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Rapid adjustment and calibration device for airplane photoelectric equipment

A technology for optoelectronic equipment and aircraft, applied in the field of rapid adjustment devices for aircraft optoelectronic equipment, can solve the problems of inconvenient adjustment of pitch angle, large test space, slow adjustment speed, etc. Effect

Active Publication Date: 2022-06-03
山东首景辉光电科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Aiming at the deficiencies of the prior art, the present invention provides a rapid adjustment device for aircraft photoelectric equipment, which solves the problem that conventional aircraft adjustment requires the cooperation of multiple people, requires a large test space, is cumbersome to use, and requires adjustment of the pitch angle. Inconvenient, unable to achieve effective fit with the aircraft attitude, resulting in slow adjustment speed, and there are certain safety risks

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  • Rapid adjustment and calibration device for airplane photoelectric equipment
  • Rapid adjustment and calibration device for airplane photoelectric equipment
  • Rapid adjustment and calibration device for airplane photoelectric equipment

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Embodiment Construction

[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0027] see Figure 1-7 , the embodiment of the present invention provides a technical solution: a rapid adjustment device for aircraft optoelectronic equipment, including two test points 1 and a test base 2 arranged on the aircraft, in order to ensure the stability of the test base 2, as shown in the attached figure 1 , attached figure 2 and attached image 3 As shown, a counterweight is fixedly installed on the top of the test base ...

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Abstract

The invention discloses a rapid adjustment and calibration device for airplane photoelectric equipment, and relates to the technical field of airplane photoelectric testing, and the rapid adjustment and calibration device comprises two test points and a test base which are arranged on an airplane, and the two test points are symmetrically arranged along the two sides of the central axis of the airplane. According to the rapid adjustment and calibration device for the airplane optoelectronic equipment, two test points are directly and symmetrically arranged on an airplane, normal use of the airplane is not affected, meanwhile, convenient conditions are provided for debugging, the pitching adjustment assembly and the first telescopic rod are arranged on the test base, matching with the pitching angle of the airplane is achieved, and under the arrangement of the angle adjustment assembly, the adjustment and calibration efficiency is improved. Synchronous angle adjustment is directly performed on the two laser range finders, the distance between test points is measured, and the corresponding relation between the target plate and the airplane can be determined after the measured distance is equal, so that the collimation of the airplane can be quickly adjusted, the operation is simple, the calibration device can adapt to test spaces with different sizes, and the calibration accuracy is improved. Therefore, the actual use effect of the device is improved.

Description

technical field [0001] The invention relates to the technical field of aircraft optoelectronic testing, in particular to a rapid adjustment device for aircraft optoelectronic equipment. Background technique [0002] When carrying out support work on the aircraft, such as the calibration of the airborne radar system and the aiming system, the disassembly of the engine, and the disassembly of the landing gear, the aircraft must be jacked up or to a horizontal position. The current common practice is: according to the jacking position marked on the aircraft, the mechanical major is responsible for operating the mechanical jack, the repair major is responsible for measuring the level of the aircraft, and other related majors carry out work, which requires the cooperation of many people to complete, time-consuming, Laborious, inefficient, and a security risk. [0003] At present, there are few methods for the optical axis test and verification of the avionics equipment in the no...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M11/02
CPCG01M11/02G01M11/0207Y02E10/50
Inventor 赵红富李艳娜刘甲勋
Owner 山东首景辉光电科技有限公司
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