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32 results about "Closed orbit" patented technology

Multiple Ion Isolation in Multi-Reflection Systems

This invention relates to a method of operating a charged particle trap in which ions undergo multiple reflections back and forth and / or follow a closed orbit around, usually, a set of electrodes. The invention allows high-performance isolation of multiple ion species for subsequent detection or fragmentation by deflecting ions out of the ion trap according to a timing scheme calculated with reference to the ions' periods of oscillation within the ion trap.
Owner:THERMO FISHER SCI BREMEN

Electromagnetic wave generator

A compact and low-cost electromagnetic wave generator in which X-rays having high intensity can be generated and the energy of generated X-rays can rapidly be switched. In an electromagnetic wave generator including a circular accelerator, a deflection electromagnet incorporated in the circular accelerator focuses injected and accelerated electrons, The circular accelerator produces stable electron closed orbits in a region with a predetermined width in the radial direction of the accelerator that are stable during injection and acceleration of electron. A target is arranged across the stable electron closed orbits and a collision region, where a circulating electron beam collides with the target and a non-collision region where a circulating electron beam does not collide with the target produced. Through control of respective patterns of changes with time in the deflection magnetic field, a given electron closed orbit is shifted between the collision and the non-collision regions, thereby generating X-rays.
Owner:MITSUBISHI ELECTRIC CORP

Orbit expansion based multi-robot tracing formulation control method

The invention discloses an orbit expansion based multi-robot tracing formulation control method, comprising the following steps of: a) for a group of target orbit in a plane, expanding vectors of the target orbit, which point to each point on the orbit along the center of the target orbit, into an orbital cluster equivalent to an orbital function, and determining the movable range of robots; b) calculating tracing error by virtue of the orbital function, and designing the virtual angular velocity of the robots to ensure the tracing error to meet design requirements; c) calculating the generalized arc length and differential coefficient of the generalized arc length when the robots move along the orbit, by virtue of the orbital function and the target orbit, and designing the control force of the robots by virtue of neighbor information obtained by communication to realize formulation; d) calculating the error between the real angular velocity and the virtual angular velocity, and designing the control moment of force of the robot to complete tracing; and e) completing motion control on the robots by virtue of a servo system. The orbit expansion based multi-robot tracing formulation control method disclosed by the invention is especially applicable to nonholonomic constraint dynamic robots and simple and convexly- closed orbits. The method is simple and reliable, has higher accuracy and can be applied to multi-robot optimized information acquisition and the like.
Owner:SOUTHEAST UNIV

Human-powered driving mechanism

A human powered drive units each including a pair of a rotatable member having a sprocket and a supporting member having a sprocket, which are arranged up and down, and including a chain extended around the rotatable member and the supporting member, are disposed at left and right sides, respectively. The left and right rotatable members 1, 100 are fixed on a driving shaft 15. A chain ring 6 on which the load is applied is mounted on the driving shaft between upper rotatable member 1 and rotatable member 100. In each of the units, constraining means including a free crank (10 for the right-hand unit, and 1000 for the left-hand unit) and arm (11 for the right-hand unit, and 1100 for the left-hand unit), is provided so as to maintain perpendicularity of a shaft of the pedal relative to the plane in which the chain moves. By the rider kicking the pedal along the closed orbit including a linear orbit portion, the force transmitted to the pedal from the foot of the rider is efficiently converted to a rotational force in a longer period of time, thus increasing the power input.
Owner:ODA NORIYUKI

Tridimensional planting system for plants

The invention relates to a plating system for plants, in particular to a tridimensional plating system for plants, which comprises a plurality of tridimensional plating units. The tridimensional plating system is characterized by also comprising a belt-shaped closed orbit and an orbit running unit, wherein the tridimensional plating units can move along the belt-shaped closed orbit by being driven by the orbit running unit. Because the belt-shaped closed orbit is adopted, each tridimensional plating unit has an opportunity to rotate to the periphery of the tridimensional plating system, thus the invention solves the problem of the insufficient lighting and the poor ventilation of high-density plating in the prior art. The invention reduces the work intensity of workers, enhances the work efficiency, saves the labor cost and the fund cost and effectively realizes the industrialized production of crops and the assembly line work of agricultural production.
Owner:田辉勤 +1

Method and device for placing a unidirectional thread layer on longitudinal conveyors, method for laying weft threads on warp knitting machines, and device to carry out said methods

InactiveCN101525809AIdeal coordination displacementHigh speedNon-woven fabricsFlat warp knitting machinesMulti axisClosed orbit
In the warp knitting machines and knitting machines for multi-axis must be one-way yarn layer (8) to mobile vertical conveyor belt installation (1,2) and hung on the conveyor belt at the vertical (1,2) on a fixed set of hooks (3 , 3a, 3b, or 4,4a, 4b) on the. Above the vertical conveyor (1,2) to send the direction (5) mobile. Described yarn (8) from the storage device (6) was extracted and transferred through the pulley off (9) transmission line to the first input device (10), referred to the input line of the device will hang the yarn to the first vertical conveyor belt (1) a fixed set of hooks (3,3a, 3b) in the. Then, the second transmission line unit (11) will be linked to the second vertical conveyor belt yarn (2) a fixed set of hooks (4,4a, 4b) in the. Described in two transmission-line device (10,11) in two mutually perpendicular extension of the direction of x axis and y-axis movement and the movement to draw a closed orbit (14 and 15). In order to grab yarn (8), referred to the input line of devices (10,11) set up branch with claws (12,13). The methods described can also be achieved through the yarn guide, which referred to the input line of devices (10,11) was designed to shift rake. Yarn made of layers is transported to a warp knitting machine knitting station (7) or knitting tools.
Owner:LIBA MASCHFAB

Multi-kind graphics output primitive mixed processing path optimization method

The invention discloses a multi-kind graphics output primitive mixed processing path optimization method. According to the method, DXF file graphics output primitive information is read, closed orbit segment figures and non-closed orbit segment figures that are formed by a single graphics output primitive or multiple graphics output primitives are subjected to sorting code number marking operation, different start points and nodes are chosen for different orbit segment figures, overall path ordering operation is performed via a genetic algorithm, local optimization searching start points are calculated according to orbit segment figure types, and therefore processing paths with minimum lengths can be obtained. The multi-kind graphics output primitive mixed processing path optimization method can be used for effectively solving a problem of multi-kind graphics output primitive mixed path optimization, and numerical control machine tool processing efficiency can be improved.
Owner:GUANGDONG INST OF INTELLIGENT MFG

Mechanical automation crown sealing equipment for trees and nursery stocks

InactiveCN104982304ARealize the whole process of automatic crown sealing operationAvoid damageForestryTree trunkDevice form
The invention discloses mechanical automation crown equipment for trees and nursery stocks. The mechanical automation crown equipment mainly comprises a centralized positioning device, a closed orbit device, a rope winding crown sealing device and a lifting device, wherein the centralized positioning device and the closed orbit device are arranged into circles which are in the same shapes and have openings, and penetrate through a tree trunk from the openings; the tree trunk is placed in the orbit device; after centralized positioning, the orbit device forms a closed circular orbit in a fastening manner through a locking device; under the action of lifting of the lifting device, the orbit device moves from bottom to top, and besides, the rope winding crown sealing device moves circularly along the orbit device, so that a winding rope winds a tree crown tightly; when the top end of the tree crown is wound, knots of the winding rope are tightened and cut off, so that the purpose of automatic crown sealing operation on the trees and the nursery stocks is realized, the artificial damage to the tree crown and the trees is avoided, the crown sealing effect is greatly improved, the labor intensity of workers is reduced, and the labor cost is reduced.
Owner:TAIAN INST OF AGRI MACHINERY SCI SHANDONG PROV

Method for designing an orbit of a spacecraft

InactiveUS20100108819A1Merit is lostEffectively availableArtificial satellitesSpacecraft guiding apparatusEngineeringClosed orbit
A method is disclosed for designing an orbit of a spacecraft which allows the spacecraft to take a small-radius halo orbit near a Lagrange point while avoiding the prohibited zone where the spacecraft may be shadowed or might be prevented from making communication. The method makes it possible to have a closed orbit although being similar to a Lissajous orbit, under a restricted condition where a propulsion force magnitude applied to a spacecraft is fixed, and where it rotates at a constant angular velocity, based on the equation of motion close to a Lagrange point. The method also provide a theory for guiding / controlling the orbit of a spacecraft, that is, the embodiment of the above orbit design method.
Owner:JAPAN AEROSPACE EXPLORATION AGENCY

Electromagnetic wave generating device

A compact and low-cost electromagnetic wave generator in which X-rays having high intensity can be generated and the energy of generated X-rays can rapidly be switched. In an electromagnetic wave generator including a circular accelerator, a deflection electromagnet incorporated in the circular accelerator focuses injected and accelerated electrons, The circular accelerator produces stable electron closed orbits in a region with a predetermined width in the radial direction of the accelerator that are stable during injection and acceleration of electron. A target is arranged across the stable electron closed orbits and a collision region, where a circulating electron beam collides with the target and a non-collision region where a circulating electron beam does not collide with the target produced. Through control of respective patterns of changes with time in the deflection magnetic field, a given electron closed orbit is shifted between the collision and the non-collision regions, thereby generating X-rays.
Owner:MITSUBISHI ELECTRIC CORP

Elliptical trainer with adjustable pedal track

The present invention relates to an elliptical sports machine with the tread-board orbit being adjustable, which comprises a skeleton, a movable bracket, a driving device, a right suspension arm, a left suspension arm, a right supporting rod, a left supporting rod, a right tread-board and a left tread-board, wherein, the movable bracket is provided with a right bracket body and a left bracket body, which are connected with each other through a motion part, and both the right and the left bracket bodies are provided with a bearing part and a rotation-shaft part, which are arranged at the back of the motion part; the rotation-shaft parts of the bracket bodies are coaxially hinged to the skeleton; the straight-line distance between the rotation-shaft part of the bracket bodies and the motion part is more than the straight-line distance between the rotation-shaft part and the bearing part; the driving device is arranged on the skeleton and is provided with a motor, and the force output thereof is connected with the power of the motion part of the movable bracket; both the right and the left suspension arms are provided with a suspension end and a swinging end; each of the right and the left supporting rod is provided with a return-winding part and a swinging part that is arranged after the return-winding part, and the return-winding part moves on a closed orbit corresponding to the skeleton, and the swinging part is hinged on the swinging end of the corresponding suspension arm; each of the right and the left tread-boards is respectively supported by the two supporting rods directly or indirectly. The driving device has high work doing efficiency; moreover, with the elliptical sports machine, the user can directly acknowledge of the inclined degree of the tread-board orbit.
Owner:JOHNSON HEALTH TECH

Method and device for improving interlayer bonding force of fiber reinforced building plate

The invention discloses a method and a device for improving interlayer bonding force of a fiber reinforced building plate. The method comprises the following basic steps of a, adding slurry to a forming cylinder layer by layer by rotating to form a wet blank; b, when the wet blank reaches a certain thickness, enabling array needles on a plurality of arc-shaped acupuncture tiles above the forming cylinder to be in contact with and inserted into the wet blank gradually, and generating corresponding array holes; c, continuing receiving the slurry by the array holes so that the array holes are filled to form array rivets, and stripping the array rivets after the wet blank reaches the thickness; and d, pulling the arc-shaped acupuncture tiles to a starting side, and repeating the process aboveto realize continuous production. The device comprises the forming cylinder, the plurality of the arc-shaped acupuncture tiles, hinges, the array needles, an elliptical closed orbit, universal joints,hanging rods, a pulling motor, a control system, a lifting system and the like. The method and device disclosed by the invention are easily combined to a conventional copying method or slurry flowingmethod production line at present, and do not have limitation on components, thickness and the like of materials; and the performance of the obtained fiber reinforced building plate with improved interlayer bonding force is greatly improved.
Owner:山东鲁泰建筑产业化材料有限公司

Human-powered driving mechanism

A human powered drive units each including a pair of a rotatable member having a sprocket and a supporting member having a sprocket, which are arranged up and down, and including a chain extended around the rotatable member and the supporting member, are disposed at left and right sides, respectively. The left and right rotatable members 1, 100 are fixed on a driving shaft 15. A chain ring 6 on which the load is applied is mounted on the driving shaft between upper rotatable member 1 and rotatable member 100. In each of the units, constraining means including a free crank (10 for the right-hand unit, and 1000 for the left-hand unit) and arm (11 for the right-hand unit, and 1100 for the left-hand unit), is provided so as to maintain perpendicularity of a shaft of the pedal relative to the plane in which the chain moves. By the rider kicking the pedal along the closed orbit including a linear orbit portion, the force transmitted to the pedal from the foot of the rider is efficiently converted to a rotational force in a longer period of time, thus increasing the power input.
Owner:ODA NORIYUKI

Compact type wideband BPM (beam position monitor) for proton synchrotron

The invention belongs to the technical field of particle accelerator beam diagnosis, particularly relates to a compact type wideband BPM (beam position monitor) for a proton synchrotron and solves theproblems that existing BPMs are narrower in bandwidth, cannot meet the requirement for turn-by-turn measurement and occupies large accelerator space. According to the technical solution, the compacttype wideband BPM for the proton synchrotron comprises a vacuum cavity, a sleeve, two right triangle electrodes, a first grounding ring, a second grounding ring, signal pickup units and an isolating ring. The vacuum cavity comprises a rectangular box and quick connection flanges arranged at two ends of the rectangular vacuum box, the sleeve is nested in the rectangular vacuum box, the two right triangle electrodes are arranged in the sleeve, and the isolating ring is arranged between the two right triangle electrodes and can move in the axial direction of the vacuum cavity. The detector is arranged in correction iron of the proton synchrotron for irradiation or medical use and is used for turn-by-turn position and closed orbit measurement of protons.
Owner:NORTHWEST INST OF NUCLEAR TECH

Permanent magnet suspension ultimate experience system

The invention discloses a permanent magnet suspension ultimate experience system, which comprises a ground permanent magnet suspension orbit (1), a lifting orbit (2), an overhead permanent magnet suspension orbit (3), a descent orbit (4), and a closed orbit formed by the ground permanent magnet suspension orbit (1), the lifting orbit (2), the overhead permanent magnet suspension orbit (3) and the descent orbit (4) connected end to end sequentially and used for running a magnet suspension vehicle (5), wherein corresponding permanent magnets are respectively arranged on the ground permanent magnet suspension orbit (1), the overhead permanent magnet suspension orbit (3) and the magnet suspension vehicle (5) so as to enable the magnet suspension vehicle (5) to run in a suspension way; the lifting orbit (2) can lift the magnet suspension vehicle (5) on the tail end of the ground permanent magnet suspension orbit (1) to the head end of the overhead permanent magnet suspension orbit (3); a buffer mechanism (6) for first-level or multi-level buffering the free-falling magnet suspension vehicle (5) is arranged on the descent orbit (4). The system provided by the invention requires no energy consumption during the magnet suspension and buffer process, is safe and reliable, and can enable visitors to have feeling of freshness and also excitement in the whole experience.
Owner:江苏金陵永磁产业研究院有限公司

Elliptical trainer with adjustable pedal track

The present invention relates to an elliptical sports machine with the tread-board orbit being adjustable, which comprises a skeleton, a movable bracket, a driving device, a right suspension arm, a left suspension arm, a right supporting rod, a left supporting rod, a right tread-board and a left tread-board, wherein, the movable bracket is provided with a right bracket body and a left bracket body, which are connected with each other through a motion part, and both the right and the left bracket bodies are provided with a bearing part and a rotation-shaft part, which are arranged at the back of the motion part; the rotation-shaft parts of the bracket bodies are coaxially hinged to the skeleton; the straight-line distance between the rotation-shaft part of the bracket bodies and the motionpart is more than the straight-line distance between the rotation-shaft part and the bearing part; the driving device is arranged on the skeleton and is provided with a motor, and the force output thereof is connected with the power of the motion part of the movable bracket; both the right and the left suspension arms are provided with a suspension end and a swinging end; each of the right and the left supporting rod is provided with a return-winding part and a swinging part that is arranged after the return-winding part, and the return-winding part moves on a closed orbit corresponding to the skeleton, and the swinging part is hinged on the swinging end of the corresponding suspension arm; each of the right and the left tread-boards is respectively supported by the two supporting rods directly or indirectly. The driving device has high work doing efficiency; moreover, with the elliptical sports machine, the user can directly acknowledge of the inclined degree of the tread-board orbit.
Owner:JOHNSON HEALTH TECH

Interactive atomic model

The present invention provides an interactive atomic model that comprises a compartment (201) that is enclosed by walls and a lid (100) that can be opened, and at least two elementary particle models (301, 302, 303) which are contained in the compartment (201). The lid (100) has an atomic model surface (101) that defines a centre area (103) and a number of closed orbits (102), whereby said centre area (103) defines resting positions that are well defined in space for at least one of said elementary particle models (301, 302, 303) and said closed orbits (102) defines resting positions that are well defined along the respective closed orbit or at least one of said elementary particle models (301, 302, 303). The interactive atomic model thereby enables simple and effective understanding for the constitution of atoms.
Owner:BRIGHT

Unstable motion analysis method based on bifurcation theory and degree-of-freedom release experiment

PendingCN114852368AObtaining Globally Stable PropertiesSustainable transportationAerodynamic testingFlight vehicleUnstable equilibrium
The invention discloses an unstable motion analysis method based on a bifurcation theory and a degree-of-freedom release experiment. The method comprises the following steps: firstly, establishing a set of degree-of-freedom release experiment system in a wind tunnel; then, a bifurcation theory is introduced into a degree-of-freedom release experiment, a continuous algorithm based on control is established, and a branch balance point and a periodic closed orbit are searched; non-invasive control is adopted, a branch search process is converted into an optimization process with a feedback control quantity tending to zero, so that the feedback control keeps the position of a balance branch while changing the stability of the balance branch, stable and unstable balance solutions are continuously tracked in an experiment, the global stability characteristic of an aircraft is obtained, and the stability of the aircraft is improved. A brand-new experimental method is provided for dynamic characteristic research of the aircraft, and accurate prediction of the stall deviation characteristic of the aircraft can be achieved.
Owner:NANCHANG HANGKONG UNIVERSITY +1

Device for generating a variable angular momentum, in particular for spacecraft attitude control

The present invention relates to a device for generating a variable angular momentum or torque, which has a container (1) partially filled with a magnetizable fluid (2) and a device for generating one or several rotating or wandering magnetic fields, with which the magnetizable fluid (2) in the container (1) can be made to continuously move on a closed orbit. The device for generating the rotating or wandering magnetic fields has several electric coils (4), whose coil axes lie in the orbital plane. This structure makes it possible to generate a variable angular momentum without mechanical moved parts or the necessity of external magnetic fields. For example, the device enables a simple and cost-effective spacecraft attitude control.
Owner:UNIV STUTTGART

A Precise Control Method for the Launching Orbit of a Launch Vehicle under Fire

ActiveCN114526647BRealize shutdown controlSelf-propelled projectilesClosed orbitLaunch vehicle
The present application belongs to the technical field of launch vehicle guidance. Specifically, a precise control method for the launch track of a launch vehicle running into fire is provided. The method includes: when the flight segment of the launch vehicle is the final stage entry segment or the terminal velocity correction segment, determining the shutdown amount of the launch vehicle in the current control period according to the first shutdown control parameter of the launch vehicle; The amount of shutdown during the cycle determines whether shutdown control of the launch vehicle is required. Based on the technical solution provided by the present application, when the operating orbit of the launch vehicle transitions from a closed orbit to a non-closed orbit, the high-precision and reliable shutdown requirements of its orbital energy state are met.
Owner:BEIJING INST OF ASTRONAUTICAL SYST ENG

Orbit expansion based multi-robot tracing formulation control method

The invention discloses an orbit expansion based multi-robot tracing formulation control method, comprising the following steps of: a) for a group of target orbit in a plane, expanding vectors of the target orbit, which point to each point on the orbit along the center of the target orbit, into an orbital cluster equivalent to an orbital function, and determining the movable range of robots; b) calculating tracing error by virtue of the orbital function, and designing the virtual angular velocity of the robots to ensure the tracing error to meet design requirements; c) calculating the generalized arc length and differential coefficient of the generalized arc length when the robots move along the orbit, by virtue of the orbital function and the target orbit, and designing the control forceof the robots by virtue of neighbor information obtained by communication to realize formulation; d) calculating the error between the real angular velocity and the virtual angular velocity, and designing the control moment of force of the robot to complete tracing; and e) completing motion control on the robots by virtue of a servo system. The orbit expansion based multi-robot tracing formulation control method disclosed by the invention is especially applicable to nonholonomic constraint dynamic robots and simple and convexly- closed orbits. The method is simple and reliable, has higher accuracy and can be applied to multi-robot optimized information acquisition and the like.
Owner:SOUTHEAST UNIV

Accurate control method of launch vehicle fire-striving launching orbit

ActiveCN114526647ARealize shutdown controlSelf-propelled projectilesRocketClosed orbit
The invention belongs to the technical field of carrier rocket guidance. The invention particularly provides an accurate control method for a launch vehicle fire-strike launching orbit. The method comprises the following steps: when a flight section of the carrier rocket is a final-stage injection section or a final speed correction section, determining a shutdown amount of the carrier rocket in a current control period according to a first shutdown control parameter of the carrier rocket; and determining whether shutdown control needs to be performed on the carrier rocket according to the shutdown amount of the carrier rocket in the current control period. Based on the technical scheme provided by the invention, when the operation orbit of the carrier rocket is transited to the non-closed orbit from the closed orbit, the high-precision and reliable shutdown requirement of the orbit energy state is met.
Owner:BEIJING INST OF ASTRONAUTICAL SYST ENG

A permanent magnetic levitation extreme experience system

The invention discloses a permanent magnet suspension ultimate experience system, which comprises a ground permanent magnet suspension orbit (1), a lifting orbit (2), an overhead permanent magnet suspension orbit (3), a descent orbit (4), and a closed orbit formed by the ground permanent magnet suspension orbit (1), the lifting orbit (2), the overhead permanent magnet suspension orbit (3) and the descent orbit (4) connected end to end sequentially and used for running a magnet suspension vehicle (5), wherein corresponding permanent magnets are respectively arranged on the ground permanent magnet suspension orbit (1), the overhead permanent magnet suspension orbit (3) and the magnet suspension vehicle (5) so as to enable the magnet suspension vehicle (5) to run in a suspension way; the lifting orbit (2) can lift the magnet suspension vehicle (5) on the tail end of the ground permanent magnet suspension orbit (1) to the head end of the overhead permanent magnet suspension orbit (3); a buffer mechanism (6) for first-level or multi-level buffering the free-falling magnet suspension vehicle (5) is arranged on the descent orbit (4). The system provided by the invention requires no energy consumption during the magnet suspension and buffer process, is safe and reliable, and can enable visitors to have feeling of freshness and also excitement in the whole experience.
Owner:江苏金陵永磁产业研究院有限公司
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