Aircraft freight cabin door positioning and guiding structure

A technology of guiding structure and cabin door, applied in aircraft accessories, door/window accessories, building structure, etc., can solve the problems of small rigidity of the fuselage in the opening area, insufficient locking, lateral swing of the cargo door, etc., so as to improve the lifting capacity. Efficiency and stability, reducing the difficulty of installation and coordination, and improving the reliability of switches

Active Publication Date: 2017-10-20
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1. The cargo door is located at the large opening of the fuselage. The rigidity of the fuselage in the opening area is relatively small, and there are different degrees of deformation under various load conditions. It is difficult to coordinate the gap between the cargo door switch and the large opening, which requires cumbersome and complicated Debugging and experimental process control;
[0004] 2. The cargo door is opened and closed on the ground or in the air. The reliability of precise locking is not high, and it is prone to problems such as insufficient locking and difficulty in opening and closing the door.
[0005] 3 Hoisting equipment is installed on the outer surface of the cargo door, and the cargo door will swing laterally when the cargo is hoisted;

Method used

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  • Aircraft freight cabin door positioning and guiding structure
  • Aircraft freight cabin door positioning and guiding structure
  • Aircraft freight cabin door positioning and guiding structure

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Embodiment Construction

[0024] Aircraft cargo door positioning and guiding structure of the present invention, as figure 1 As shown, it includes: hatch 1, slide rail assembly 2 and upper lock 3; hatch 1 is fixed to the rear of the fuselage with a hinge structure; hatch 1 needs to be opened upwards when in use; hatch 1 needs to be opened by fixing The slide rail on the side wall of the fuselage and the roller installed on the hatch 1 form a slide rail assembly 2 for guidance, and the hatch 1 is opened upward to the highest point and needs to be suspended by the upper lock 3 installed on the upper part of the fuselage; in this process Among them, the opening and positioning accuracy of the hatch 1 firstly depends on the accuracy of the installation of the hinge structure of the hatch 1 and the coordination of the upper lock mechanism;

[0025] The hinge structure of the hatch door 1 adopts the shaft-hole fit. In order to ensure the installation accuracy of the hatch 1 and simplify the assembly difficul...

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Abstract

The invention belongs to the technical field of aircraft structure design and particularly relates to an aircraft freight cabin door positioning and guiding structure. The structure comprises a cabin door (1), a sliding rail assembly (2) and an uplatch (3). The cabin door (1) is hinged to an aircraft body, the sliding rail assembly (2) is mounted on the aircraft body and the cabin door (1), and the uplatch (3) is mounted on the aircraft body and the cabin door (1). According to the structure, stable and reliable positioning and guiding of the aircraft freight cabin door are achieved.

Description

technical field [0001] The technical invention belongs to the technical field of aircraft structure design, and in particular relates to a positioning and guiding structure of an aircraft cargo cabin door. Background technique [0002] In domestic and foreign transport aircraft, most of the aircraft cargo doors adopt a double-door structure that opens up and down. Cargo hoisting equipment is added to the outer surface of the cabin door. Transport aircraft with double-door structure usually have the following technical problems: [0003] 1. The cargo door is located at the large opening of the fuselage. The rigidity of the fuselage in the opening area is relatively small, and there are different degrees of deformation under various load conditions. It is difficult to coordinate the gap between the cargo door switch and the large opening, which requires cumbersome and complicated Control the debugging and experiment process; [0004] 2. The cargo door is opened and closed o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/14E05B15/00E05B65/00E05F5/02
CPCB64C1/14E05B15/00E05B65/00E05F5/02
Inventor 孙锐石鹏飞何倦户张军曹红伟贺宁龙何红芳张小梅胡斌欧宇李敏敏刘世群龚丽娟王健孙乐
Owner SHAANXI AIRCRAFT CORPORATION
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