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41results about How to "Damping force adjustment" patented technology

Semi-active energy regenerative suspension shock absorber based on mixed excitation and size determining method of shock absorber

The invention discloses a semi-active energy regenerative suspension shock absorber based on mixed excitation and a size determining method of the shock absorber. The shock absorber comprises an upper hoisting lug, a dust cover, a lower hoisting lug, a hydraulic shock absorber body and a mixed excitation mechanism. The hydraulic shock absorber body provides the constant viscous damping coefficient. The mixed excitation mechanism provides the adjustable electromagnetic damping force and converts vibration energy into electric energy for storage. Meanwhile, the invention provides the size determining method. The model selection of the hydraulic shock absorber body is determined according to the rating requirements, an electromagnetic damping force expression is derived, the primary size of the mixed excitation mechanism is determined through a particle swarm optimization algorithm, finite element analysis is conducted, the gas length is optimized, and the final size is determined. According to the shock absorber and the size determining method, the hydraulic shock absorber body and a mixed excitation cylindrical linear motor are integrated, the damping force is adjustable, energy is recovered in the working process, the structure is simple, the shock isolation performance and the energy regenerative performance of a vehicle suspension are coordinated, and the Fail-safe function is also achieved; and in addition, the size determining method is clear in step, easy to implement and obvious in optimization result, and has high practicalness.
Owner:JIANGSU UNIV

Magneto-rheological damper with unidirectional damping property

The invention discloses a magneto-rheological damper with unidirectional damping property, and relates to the technical field of devices for adjusting damping property by changing fluid viscosity. The magneto-rheological damper comprises a damping cylinder, a unidirectional damping piston assembly, a coil assembly, a piston rod and magneto-rheological liquid, wherein the unidirectional damping piston assembly comprises a damping piston, a spring sheet and a gasket; a first annular through hole and a second annular through hole are formed in the damping piston; a magneto-rheological fluid passage is arranged on the coil assembly and is communicated with the first annular through hole, and the coil assembly does not cover the second annular through hole. The magneto-rheological damper has the advantages that when the damping piston moves up, the spring sheet seals the second annular through hole, the magneto-rheological fluid only passes through the magneto-rheological liquid passage under the action of a magnetic field, and the damping force can be adjusted by adjusting the intensity of the magnetic field; when the damping piston moves down, the second annular through hole is opened under the action of no magnetic field, and the produced damping force is little, so that the unidirectional damping property of the magneto-rheological damper is realized.
Owner:SHIJIAZHUANG TIEDAO UNIV +2

Concrete pumping equipment and arm-support-vibration semi-active control device and arm-support-vibration semi-active control method thereof

The invention provides concrete pumping equipment and an arm-support-vibration semi-active control device and an arm-support-vibration semi-active control method thereof. The arm-support-vibration semi-active control device comprises a plurality of sections of arm supports (10) and extension mechanisms (20) connected between two adjacent sections of arm supports (10). The arm-support-vibration semi-active control device further comprises changing dampers arranged at the extension ends or fixed ends of the extension mechanisms (20) in series connection mode, sensors arranged on the arm supports (10) and controllers (40) connected with the sensors. Signal output ends of the controllers (40) are connected with the changing dampers to control damping force of the changing dampers, and the changing dampers exert damping force in the reversed direction with the vibration direction of the arm supports (10) on the arm supports (10). The arm-support-vibration semi-active control device can not only passively play the roles of damping, energy consumption and vibration reduction, but also actively play the roles of vibration control, thereby being good in control effect on arm support vibration, simple in structure and flexible and convenient to use.
Owner:ZOOMLION HEAVY IND CO LTD

Magnetorheological damper with multi-piece piston and single rod

The invention discloses a magnetorheological damper with a multi-piece piston and a single rod. The magnetorheological damper consists of a working cylinder, an external electromagnet, a compensating air bag, the multi-piece piston and a piston rod, wherein the multi-piece piston consists of three or more groups of dynamic pieces; each group of dynamic piece has a circular ring form, and consistsof a strip flat plate which has a round hole in the center and two semicircular arc flat plates; the circular ring form is formed by respectively connecting one semicircular arc flat plate to one of two parallel straight edges of the strip flat plate which has the round hole in the center by a hinge; the outer diameters of the dynamic pieces are smaller than the inner diameter of the working cylinder; the flowing gaps of magnetorheological liquid are left; the groups of dynamic pieces of the multi-piece piston are fixed at one end of the piston rod at certain intervals through the round holeson the dynamic pieces; the other end of the piston rod is stretched out of the working cylinder through a sealing device and a bearing on the end face of the working cylinder; the compensating air bag is arranged at the bottom in the working cylinder; the external electromagnet is fixed on the external circumference of the working cylinder; the working cylinder is made of a magnetically-nonconductive material; and the magnetorheological liquid is fully filled in the working cylinder.
Owner:CHONGQING MATERIALS RES INST

Terrain self-adaptive biomimetic ankle device

The invention relates to a terrain self-adaptive biomimetic ankle device comprising a crus dry interface seat, a hydraulic cylinder connecting sleeve and a rotary micro hydraulic cylinder; liquid cylinder sealing plates are arranged on two sides of the rotary micro hydraulic cylinder; oil liquid is filled in the rotary micro hydraulic cylinder; an inner cavity of the rotary micro hydraulic cylinder is a sectional main chamber; the middle at the lower end of the sectional main chamber is connected with a piston rotating shaft fixedly connected with a rotary hydraulic piston by which the sectional main chamber is divided into a left chamber and a right chamber; the left chamber and the right chamber are respectively communicated with a plantar flexion pipeline and a dorsal flexure pipeline; and a plantar flexion damping system and a dorsal flexure damping system which are arranged at the bottom of the rotary micro hydraulic cylinder are respectively arranged in the plantar flexion pipeline and the dorsal flexure pipeline. The human ankle rotation can be simulated by using the rotary hydraulic piston to rotate in the hydraulic cylinder round a rotating center; meanwhile, the stability of the ankle at any angle can be kept by using a damping force generated by the flowing of oil liquid between the left chamber and the right chamber through a needle valve.
Owner:UNIV OF SHANGHAI FOR SCI & TECH

Single-actuating type magneto-rheological shock absorber used for aircraft landing gear

The invention relates to a single-actuating type magneto-rheological shock absorber used for an aircraft landing gear. The single-actuating type magneto-rheological shock absorber comprises an outer cylinder barrel, an inner cylinder barrel, a piston rod, a piston assembly and an aircraft wheel axle base, wherein an end cover is installed on the top of the outer cylinder barrel coaxially in a sealed mode; the inner cylinder barrel is coaxially installed in the lower end of the outer cylinder barrel in a sliding mode; the aircraft wheel axle base is installed at the lower end of the inner cylinder barrel in a threaded mode; the inner and outer cylinder barrels are coaxially provided with the piston rod, the upper end of the piston rod is fixedly installed on the end cover, and the piston assembly is installed at the lower end of the piston rod; the outer edge of the piston assembly makes friction contact with the inner wall of the inner cylinder barrel. Based on an existing aircraft landing gear buffer structure, the piston assembly capable of applying the magneto-rheological fluid technology is added, so that the shock absorber is simple in structure, low in energy consumption, small in size and fast in response, and damping force output by the shock absorber continuously changes, is adjustable and is reversible. Closed-loop semi-active control is achieved by being combined with a computer, an optimization control algorithm, a sensor, a controller and a power source, and the buffering efficiency and shock absorption effect of the shock absorber are improved.
Owner:CIVIL AVIATION UNIV OF CHINA

Impact load self-adaptive buffer device

The invention relates to a hydraulic variable-damping self-adaptive buffer device, in particular to an impact load self-adaptive buffer device. The device comprises an air storage barrel and a bufferbarrel. The air storage barrel is arranged in the buffer barrel in a sealed mode, a piston is arranged in the air storage barrel, a cavity I is formed by one side of the piston and the air storage barrel, a piston rod is arranged on the other side of the piston, and one end of the piston rod stretches out of the air storage barrel. A floating piston is arranged between the air storage barrel and the buffer barrel, the floating piston divides a cavity between the air storage barrel and the buffer barrel into a cavity II and a cavity III, a buffer valve and a rest valve are arranged between theair storage barrel and the buffer barrel, the opening of the buffer valve is adjusted through a buffer valve adjusting device, the opening of the reset valve is adjusted through a reset valve adjusting device, the buffer valve and the reset valve are communicated with the cavity I respectively, a liquid injection device communicated with the exterior is arranged on the cavity I, the cavity II is communicated with a liquid flow hole in the buffer valve, a small liquid flow hole is formed between the cavity II and the cavity I, and an air injection device communicated with the cavity III is arranged on the buffer barrel.
Owner:ZHONGBEI UNIV

Magnetorheological damper with float ring and double outlet rods

The invention discloses a magnetorheological damper with a float ring and double outlet rods. The magnetorheological damper comprises a working cylinder, the float ring, a piston, two piston rods and an external electromagnet. End covers are fixed to two ends of the cylindrical working cylinder; a plurality of identical annular discs are fixed onto the same core column to form the piston, and excitation coils are wound in annular gaps among the various annular discs of the piston; the piston is mounted in the working cylinder, and magnetorheological fluid flowing gaps are reserved between the outer peripheral wall of the piston and the inner peripheral wall of the float ring and between the outer peripheral wall of the float ring and the inner peripheral wall of the working cylinder; one ends of the two piston rods are respectively fixed to two ends of the piston, and the other ends of the two piston rods extend out of the two ends of the working cylinder via sealing devices and sliding bearings on the two end covers of the working cylinder; the gaps in the working cylinder, between the inner peripheral wall of the float ring and the outer peripheral wall of the piston and between the outer peripheral wall of the float ring and the inner peripheral wall of the working cylinder are filled with magnetorheological fluid; the external electromagnet is fixed onto the outer circumference of the working cylinder.
Owner:STATE GRID CORP OF CHINA +1

A rotary plate type magneto-rheological damper for aircraft landing gear

The invention relates to a rotating plate type magneto-rheological shimmy damper for a landing gear of an aircraft comprising a cylinder tube, end caps, stator assemblies and a rotor assembly, wherein the end caps are coaxially and hermetically mounted at both ends of the cylinder tube; each stator assembly is fixedly and symmetrically mounted in the part of the cylinder tube inside the corresponding end cap; a drive shaft is coaxially arranged in the cylinder tube between the two stator assemblies in a running-through manner; the drive shaft in the cylinder tube is provided with the rotor assembly and drives the rotor assembly to rotate in the cylinder tube; and one end of the drive shaft is provided with a double rocker mechanism. The rotating plate type magneto-rheological shimmy damper for the landing gear of the aircraft is a semi-active shimmy control device which is capable of guaranteeing a minimum damping under zero magnetic field conditions and increasing the adjustment range of damping force of the shimmy damper, and has the advantages of simple structure, low energy consumption, small size, fast response and continuously adjustable direction of the damping force in a large range; and the same overcomes the problems of unmeasured state feedback quantity, large energy consumption of active control force, time delay and spillovers of a traditional passive damper in the prior art, and is useful as an actuator for structural shimmy control.
Owner:CIVIL AVIATION UNIV OF CHINA

A small viscous damper

The invention discloses a small viscous damper which comprises a damping box body, a connection plate and shearing plates, wherein the top of the damping box body is provided with an opening, the bottom of the damping box body is provided with a connection bottom plate connected with a lower layer building structure, a plurality of adjustable baffles are inserted on the two sides of the inner wall of the damper, a plurality of shearing areas which are vertically arranged can be formed on the two sides of the interior of the damping box body, and the shearing areas are filled with damping filler; the upper end of the connection plate is provided with a connection top plate connected with the upper layer building structure, and the lower end of the connection plate penetrates through the opening and is inserted into the damping box body; the first end of each shearing plate is connected with the connection plate, and the second end of each shearing plate is inserted into the damping filler in the shearing areas. According to the small viscous damper, multiple layers of the shearing plates are inserted into the damping box body through the connection plate, multiple layers of shearing faces are formed, and larger damping force is guaranteed under the situation that the appearance size of the damper is reduced.
Owner:SHANGHAI KUNYI SEISMIC DAMPING ENG TECH CO LTD

A single-acting magneto-rheological shock absorber for aircraft landing gear

The invention relates to a single-action magneto-rheological shock absorber for aircraft landing gear, comprising an outer cylinder, an inner cylinder, a piston rod, a piston assembly and a wheel shaft base, and the top of the outer cylinder is coaxially sealed and installed End cover, the lower end of the outer cylinder is coaxially slid to install the inner cylinder, the lower end of the inner cylinder is threaded to install the wheel shaft base, the inner and outer cylinders are coaxially installed with the piston rod, and the upper end of the piston rod is fixed to the end cover Together, the lower end of the piston rod mounts a piston assembly whose outer edge is in frictional contact with the inner wall of the inner cylinder. On the basis of the existing aircraft landing gear buffer structure, the present invention adds a piston assembly that can apply magneto-rheological fluid technology, so that the shock absorber has simple structure, low energy consumption, small volume, fast response, and its output damping force can be continuously changed. Adjustable and reversible, the closed-loop semi-active control is realized by combining with computer, optimized control algorithm, sensor, controller and power supply, which improves the buffering efficiency and shock absorption effect of the shock absorber.
Owner:CIVIL AVIATION UNIV OF CHINA
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