CN104014447A - Paint spraying equipment in aircraft - Google Patents
Paint spraying equipment in aircraft Download PDFInfo
- Publication number
- CN104014447A CN104014447A CN201410227029.3A CN201410227029A CN104014447A CN 104014447 A CN104014447 A CN 104014447A CN 201410227029 A CN201410227029 A CN 201410227029A CN 104014447 A CN104014447 A CN 104014447A
- Authority
- CN
- China
- Prior art keywords
- paint spraying
- paint
- aircraft
- imaging
- nozzle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
- B05B13/06—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00 specially designed for treating the inside of hollow bodies
- B05B13/0627—Arrangements of nozzles or spray heads specially adapted for treating the inside of hollow bodies
- B05B13/0636—Arrangements of nozzles or spray heads specially adapted for treating the inside of hollow bodies by means of rotatable spray heads or nozzles
Landscapes
- Nozzles (AREA)
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
The present invention relates to the aircraft field of spraying paint, relate to specifically a kind of interior of aircraft paint spraying apparatus.
Background technology
Consider assembly technology, maintaining, the repairing needs of aircaft configuration, in design process, housing construction can be reserved corresponding construction access (being generally technique through hole, equipment lid etc.), to the riveted joint of structure, be spirally connected and internal duct and the assembling, decomposition and the repairing that become annex.But, the maintainability of housing construction and its economy and overall performance are conflicting to a certain extent, improve its any one quality and all can need to pay on the other hand certain cost: at the structural region that need to retain construction access, member needs local reinforcement to ensure integrality, the patency of its structural strength holding structure power transmission route conventionally, will cause like this construction weight to increase and affects economy and the overall performance of aircraft; If desired the continuity that as far as possible reduces construction weight, ensure structure, to improve the overall performance of aircraft, will inevitably weaken the maintainability of housing construction.
The housing construction layout of any type is all the product of comprehensive coordination maintainability, weight and overall performance, can not occur occurring in order to improve the maintainability of structure that path spreads all over full machine, construction weight and rolls up and cause the technical indicator situation that is beyond one's reach, also can not occur blindly pursuing index performance and abandoning the situation that maintainability causes structure to assemble or to keep in repair.Therefore, normal conditions are to ensure under the prerequisite of basic construction access, the maintainability of structure all can be subject to impact in various degree, after causing assembling difficulty, complex process or Standard to complete, difficulty etc. is carried out in maintenance work, in the regular maintenance and repair work of aircaft configuration, visual inaccessible inside configuration region exists in a large number, when the enamelled coating in these regions come off or structure repair after while needing to fill spray enamelled coating, conventional paint spraying apparatus, because all restrictions cannot be carried out, at this time just needs a kind of special paint spraying apparatus.
Current conventional paint spraying apparatus (spray gun for paint) is divided into the formula of sucting, gravity type, pressure sending type by coating supply mode, all kinds spray gun for paint has derivative version, as lengthen pressure feed type spray gun and lengthen pressure sending type internal proprietary spray gun for paint, but in the time running into more complicated structure, the paint spraying apparatus that this type of rifle mouth maybe cannot curve greatly cannot meet the requirement of spraying paint.
Summary of the invention
The object of the invention is to address the above problem, a kind of interior of aircraft paint spraying apparatus is provided.
In order to realize object of the present invention, the technical solution used in the present invention is:
A kind of interior of aircraft paint spraying apparatus, comprise coating force feed system and imaging and control system, coating force feed system comprises paint spraying hose, switch sprays paint, be coated with material conveying tube, coating force feed device, imaging and control system comprise illumination imaging integrating device, actuation means, nozzle rod, integrated shower nozzle, integrated shower nozzle comprises and sprays paint monitoring probe and electronic controllable rotating tuning elbow and be connected to the adjustable aperture nozzle of paint spraying hose, coating force feed device, be coated with material conveying tube, switch sprays paint, paint spraying hose is UNICOM successively, paint spraying hose is fixed on integrated shower nozzle through nozzle rod, illumination imaging integrating device is connected with spray paint monitoring probe and actuation means by holding wire, actuation means is connected with electronic controllable rotating tuning elbow by holding wire.
Paint spraying hose is fixed on electronic controllable rotating tuning elbow by clip.
Coating force feed device is provided with pressure-regulating valve, pressure display table.
Actuation means is provided with electronic controllable rotating tuning elbow joystick and monitoring display screen.
The monitoring probe that sprays paint is provided with removable protection diaphragm.
Beneficial effect of the present invention is: simple in structure, easy to use, integrated shower nozzle position is small and exquisite flexibly, can not enter the position of spraying paint because paint can profile affects, in the rotatable situation of integrated shower nozzle, spray painting extremely can be fixed to the spraying dead angle of integrated shower nozzle, and whole process can be carried out video monitoring in real time by monitoring probe.
Brief description of the drawings
Fig. 1 is structural representation of the present invention,
Fig. 2 is integrated nozzle structure schematic diagram of the present invention,
Fig. 3 is actuation means structural representation of the present invention.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is further described:
Embodiment: referring to Fig. 1, Fig. 2, Fig. 3.
A kind of interior of aircraft paint spraying apparatus, comprise coating force feed system and imaging and control system, coating force feed system comprises paint spraying hose 8, switch 6 sprays paint, be coated with material conveying tube 5, coating force feed device 1, imaging and control system comprise illumination imaging integrating device 13, actuation means 16, nozzle rod 7, integrated shower nozzle 4, integrated shower nozzle 4 comprises and sprays paint monitoring probe 12 and electronic controllable rotating tuning elbow 11 and be connected to the adjustable aperture nozzle 9 of paint spraying hose 8, coating force feed device 1, be coated with material conveying tube 5, switch 6 sprays paint, paint spraying hose 8 UNICOM successively, paint spraying hose 8 is fixed on integrated shower nozzle 4 through nozzle rod 7, illumination imaging integrating device 13 is connected with spray paint monitoring probe 12 and actuation means 16 by holding wire, actuation means 16 is connected with electronic controllable rotating tuning elbow 11 by holding wire.
Paint spraying hose 8 is fixed on electronic controllable rotating tuning elbow 11 by clip 10.
Coating force feed device 1 is provided with pressure-regulating valve 2, pressure display table 3.
Actuation means 16 is provided with electronic controllable rotating tuning elbow joystick 14 and monitoring display screen 15.
The monitoring probe 12 that sprays paint is provided with removable protection diaphragm.
Specification: the design be similar to fibre opic endoscope (hose type) in peep and control mechanism, connect coating force feed device and imaging and control system power supply, inject coating by coating charge door, be adjusted to required pressure.Hard hand-held shower bar and integrated shower nozzle are positioned over to inside configuration appropriate location, open monitor switch, observe internal structure by monitoring display screen and monitoring probe, adjust integrated shower nozzle direction joystick and determine that opening the gauge tap that sprays paint behind the position of spraying paint sprays paint.The also hand-held spray boom of capable of regulating and by the electronic rotatable tuning elbow of actuation means control in painting process, electronic rotatable tuning elbow drives the nozzle motion of paint spraying hose, and spray painting, in the position of needs, is completed to interior of aircraft structure spray painting operation.Replaceable protection diaphragm is not polluted by coating in the time spraying paint with len, and adjustable nozzle can carry out atomization to coating according to coating fineness.
What embodiments of the invention were announced is preferred embodiment, but is not limited to this, those of ordinary skill in the art; very easily, according to above-described embodiment, understand spirit of the present invention, and make different amplifications and variation; but only otherwise depart from spirit of the present invention, all in protection scope of the present invention.
Claims (5)
1. an interior of aircraft paint spraying apparatus, comprise coating force feed system and imaging and control system, it is characterized in that: coating force feed system comprises paint spraying hose, switch sprays paint, be coated with material conveying tube, coating force feed device, imaging and control system comprise illumination imaging integrating device, actuation means, nozzle rod, integrated shower nozzle, integrated shower nozzle comprises and sprays paint monitoring probe and electronic controllable rotating tuning elbow and be connected to the adjustable aperture nozzle of paint spraying hose, coating force feed device, be coated with material conveying tube, switch sprays paint, paint spraying hose is UNICOM successively, paint spraying hose is fixed on integrated shower nozzle through nozzle rod, illumination imaging integrating device is connected with spray paint monitoring probe and actuation means by holding wire, actuation means is connected with electronic controllable rotating tuning elbow by holding wire.
2. a kind of interior of aircraft paint spraying apparatus according to claim 1, is characterized in that: paint spraying hose is fixed on electronic controllable rotating tuning elbow by clip.
3. a kind of interior of aircraft paint spraying apparatus according to claim 1, is characterized in that: coating force feed device is provided with pressure-regulating valve, pressure display table.
4. a kind of interior of aircraft paint spraying apparatus according to claim 1, is characterized in that: actuation means is provided with electronic controllable rotating tuning elbow joystick and monitoring display screen.
5. a kind of interior of aircraft paint spraying apparatus according to claim 1, is characterized in that: the monitoring probe that sprays paint is provided with removable protection diaphragm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410227029.3A CN104014447A (en) | 2014-05-27 | 2014-05-27 | Paint spraying equipment in aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410227029.3A CN104014447A (en) | 2014-05-27 | 2014-05-27 | Paint spraying equipment in aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104014447A true CN104014447A (en) | 2014-09-03 |
Family
ID=51431609
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410227029.3A Pending CN104014447A (en) | 2014-05-27 | 2014-05-27 | Paint spraying equipment in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104014447A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000292937A (en) * | 1999-04-07 | 2000-10-20 | Sony Corp | Developing device and developing method |
| CN201482768U (en) * | 2009-05-25 | 2010-05-26 | 金银龙 | Visible flexible shaft cleaning device for cleaning air duct of central air conditioner |
| CN103640711A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Washing device enabling machine body structure inside to be visible |
| CN203842754U (en) * | 2014-05-27 | 2014-09-24 | 江西洪都航空工业集团有限责任公司 | Interior paint spraying device for airplane |
-
2014
- 2014-05-27 CN CN201410227029.3A patent/CN104014447A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000292937A (en) * | 1999-04-07 | 2000-10-20 | Sony Corp | Developing device and developing method |
| CN201482768U (en) * | 2009-05-25 | 2010-05-26 | 金银龙 | Visible flexible shaft cleaning device for cleaning air duct of central air conditioner |
| CN103640711A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Washing device enabling machine body structure inside to be visible |
| CN203842754U (en) * | 2014-05-27 | 2014-09-24 | 江西洪都航空工业集团有限责任公司 | Interior paint spraying device for airplane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20160296980A1 (en) | Portable visual cleaning device | |
| CN104801437A (en) | Inner wall spraying device of round pipeline | |
| CN203842754U (en) | Interior paint spraying device for airplane | |
| CN205833694U (en) | A kind of mechanical type visually cleans device | |
| US1643969A (en) | Means for controlling the distribution of liquids | |
| CN104014447A (en) | Paint spraying equipment in aircraft | |
| US2602004A (en) | Spray gun | |
| WO2012013574A1 (en) | Apparatus for spraying liquids with radio control. | |
| CN103640711A (en) | Washing device enabling machine body structure inside to be visible | |
| JP2012112503A (en) | Foamable urethane filling device, and injection gun for filling foamable urethane | |
| CN103551715A (en) | Anti-blocking processing system for welding gun nozzles for carbon dioxide arc welding | |
| CN110665663A (en) | Air curtain spray head and spraying gun applying same | |
| US9481002B2 (en) | Device for manually painting a large surface, in particular an outer surface of an aircraft | |
| CN203695274U (en) | Electric spraying gun capable of remotely spraying | |
| CN215313222U (en) | Rotary spray gun | |
| CN209287554U (en) | A kind of injection apparatus and sterilizing equipment decontaminating apparatus | |
| CN208275616U (en) | A kind of aqueous electrostatic rotating cup rifle | |
| CN104307658B (en) | A kind of high viscosity fluid atomizer | |
| US7037374B2 (en) | Pneumatic pump switching apparatus | |
| US20090014558A1 (en) | Portable sprayer/mister/fogging system for dispersing media in a uniform and controlled manner | |
| CN105888214A (en) | Wall color paint spraying equipment | |
| CN204870925U (en) | Portable visual cleaning equipment | |
| CN207401614U (en) | A kind of quick spray gun of paint | |
| CN209334037U (en) | A kind of spraying robot hand | |
| CN208194762U (en) | A kind of Ou Ye furnace cupola well reparation spray nozzle device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140903 |