Warplane cabin transparent piece fastening structure and method

A technology for fastening structures and transparent parts, applied in aircraft parts, aircraft accessories, fuselage, etc., can solve problems such as stress concentration, achieve the effects of ensuring integrity, improving assembly interchangeability, and convenient assembly

Inactive Publication Date: 2014-11-26
YIHE TECH DEV SHANGHAI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0037] The purpose of the present invention is to overcome the defects of the prior art that punching holes on the edge of the transparent part of the fighter cockpit for fastening and installation is prone to stress concentration, and to provide a brand-new fastening and installation structure for the transparent part of the cockpit without drilling

Method used

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  • Warplane cabin transparent piece fastening structure and method
  • Warplane cabin transparent piece fastening structure and method
  • Warplane cabin transparent piece fastening structure and method

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Embodiment Construction

[0093] See Figure 1-13 , in the first preferred embodiment of the present invention, a fastening structure of a fighter cockpit transparent part of the present invention includes a body 1 and a cockpit transparent part 2 installed on the body 1; the periphery of the cockpit transparent part 2 is combined with a border 3 . An installation structure matching the body 1 is formed on the frame 3. The frame 3 includes a pressing component 31 and a fastening component 32. The pressing component 31 and the cabin transparent part 2 press the fastening component 32 to generate prestress and then fasten the cabin transparent part 2. . Among them, the fighter can adopt such as figure 1 Shown adopts the structure of whole cockpit transparent part 2; Also can adopt as Figure 8 Shown adopts the structure of multi-piece cockpit transparent part 2. see Figure 14-17 , for the convenience of description, the following definitions are now made in this embodiment: with Figure 14 , 15 T...

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Abstract

A fastening structure for a transparent member of a fighter plane cockpit and a fastening method therefor. The fastening structure comprises an aircraft body (1) and a cockpit transparent member (2) installed thereupon; the periphery of the cockpit transparent member (2) is fitted with an edge frame (3), said edge frame (3) comprising a compression component (31) and a fastening component (32). The combined pressure on the fastening component (32) of the compression component (31) matched to the cockpit transparent member (2) creates a prestressing force which serves to fasten the cockpit transparent member (2). The present fastening structure is very strong, and has a wide range of application.

Description

technical field [0001] The invention relates to military aircraft such as various fighter jets in the field of national defense construction, in particular to a fastening installation structure and a fastening method for a transparent part of a fighter cockpit. Background technique [0002] The transparent parts of the fighter cockpit generally include the fixed windshield transparent part and the movable canopy transparent part. At present, the integral canopy that combines the two is not uncommon. Under the current situation, military aircraft has become an important manifestation of a country's military strength, and the transparent cockpit as an important optical structural part on a fighter must have the following functions: firstly, it is called a structural part, and must have sufficient strength. To withstand the cockpit pressure of fighter jets, aerodynamic loads, body structure loads and bird impact loads, etc.; the second is that as a transparent observation windo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E06B3/58E06B3/06B64C1/14
CPCB64C1/1492
Inventor 谢晓斌邹彤李震谢隽永
Owner YIHE TECH DEV SHANGHAI
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