Drainage structure of airplane cabin door

A drainage structure and hatch technology, which is applied to aircraft parts, aircraft accessories, fuselage, etc., can solve the problems of air pressure influence, accumulated water is not clean, and safety is not high, so as to ensure the air pressure and ensure the effect of safe take-off

Pending Publication Date: 2017-10-10
NANJING VOCATIONAL UNIV OF IND TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is that the air pressure in the flight of the aircraft will be affected in the current technology, the safety is not high, and there will also be the situation that the accumulated water cannot be drained cleanly.

Method used

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  • Drainage structure of airplane cabin door
  • Drainage structure of airplane cabin door
  • Drainage structure of airplane cabin door

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Embodiment Construction

[0021] Such as Figure 1-4 As shown, the drainage structure of the aircraft cabin door of the present invention includes: a drainage bottom groove 1, a water retaining strip 2, a drain pipe 3 and a check valve 4; The water storage tank 102, the drive chamber 104 and the water retaining tank 103; the water storage tank 102 is located on the left side of the tank base 101, the driving chamber 104 and the water retaining tank 103 are located on the right side of the tank base 101, and the driving chamber 104 is located below the water retaining tank 103; Be provided with tapered hole 128 at the groove bottom of pond 102; Horizontally be provided with horizontal support 107 on the left and right side inner wall of pond 102, be provided with fixed bar 108 vertically below transverse support 107; Cover on fixed bar 108 A sliding sleeve 109 is provided; a tapered sealing head 110 opposite to the tapered hole 128 is provided on the lower end of the sliding sleeve 109; a sealing rib 12...

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PUM

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Abstract

The invention provides a drainage structure of an airplane cabin door. The drainage structure comprises a drainage bottom tank, a water retaining bar, a drainage tube and a check valve, wherein the drainage bottom tank comprises a tank base as well as a water collecting tank, a drive chamber and a water retaining tank which are arranged in the length direction of the tank base; a tapered hole is formed in the bottom of the water collecting tank; the drainage tube is fixedly connected with the bottom of the tapered hole; the check valve is connected in series onto the drainage pipe. According to the drainage structure of the airplane cabin door, complete sealing can be realized when the tapered hole is plugged by a tapered seal head, automatic seal is realized when the cabin door is closed, normal air pressure is ensured,and safe take-off is guaranteed; when the airplane cabin door is opened, drainage is realized automatically, and water droplets at the edge of the cabin door are also blocked under the action of the water retaining bar, and water cannot be accumulated.

Description

technical field [0001] The invention relates to a drainage structure, in particular to a drainage structure for an aircraft cabin door. Background technique [0002] With the prosperity of the economy, the continuous improvement of people's living standards, the development of production technology is getting better and better, and people's requirements for travel safety and comfort are getting higher and higher. Airplanes are a relatively convenient and fast way of travel. One of the methods is that the aircraft will inevitably encounter water ingress during the opening process of the cabin door. Therefore, a drainage structure is added to the cabin door of the aircraft. Negative Effects. In the current technology, a skin with small holes is provided at the lower end of the fuselage to guide the water out of the cabin, but it will also affect the air pressure in the flight of the aircraft, the safety is not high, and there will be accumulated water that cannot be drained c...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/14
CPCB64C1/1453
Inventor 许振腾王绍贺徐雨欣赵超群陈昕
Owner NANJING VOCATIONAL UNIV OF IND TECH
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