Dual-spreading solar wing vibration measuring device and method

A technology of vibration measurement and vibration detection, which is applied to measuring devices, measuring ultrasonic/sonic/infrasonic waves, instruments, etc., can solve the problems of low precision and achieve high precision

Pending Publication Date: 2018-10-26
SOUTH CHINA UNIV OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, non-contact measurements are generally less accurate than contact measurements

Method used

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  • Dual-spreading solar wing vibration measuring device and method
  • Dual-spreading solar wing vibration measuring device and method
  • Dual-spreading solar wing vibration measuring device and method

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Embodiment 1

[0040] Such as Figure 1 to Figure 4 As shown, the present embodiment provides a double-spread solar wing vibration measurement device, which includes a double-spread solar wing, a vibration excitation mechanism and a vibration detection mechanism, figure 1 The dotted lines in the figure indicate the connection relationship between various devices, and the direction arrows indicate the transmission direction of the detection and control signal flow.

[0041] The double-rolled solar wing is a flexible structure, which includes a coiled unfolding part 1, a triangular truss 2, a fixing part 3, an unrolling part 4, a first solar cell film 5 and a second solar cell film 6, the fixing part 3 and the unwinding part Parts 4 are used as the front and rear ends of the double-rolled solar wings respectively. The coiled deployment part 1 is arranged in the middle of the fixed part 3. One end of the triangular truss 2 is connected to the coiled deployment part 1, and the other end of the t...

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PUM

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Abstract

The invention discloses a dual-spreading solar wing vibration measuring device and method. The device comprises a dual-spreading solar wing, a vibration excitation mechanism and a vibration detectingmechanism; the vibration excitation mechanism is connected with the dual-spreading sun wing and is used for exciting the dual-spreading solar wing to generate vibration; the vibration detecting mechanism comprises two sets of binocular vision systems and two trusses; the two trusses are arranged in parallel from front to back; the two sets of binocular vision systems and two trusses are in one-to-one correspondence; and each set of binocular vision systems are arranged on the corresponding truss; the two sets of binocular vision systems are used to detect vibration detection marker point areason the front and rear upper surfaces of the dual-spreading solar wing. The two sets of binocular vision systems are arranged on two trusses arranged in parallel from front to back, the two sets of binocular vision systems are used to detect the vibration detection marker point areas on the front and rear upper surfaces of the dual-spreading solar wing, non-contact measurement of the dual-spreading solar wing can be achieved, and more accurate vibration information of the dual-spreading solar wing can be obtained.

Description

technical field [0001] The invention relates to a vibration measurement device, in particular to a vibration measurement device and method for double-deployed solar wings, belonging to the field of vibration measurement. Background technique [0002] In recent years, the complexity of the tasks undertaken by spacecraft has been increasing, and people have higher and higher requirements for its structure. On the one hand, it is required to increase the carrying capacity, and on the other hand, it is required to reduce the total mass of the structure. , flexibility, and large-scale development, great flexibility has become a major feature of modern spacecraft. Flexible structures widely exist in spacecraft, such as solar panel structures of satellites or space workstations, spaceflight wings, flexible robotic arms of space stations, large parabolic antennas, etc. From their structural characteristics, spacecraft with flexible structures can be divided into three categories : ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01H9/00
CPCG01H9/00
Inventor 邱志成王嘉玺
Owner SOUTH CHINA UNIV OF TECH
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