical force (N) resultant force "pull" type "vertical pull";

[0179] 4-3. Magnetic force (T:N) "repulsion" + gravity (G=m·g) + magnetic force (T:N) "attraction" resultant force "pulling" type;

[0180] 4-4. Magnetic force (T:N) "repulsion" + gravity (G=m·g) + mechanical force (N) "pull" resultant force "pulling" type;

[0181] 4-5. The resultant force of mechanical force (N) "push" + gravity (G=m·g) + mechanical force (N) "pull" is of the "pulling" type;

[0182] 4-6. Other mechanical forces (N) "push" + gravity (G=m·g) + magnetic force (T:N) "repel" pull + gravity (G=m·g) "pull" type...

[0183] 4.4-1. Appendix Figure 31 , 32 The object's weight (G = m·g) is of the "hanging" type.

[0184] The module structure model is configured with the intrinsic force NS“F”-Lx [object gravity type NS(1-1, or 1-2)(m·g(1…), or m·g(1+…1)] “hanging” force value of the unit DY endogenous force NS“F”-Lx [object gravity type NS(1-1, or 1-2)(m·g(1…), or m·g(1+…1)] “hanging” force value of the module structure model. The inner ring of the bearing wheel J11(y0) is connected by zipper 29.

[0185] ① Appendix Figure 31 As shown: The endogenous force "F" module structure with a gravity type NS(1-1) [m·g(1…)] value, which is used for fixed-point operation and operation in a relatively small physical space, and has low manufacturing and production costs. It is suspended in the inner ring of the bearing wheel J11(y0) and has low specific gravity.

[0186] ② Appendix Figure 32 As shown: a fixed-point positioning operation scenario with sufficient physical space, and an endogenous force NS“F”-Lx module structure with low manufacturing and production costs, which is a large-volume object suspended in the inner ring of the bearing wheel J11(y0) with a gravity type NS(1-2) [m·g(1+…1)].

[0187] ③ Top view of the appendix Figure 35 Forward view section 00 / ns-00 / ns (1, 2) Figure 33 , 34 , attached Figure 33 Top view profile 01 / ns-01 / ns Figure 35 The large-volume object gravity type NS(1-2) [m·g(1+…1)] frame J64 is placed in the endogenous force generation “F” module compartment J2-1-4 frame.

[0188] ③-1. The long or square frame connection interface 63-〔(1)-(4)〕 on the gravity frame J64-1 is connected to the connecting part J61 of the hanging zipper 29 by the chain 62-(1-4) respectively, so as to realize the hanging connection between the gravity frame and the liquid m·g(1+…1) it carries and the inner ring of the bearing wheel J11(y0) through the zipper 29;

[0189] ③-2. The upper part of the gravity frame J64, or the square frame J64-1 and the lower part, the square frame J64-2 and the four upright body 66-(1-4) are connected and constructed by the connection interface 63-〔(1)-(4)〕.

[0190] ④ Appendix Figure 33 , 3435, pressure water valve box 68, pressure water outlet interface 67, physical water source positioning interface 76, pressure chamber water pressure variable stabilizing spring positioning component 65-〔(1)-(4)〕 at the four corners, gravity water tank J74, water pressure stabilizing spring 71-〔(1)-(4)〕 is configured between the spring positioning component 65-〔(1)-(4)〕 at the upper end of gravity frame column body 66-(1-4) and the upper end of gravity water tank body J74.

[0191] ⑤ The gravity-type NS(1-2) is a dual-compartment liquid m·g(1+…1) gravity composite structure with an endogenous force "F".

[0192] Throughout the process, the variable [m·g(1+…1)] in liquid state is changed to “0”. The gravity water tank slides up and down along the 1 / J74 gravity frame column body 66-(1-4) inside the track hole.

[0193] ⑥ Closed-loop control process of pressure water m·g(…1) output and gravity water m·g(1…) inflow: Pressure water valve box 68 is equipped with pressure water outlet valve 69. When the water pressure in the pressure water outlet port 67 is greater than the water pressure in the hose 72, the lower section of the outlet valve 69 abuts and closes with the port 70; when the water pressure in the port 67 is less than the water pressure in the hose 72, the lower section of the outlet valve 69 disengages from the port 70, and the pressure water enters the pressure water valve box 68 through the outlet valve 69 to the pressure water outlet port 67.

[0194] ⑦ The pressurized water in the pressure water valve box 68 flows out from the interface 67, and the water pressure in the pressure chamber water tank 83 drops.

[0195] ⑦-1. At the same time, the gravity water tank J74 descends, the gravity water level drops, the water pressure at the water supply interface 76 is greater than the water pressure at the lower end of the inlet valve component 79, the inlet valve component 79 disengages from the inlet pipe, and the high physical water level water source at the interface 76 enters the gravity water tank J74 through the inlet valve component 79, increasing the pressure on the pressure water tank 83;

[0196] ⑦-2. The water outlet of the pressure water tank 83 through the outlet valve 69 is equal to the water inlet of the gravity water tank J74 through the inlet valve 79, keeping the gravity variable within the gravity frame → "0", so as to realize that the endogenous force "F" variable of the ring suspended in the power bearing wheel J11(y0) → "0".

[0197] ⑦-3. As the amount of water from the water source interface 76 enters the gravity water tank J74 through the inlet gate component 79, the pressure of the water in the pressure tank 83 increases accordingly. Meanwhile, the pressure of the pressure stabilizing spring 71-〔(1)-(4)〕 on the pressure tank 83 decreases synchronously with the decrease of the spring force of the track hole 1 / J74 of the gravity water tank J74 sliding down along the gravity frame column body 66-(1-4), thus realizing the pressure variable of the water in the pressure tank 83 → "0".

[0198] ⑧. Appendix Figure 33 ,and Figure 41 The bottom plane of gravity water tank J74 is connected to the upper plane of pressure water tank 83, and the lower plane of pressure water tank 83 is connected to J64-2 at the bottom of gravity frame through connecting device 84.

[0199] ⑨ Appendix Figure 39 The pressure water tank 83 volume and water replenishment assembly are connected by gear 38 and ratchet gear 36 of the lifting device TS-(1-4, or more); the multi-faceted transmission shafts 12-2 and 12-1, which mesh with the multi-faceted inner ring of gear 38 and ratchet gear 36, are connected to the parallelogram frame J64-1 on the gravity frame through bearings.

[0200] ⑨-1. The 38 teeth of the lifting device TS gear mesh with the rack 1 / J85 teeth of the rack frame body J85, and the 36 teeth of the ratchet gear mesh with the rack 2 / J85 teeth of the rack frame body J85.

[0201] ⑨-2. The lower crossbeam of the rack and pinion frame body J85 of the lifting device TS is connected to the upper frame of the gravity water tank J74;

[0202] ⑨-3. When the volume (water volume) in the pressure tank 83 decreases to the set value, the rotational power of the external control force is transmitted to the specific "power motion adapter transmission device" through the meshing connection of the multi-faceted transmission shaft 12WK-2 configured in the J2-1-23 interface. The "power motion adapter transmission device" links and drives the transmission shaft 12-2 of the ratchet gear 36 of the lifting component TS-(1-4, or even more) connected to the gravity tank J74 to rotate counterclockwise.

[0203] ⑨-4. The ratchet gear 36 drives the gear 38 to rotate clockwise in sync. The rack frame J85 is driven to move upward through the teeth of the meshing rack 2 / J85 and rack 1 / J85, which in turn compresses the spring 71-〔(1)-(4)〕 and pulls the gravity water tank J74 and the upper frame of the pressure water tank 83 connected to the lower frame of the gravity water tank J74 to lift upward.

[0204] ⑨-5, Appendix Figure 40As the space of the pressure water tank 83 expands, the water pressure of the pressure water tank 83 becomes less than the water pressure of the channel interface 81 connecting the gravity water tank J74 and the pressure water tank 83. The lower body of the inlet gate mechanism 82 disengages from the channel 81, and the water in the gravity water tank J74 enters the chamber of the pressure water tank 83 through the gate mechanism 82.

[0205] ⑨-6. When the gravity water tank J74 is raised to the design height, the external control rotation cooperation of the polyhedral transmission shaft 12WK-2 configured through the J2-1-23 interface is canceled, and the transmission shaft 12-2 of the ratchet gear 36 of the lifting component TS-(1-4, or even more) is in a free state.

[0206] ⑨-7. When the water pressure in the interface 67 decreases, the pressure water in the pressure water valve box 68 flows out from the interface 67, the pressure in the pressure chamber water tank 83 decreases, the pressure stabilizing spring 71-〔(1)-(4)〕 springs and the gravity water tank J74 squeezes the pressure water tank 83, and the track hole 1 / J74 of the gravity water tank J74 slides down along the gravity frame column body 66-(1-4) dynamically.

[0207] ⑨-8. During each transition process in ⑨-(3-7) above, the gravity variable within the gravity frame randomly → "0", and the endogenous force "F" variable suspended by the zipper 29 in the inner ring of the chain guide wheel J11(y0) → "0"; the water pressure in the pressure tank 83 meets the water pressure setting value of the outlet port 67.

[0208] 4.4-2. The resultant force of gravity (G=m·g) + mechanical force "pulling" (N) is "vertical pulling" type.

[0209] Appendix Figure 42 Based on the operating scenario, the inner ring of the bearing wheel J11(y0) is connected by zipper 29 to the unit DY endogenous force NS“F”-Lx [object gravity type NS(G=m·g)+mechanical contraction force (N)] configured in the vertical tension module compartment J2-1-4 frame to synthesize the endogenous force “F” module structure model of the “tension” force value.

[0210] ① The gravity object (m·g) 26 is connected to the interface 5 / 26 through the machine part 6-2, which is connected to the zipper 29 and the power bearing wheel J11 (y0) inner ring body for vertical pull connection.

[0211] ② The bottom plane of the gravitational object (m·g) 26 is connected to the upper plane of the clockwise threaded part 31. The lower top plate 25 is fixedly connected to the lower edge of the module compartment J2-1-4 frame, and the lower plane of the counterclockwise threaded part 32 is connected to the lower top plate 25.

[0212] ③ The upper spring body of the upper clockwise and lower counterclockwise spiral spring composite body J33 is engaged with the inner hole of the component 31 by a clockwise thread, and the lower spring body is engaged with the inner hole of the component 32 by a counterclockwise thread. The tension state of the spring body J33 between the clockwise and counterclockwise threaded components 31 and 32 generates the intrinsic mechanical tension f (N) of the spring body J33 between the threaded components 31 and 32.

[0213] ④ The bottom plane of object (m·g)26 can be connected to several spring bodies J33 and parts 31 and 32, forming a spring tension matrix composed of the tensile mechanical force values ​​(x*n) of several elastic interactive bodies.

[0214] ⑤ As needed, the control force transmitted to component 12wk-2 is transmitted to the drive power dynamic transmission adapter body configured through channel J2-1-23, which links the rotation angle of the middle polyhedron 1 / J33 of the drive spring component J33, thereby realizing the random adjustment of the spring mechanical tension f(N) value of the spring tension force matrix.

[0215] 4.4-3. The resultant force type of magnetic repulsion f(N) + gravity f(m·g) + magnetic attraction f(N).

[0216] Appendix Figure 43 As shown: Based on the operating scenario, the module structure model of the unit DY internal force NS“F”-Lx [magnetic force f(N) of magnet terminal pair (nn) or f(ss) + gravity f(m·g) of specific material object + magnetic force f(N) of magnet terminal pair (ns)] is connected in series to synthesize the "tension" force value according to the module structure model of the module DY, which is configured in the module compartment J2-1-4 frame through zipper 29.

[0217] ① The top plate 25-1 of the endogenous force NS“F”-Lx module is connected and fixed to the upper frame of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25, and the bottom plate 25-2 is connected to the lower edge of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25.

[0218] ② The connecting component (m·g) 27 and the connecting interface 5 / 27 are connected to the zipper 29 through the component 12. The zipper 29 is connected to the inner ring of the power bearing wheel J11 (y0) through the center channel of the magnet terminal J21 (ss), the center channel of the magnet terminal J20 (nn), the center channel of the rotation drive control component J24-1, and the channel 7 / 25 of the top plate 25-1.

[0219] ③ The top plate 25-1 is connected to the rotary drive gear J24-1 and the magnet terminal J20.

[0220] ③-1, Appendix Figure 44 , 47The upper top plate 25-1 is connected to the inner ring of the bearing 6 by meshing with the convex polyhedron 9 / 25. The inner ring of the rotation drive gear J24-1 achieves rotational movement around the convex polyhedron 9 / 25 of the upper top plate 25-1 by connecting with the outer ring of the bearing 6.

[0221] ③-2, Appendix Figure 45 , 46 The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the upper surface of the drive gear J24-1 abut against the ball concave track ring 8 / 25 on the lower surface of the upper top plate 25-1, thereby achieving a gapless, rotatable motion connection between the drive gear J24-1 and the upper top plate 25-1.

[0222] ③-3, Appendix Figure 49 The "n" and "s" magnetic pole parts of the magnet correspond to the physical domain marked by the digital codes "1" and "0" of the terminal frame, respectively. For example, the top view of magnet terminals J20, J21, J22, J23, etc. shows that multiple magnets are embedded in the frame marked by the digital codes "1" and "0" in a specific combination arrangement of the "n" and "s" magnetic pole parts, and the physical domains are fixed, forming a magnet terminal with the magnetic pole layout structure represented by the digital codes "1" and "0".

[0223] ③-4, Appendix Figure 44 The connecting holes (1-4) / 20 on the upper surface of the magnetic terminal J20 frame are connected and fixed to the connecting holes (1-4) / 24-1 on the lower surface of the gear J24-1 ring body through the connecting parts.

[0224] ④ The upper and lower planes of the connecting component 27 are respectively connected and fixed to the frames of magnet terminals J21 and J22.

[0225] ⑤ Appendix Figure 43 , 50 A linking component 27 made of a specific material (its own mass m·g→“min”) is selected. The zipper 29 passes through the inner opening 5 / 27 of its channel through the linking component to achieve a pulling connection with the inner ring of the bearing wheel J11(y0).

[0226] ⑤-1, Appendix Figure 51 , 52 53, the upper plane connecting hole (1-4) / 27 of the connecting component J27 is connected to the lower plane connecting hole (1-4) / 21 of the magnetic terminal J21 frame through the connecting component, and the lower plane connecting hole (1-4) / 27 is connected and fixed to the upper plane connecting hole (1-4) / 22 of the magnetic terminal J22 frame through the connecting component;

[0227] ⑤-2, Appendix Figure 43 , 54 The rotary drive gear J24-2 is connected to the magnet terminal J23 in a combined frame;

[0228] ⑤-3, Appendix Figure 44 , 45 46. ​​The inner ring of the rotary drive gear J24-2 is connected to the outer ring of the bearing 6. The lower top plate 25-2 is fixed by meshing with the polyhedral inner ring of the bearing 6 inside the rotary drive gear J24-2 through the convex polyhedron 9 / 25.

[0229] ⑤-4, Appendix Figure 44 , 47 53, the connecting hole (1-4) / 23 on the lower plane of the magnet terminal J23 frame is connected to the connecting hole (1-4) / 24-2 on the upper plane of the gear J24-2 ring body through the connecting parts;

[0230] ⑤-5, Appendix Figure 44 , 45 46. ​​The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the lower surface of gear J24-2 abut against the upper surface of the lower top plate 25-2 ball concave track ring 8 / 25, so as to achieve a gapless connection between the lower surface of gear J24-2 and the upper surface of the lower top plate 25-2.

[0231] ⑤-6. Appendix Figure 44 , 45 46, The longitudinal (y) physical "link" positioning of gear J24-2 and lower top plate 25-2 is achieved by embedding the ball between the inner and outer rings of bearing 6 into the track groove structure of the inner and outer rings. This limits the longitudinal (y) physical displacement of gear J24-2 due to the attraction of magnet terminals J23 and J22, and the rotational movement of magnet terminal J23 around the convex polyhedron 9 / 25 of lower top plate 25-2 along with bearing 6 inside gear J24-2.

[0232] ⑥ Synthesis and regulation of endogenous force NS "F" formed by connecting endogenous force "F" linking component 27f(m·g→"min") and magnetic force (repulsion) f(N) + magnetic force (attraction) f(N) in series within the endogenous force "F" module.

[0233] ⑥-1. The control and coordination force transmitted by the 12wk-2 component is transmitted through the endogenous force "F" module compartment channel J2-1-23 and the drive power dynamic transmission of the 5 / 25 and 6 / 25 configuration of the upper top plate 25. The body drives the gears J24-1 and J24-2 as needed to drive the connecting magnet terminals J20 and J23 to rotate by a specific angle.

[0234] ⑥-2. Within the domain of a specific transition process, the rotation of gears J24-1 and J24-2 is randomly adjusted by sending the cooperative force to component 12wk-2. By modifying the deflection angle difference between the magnetic poles corresponding to the magnetic poles of magnet terminals J20 and J21, J22 and J23, the pulling force between the inner ring of the power bearing wheel J11(y0) and the NS(3…)NS“F”-Lx is changed in real time through the linking component 27f(m·g→“min”) and the pulling force between (magnetic force (repulsion)f(N)+magnetic force (attraction)f(N))“0” to the maximum max value.

[0235] ⑦ Appendix Figure 55 A top view showing the symmetrical interaction of the magnet terminals with the J20-J23 magnetic poles, and the associated magnetic attraction and repulsion combinations.

[0236] ⑦-1. Symmetrical positioning of magnetic poles of magnetic terminal J23-1 and magnetic terminal J23-2, and the transition process of the angle of the rotating point of terminal J23-1 and the magnetic repulsion force f(N) of the symmetrical phase of magnetic poles of magnetic terminal J23-2.

[0237] ⑦-2, The symmetrical positioning of magnetic poles of magnetic terminal J23 and magnetic terminal J22, and the transition process of the angle of the rotating point of terminal J22 and the magnetic attraction force f(N) of the symmetrical phase of magnetic poles of magnetic terminal J23...

[0238] ⑦-3. Symmetrical positioning of magnetic poles of magnetic terminal J20-1 and magnetic terminal J20-2, and the transition process of the angle of the rotating point of terminal J20-1 and the magnetic repulsion force f(N) of the symmetrical phase of magnetic poles of magnetic terminal J20-2 and the magnetic attraction force f(N) of the symmetrical phase of magnetic poles…

[0239] ⑦-4. Symmetrical positioning of magnetic poles of magnetic terminal J20 and magnetic terminal J21, and the transition process of the angle of the rotating point of terminal J21 and the magnetic attraction (attraction) f(N) and magnetic repulsion (attraction) f(N) values ​​of the symmetrical phase of magnetic poles of magnetic terminal J20.

[0240] ⑧. Appendix Figure 56 The front view shows the symmetrical interaction between the magnet terminals and the J20-J23 magnet cross-section, with magnetic pole hole codes "n:1" and "s:0" indicating the interaction between the attraction force f(N) and repulsion force f(N).

[0241] ⑧-1. The code “1”, “0”, “1”, “0” on the surface of the magnet pole of terminal body J23-1 and the code “1”, “0”, “1”, “0” on the surface of the magnet pole of terminal body J23-2 are symmetrically positioned to the rotational movement point of terminal J23-1. The magnetic pole code “1”, “0”, “1”, “0” and the magnetic pole code “1”, “0”, “1”, “0” of magnetic terminal J23-2 are symmetrically repelled by the magnetic force f(N) value at the symmetrical angle. The transition process is as follows:

[0242] ⑧-2. The code “1”, “0”, “1”, “0” on the surface of the magnet pole of terminal body J23-1 and the code “0”, “1”, “0”, “1” on the surface of the magnet pole of terminal body J23-2 are symmetrically positioned to the rotational movement point of terminal J23-1. The magnetic pole code “1”, “0”, “1”, “0” and the magnetic pole code “0”, “1”, “0”, “1” of magnet terminal J23-2 are symmetrically attracted by the magnetic force f(N) value at the symmetrical angle... transition process;

[0243] ⑧-3. The code “1”, “1”, “0”, “0” on the surface of the magnet pole of terminal body J20-1 and the code “1”, “1”, “0”, “0” on the surface of the magnet pole of terminal body J20-2 are symmetrically positioned to the rotational movement point of terminal J20-1. The magnetic pole code “0”, “0”, “1”, “1” and the magnetic pole code “1”, “1”, “0”, “0” of magnet terminal J20-2 are symmetrically positioned. The repulsive magnetic force f(N) value - the symmetrically attracted magnetic force f(N) value... transition process;

[0244] ⑧-4. The code “0”, “0”, “1”, “1” on the surface of the magnet pole of terminal body J21-1 and the code “1”, “1”, “0”, “0” on the surface of the magnet pole of terminal body J20-1 are symmetrically positioned to the rotational movement point of terminal J21-1. The magnetic pole code “1”, “1”, “0”, “0” and the magnetic pole code “1”, “1”, “0”, “0” of magnet terminal J20-1 are symmetrically attracted by the magnetic force f(N) value - repelled by the magnetic force f(N) value at the symmetrical angle... transition process.

[0245] 4. Magnetic force f(N) attraction / repulsion + gravity f(m·g) + spring mechanical force f(N) elastic / pulling force type.

[0246] Appendix Figure 57Based on the operating scenario, the module structure model is composed of the intrinsic force NS“F”-Lx of the unit DY, which is the "pull" force value synthesized by the unit DY, which is the inner ring of the bearing wheel J11(y0) pulled by the zipper 29. The intrinsic force NS“F” is the result of the magnet terminal (nn) or (ss)f(N) + the gravity of the object of specific material f(m·g) + the mechanical force of the spring f(N) in series.

[0247] ① The top plate 25-1 of the endogenous force "F" module is connected and fixed to the upper frame of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25, and the bottom plate 25-2 is connected to the lower edge of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25.

[0248] ② The connecting interface 5 / 27 of the connecting component (m·g) 27 is connected to the zipper 29 through the component 12. The zipper 29 is connected to the specific mass connecting component 27 through the internal force "F" of the upper top plate 25-1, the power bearing connecting channel 7 / 25, and the connecting channel of the rotation drive control component J24-1. This achieves the following: gravity f (m·g → "min") + repulsion (nn) between magnet terminal J20 and magnet terminal J21, magnetic force f (N) or (s-sf (N) + spring body J33 generates mechanical pulling force f (N) between gravity component (m·g) 27 and lower top plate 25-2. The three forces combined into one NS (4...) internal force "F" is pulled and connected to the inner ring of the power bearing wheel J11 (y0).

[0249] ③ The top plate 25-1 is connected to the rotary drive magnet J24-1 and the magnetic terminal J20.

[0250] ③-1, Appendix Figure 44 , 47 The upper top plate 25-1 is connected to the inner ring of the bearing 6 by meshing through the convex polyhedron 9 / 25. The inner ring of the gear J24-1 is connected to the outer ring of the bearing 6 to realize the rotational drive of the gear J24-1 around the convex polyhedron 9 / 25 of the upper top plate 25-1.

[0251] ③-2, Appendix Figure 45 , 46 The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the upper surface of gear J24-1 abut against the ball concave track ring 8 / 25 on the lower surface of the upper top plate 25-1, realizing a gapless, rotatable motion connection between gear J24-1 and upper top plate 25-1.

[0252] ③-3, Appendix Figure 49The (ns) magnetic poles of the magnets correspond to the physical areas marked by the numbers 1 and 0 on the terminal frame, such as the top view of magnet terminals J20, J21, etc. Multiple magnets are fixed in the physical areas marked by the numbers 1 and 0 on the frame with a specific combination of (ns) magnetic poles.

[0253] ③-4, Appendix Figure 43 The connecting holes (1-4) / 20 on the upper surface of the magnet terminal J20 frame are connected and fixed to the connecting holes (1-4) / 24-1 on the lower surface of the gear J24-1 ring body through the connecting parts.

[0254] ④ The upper and lower planes of the connecting component 27 are connected to the magnet terminal J21 and the threaded component 31, respectively.

[0255] ④-1, Appendix Figure 30 , Figure 50 A connecting component 27 with a specific mass (its own mass m·g → “min””) is selected, and its interface 5 / 27 is connected to the zipper 29 by means of the connecting component;

[0256] ④-2, Appendix Figure 40 , 41 42. The upper plane connecting hole (1-4) / 27 of the connecting component J27 is connected to the lower plane connecting hole (1-4) / 21 of the magnetic terminal J21 frame through the connecting component. The lower plane connecting hole (1-4) / 27 is connected to the upper plane of the inner hole clockwise threaded component 31 through the connecting component. The lower top plate 25-2 is connected and fixed to the lower edge of the module compartment J2-1-4 frame. The lower plane of the inner hole counterclockwise threaded component 32 is connected to the lower top plate 25-2.

[0257] ④-3. The spring body of the composite body J33 with the clockwise thread of the upper spiral spring and the counterclockwise thread of the lower spiral spring meshes with the clockwise thread of the hole of the component 31 and the counterclockwise thread of the inner hole of the component 32 respectively. The spring component of the body J33 generates the internal mechanical tension f (N) of the spring body J33 between the threaded components 31 and 32 in the tensile state between the threaded components 31 and 32.

[0258] ④-4. The bottom plane of object (m·g)27 can be connected to 1 or more spring bodies J33 and parts 31 and 32 to form a spring mechanical tension matrix composed of the pulling mechanical force value (x*n) of 1 or more pulling interactive bodies.

[0259] ④-5. As needed, the control force transmitted to component 12wk-2 is transmitted to the drive power dynamic transmission adapter body configured through channel J2-1-23, which links the rotation angle of the middle polyhedron 1 / J33 of the drive spring component J33, thereby realizing the random adjustment of the spring mechanical tension f(N) value of the spring tension matrix.

[0260] 4. 4-5. The resultant force type of spring mechanical contraction force f(N·x) + gravity f(m·g) + mechanical contraction force f(N).

[0261] Appendix Figure 59 Based on the operating scenario, the module structure model is composed of the intrinsic force NS“F”-Lx [spring mechanical thrust f(N·x) + gravity of specific material object f(m·g) + spring mechanical tension f(N)] in the module compartment J2-1-4 frame, which is pulled by the zipper 29, and the intrinsic force NS“F” is a series synthesis of the “tension” force value.

[0262] ① The top plate 25-1 of the endogenous force "F" module is connected and fixed to the upper frame of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25, and the bottom plate 25-2 is connected to the lower edge of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25.

[0263] ② The connecting interface 5 / 27 of the connecting component (m·g)27 is connected to the zipper 29 through the component 12. The zipper 29 is connected to the power-bearing connecting channel 7 / 25 of the upper top plate 25-1 and the rotating drive control component J24-1 connecting channel through the internal force "F" of the upper top plate 25-1 and the connecting channel. This achieves the effect of the gravity f (m·g→"min") of the connecting component 27 of a specific mass + the mechanical thrust f (N·x) generated between the gravity component (m·g)27 and the upper top plate 25-1 by the spring body matrix J33-(2-n) + the mechanical pull f (N·x) generated between the gravity component (m·g)27 and the lower top plate 25-2 by the spring body J33-1 (or the spring body matrix x) [three forces combined into one]. The internal force "F" of NS (5...) and the pulling connection force of the inner ring of the power-bearing wheel J11 (y0) are also combined.

[0264] ③ The upper and lower planes (1-4) / 27 holes of the connecting part 27 are connected to the threaded parts 32 and 31 respectively.

[0265] ③-1, Appendix Figure 59 A connecting component 27 with a specific mass (its own mass m·g → “min”) is selected, and its interface 5 / 27 is connected to the zipper 29 by means of the connecting component;

[0266] ③-2, Appendix Figure 50 , 51 58, the upper plane connecting hole (1-4... etc.) / 27 of the connecting component J27 is connected to the lower plane connecting hole 1 / 32 of the counterclockwise threaded component of the spring body matrix J33-(2-x) through the connecting component; the upper top plate 25-1 is connected and fixed to the upper edge of the module compartment J2-1-4 frame; the upper plane connecting hole 1 / 31 of the clockwise threaded component of the spring body matrix J33-(2-x) is connected to the upper top plate 25-1.

[0267] The lower plane connecting hole (1-4…) / 27 is connected to the upper plane of the clockwise threaded part inner hole 1 / 31 through the connecting part. The lower top plate 25-2 is connected and fixed to the lower edge of the module compartment J2-1-4 frame, and the lower plane inner hole 1 / 32 of the counterclockwise threaded part 32 is connected to the lower top plate 25-2.

[0268] ③-3. Several spring bodies of the composite body J33-(1-x) matrix of clockwise and counterclockwise spiral springs respectively mesh with the clockwise thread of the inner hole of part 31 and the counterclockwise thread of the inner hole of part 32. The spring components of each body J33 generate an endogenous mechanical push / pull force f (N·x) of the spring body J33-(1-x) matrix between the threaded parts 31 and 32 in the push / pull state of the clockwise and counterclockwise threaded parts 31 and 32.

[0269] ④ As needed, the control force transmitted to component 12wk-2 is transmitted to the drive power dynamic transmission adapter body configured through channel J2-1-23, which is connected to the rotation angle of the middle polyhedron 1 / J33 of the drive spring component J33, so as to realize the positioning and random adjustment of the spring mechanical pull force f(N·x) value of the spring pull force matrix.

[0270] 4. 4-6. The resultant force type is: spring mechanical spring / contraction force f(N) + gravity f(m·g) + magnet pair (ns) magnetic force f(N).

[0271] Appendix Figure 60 Based on the application scenario, the module structure model is composed of the intrinsic force NS“F”-Lx of the unit DY, which is the mechanical elastic force f(N·x) of the spring matrix + the gravity of the object of specific material f(m·g) + the magnetic force of the magnet pair (ns) f(N) through the zipper 29, which is a series synthesis of the intrinsic force NS“F”.

[0272] ① Reference Appendix Figure 59 The connection structure between the spring body matrix J33-(2-n) and the upper top plate 25-1, and the connection structure between the spring body matrix J33-(2-n) and the upper plane of the connecting component (m·g) 27 are the same.

[0273] ② Reference Appendix Figure 43 The connection structure between the magnet terminals J22 and J23 and the lower plane of the connecting component (m·g)27, and the connection structure with the lower top plate 25-2 are the same.

[0274] ③ As needed, the control force transmitted to component 12wk-2 is connected to the drive power dynamic transmission adapter body configured in channel J2-1-23, which respectively links the rotation angle of the middle polyhedron 1 / J33 of each spring component J33, so as to realize the positioning and random adjustment of the mechanical thrust f(N) value of the spring component matrix;

[0275] The control force transmitted to component 12wk-2 is transmitted through the drive power dynamic transmission adapter gear J24-2 configured in channel J2-1-23. As needed, the gear J24-2 is randomly rotated by the control force sent to component 12wk-2. By modifying the deflection angle difference corresponding to the magnetic forces J22 and J23, the mechanical thrust f(N) of the spring component matrix of NS(6…)NS“F”-Lx pulled by the zipper 29 is changed in real time from “0” to the maximum value of the maximum value of the weight of a specific mass object f(m·g→“min”) + magnetic pull f(N) from “0” to the maximum value of the maximum value of the maximum mass object.

[0276] Note 1:

[0277] 1. The unit box is a closed structure, with the front and back, and left and right sides symmetrical.

[0278] 2. The dimensions, quantity, and spacing of the horizontal and vertical ribs are based on factors such as the type, assembly layout, load-bearing capacity, movement stroke, and trajectory of the internal structural components.

[0279] ① Vertical tendons and ligaments on the inner posterolateral side 1-1-A0(“Aa”)1-1-A1

[0280] ②, Vertical tendons and ligaments on the inner anterior side 1-2-A0(“Aa”)1-2-A1

[0281] ③, Transverse tendons and ligaments on the inner posterolateral side 1-1-B0(“Bb”)1-1-B1

[0282] ④ Transverse ligaments on the inner anterior side 1-2-B0(“Bb”)1-2-B1

[0283] ⑤, Left side transverse fascia 1-3-C0(“Cc”)1-3-C1

[0284] ⑥, Right side transverse fascia 1-4-C0(“Cc”)1-4-Cc

[0285] ⑦ Structure of the left, right, front, and rear sides inside the box

[0286] Note 2:

[0287] 1. The front and rear, left and right sides of the unit box are positioned and connected to the fixing slots, as well as the type, shape and size, according to the internal structural components, assembly layout, load-bearing capacity, movement stroke, trajectory and other factors.

[0288] 2. Based on the type, specifications, and movement of the internal and external connecting parts, set the positioning, type, and dimensions of the internal and external channels.

[0289] Appendix 2: Types, positioning, and connections of unit enclosure facilities and static components

[0290] 2. Front view of the module connector on the rear side of the functional module box.

[0291] 2.1 Intrinsic force vertical coordinate value |→0| 2.2 Symmetrical support point of the lever scale module, power

[0292] Note 3:

[0293] 1. The connection holes between each functional module panel and the rear side of the enclosure are numbered 2-1-(11……44);

[0294] 2. The connection holes between each functional module panel and related components are numbered 2-1-“11……44”;

[0295] 2.8 Front view of the installation and positioning of the rear functional panel device inside the module box.

[0296] Figure 71

[0297] 3. The corresponding numbered holes on the connection panel of each functional module are connected and fixed together with the corresponding numbered holes on the rear panel inside the box by connecting elements;

[0298] 4. Similarly, the corresponding numbered holes on the connection panels of the same functional modules and the corresponding numbered holes on the front panel inside the box are connected and fixed together as one unit by connecting elements;

[0299] 5. The connection holes of the functional modules on the front and rear connecting panels inside the box form a corresponding relationship.

[0300] 6. The symmetrical fulcrum and power transmission shaft of the lever scale module are connected by the inner ring of the bearing J2-1-21 to realize the symmetrical fulcrum and power transmission of the lever scale;

[0301] 7. The external control components are all connected inside the bearings 28, which are fixed by holes J-1-"22, 23".

[0302] The present invention and its embodiments have been described above. This description is not restrictive, and the actual scope of protection is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this invention should be included within the scope of protection of this invention. Therefore, the scope of protection of this invention should be determined by the scope of the claims.

Claims

1. A dynamic system for the interaction of energy storage endogenous force and load force in a lever balance-type structure, characterized in that, This includes a working structure that connects the dual-unit output power dynamic convergence and links the load components for seamless 360° operation. The structure also includes the component characteristics, combination links, proportioning, interaction, and logical relationships of the physically symmetrical structure of the lever balance mode energy storage endogenous force and load reaction force within the unit. ① The lever scale assembly of the unit lever scale module uses a specific type of machine part 3 as the basic component of the lever scale module; wherein the polyhedral hole 1 / 3 in the middle part of the left and right sides of the lever 3 of the basic component meshes with the polyhedral fulcrum shaft 18; ①-1. The bearing brackets J7z and J7y, which are fixed on the left and right sides of the upper plane of the weighing rod 3, have their multifaceted inner rings meshing with the end points of the left and right multifaceted parts of the reversing screw 4, respectively. ①-2. The symmetrical reversing motion of the screw components 10z and 10y, which bear the internal force on the left and right sides of the weighing rod 3, engages with the screw thread 4. ①-3. The left and right polyhedral holes 2 / 3, 3 / 3 and 4 / 3, 5 / 3 of the machine part 3 respectively mesh with the ratchet gears 13z and 14y through the left and right polyhedral shafts 12z and 12y, or the multi-faceted inner ring of the chain guide wheel J11 at the same point; ② The front and rear force reversing mechanism J9-(1,2) with physical symmetry at the fulcrum is embedded in the front and rear triangular concave guide rails 7 / 3 of the mechanism 3 respectively; ③ The left rear view of the lever scale J3 and the front frame column J8-(1-2) connection hole 1 / 8 are respectively connected and fixed through the connection parts and the connection holes 3 / 10 and 4 / 10 of the physical symmetrical force reversing motion screw part 10z; ④ The front and rear frame columns J8-(3-4) of the weighing beam component 3 are connected and fixed through the connecting holes 4 / 10 and 3 / 10 of the connecting component and the connecting holes 4 / 10 and 3 / 10 of the spiral component 10y of the physical symmetrical force reversal motion, respectively. ⑤ The left rear view of the lever scale J3 and the front frame column J8-1 connection hole 2 / 8 are respectively connected and fixed through the connecting parts and the physical symmetrical force reversing mechanism J9-2 connection hole J9h. The frame column J8-2 connection hole 2 / 8 are respectively connected and fixed through the connecting parts and the physical symmetrical force reversing mechanism J9-1 connection hole J9q. ⑥ The front and rear frame columns J8-3 connecting holes 2 / 8 of the weighing beam component 3 are connected and fixed to the front reversing component J9-1 of the physical symmetrical force through the connecting components and the connecting holes J9q. The frame columns J8-4 connecting holes 2 / 8 are connected and fixed to the front reversing component J9-1 of the physical symmetrical force through the connecting components and the connecting holes J9h. ⑦ The left rear view of the weighing beam component 3 and the front frame column J8-(1-2) connection holes 3 / 8 are respectively connected and fixed to the physical symmetry endogenous force left polyhedral bearing shaft 12z through the connecting components; ⑧. The front and rear frame columns J8-(3-4) of the weighing beam component 3 are connected and fixed to the bearing shaft 12y of the physically symmetrical endogenous right polyhedron through the connecting components.

2. The lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 1, characterized in that, The unit lever scale mode fulcrum bearing endogenous force NS"F"-Lx specific gravity"% value physical symmetrical reversing component includes: ① The external control micro-force of the connecting component 12wk-1 is connected to the transmission shaft 12 through the configured special power dynamic adapter component; ② The multifaceted body 3 / 4 of the reversing screw 4 is meshed with the multifaceted inner hole 4 / 5 of the force shifting gear J5, and the multifaceted inner hole 1 / 30 of the transmission gear 30 is meshed with the multifaceted transmission shaft 12. The transmission gear 30 meshes with the multifaceted body 3 / 4 of the reversing screw 4 through the multifaceted inner hole 4 / 5 of the shifting gear J5. ②-1, The inner ring of the bearing of the bracket J7(0) connected to the middle of the upper end face of the scale bar 3 by the left extension polyhedral body 3 / 5 of the reversing gear J5 meshes with the inner ring of the bearing of the left and right bracket J7z and J7y. ②-2, The inner ring of the bearing of the bracket J7(0) connected to the middle of the upper end face of the scale bar 3 by the left extension polyhedral body 3 / 5 of the reversing gear J5 meshes with the inner ring of the bearing of the left and right brackets J7z and J7y; the end points of the left and right polyhedral bodies of the reversing screw 4 mesh with the inner ring of the bearing of the left and right brackets J7z and J7y. ③ When the bearing component 12a approaches the static point at za|45|° throughout its entire stroke, the teeth of the transmission gear 30 mesh with 1 / 5 of the teeth of the force reversing gear J5; ③-1. When the bearing component 12y approaches the static point ya|45|° throughout its entire stroke, the teeth of the transmission gear 30 mesh with 2 / 5 of the teeth of the force reversing gear J5; ③-2. The screw component 10 (z, y) with the screw 4 thread meshes with the screw thread, which is a symmetrical force reversing motion. ④ The clockwise and counterclockwise rotational micro-force of the driving component 12wk-1 is transmitted to the polyhedral transmission shaft 12, which meshes with the inner hole of the multi-faceted gear 30, through the configured adapter connection device. The teeth of the gear 30 mesh with 2 / 5 and 1 / 5 of the teeth of the force reversing gear J5 in a time-sharing or continuous manner. ④-1. The inner hole of the polyhedral gear J5 meshes with the polyhedral 3 / 4 section in the middle of the transposition screw 4. ④2. The thread of the transposition screw 4 meshes with the internal thread of the physically symmetrical reversing motion spiral component 10 (z, y); ⑤ The physical symmetry of the lever scale module structure is that the left and right center polyhedral inner hole 1 / 3 of the lever scale 3 is connected to the central axis 18 of the polyhedron, and the center point of the left and right center polyhedral inner hole 1 / 3 of the lever scale 3 is on a parallel line with the center point of the fulcrum axis 18, as well as the center points of the endogenous force NS"F"-Lx bearing components 12z and 12y.

3. A lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 1 or 2, characterized in that, The endogenous force NS"F"-Lx [object gravity type NS((1-1, or 1-2)(m·g(1…), or m·g(1+…1))] of the unit DY module compartment J2-1-4 is suspended by zipper 29 from the module structure of the inner ring of the bearing wheel J11(y0), including: ① The long or square frame connection interface 63-〔(1)-(4)〕 on the gravity frame J64-1 is connected to the linking mechanism J61 of the hanging chain 29 through the chain 62-(1-4) respectively, so as to realize the vertical connection between the gravity frame and the gravity of the liquid mg(1+…1) it carries and the inner ring of the bearing wheel J11(y0); ② The upper part of the gravity frame J64, or the square frame J64-1 and the lower part of the square frame J64-2, and the four upright body 66-(1-4) are connected and constructed by the connection interface 63-〔(1)-(4)〕; ③, Pressure water valve box 68, pressure water outlet interface 67, physical water source positioning interface 76, pressure chamber water pressure variable stabilizing spring positioning component 65-〔(1)-(4)〕 at the four corners, gravity water tank J74, water pressure stabilizing spring 71-〔(1)-(4)〕 is configured between the spring positioning component 65-〔(1)-(4)〕 at the upper end of gravity frame column body 66-(1-4) and the upper end of gravity water tank body J74; ④ The bottom plane of gravity water tank J74 is connected to the upper plane of pressure water tank 83, and the lower plane of pressure water tank 83 is connected to J64-2 at the bottom of gravity frame through connecting device 84; ⑤ The pressure water tank 83 volume and water replenishment assembly are connected by gear 38 and ratchet gear 36 of the lifting device TS-(1-4, or more); the multi-faceted transmission shafts 12-2 and 12-1 that mesh with the multi-faceted inner ring of gear 38 and ratchet gear 36 are connected to the parallelogram frame J64-1 on the gravity frame through bearings; ⑥ The 38 teeth of the lifting device TS gear mesh with the rack 1 / J85 teeth of the rack frame body J85, and the 36 teeth of the ratchet gear mesh with the rack 2 / J85 teeth of the rack frame body J85. ⑦ The lower crossbeam of the rack and pinion frame body J85 of the lifting device TS is connected to the upper frame of the gravity water tank J74. ⑧ The 38 teeth of the lifting device TS gear mesh with the rack 1 / J85 teeth of the rack frame body J85, and the 36 teeth of the ratchet gear mesh with the rack 2 / J85 teeth of the rack frame body J85. ⑨ The lower crossbeam of the rack and pinion frame body J85 of the lifting device TS is connected to the upper frame of the gravity water tank J74.

4. A lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 1 or 2, characterized in that, The endogenous force NS"F"-Lx [object gravity type NS(G=m·g) + spring mechanical contraction force f(N)] of the unit DY module compartment J2-1-4 is connected in series to form a "pull" force value, which is then vertically pulled to the inner ring of the supporting wheel J11(y0) module via zipper 29, including: ① The gravity object (m·g) 26 is connected to the interface 5 / 26 through the machine part 6-2, which is connected to the zipper 29 and the power bearing wheel J11 (y0) inner ring body for vertical pull connection; ② The bottom plane of the gravitational object (m·g) 26 is connected to the upper plane of the clockwise threaded part 31; the lower top plate 25 is connected and fixed to the lower edge of the module compartment J2-1-4 frame, and the lower plane of the counterclockwise threaded part 32 is connected to the lower top plate 25. ②-1. The upper spring body of the composite body J33 with the clockwise thread of the upper helical spring and the counterclockwise thread of the lower spring body engages with the inner hole of the component 32 with the clockwise thread. ②-2. The bottom plane of the object (m·g)26 can be connected to several spring-loaded interactive bodies J33 and parts 31 and 32, forming a spring tension matrix composed of one or more elastic interactive bodies with tensile mechanical force values ​​f ((N) or (x*N)) in series. ③ The control force transmitted to component 12wk-2 is transmitted to the drive power dynamic transmission adapter body configured through channel J2-1-23, and linked to the middle polyhedron 1 / J33 of each spring component J33.

5. A dynamic system for the interaction of endogenous energy storage force and load force in a lever balance structure according to claim 1 or 2, characterized in that, The intrinsic force NS"F"-Lx [magnetic force f(N) of magnet terminal pair (nn) or f(ss) + gravity f(m·g) of specific material object + magnetic force f(N) of magnet terminal pair (ns)] of the unit DY module compartment J2-1-4 is combined in series to form a "pull" force value, which is pulled by the module to the inner ring of the bearing wheel J11(y0) through zipper 29, including: ① The top plate 25-1 of the endogenous force NS"F"-Lx module is connected and fixed to the upper frame of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25, and the bottom plate 25-2 is connected to the lower edge of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25. ② The connecting component (m·g) 27 and the connecting interface 5 / 27 are connected to the zipper 29 through the component 12. The zipper 29 is connected to the inner ring of the power bearing wheel J11 (y0) through the center channel of the magnet terminal J21 (ss), the center channel of the magnet terminal J20 (nn), the center channel of the rotary drive control component J24-1, and the channel 7 / 25 of the top plate 25-1. ②-1. The upper top plate 25-1 is connected to the inner ring of the bearing 6 by meshing with the convex polyhedron 9 / 25. The inner ring of the rotation drive gear J24-1 achieves rotational movement around the convex polyhedron 9 / 25 of the upper top plate 25-1 by connecting with the outer ring of the bearing 6. ②-2. The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the upper surface of the drive gear J24-1 abut against the ball concave track ring 8 / 25 on the lower surface of the upper top plate 25-1, so as to realize the gapless and rotatable motion connection between the drive gear J24-1 and the upper top plate 25-1. ②-3. The "n" and "s" magnetic poles of the magnet correspond to the physical domain marked by the digital codes "1" and "0" of the terminal frame, such as magnet terminals J20, J21, J22, J23, etc. Multiple magnets are arranged in a specific combination of "n" and "s" magnetic poles, and the physical domain marked by the frame numbers "1" and "0" is fixedly embedded in the disk. ②-4. The connection hole (1-4) / 20 on the upper plane of the magnetic terminal J20 frame is connected and fixed to the connection hole (1-4) / 24-1 on the lower plane of the gear J24-1 ring body through the connecting parts; ③ Select a connecting part 27 made of a specific material (its own mass m·g→"min"), and the zipper 29 is connected to the inner ring of the bearing wheel J11(y0) by passing the connecting part through its inner opening 5 / 27. ④ The upper plane connecting hole (1-4) / 27 of the connecting component J27 is connected to the lower plane connecting hole (1-4) / 21 of the magnetic terminal J21 frame through the connecting component, and the lower plane connecting hole (1-4) / 27 is connected and fixed to the upper plane connecting hole (1-4) / 22 of the magnetic terminal J22 frame through the connecting component; ⑤ The inner ring of the rotary drive gear J24-2 is connected to the outer ring of the bearing 6, and the lower top plate 25-2 is fixed by meshing with the polyhedral inner ring of the bearing 6 inside the rotary drive gear J24-2 through the convex polyhedron 9 / 25. ⑤-1. The connecting hole (1-4) / 23 on the lower plane of the magnet terminal J23 frame is connected to the connecting hole (1-4) / 24-2 on the upper plane of the gear J24-2 ring body through the connecting parts; ⑤-2. The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the lower surface of gear J24-2 abut against the upper surface of the lower top plate 25-2 ball concave track ring 8 / 25, so as to achieve a gapless connection between the lower surface of gear J24-2 and the upper surface of the lower top plate 25-2. ⑤-3. The longitudinal (y) physical "link" positioning of gear J24-2 and lower top plate 25-2 is achieved by embedding the balls between the inner and outer rings of bearing 6 into the track grooves of the inner and outer rings.

6. The lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 5, characterized in that, The intrinsic force NS"F"-Lx [magnet terminal (nn) or (ss)f(N) + gravity of the object of specific material f(m·g) + spring mechanical force f((N), or (N*x))] of the unit DY module compartment J2-1-4 is connected in series to form a "pull" force value, which is pulled by the module to the inner ring of the bearing wheel J11(y0) through zipper 29, including: ① The inner ring of the power bearing wheel J11(y0) is connected to the zipper 29. The zipper 29 is connected to the specific mass linking component 27(m·g)27 and the connection interface 5 / 27 through the internal force "F" power bearing linking channel 7 / 25 of the upper top plate 25-1 and the linking channel of the rotation drive control component J24-1. ② The upper top plate 25-1 is connected to the inner ring of the bearing 6 by meshing with the convex polyhedron 9 / 25, and the inner ring of the gear J24-1 is connected to the outer ring of the bearing 6. ②-1. The balls arranged in several 81 / 24-8n / 24 concave ball cavities on the upper surface of gear J24-1 abut against the lower surface of the upper top plate 25-1 ball concave track ring 8 / 25. ②-2. The magnet terminals of multiple magnets such as J20 and J21 are arranged in a specific combination of (ns) magnetic pole positions and are fixed in the physical area marked by the numbers 1 and 0 in the frame inside the outer circle. ②-3. The connecting hole (1-4) / 20 on the upper plane of the magnet terminal J20 frame is connected and fixed to the connecting hole (1-4) / 24-1 on the lower plane of the gear J24-1 ring body through the connecting parts; ②-4. The upper plane connection hole (1-4) / 27 of the connecting component J27 is connected to the lower plane connection hole (1-4) / 21 of the magnetic terminal J21 frame through the connecting component; ③ The connecting hole (1-4) / 27 on the lower plane of the connecting component J27 is connected to the upper plane of the inner hole clockwise threaded component 31, which is a spring tension matrix composed of one or more elastic interactive mechanical forces f ((N) or (N*x)) in series; the lower top plate 25-2 is connected and fixed to the lower edge of the module compartment J2-1-4 frame, and the lower plane of each inner hole counterclockwise threaded component 32 is connected to the lower top plate 25-2; ④ The spring body of the composite body J33 with the clockwise and counterclockwise spiral springs engages with the clockwise thread of hole 31 and the counterclockwise thread of inner hole 32, respectively; ④-1. The bottom plane of object (m·g)27 can be connected to 1 or even multiple spring bodies J33 and parts 31 and 32 elastic interaction body matrix; ④-2. The control force transmitted to component 12wk-2 is transmitted to the drive power dynamic transmission adapter body configured through channel J2-1-23, and links the drive spring component J33 middle polyhedron 1 / J33.

7. A lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 1 or 2, characterized in that, The endogenous force NS"F"-Lx of the unit DY module compartment J2-1-4 [spring matrix mechanical thrust f(N*x) + gravity of the specific material object f(mg) + spring mechanical tension f(N)] is combined in series to form a "pull" force value, which is pulled by the module to the inner ring of the bearing wheel J11(y0) through zipper 29, including: ① The top plate 25-1 of the endogenous force "F" module is connected and fixed to the upper frame of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25, and the bottom plate 25-2 is connected to the lower edge of the module compartment J2-1-4 frame through the connecting parts configured in the connecting holes (1-4) / 25; ② The connecting component (m·g) 27 connects to the zipper 29 via the component 12. The zipper 29 connects to the inner ring of the bearing wheel J11 (y0) via the internal force "F" power bearing connecting channel 7 / 25 of the upper top plate 25-1 and the rotating drive control component J24-1 connecting channel. ③ The upper plane connecting holes (1-4... etc.) / 27 of the connecting component J27 are connected to the lower plane connecting holes 1 / 32 of the counterclockwise threaded component of the spring body matrix through the connecting component, and the upper plane connecting holes 1 / 31 of the clockwise threaded component are connected to the upper top plate 25-1. ④ The lower plane connecting hole (1-4…) / 27 of the connecting component J27 is connected to the upper plane connecting hole 1 / 31 of the clockwise threaded component through the connecting component; the lower plane of the inner hole 1 / 32 of the counterclockwise threaded component is connected to the lower top plate 25-2. ⑤ The spring bodies of each upper clockwise and lower counterclockwise spiral spring assembly body J33 respectively engage with the clockwise thread in the hole of part 31 and the counterclockwise thread in the inner hole of part 32; ⑥ The control force transmitted to component 12wk-2 is connected to the drive power dynamic transmission adapter body configured through channel J2-1-23, and respectively to the spring component J33 middle polyhedron 1 / J33 on component J27, or the spring component J33 middle polyhedron 1 / J33 below.

8. A lever balance-mode structure energy storage endogenous force and load force interaction dynamic system according to claim 1 or 2, comprising a shaping component for dual-unit output power dynamic shaping, characterized in that, ① The unit output fulcrum shaft 18 of the multifaceted auxiliary gear 39wk-1 meshes with the inner hole of the ratchet gear 36, 37 and is connected to the ratchet gear 36. ② The ratchet gear 36, which transmits power through the counterclockwise rotation of the polyhedral internal bore, meshes with the ratchet gear 37, which transmits power through the clockwise rotation of the polyhedral internal bore. ③ The counterclockwise rotation of the multifaceted internal hole transmits the meshing of the ratchet gear 36 and gear 38-1; ④ The clockwise rotation of the multifaceted internal hole transmits the meshing of the ratchet gear 37 and gear 38-2; ⑤ Gear 38-1 and gear 38-2 mesh.

Images