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Aircraft Surface Steam Cleaning System

A cleaning system and aircraft surface technology, which is applied in the field of aircraft surface steam cleaning system, can solve the problems of large water consumption and unclean cleaning, and achieve the effect of strong decontamination ability and high pressure

Active Publication Date: 2019-01-18
沈阳飞机设计研究所扬州协同创新研究院有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the method of cleaning the surface of the aircraft mainly adopts the method of water rinsing. Although this method is simple, direct, mature and reliable, it also has the disadvantages of large water consumption and unclean cleaning.

Method used

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  • Aircraft Surface Steam Cleaning System

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Embodiment Construction

[0019] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a steam cleaning system for an aircraft surface. The steam cleaning system for the aircraft surface comprises a steam generating device (1), a cleaning liquid tank (2), a booster pump (3), a cooling system (4) and a spray nozzle (5), wherein the steam generating device (1) is provided with an output end; the output end of the cleaning liquid tank (2) is connected with the output end of the steam generating device (1) through a pipeline, so that the same output pipeline is formed; the input end of the booster pump (3) is connected with the output pipeline formed by the cleaning liquid tank (2) and the steam generating device (1); the cooling system (4) is arranged in the output pipeline formed by the cleaning liquid tank (2) and the steam generating device (1); the spray nozzle (5) is connected with the output end of the booster pump (3). Compared with the prior art, the stain removal capacity of the steam cleaning system is higher, and the situation that the aircraft surface is damaged due to excessively-high temperature is avoided.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft surface steam cleaning system. Background technique [0002] After flying or long-term parking, the surface of the aircraft often absorbs a large amount of dust, chemical particles and other substances. These substances combine with water vapor in the air to easily form corrosive media. If not cleaned in time, it will cause serious corrosion damage to the aircraft structure , not only shorten the service life of the aircraft, but also easily cause flight safety hazards. Therefore, aircraft surface cleaning technology has always been one of the important technologies that cannot be ignored in the field of aviation maintenance support. At present, the method of washing the surface of the aircraft mainly adopts the method of water rinsing. Although this method is simple, direct, mature and reliable, it also has the disadvantages of large water consumption and unclean c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B08B3/02B08B3/08B08B3/10B08B13/00
CPCB08B3/02B08B3/08B08B3/10B08B13/00
Inventor 王健志邱涛孙卫华李国峰
Owner 沈阳飞机设计研究所扬州协同创新研究院有限公司