Novel new energy engine
Through the reaction characteristics of A1 and A2 elements and the precise mechanical structure design, the power demand and emission problems of large-scale equipment are solved, and a new type of new energy engine with zero emissions and ultra-high power output is realized, which is suitable for a variety of high-power scenarios.
Patent Information
- Application Number
- CN202511196274.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-08-26
- Publication Date
- 2025-10-28
AI Technical Summary
Existing new energy technologies are insufficient to meet the power requirements of large-scale equipment and suffer from high carbon emissions and high maintenance costs.
The reaction characteristics of A1 and A2 elements are combined with precision mechanical structure design. Initial power is provided by diesel engine startup, and the operation phase is driven by the autonomous reaction of A1 and A2 elements to achieve zero emissions and ultra-high power output.
It achieves ultra-high power output, is suitable for large equipment, has zero emissions, low noise, low temperature, and high mechanical efficiency. It is suitable for shipborne power, full ship power, large-scale fixed and mobile power generation and other scenarios, and has high practicality and promotion value.
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Figure CN120845174A_ABST
Abstract
Description
Technical Field
[0001] This application relates to the technical field of new energy power, and in particular to a novel new energy engine. Background Technology
[0002] Currently, traditional power equipment relies heavily on fossil fuels, resulting in serious emissions pollution, low energy efficiency, and limited power output. Existing new energy technologies, such as electromagnetic drives and fuel cells, either require continuous external power consumption or their power output is insufficient to meet the needs of large-scale equipment such as aircraft carrier propulsion and megawatt-class power plants.
[0003] For example, existing aircraft carrier electromagnetic catapult systems rely on massive energy storage devices and consume a lot of electricity, with limited flexibility in power adjustment; gas turbines or steam turbines in large power plants suffer from high carbon emissions and high maintenance costs. Therefore, developing a new type of power equipment that can provide initial drive through conventional power (such as diesel engines) during startup, requires no external energy input during operation, has zero emissions, and boasts ultra-high power has become an urgent need for the industry.
[0004] Based on the unique reaction characteristics of Al and A2 elements and combined with precision mechanical structure design, this invention proposes a new type of new energy engine that can replace traditional power equipment, filling the technological gap in the field of new energy power with ultra-high power and zero external energy consumption during operation. Summary of the Invention
[0005] The present application aims to solve one of the technical problems in the related art at least to a certain extent.
[0006] To achieve the above objectives, the first aspect of this application proposes a novel new energy engine, including a power-operating body and a diesel engine starter. The power-operating body comprises: an outer steel sleeve forming a vertical support frame, with a top cover fixed to the top by an upper bolt; an upper O-ring gasket is sandwiched between the upper cover and the outer steel sleeve to achieve axial sealing; air inlet and outlet holes are opened on the side wall of the outer steel sleeve, connecting to the internal chamber to balance air pressure; a left fixing inner sleeve bolt is provided on the left side of the outer steel sleeve, the left fixing inner sleeve bolt being threadedly connected to the outer steel sleeve for clamping the positioning piston inner sleeve; the positioning piston inner sleeve houses an A1 piston, above which are sequentially arranged an upper A2 element, an upper A2 spring, and an upper spacing positioning seat (spacing 0.3-0.5mm). The following components are arranged sequentially below: a lower A2 element, a lower A2 spring, and a lower spacing positioning seat (spacing 0.3-0.5mm); the bottom end of the outer steel sleeve is connected by a lower bolt, and an O-ring seal is sandwiched between the outer steel sleeve and the lower bolt to achieve axial sealing; an oil inlet bolt is provided at the bottom end of the outer steel sleeve, and an oil level line is provided on the side wall for observing the oil level; the diesel engine starting includes: the top end of the round shaft is connected to the bottom end of the outer steel sleeve of the working body, a positioning round shaft seat is fitted on the outer side of the round shaft, and an oil seal is sandwiched between the two to achieve radial sealing; an oil drain bolt is provided below the positioning round shaft seat; the bottom end of the round shaft is connected to the crankshaft through a connecting rod, and the crankshaft is connected to the transmission gear; the transmission gear meshes with the magnetic cylinder rotor, the outer side of the magnetic cylinder rotor is fitted with the stator, and the rotating parts are supported by bearings.
[0007] In addition, the novel new energy engine proposed in this application may also have the following additional technical features:
[0008] In one embodiment of this application, the upper A2 element and the lower A2 element are symmetrically distributed on both sides of the A1 piston. The upper A2 spring and the lower A2 spring provide elastic preload, and the upper spacing positioning seat and the lower spacing positioning seat limit the axial displacement range, so that the A1 piston can reciprocate within the inner sleeve of the positioning piston to trigger the reaction of the A1 and A2 elements.
[0009] In one embodiment of this application, the upper O-ring gasket and the lower O-ring gasket are annular elastic elements, which are respectively interference-fitted with the top and bottom ends of the outer steel sleeve to achieve axial sealing.
[0010] In one embodiment of this application, the left fixing inner sleeve bolt is connected to the outer steel sleeve by a thread and clamps the positioning piston inner sleeve to limit its radial movement.
[0011] In one embodiment of this application, the diesel engine starting module comprises a transmission gear, a magnetic cylinder rotor, and a stator forming an electromagnetic drive structure, which converts electrical energy into mechanical energy during the starting phase to drive the A1 piston to initially reciprocate and trigger the reaction of A1 and A2 elements; when the reciprocating frequency of the A1 piston reaches 50 times / second, the module automatically stops working.
[0012] In one embodiment of this application, the inner wall of the positioning round shaft seat is provided with a guide groove, which slides with the protrusion on the outer wall of the round shaft to restrict the rotational freedom of the round shaft, allowing it to only perform reciprocating motion in the axial range of 0-90mm.
[0013] The advantages of this application compared to existing technologies are:
[0014] (1) Relying on the high efficiency reaction characteristics of A1 and A2 elements, it can output ultra-high power, which can meet the power requirements of various large-scale equipment and is suitable for various high-power scenarios such as shipboard power, shipboard power, large-scale fixed and mobile power generation.
[0015] (2) During the operation, A1 and A2 elements are continuously driven by a diesel engine to maintain the reaction operation. The whole process achieves zero emissions, and is radiation-free, low-temperature, and low-noise. The stable drive of the diesel engine ensures the continuity of power output, and also improves the pollution problem caused by the reliance on fossil fuels in traditional power equipment.
[0016] (3) Through detailed design of the positioning piston inner sleeve, sealing gasket, guide groove, etc., the mechanical working efficiency is significantly improved, which can ensure the efficient conversion of energy and the long-term stable operation of the system, reduce the occurrence of failures, and improve the durability of the equipment.
[0017] (4) It can be adapted to various scenarios such as large mobile devices, large fixed power stations, industrial and agricultural power, and can be used from large aircraft carriers to automobiles and industrial equipment. It has strong practicality and promotion value.
[0018] Additional aspects and advantages of the present application will be given in part in the description below, and in part will become apparent from the description below, or will be learned through practice of the present application. Attached Figure Description
[0019] The above and / or additional aspects and advantages of the present application will become apparent and easily understood from the following description of the embodiments in conjunction with the accompanying drawings, in which:
[0020] Figure 1 This is a schematic diagram of the structure of a novel new energy engine according to an embodiment of this application;
[0021] As shown in the figure: 1. Upper bolt; 2. Upper cover; 3. Upper O-ring gasket; 4. Air inlet / outlet; 5. Left fixing inner sleeve bolt; 6. Outer steel sleeve; 7. Lower bolt; 8. Lower O-ring gasket; 9. Oil inlet bolt; 10. Positioning piston inner sleeve; 11. Upper A2 spring; 12. Upper A2 element; 13. A1 piston; 14. Lower A2 element; 15. Lower A2 spring; 16. Lower spacing positioning seat; 17. Upper spacing positioning seat; 18. Oil level line; 19. Round shaft; 20. Positioning round shaft seat sleeve; 21. Oil drain bolt; 22. Oil seal; 23. Connecting rod; 24. Crankshaft; 25. Transmission gear; 26. Magnet cylinder rotor; 27. Stator; 28. Bearing. Detailed Implementation
[0022] Embodiments of this application are described in detail below, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and intended to explain this application, and should not be construed as limiting this application. Rather, embodiments of this application include all variations, modifications, and equivalents falling within the spirit and scope of the appended claims.
[0023] The following describes a novel new energy engine according to an embodiment of this application, with reference to the accompanying drawings.
[0024] like Figure 1 As shown in the figure, a novel new energy engine according to an embodiment of this application includes two core modules: a power-generating body and a diesel engine starting module. The power-generating body is the core of energy generation and conversion, outputting power through the reaction of Al and A2 elements; the diesel engine starting module is only used to provide initial power to start the engine (it automatically shuts down after starting). The two are rigidly connected by a mechanical structure and work together to achieve power output.
[0025] Example 1: Detailed Structure and Component Description of the Main Working Body
[0026] 1. Outer steel sleeve 6
[0027] The outer steel sleeve 6 serves as the supporting frame for the entire working body. It is made of high-strength alloy steel through forging and is shaped like a vertical cylinder. The inner wall is precision ground (surface roughness ≤0.8μm) to ensure the assembly accuracy of internal components. The outer steel sleeve 6 provides a stable mounting reference and protection for the internal components.
[0028] 2. Top sealing structure
[0029] The top of the outer steel sleeve 6 is fixed to the top cover 2 by the upper bolt 1. The top cover 2 is a circular steel plate that fits against the top surface of the outer steel sleeve 6. The upper bolt 1 is an M16 high-strength bolt, a total of 6 bolts, which are evenly distributed along the circumference of the top cover 2. After passing through the through hole of the top cover 2, the bolts are threadedly connected to the threaded hole at the top of the outer steel sleeve 6.
[0030] An O-ring gasket 3 is sandwiched between the upper cover 2 and the outer steel sleeve 6. The gasket is made of fluororubber and fills the gap through elastic deformation to achieve axial sealing and prevent leakage of internal energy or lubricant.
[0031] 3. Air inlet and outlet 4
[0032] Two air inlet and outlet holes 4 are symmetrically opened on the side wall of the outer steel sleeve 6 in the horizontal direction. The air inlet and outlet holes 4 connect the internal cavity of the outer steel sleeve 6 with the outside. A one-way valve is installed in the hole. When the pressure in the internal cavity is too high, the one-way valve will automatically open to release pressure. When the pressure is too low, the outside gas will be replenished through the air hole to balance the internal and external air pressure and avoid pressure fluctuations from affecting the operation of the component.
[0033] 4. Positioning piston inner sleeve 10 and fixing structure
[0034] The left side wall of the outer steel sleeve 6 is provided with a left fixing inner sleeve bolt 5. This bolt is an M12 fine-thread bolt, which mates with the threaded hole on the side wall of the outer steel sleeve 6. The end of the bolt extends into the interior of the outer steel sleeve 6 and contacts the outer wall of the positioning piston inner sleeve 10. The positioning piston inner sleeve 10 has a cylindrical structure, and its outer wall is clearance-fitted with the inner wall of the outer steel sleeve 6. It is clamped and fixed by the tightening force of the left fixing inner sleeve bolt 5, which restricts its radial wobble and ensures the coaxiality of the internal components.
[0035] 5. Internal components of the positioning piston inner sleeve 10
[0036] The inner sleeve 10 of the positioning piston houses the piston 13 of A1, which is a solid cylinder (made of high-temperature resistant ceramic) and is in clearance fit with the inner wall of the inner sleeve 10 of the positioning piston, allowing it to slide freely along the axial direction.
[0037] Above piston A1 13, elements A2 12, spring A2 11, and positioning seat 17 are arranged sequentially:
[0038] The upper A2 element 12 is a ring structure, made of rare earth permanent magnet material, and is bonded and fixed to the top surface of the A1 piston 13 by high temperature resistant adhesive.
[0039] The upper A2 spring 11 is a cylindrical helical compression spring made of 60Si2Mn with a free length of 75mm. After assembly, it is pre-compressed to 45mm to provide an elastic preload of 2800N, which makes the upper A2 element 12 and the A1 piston 13 fit tightly together.
[0040] The upper spacing positioning seat 17 is a ring-shaped gasket made of polytetrafluoroethylene, which is fixed on the annular step on the inner wall of the positioning piston inner sleeve 10. A gap of 0.3-0.5mm is reserved between its lower end face and the top face of the A1 piston 13 to limit the maximum upward displacement of the A1 piston 13 and avoid rigid collision with the upper cover 2.
[0041] Symmetrically positioned below piston A1 13 are lower A2 element 14, lower A2 spring 15, and lower spacing positioning seat 16.
[0042] The lower A2 element 14 is a ring structure with the same structure as the upper A2 element 12. It is made of rare earth permanent magnet material (forming a reaction pair with the upper A2 element) and is bonded and fixed to the bottom end face of the A1 piston 13.
[0043] The structural parameters of the lower A2 spring 15 are the same as those of the upper A2 spring 11, providing symmetrical elastic preload.
[0044] The lower spacing positioning seat 16 has the same structure as the upper spacing positioning seat 17. It is fixed on the annular step at the lower part of the inner wall of the inner sleeve 10 of the positioning piston, and a gap of 0.3-0.5mm is reserved between it and the bottom end face of the A1 piston 13 to limit its maximum downward displacement.
[0045] 6. Bottom sealing and lubrication structure
[0046] The bottom end of the outer steel sleeve 6 is connected and fixed by the lower bolt 7. The lower bolt 7 is an M16 high-strength bolt of the same specification as the upper bolt 1, and there are 6 of them. They are evenly distributed along the circumference of the bottom end. The lower O-ring gasket 8 is sandwiched between the lower bolt 7 and the outer steel sleeve 6. Its material, structure and sealing principle are the same as those of the upper O-ring gasket 3, so as to achieve axial sealing at the bottom end.
[0047] An oil inlet bolt 9 is located at the center of the bottom end of the outer steel sleeve 6. This bolt is an M10 hexagon socket head cap bolt with an internal axial oil passage that connects to the mating surfaces of the inner sleeve of the positioning piston 10 and the A1 piston 13. It is used to inject special lubricating oil (viscosity grade ISO VG 68) to reduce the coefficient of friction between the two through the lubricating oil film. An oil level line 18, which is an embedded transparent quartz tube, is located on the lower part of the side wall of the outer steel sleeve 6. It is arranged vertically to visually observe the internal lubricating oil level and ensure that the lubrication system has sufficient oil (lubricating oil needs to be added when the oil level is below the lower limit).
[0048] Example 2: Detailed Structure and Component Description of the Diesel Engine Starting Module
[0049] (Note: This module is only used to provide initial power during the start-up phase. It will automatically stop working once the engine reaches stable operation.)
[0050] 1. Circular shaft 19 and positioning structure
[0051] The circular shaft 19 is a stepped cylinder. Its top end is bolted to the bottom end of the outer steel sleeve 6 of the working body through a flange. A copper gasket is provided between the flange and the bottom end of the outer steel sleeve 6 to ensure a tight connection without loosening.
[0052] A positioning round shaft seat 20 is fitted on the outer side of the round shaft 19. The bushing is made of tin bronze and is cylindrical. The inner wall has three guide grooves along the axial direction, which correspond to the three protrusions on the outer wall of the round shaft 19 and slide in fit, restricting the rotational freedom of the round shaft 19 and allowing it to reciprocate along the axial direction only.
[0053] 2. Sealing and oil draining structure
[0054] An oil seal 22 is provided at the upper and lower parts between the round shaft 19 and the positioning round shaft seat 20. The oil seal is a skeleton-type nitrile rubber oil seal (model TC75×110×14), with the lip facing inward. It is clamped to the outer wall of the round shaft 19 by a spring to prevent lubricating oil from leaking from the gap between the two.
[0055] The bottom side of the positioning round shaft seat 20 is provided with an oil drain bolt 21. This bolt is an M8 socket head cap screw with a magnetic suction cup integrated in the head, which is used to adsorb impurities such as iron filings in the lubricating oil. Regularly loosening the oil drain bolt 21 can drain waste oil and clean impurities at the same time, ensuring the cleanliness of the lubrication system.
[0056] 3. Transmission Structure
[0057] The bottom end of the round shaft 19 is connected to the crankshaft 24 via a connecting rod 23. The connecting rod 23 has an I-shaped cross section (material QT500-7) and shaft holes at both ends. It is hinged to the journal at the bottom end of the round shaft 19 and the crank pin of the crankshaft 24 via a bearing bush (material Babbitt alloy). The clearance between the bearing bush and the journal is 0.05-0.08mm to ensure flexible rotation without jamming.
[0058] The crankshaft 24 is an integral forged structure (material 42CrMo) and is supported on the machine body by two bearings 28. The bearings are self-aligning roller bearings (model 22219) with a rated dynamic load ≥190kN, which can withstand the radial and axial forces when the crankshaft 24 rotates, ensuring stable rotation.
[0059] One end of the crankshaft 24 is connected to the transmission gear 25 via a flat key (specification 18×11×75). The transmission gear 25 is a spur gear (module 5, number of teeth 25, pressure angle 20°), and the tooth surface is carburized and quenched (hardness HRC58-62), which has excellent wear resistance. The transmission gear 25 meshes with the external teeth of the magnetic cylinder rotor 26 (meshing clearance 0.2-0.3mm) to realize power transmission.
[0060] 4. Electromagnetic drive structure
[0061] The magnetic cylinder rotor 26 is a cylindrical permanent magnet rotor with 36 neodymium iron boron magnets (grade N42) evenly embedded on its surface. The magnetic poles are arranged alternately along the circumference (N poles and S poles are distributed alternately). The stator 27 is fitted on the outside of the magnetic cylinder rotor 26. The stator is a toroidal iron core with three-phase windings wound on it. When three-phase alternating current is applied, a rotating magnetic field is generated, which interacts with the permanent magnet magnetic field of the magnetic cylinder rotor 26 to drive the magnetic cylinder rotor 26 to rotate. In turn, the crankshaft 24 is driven to rotate through gear meshing.
[0062] Example 3: Workflow
[0063] 1. Start-up Phase
[0064] Start the diesel engine starting module: Three-phase alternating current is supplied to the stator 27, the stator generates a rotating magnetic field, which drives the magnetic cylinder rotor 26 to rotate.
[0065] The magnetic cylinder rotor 26 drives the transmission gear 25 and crankshaft 24 to rotate through gear meshing. The rotational motion of the crankshaft 24 is converted into the axial reciprocating motion of the round shaft 19 through the connecting rod 23.
[0066] The round shaft 19 drives the outer steel sleeve 6 and the A1 piston 13 in the inner sleeve 10 of the positioning piston to move up and down. The upper A2 spring 11 and the lower A2 spring 15 are alternately compressed and extended, so that the upper A2 element 12 and the lower A2 element 14 gradually approach and contact each other (trigger reaction conditions).
[0067] When the reciprocating frequency of piston 13 in A1 reaches 50 times / second, the diesel engine starting module automatically cuts off power and stops working (completing the starting mission).
[0068] 2. Operational Phase
[0069] Under the initial inertia, piston 13 of A1 continues to move up and down. After the upper A2 element 12 and the lower A2 element 14 come into contact, they react continuously, generating energy to drive piston 13 of A1 to reciprocate at high speed along the inner sleeve of the positioning piston 10 (autonomously maintaining the motion state).
[0070] The reciprocating motion of piston 13 is transmitted to crankshaft 24 through outer steel sleeve 6, round shaft 19, and connecting rod 23, and is converted into continuous rotational motion of crankshaft 24 to achieve power output;
[0071] During operation, the air inlet and outlet ports 4 automatically balance the air pressure in the cavity through the one-way valve to avoid abnormal pressure; the oil inlet bolt 9 continuously injects lubricating oil, and the oil level line 18 monitors the oil quantity to ensure that the mating surfaces of the A1 piston 13 and the positioning piston inner sleeve 10 are sufficiently lubricated.
[0072] The upper spacing positioning seat 17 and the lower spacing positioning seat 16 strictly limit the displacement range of piston 13 A1 to prevent overtravel collision; the guide groove of the positioning round shaft seat 20 cooperates with the protrusion of the round shaft 19 to ensure that the round shaft 19 only moves axially and avoids rotational interference.
[0073] 3. Shutdown phase
[0074] By externally controlling the cutoff of the reaction conditions of elements A1 and A2 (such as forcibly separating element contact), the movement of piston 13 of A1 gradually decelerates.
[0075] Under the restoring force of the upper and lower springs, piston 13 returns to its initial position, and element 12 of upper A2 separates from element 14 of lower A2, thus stopping the reaction.
[0076] Loosen the drain plug 21 to drain the waste oil and clean up impurities; close the oil inlet plug 9 to complete the shutdown maintenance.
[0077] In summary, the novel new energy engine of this application clearly defines the power logic through the collaborative design of the power-generating main body and the diesel engine starting module: the diesel engine starting module only provides short-term initial power during the startup phase to drive elements A1 and A2 to reach the reaction conditions; once the stable operation phase is reached, the power-generating main body continuously outputs power entirely driven by the autonomous reaction of elements A1 and A2, without the need for the diesel engine or other external power sources. This design not only ensures smooth system startup through the short-term starting of the diesel engine, but also achieves autonomous driving during the operation phase based on the reaction characteristics of elements A1 and A2, completely resolving the logical contradiction of the power source and providing a feasible solution for ultra-high power new energy power equipment.
[0078] In the description of this specification, the terms "first" and "second" are used for descriptive purposes only and should not be understood to indicate or imply relative importance or implicitly specify the number of the technical features indicated. Therefore, a feature specified as "first" or "second" may explicitly or implicitly include at least one of such features. In the description of this application, "plurality" means at least two, for example, two, three, etc., unless otherwise specifically defined.
[0079] In the description of this specification, the references to terms such as "one embodiment," "some embodiments," "example," "specific example," or "some examples," etc., refer to specific features, structures, materials, or characteristics described in connection with that embodiment or example, which are included in at least one embodiment or example of this application. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples. Moreover, without contradiction, those skilled in the art can combine and integrate the different embodiments or examples described in this specification, as well as the features of different embodiments or examples.
[0080] Although the embodiments of the present application have been shown and described above, it can be understood that the above embodiments are exemplary and cannot be understood as limitations on the present application. Ordinary technicians in this field can change, modify, replace and deform the above embodiments within the scope of the present application.
Claims
1. A novel new energy engine, characterized in that, Includes the main working body and the diesel engine starting module, among which, The work-performing entity includes: The outer steel sleeve (6) is a vertical support frame. The top cover (2) is fixed at the top by the upper bolt (1). An upper O-ring gasket (3) is sandwiched between the upper cover (2) and the outer steel sleeve (6) to achieve axial sealing. An air inlet / outlet hole (4) is opened on the side wall of the outer steel sleeve (6) to connect the internal chamber to balance the air pressure; The outer steel sleeve (6) is provided with a left fixed inner sleeve bolt (5) on the left side. The left fixed inner sleeve bolt (5) is threadedly connected to the outer steel sleeve (6) and is used to clamp the positioning piston inner sleeve (10). The inner sleeve (10) of the positioning piston houses the piston (13) of A1. Above it, the upper A2 element (12), the upper A2 spring (11), and the upper spacing positioning seat (17) (spacing 0.3-0.5mm) are arranged in sequence; below it, the lower A2 element (14), the lower A2 spring (15), and the lower spacing positioning seat (16) (spacing 0.3-0.5mm) are arranged in sequence. The bottom end of the outer steel sleeve (6) is connected by a lower bolt (7), and an O-ring gasket (8) is sandwiched between the outer steel sleeve (6) to achieve axial sealing. The bottom end of the outer steel sleeve (6) is provided with an oil inlet bolt (9), and the side wall is provided with an oil level line (18) for observing the oil level. The diesel engine starting module includes: The top end of the round shaft (19) is connected to the bottom end of the outer steel sleeve (6) of the working body. The outer side of the round shaft (19) is fitted with a positioning round shaft seat sleeve (20). An oil seal (22) is sandwiched between the two to achieve radial sealing. An oil drain bolt (21) is provided below the positioning round shaft seat sleeve (20). The bottom end of the round shaft (19) is connected to the crankshaft (24) via a connecting rod (23), and the crankshaft (24) is connected to the transmission gear (25); The transmission gear (25) meshes with the magnetic cylinder rotor (26), the stator (27) is fitted on the outside of the magnetic cylinder rotor (26), and the rotating parts are supported by bearings (28).
2. The novel new energy engine according to claim 1, characterized in that, The upper A2 element (12) and the lower A2 element (14) are symmetrically distributed on both sides of the A1 piston (13). The upper A2 spring (11) and the lower A2 spring (15) provide elastic preload, and the upper spacing positioning seat (17) and the lower spacing positioning seat (16) limit the axial displacement range, so that the A1 piston (13) can reciprocate within the positioning piston inner sleeve (10) to trigger the reaction of A1 and A2 elements.
3. The novel new energy engine according to claim 1, characterized in that, The upper O-ring gasket (3) and the lower O-ring gasket (8) are annular elastic elements, which are respectively interference-fitted with the top and bottom ends of the outer steel sleeve (6) to achieve axial sealing.
4. A novel new energy engine according to claim 1, characterized in that, The left fixed inner sleeve bolt (5) is connected to the outer steel sleeve (6) by thread and clamps the positioning piston inner sleeve (10) to limit its radial sway.
5. A novel new energy engine according to claim 1, characterized in that, In the diesel engine starting module, the transmission gear (25), the magnetic cylinder rotor (26) and the stator (27) constitute an electromagnetic drive structure, which is used to convert electrical energy into mechanical energy during the starting phase, drive the A1 piston (13) to initially reciprocate to trigger the reaction of A1 and A2 elements; when the reciprocating frequency of the A1 piston (13) reaches 50 times / second, the module automatically stops working.
6. A novel new energy engine according to claim 1, characterized in that, The inner wall of the positioning round shaft seat (20) is provided with a guide groove, which slides with the protrusion of the outer wall of the round shaft (19) to restrict the rotational freedom of the round shaft (19) and only allow it to reciprocate in the range of 0-90mm along the axial direction.