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Mars rover moving system vibration loading mechanism and performance testing device

A mobile system and loading mechanism technology, which is used in vibration testing, machine/structural component testing, measuring devices, etc., can solve the problems of inability to complete the performance test of the mobile system of the Mars rover, and achieve a simple structure, high precision, and accurate testing. Effect

Active Publication Date: 2020-06-05
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The problem solved by the invention is that the performance test of the Mars rover mobile system on the ground cannot be completed in the prior art

Method used

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  • Mars rover moving system vibration loading mechanism and performance testing device
  • Mars rover moving system vibration loading mechanism and performance testing device
  • Mars rover moving system vibration loading mechanism and performance testing device

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Embodiment Construction

[0032] In the description of the present invention, it should be understood that the positive direction of "X" in the drawings represents the right, the reverse of "X" represents the left, the positive direction of "Y" represents the top, and the reverse of "Y" Represents downward, the positive direction of "Z" represents the front, the reverse direction of "Z" represents the rear, and the orientation or positional relationship indicated by the terms "X", "Y", "Z" etc. is based on the orientation shown in the drawings of the specification Or positional relationship is only for the convenience of describing the present invention and simplifying the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as limiting the present invention. The terms "first", "second", and "third" are used for descriptive purposes only, and should...

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Abstract

The invention provides a Mars rover moving system vibration loading mechanism and a performance testing device and belongs to the technical field of Mars detection testing equipment. The mechanismcomprises a first vibration platform, a cam structure and a second vibration platform which are sequentially arranged from top to bottom, the first vibration platform is connected with the cam structure,the first vibration platform is further connected with the second vibration platform through an elastic structure, and the first vibration platform is arranged at the bottom of a wheel of the tested Mars rover. Compared with the prior art, performance testing is completed through a cam structure with the variable eccentric distance, the amplitude and frequency of wheels are adjusted, single-degree-of-freedom vibration loading of thetested Mars rover within the range of 0-10 Hz is achieved, the structure is simple, testing is accurate, and precision is high.

Description

technical field [0001] The invention relates to the technical field of Mars exploration and testing equipment, in particular to a vibration loading mechanism and a performance testing device of a Mars rover moving system. Background technique [0002] my country's Mars exploration is in full swing, but because Mars is farther away from the earth and the environment is more complex, the exploration of Mars is more difficult and risky. Therefore, it is necessary to conduct a large number of test experiments on the ground to conduct comprehensive checks and tests on the Mars rover to ensure the reliability of the Mars rover. [0003] The performance test of the Mars rover mobile system on the ground is an important part of the design and experimental verification stage of the Mars rover, and the performance test process of the Mars rover mobile system on the ground includes simulating the vibration of the wheels of the Mars rover on different terrains, However, the vibration l...

Claims

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Application Information

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IPC IPC(8): G01M99/00G01M7/02B64G7/00
CPCG01M99/008G01M99/005G01M99/007G01M99/002G01M7/02B64G7/00
Inventor 高海波田保林于海涛刘振李楠丁亮
Owner HARBIN INST OF TECH
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