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Double-bent-section and semi-blocking type cargo space door of civil airplane

A technology of civil aircraft and hyperbolic section, which is applied in the field of civil aircraft cargo doors, can solve the problems of low safety performance and low utility model of the doors, and achieve the effects of high safety, high versatility and saving internal space

Active Publication Date: 2016-06-15
AVIC SAC COMML AIRCRAFT
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It solves the technical problems of low utility model and low safety performance of the cabin door existing in the prior art

Method used

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  • Double-bent-section and semi-blocking type cargo space door of civil airplane
  • Double-bent-section and semi-blocking type cargo space door of civil airplane
  • Double-bent-section and semi-blocking type cargo space door of civil airplane

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Embodiment Construction

[0031] A civil aircraft hyperbolic section semi-blocking cargo door, characterized in that: an outer handle mechanism 17 is connected to the handle shaft 20 inside the door, the vent mechanism 18 is linked with the handle shaft 20, and the left and right ends of the handle shaft 20 A lock mechanism 14 is provided, and a visual detection mechanism 15 capable of checking the rotational position is arranged on the lock mechanism 14; the handle shaft 20 is linked with the latch shaft 21, and a latch mechanism 16 is provided at both ends of the latch shaft 21; on the handle shaft 20 There is also an opening mechanism 12 in linkage, and the opening mechanism 12 includes a crank II36 hinged with the hatch structure and an opening mechanism connecting rod 40 connected to the suspension arm 41, and the linkage hatch moves up and down relative to the fuselage structure;

[0032] The handle shaft 20 and the air vent mechanism 18, the handle shaft 20 and the latch shaft 21, and the handle ...

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Abstract

The invention provides a double-bent-section and semi-blocking type cargo space door of a civil airplane. The double-bent-section and semi-blocking type cargo space door of the civil airplane has the structure as follows: a handle shaft in a cargo space door is connected with an outer handle mechanism; a ventilation opening mechanism is linked with a handle shaft; locking mechanisms are arranged at the left and right ends of the handle shaft; each locking mechanism is provided with a visual investigation mechanism capable of checking a rotary position of the handle shaft; the handle shaft is linked with a latch shaft; latch mechanisms are arranged at the two ends of the latch shaft; the handle shaft is further linked with an opening mechanism; the opening mechanism comprises a crank II hinged to the cargo space door and an opening mechanism connecting rod connected with a suspension arm; and the cargo space door is linked to do up and down movement relative to a machine body structure. The cargo space door is at a convergence section of the machine body, is a double-bent-section cargo space door and has the advantages of high safety, strong operability and high commonality.

Description

technical field [0001] The invention relates to a cargo compartment door of a civil aircraft, in particular to a large-opening semi-blocking hazardous cargo compartment door located in a hyperbolic section of the fuselage, which is applied to a civil aircraft. Background technique [0002] Civil aircraft doors can be divided into two types: blocked doors and non-blocked doors. Among them, the blocked hatch is divided into full blocked and half blocked hatch. [0003] The initial movement direction of the fully blocked cargo door is inward relative to the average pressure plane. After opening, the door structure is inside the fuselage. After being fully opened, it occupies the cabin space and has a great impact on the net opening. It has been adopted in the design of civil aircraft cargo doors today. Rarely used. The initial movement direction of the non-blocking door is outward relative to the average pressure plane, and the reliability and safety are not high. In addition...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/14
CPCB64C1/1415
Inventor 陶金库由振华马岩杜尚飞丛家勇孙帆马超赵小龙毕波梁东明金菲于磊
Owner AVIC SAC COMML AIRCRAFT
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