A hinge for an aircraft

An aircraft and hinge technology, which is applied to pin hinges, aircraft accessories, aircraft parts, etc., can solve the problems of time-consuming and laborious disassembly of hinges, prolong aircraft maintenance time, etc. Effect

Active Publication Date: 2022-02-15
TIANJIN ISTAR ADVANCED MATERIAL TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In some special cases, the cover needs to be completely removed. The conventional hinge removal is time-consuming and laborious, which prolongs the maintenance time of the aircraft.

Method used

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  • A hinge for an aircraft
  • A hinge for an aircraft
  • A hinge for an aircraft

Examples

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Embodiment Construction

[0027] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.

[0028] Such as Figure 1 to Figure 4 As shown, the embodiment of the present invention provides a hinge for an aircraft, including: a cover connecting seat 1, a connecting arm 3 and a cabin connecting seat 7; Fixedly connected, the other end of the connecting arm 3 is fixedly connected with the cabin connecting seat 7 .

[0029] In an optional embodiment of the present invention, such as image 3 with Figure 4 As shown, the hin...

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PUM

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Abstract

An embodiment of the present invention provides a hinge for an aircraft, including: a cover connecting seat, a connecting arm, and a cabin connecting seat; the cover connecting seat is fixedly connected to one end of the connecting arm, and the limiting arm The other end is fixedly connected with the cabin connecting seat. The solution of the present invention can stably and quickly disassemble the cover and the cabin within a limited space, and has a large load-carrying capacity, and at the same time meets the installation requirements of the arc-shaped cover, reduces maintenance time of the aircraft, and improves work efficiency.

Description

technical field [0001] The invention relates to the technical field of connecting structures of aviation and aerospace vehicles, in particular to a hinge for the aircraft. Background technique [0002] At present, aerospace vehicles such as airplanes are equipped with flaps for purposes such as maintenance and monitoring, and the flaps have to be opened during routine maintenance and repair. For the convenience of flap opening and closing, hinges are usually installed. In some special cases, the cover needs to be completely removed, and the conventional hinge removal is time-consuming and laborious, which prolongs the maintenance time of the aircraft. Contents of the invention [0003] The invention provides a hinge for an aircraft. It can stably and quickly disassemble the cover and cabin in a limited space, and has a large load-carrying capacity. At the same time, it meets the installation requirements of the curved cover, reduces the maintenance time of the aircraft, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): E05D3/06E05D7/10E05D5/02E05D11/00B64C1/14
CPCE05D3/06E05D7/10E05D5/02E05D11/00B64C1/1446E05Y2900/502
Inventor 王志勇张鹏金一唐占文丁常方王非刘发杰
Owner TIANJIN ISTAR ADVANCED MATERIAL TECH CO LTD
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