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Paint spraying equipment in aircraft

A technology for spray painting equipment and aircraft, applied in the field of aircraft painting, can solve the problems of large gun nozzles and the inability of painting equipment to meet painting requirements, and achieve the effects of convenient use, simple structure, small and flexible parts

Inactive Publication Date: 2014-09-03
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Currently commonly used painting equipment (paint spray gun) is divided into suction type, gravity type, and pressure-feed type according to the paint supply method. Various types of paint spray guns will have derived structural forms, such as extended pressure-feed spray guns and extended pressure-feed types. Internal special paint spray guns, but when encountering more complex structures, such spray equipment with large nozzles or cannot be bent cannot meet the painting requirements

Method used

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  • Paint spraying equipment in aircraft
  • Paint spraying equipment in aircraft
  • Paint spraying equipment in aircraft

Examples

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Embodiment

[0017] Example: see figure 1 , figure 2 , image 3 .

[0018] An aircraft interior painting equipment, including paint pressure feeding system and imaging and control system, paint pressure feeding system includes paint spray hose 8, paint spray switch 6, paint delivery pipe 5, paint pressure feeding device 1, imaging and control system includes lighting imaging Integrated device 13, control device 16, spray head rod 7, integrated spray head 4, integrated spray head 4 includes spray paint monitoring probe 12, electric controllable rotation and steering elbow 11 and adjustable aperture nozzle 9 connected to paint spray hose 8, paint pressure The delivery device 1, the paint delivery pipe 5, the paint spray switch 6, and the paint spray hose 8 are connected in sequence, the paint spray hose 8 passes through the nozzle rod 7 and is fixed on the integrated nozzle 4, and the lighting and imaging integrated device 13 communicates with the paint spray monitoring probe 12 and The ...

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Abstract

The invention relates to the field of aircraft painting, in particular to paint spraying equipment in an aircraft. The paint spraying equipment comprises a coating pressure feed system and an imaging and controlling system, the coating pressure feed system comprises a paint spraying hose, a paint spraying switch, a coating conveying pipe and a coating pressure feed device, the imaging and controlling system comprises an illuminating and imaging integrated device, an operating device, a spray head rod and an integrated spray head, the integrated spray head comprises a paint spraying monitoring probe, an electric controllable rotating and turning bend and a controllable aperture nozzle connected with the paint spraying hose, the coating pressure feed device, the coating conveying pipe, the paint spraying switch and the paint spraying hose are communicated in sequence, the paint spraying hose penetrates through the spray head rod and is fixedly arranged on the integrated nozzle, the illuminating and imaging integrated device is connected with the paint spraying monitoring probe and the operating device through signal lines, and the operating device is connected with the electric controllable rotating and turning bend through a signal line. The paint spraying equipment is simple in structure and convenient to use, the integrated nozzle is small, exquisite and flexible, the paint spaying position where the nozzle enters cannot be influenced by the appearance of a paint tank, coatings can be sprayed to a spray dead angle, and real-time monitoring can be achieved.

Description

technical field [0001] The invention relates to the field of aircraft painting, in particular to an aircraft interior painting equipment. Background technique [0002] Considering the assembly process, maintenance, and repair needs of the aircraft structure, during the design process, the airframe structure will reserve corresponding construction accesses (usually process through holes, equipment access covers, etc.) to facilitate the riveting, screwing, and internal Assembly, disassembly and repair of piping and accessories. However, the maintainability of the airframe structure and its economy and overall performance are contradictory to some extent. To improve its quality in any aspect will need to pay a certain price on the other side: in the structural area where construction access needs to be preserved , the components usually need to be locally reinforced to ensure their structural strength and maintain the integrity and smoothness of the structural force transmissi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B05B13/04B05B15/08B05B15/68
CPCB05B13/0636
Inventor 王学强彭志军叶彬吕万韬石飞朱亲强张海周王红飞杜兴刚姜亚娟李朝光徐丹
Owner JIANGXI HONGDU AVIATION IND GRP
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