Test workbench and system for head cabin aircraft

A test workbench and test system technology, applied in the direction of aircraft component testing, etc., can solve the problems of high labor input, long time period, safety risks, etc., and achieve the effect of improving work efficiency, high test efficiency, and ensuring stability.

Pending Publication Date: 2022-01-28
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the workbench needs to fix the head compartment and drive it to rotate together, the requirements for its connection reliability and stability are high, but the current workbench cannot meet the needs well
[0003] In addition, in the past, the sub-aircraft in the cockpit was regularly tested and calibrated. There was a step of dismantling the sub-aircraft from the cockpit, which required multiple hoisting and transfer of the cockpit and the sub-aircraft. There are also many; because the sub-aircraft is equipped with pyrotechnics, there are certain safety risks when performing multiple mechanical operations on the sub-aircraft, which will also affect the reliability of the aircraft.

Method used

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  • Test workbench and system for head cabin aircraft
  • Test workbench and system for head cabin aircraft
  • Test workbench and system for head cabin aircraft

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Embodiment Construction

[0042] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of this application, but not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present application.

[0043] The embodiments of the present application provide a test workbench for a head-cabin aircraft, which can solve the problems of connection reliability and stability of the workbench.

[0044] figure 1 It is a schematic diagram of the structure of the test bench for the aircraft in the head cabin, which includes a support pla...

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PUM

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Abstract

The invention discloses a test workbench and system for a head cabin aircraft, and relates to the field of experimental testing, and the test workbench comprises a supporting plate part which is used for fixing a to-be-tested head cabin, a rotating mechanism used for driving the supporting plate piece to rotate, a solenoid mechanism arranged below the supporting plate part and configured to send out a rotation stopping signal when the supporting plate piece rotates to the first position or the second position, and at least one locking mechanism arranged below the supporting plate part; and when the supporting plate part rotates to the first position or the second position, the locking mechanism is used for locking the supporting plate part. Requirements on reliability and stability in the testing process can be met.

Description

technical field [0001] The invention relates to the field of testing and testing, in particular to a testing workbench and a system for a head-cabin aircraft. Background technique [0002] The sub-aircraft in the head cabin needs to be regularly tested and calibrated, and the number of inertial pulses usually needs to be tested in the static state and the rotating state. Since the workbench needs to fix the head cabin and drive it to rotate together, the requirements for its connection reliability and stability are high, but the current workbench cannot meet the needs well. [0003] In addition, in the past, when testing and calibrating the sub-aircraft in the head cabin on a regular basis, there was a step of removing the sub-aircraft from the head cabin. The head cabin and the sub-aircraft need to be hoisted and transported multiple times, which takes a long time period, involves a lot of equipment, and requires different professional manpower input. There are also many; ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 吴翔
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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