Vibration test method, device and aircraft

A test method and aircraft technology, applied in vibration testing, measuring devices, aircraft component testing, etc., can solve the problems that cannot truly reflect the aircraft, achieve the effect of speeding up the research and development progress and avoiding the resonance of the aircraft body

Active Publication Date: 2022-02-18
GUANGZHOU XAIRCRAFT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the environment of the aircraft on the ground is different from that in the air, the vibration response value of the aircraft measured by the hammer tapping method can only be used as a reference, and cannot truly reflect the vibration data of the aircraft during the actual flight.

Method used

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  • Vibration test method, device and aircraft
  • Vibration test method, device and aircraft
  • Vibration test method, device and aircraft

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Embodiment Construction

[0049] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0050] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without making creative efforts belong to the protection scope of the present invention.

[0051]It should be noted that relative term...

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PUM

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Abstract

Embodiments of the present invention provide a vibration testing method, device and aircraft, which relate to the technical field of vibration testing. The vibration test method includes: obtaining an adjustment signal; adjusting the control signal of the motor according to the adjustment signal, so that the rotational speed of the motor changes, thereby making the aircraft in a target vibration state; Vibration signals of ; Among them, different structural parts represent structural parts with the same purpose and different composition and structure. The vibration testing method, device and aircraft provided by the invention can measure vibration signals generated by the aircraft during actual flight.

Description

technical field [0001] The invention relates to the technical field of vibration testing, in particular to a vibration testing method, device and aircraft. Background technique [0002] The existing vibration test method is to measure the vibration response value of the aircraft by using the force hammer knocking method. Since the environment of the aircraft on the ground is different from that in the air, the vibration response value of the aircraft measured by the hammer tapping method can only be used as a reference, and cannot truly reflect the vibration data of the aircraft during the actual flight. Contents of the invention [0003] In view of this, the object of the present invention is to provide a vibration testing method, device and aircraft, which can measure the vibration signals generated by the aircraft during actual flight. [0004] In order to achieve the above object, the technical solution adopted in the embodiment of the present invention is as follows:...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60G01M7/02
CPCB64F5/60G01M7/02G01M7/022
Inventor 许明护吴斌赵智博
Owner GUANGZHOU XAIRCRAFT TECH CO LTD
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