A modal test support device and using method thereof

A technology of support device and modal test, applied in the field of machinery, can solve the problems that the support tooling is difficult to meet the test requirements, the test reliability is reduced, and the size of the test piece is large, so as to improve the test reliability, easy operation, Composing simple effects

Active Publication Date: 2022-04-12
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The modal test is a test that must be completed for large-scale and flexible solar drones, aircraft or structural parts. However, due to the large size and flexibility of the test piece, its natural frequency is generally very low, and conventional support tools are difficult to meet the test requirements. requirements, the reliability of the test is greatly reduced

Method used

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  • A modal test support device and using method thereof
  • A modal test support device and using method thereof
  • A modal test support device and using method thereof

Examples

Experimental program
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Embodiment

[0059] figure 1 A structural block diagram of a modal test support device according to an embodiment of the present invention is shown. figure 2 A structural schematic diagram of an anti-stiffness diamond frame of a modal test support device according to an embodiment of the present invention is shown.

[0060] combine figure 1 with figure 2 As shown, the modal test support device includes: a suspension structure 1, the suspension structure 1 is used to suspend the test piece 2; a support structure, the support structure is arranged under the suspension structure 1, and is used to support the test piece 2 , the suspension structure 1 is matched with the support structure, so that the stiffness of the modal test support device is zero; the support structure includes a counter-stiffness diamond frame 4, a telescopic sleeve, a horizontal elastic member 49 and a base 6, and the base 6 is set on the counter-stiffness Below the diamond frame 4, the telescopic sleeve is respecti...

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PUM

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Abstract

The invention discloses a modal test support device and a using method thereof. The device comprises: a suspension structure for suspending a test piece; a support structure arranged under the suspension structure for supporting the test piece; The structure matches the support structure so that the stiffness of the modal test support device is zero; the support structure includes a counter-stiffness diamond frame, a telescopic sleeve, a horizontal elastic component and a base, and the telescopic sleeve is respectively connected to the counter-stiffness diamond frame and the base , the horizontal elastic component connects the diagonal of the anti-stiffness rhombus; wherein, the suspension structure includes a suspension beam, a first elastic component and a second elastic component, and the first elastic component and the second elastic component are connected to the suspension beam in parallel, It is used to suspend the test piece, and the elastic stiffness coefficients of the first elastic component and the second elastic component are both half of the elastic stiffness coefficient of the horizontal elastic component. The modal test support device of the invention has low rigidity, meets the modal test requirements of low-frequency structures, and further improves test reliability.

Description

technical field [0001] The invention belongs to the field of machinery, and more specifically relates to a modal test support device and a use method thereof. Background technique [0002] Experimental modal analysis, also known as the experimental process of modal analysis, referred to as modal experiment, is the inverse process of theoretical modal analysis, one of the methods to verify the reliability of finite element analysis, and a necessary and effective means for structural dynamic design one. In the modal experiment, it is very important whether the support method of the tested structural member is appropriate, because the structure will have different modal parameters under different boundary conditions. The modal test is a test that must be completed for large-scale and flexible solar drones, aircraft or structural parts. However, due to the large size and high flexibility of the test piece, its natural frequency is generally very low, and conventional support to...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 康传明安佰华梁晗星林谢伟郭懿霆
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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