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An aircraft windshield safety monitoring device

A technology for windshield and safety monitoring, applied in the field of aircraft maintenance, can solve problems such as danger to aircraft pilots, loss of cabin pressure, and endangering the safety of the entire aircraft.

Active Publication Date: 2019-01-15
HENGCHENG AVIATION TECH(NANTONG) CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The windshield of the high-altitude aircraft falls off, causing severe environmental conditions such as loss of pressure, low temperature, strong wind, and lack of oxygen inside the cabin, which brings great danger to the pilots of the aircraft and endangers the safety of all personnel on the plane. It is caused by defects in the fuselage and connecting device near the windshield, defects in the windshield itself, and defects in sealing near the windshield, but there is no detection device for the above defects on the market

Method used

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  • An aircraft windshield safety monitoring device
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  • An aircraft windshield safety monitoring device

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Embodiment Construction

[0013] The present invention is achieved through the following technical solutions: an aircraft windshield safety monitoring device, which is composed of a vehicle body 1, a brake device 2, a brake handle 201, a steel wire rope 202, a brake plate 203, a wheel 3, and a seal detection device control panel 4 , sealing detection device 5, vacuum pump 501, sealing suction cup 6, catheter 7, data line 8, crack detection device 9, crack detection device control panel 901, transmission gear 210, transmission gear 111, motor 12, body vibration signal generating device 13, Magnet 1301, body vibration signal generator signal input hole 1302, glass vibration signal generator 14, suction cup 1401, glass vibration signal generator signal input hole 1302, glass vibration signal collection device 15, glass vibration signal output hole 1501, body vibration signal The collecting device 16 is composed of the vibration signal output hole 1601 of the body. The brake device 2 is composed of a brake...

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Abstract

The invention relates to an aircraft windshield safety monitoring device which belongs to the technical field of aircraft maintenance. The device consists of a body, a brake device, a brake handle, awire rope, a brake plate, a wheel, a seal detection device control panel, a seal detection device, a vacuum pump, a sealed suction cup, a conduit, a data line, a crack detection device, a crack detection device control panel, a transmission gear 2, a transmission gear 1, a motor, a body vibration signal generating device, a magnet, a body vibration signal generating device signal input hole, a glass vibration signal generating device, a suction cup, a glass vibration signal generating device signal input hole, a glass vibration signal collecting device, a glass vibration signal output hole, abody vibration signal collecting device and a body vibration signal output hole.

Description

technical field [0001] The invention relates to an aircraft windshield safety monitoring device, specifically a multifunctional device including a detection device for the condition of the fuselage around the windshield, a detection device for the condition of the windshield itself and a detection of the airtightness of the windshield, belonging to aircraft maintenance technology field. Background technique [0002] The windshield of the high-altitude aircraft falls off, causing severe environmental conditions such as loss of pressure, low temperature, strong wind, and lack of oxygen inside the cabin, which brings great danger to the pilots of the aircraft and endangers the safety of all personnel on the plane. It is caused by defects in the fuselage and connecting device near the windshield, defects in the windshield itself, and defects in sealing near the windshield, but there is no detection device for the above defects on the market. Contents of the invention [0003]...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 梁定璿陈伟忠
Owner HENGCHENG AVIATION TECH(NANTONG) CO LTD