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Apparatus for realizing whole-satellite self-energy-supply active and passive integrated nonlinear vibration control

A non-linear, self-powered technology, applied in generators/motors, piezoelectric effect/electrostrictive or magnetostrictive motors, electrical components, etc. practical effect

Active Publication Date: 2016-10-26
SHANGHAI UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in practical applications, active and passive integrated control will be limited by the energy of the actual engineering environment, especially the environment in which the spacecraft itself is located.

Method used

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  • Apparatus for realizing whole-satellite self-energy-supply active and passive integrated nonlinear vibration control

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Embodiment Construction

[0015] The specific implementation of the present invention will be further described below in conjunction with the accompanying drawings.

[0016] Such as figure 1 As shown, an active-passive integrated nonlinear vibration control device that realizes the self-supply of the whole star, including a cone shell adapter 1, a damping material 2, a cubic nonlinear spring 3, a mass 4, a guide rod 5, an energy harvester 6, and a wire 7. An actuator 8, a controller 9 and a sensor 10; one end of the damping material 2 and the cubic nonlinear spring 3 is fixed on the inner side of the upper end surface of the conical shell adapter 1, and the other end is fixed on the mass block 4, and the damping material 2, The cubic nonlinear spring 3 and the mass block 4 form a nonlinear energy sink, that is, NES; one end of the energy harvester 6 is fixed on the inner side of the upper end face of the cone shell adapter 1, and the other end is fixed on the mass block 4 to realize NES and energy The...

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Abstract

The invention relates to an apparatus for realizing whole-satellite self-energy-supply active and passive integrated nonlinear vibration control. The apparatus comprises a conical shell adapter, a damping material, a cubic nonlinear spring, a mass block, a guide rod, an energy gatherer, a lead wire, an actuator, a controller and a sensor, wherein the damping material, the cubic nonlinear spring and the mass block form a nonlinear energy sink, i.e., an NES; one end of the energy gatherer is fixed at the inner side of the upper end surface of the conical shell adapter, the other end is fixed on the mass block, and thus the NES and the energy gatherer are combined together; the two ends of the guide rod are fixed to the upper end surface and the lower end surface of the conical shell adapter, for constraining the vibration direction of the mass block; and the actuator is in contact with the upper end surface and the lower end surface of the conical shell adapter and is connected with the energy gatherer through the lead wire, and the controller converts feedback signals of a sensor installed at the upper end of the conical shell adapter into control signals for transmitting to the actuator. The problem of energy restrictions of a spacecraft in actual environment is solved to a quite large degree, and the actual application significance is great.

Description

technical field [0001] The invention relates to an active and passive integrated nonlinear vibration control device for realizing self-supply of the whole star. Background technique [0002] In the field of aerospace engineering, satellites will be subjected to different forms of loads during launch, including periodic, random and transient excitations. Based on the entire satellite vibration isolation technology, the predecessors added a vibration isolation device to the satellite-aircraft connection adapter (PAF) to reduce the damage of the load to the structure to a certain extent. [0003] In recent years, the technology of using nonlinear energy sink (NES) to realize mechanism vibration control has been studied by many scholars at home and abroad. NES is mainly composed of cubic nonlinear stiffness, damping material and mass block, which can realize the unidirectional and irreversible transfer of vibration energy from the main system to the nonlinear part, and achieve ...

Claims

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Application Information

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IPC IPC(8): H02N2/18H02N2/06
CPCH02N2/062H02N2/186
Inventor 陈立群张业伟李响方智伟丁虎
Owner SHANGHAI UNIV
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