CN204507276U - A kind of high pressure dry-chemical fire extinguishing aircraft - Google Patents
A kind of high pressure dry-chemical fire extinguishing aircraft Download PDFInfo
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- CN204507276U CN204507276U CN201520152239.0U CN201520152239U CN204507276U CN 204507276 U CN204507276 U CN 204507276U CN 201520152239 U CN201520152239 U CN 201520152239U CN 204507276 U CN204507276 U CN 204507276U
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- aircraft
- high pressure
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The utility model relates to a kind of high pressure dry-chemical fire extinguishing aircraft, aircraft supporting leg is arranged on aircraft bottom, high pressure powder extinguisher is arranged on aircraft and props up inboard leg, video camera is arranged on aircraft side, jet pipe is arranged on self-priming blending box right-hand member, be communicated with dry powder can by connection pipe A in the middle part of self-priming blending box, self-priming blending box left end is connected with electrically-controlled valve right-hand member, electrically-controlled valve left end is connected with T-pipe joint right-hand member, T-pipe joint left end is connected with limiting valve right-hand member, T-pipe joint lower end is connected with hand valve upper end, hand valve lower end connects liquid carbonic acid cylinder, between hand valve and liquid carbon dioxide bottle, compression indicator is set, limiting valve left end is communicated with dry powder can by connection pipe B.The beneficial effect of utility model: solve high-rise fire fighting difficulty, not easily observe a difficult problem for the condition of a fire, fire fighting efficiency is high, alleviates the life security hidden danger to firefighter, has very high market using value.
Description
Technical field
The utility model relates to a kind of fire-fighting aircraft, particularly relates to a kind of high pressure dry-chemical fire extinguishing aircraft.
Background technology
Current control high-rise fire mainly stands on fire-fighting bay-lift by the hand-held water blast gun of firefighters and puts out a fire, high-rise due to the number of plies many, outside appendage is easy to come off under the scorching of big fire, very large dangerous hidden danger is caused to the fire-fighting bay-lift of building side, and big fire dense smoke not easily observes comparatively greatly the condition of a fire in building, causes difficulty to fire fighting work.
Utility model content
Technical problem to be solved in the utility model is: provide a kind of high pressure dry-chemical fire extinguishing aircraft, solves high-rise fire fighting difficulty, not easily observes a difficult problem for the condition of a fire.
The technical scheme that the problem that the utility model is the above-mentioned proposition of solution adopts is:
A kind of high pressure dry-chemical fire extinguishing aircraft, comprises aircraft supporting leg 9, aircraft 10, high pressure powder extinguisher 14 and video camera 15, aircraft supporting leg 9 is arranged on aircraft 10 bottom, and high pressure powder extinguisher is arranged on inside aircraft supporting leg 9, and video camera 15 is arranged on aircraft 10 side, and described high pressure powder extinguisher 14 comprises jet pipe 1, self-priming blending box 2, electrically-controlled valve 3, limiting valve 4, hand valve 5, compression indicator 6, dry powder can 7, liquid carbon dioxide bottle 8, connection pipe A11, connection pipe B12 and T-pipe joint 13, jet pipe 1 is arranged on self-priming blending box 2 right-hand member, be communicated with dry powder can 7 by connection pipe A11 in the middle part of self-priming blending box 2, self-priming blending box 2 left end is connected with electrically-controlled valve 3 right-hand member, electrically-controlled valve 3 left end is connected with T-pipe joint 13 right-hand member, T-pipe joint 13 left end is connected with limiting valve 4 right-hand member, T-pipe joint 13 lower end is connected with hand valve 5 upper end, hand valve 5 lower end connects liquid carbonic acid cylinder 8, arrange compression indicator 6 between hand valve 5 and liquid carbon dioxide bottle 8, limiting valve 4 left end is communicated with dry powder can 7 by connection pipe B12.
Described jet pipe 1 front end geometry is taper, is convenient to aim at flame position.
Described dry powder can 7 is wheel the form of the foetus metallic steel tank, is easily installed in aircraft and props up inboard leg.
Described liquid carbon dioxide bottle 8 is arranged on inside dry powder can 7, is convenient to lay.
Described aircraft supporting leg 9 is trapezoidal metallic support, lands more steady.
Described aircraft 10 is rotor craft, can better rest on aerial.
Described video camera 15 is thermal infrared imager, can penetrate dense smoke completely, and part penetrates thick fog damply.
Principle of work of the present utility model: make rotor craft rest on fire location, the condition of a fire is observed by video camera, jet pipe is made to aim at place on fire, open electrically-controlled valve, liquid carbon dioxide one tunnel enters in dry powder can through limiting valve, and a road sprays at a high speed along jet pipe with dry powder through self-priming mixer.
The beneficial effects of the utility model are: 1, solve high-rise fire fighting difficulty, not easily observe a difficult problem for the condition of a fire, fire fighting efficiency is high, alleviates the life security hidden danger to firefighter, has very high market using value.2, jet pipe front end geometry is taper, is convenient to aim at flame position.3, dry powder can is wheel the form of the foetus metallic steel tank, is easily installed in aircraft and props up inboard leg.4, liquid carbon dioxide bottle is arranged on inside dry powder can, is convenient to lay.5, aircraft supporting leg is trapezoidal metallic support, lands more steady.6, aircraft is rotor craft, can better rest on aerial.7, video camera is thermal infrared imager, can penetrate dense smoke completely, and part penetrates thick fog damply.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Wherein, 1-jet pipe, the self-priming blending box of 2-, 3-electrically-controlled valve, 4-limiting valve, 5-hand valve, 6-compression indicator, 7-dry powder can, 8-liquid carbon dioxide bottle, 9-aircraft supporting leg, 10-aircraft, 11-connection pipe A, 12-connection pipe, 13-T-pipe joint, 14-high pressure powder extinguisher, 15-video camera.
Detailed description of the invention
Embodiment of the present utility model is further illustrated below in conjunction with accompanying drawing.
With reference to Fig. 1, a kind of high pressure dry-chemical fire extinguishing aircraft described in this detailed description of the invention, comprise aircraft supporting leg 9, aircraft 10, high pressure powder extinguisher 14 and video camera 15, aircraft supporting leg 9 is arranged on aircraft 10 bottom, high pressure powder extinguisher is arranged on inside aircraft supporting leg 9, video camera 15 is arranged on aircraft 10 side, described high pressure powder extinguisher 14 comprises jet pipe 1, self-priming blending box 2, electrically-controlled valve 3, limiting valve 4, hand valve 5, compression indicator 6, dry powder can 7, liquid carbon dioxide bottle 8, connection pipe A11, connection pipe B12 and T-pipe joint 13, jet pipe 1 is arranged on self-priming blending box 2 right-hand member, be communicated with dry powder can 7 by connection pipe A11 in the middle part of self-priming blending box 2, self-priming blending box 2 left end is connected with electrically-controlled valve 3 right-hand member, electrically-controlled valve 3 left end is connected with T-pipe joint 13 right-hand member, T-pipe joint 13 left end is connected with limiting valve 4 right-hand member, T-pipe joint 13 lower end is connected with hand valve 5 upper end, hand valve 5 lower end connects liquid carbonic acid cylinder 8, compression indicator 6 is set between hand valve 5 and liquid carbon dioxide bottle 8, limiting valve 4 left end is communicated with dry powder can 7 by connection pipe B12.
Described jet pipe 1 front end geometry is taper, is convenient to aim at flame position.
Described dry powder can 7 is wheel the form of the foetus metallic steel tank, is easily installed in aircraft and props up inboard leg.
Described liquid carbon dioxide bottle 8 is arranged on inside dry powder can 7, is convenient to lay.
Described aircraft supporting leg 9 is trapezoidal metallic support, lands more steady.
Described aircraft 10 is rotor craft, can better rest on aerial.
Described video camera 15 is thermal infrared imager, can penetrate dense smoke completely, and part penetrates thick fog damply.
The principle of work of this detailed description of the invention: make rotor craft rest on fire location, the condition of a fire is observed by video camera, jet pipe is made to aim at place on fire, open electrically-controlled valve, liquid carbon dioxide one tunnel enters in dry powder can through limiting valve, and a road sprays at a high speed along jet pipe with dry powder through self-priming mixer.
The beneficial effect of this detailed description of the invention is: 1, solve high-rise fire fighting difficulty, not easily observe a difficult problem for the condition of a fire, fire fighting efficiency is high, alleviates the life security hidden danger to firefighter, has very high market using value.2, jet pipe front end geometry is taper, is convenient to aim at flame position.3, dry powder can is wheel the form of the foetus metallic steel tank, is easily installed in aircraft and props up inboard leg.4, liquid carbon dioxide bottle is arranged on inside dry powder can, is convenient to lay.5, aircraft supporting leg is trapezoidal metallic support, lands more steady.6, aircraft is rotor craft, can better rest on aerial.7, video camera is thermal infrared imager, can penetrate dense smoke completely, and part penetrates thick fog damply.
Specific embodiment of the utility model does not form restriction of the present utility model, and every employing analog structure of the present utility model and change, all in protection domain of the present utility model.
Claims (7)
1. a high pressure dry-chemical fire extinguishing aircraft, it is characterized in that: comprise aircraft supporting leg (9), aircraft (10), high pressure powder extinguisher (14) and video camera (15), aircraft supporting leg (9) is arranged on aircraft (10) bottom, high pressure powder extinguisher is arranged on aircraft supporting leg (9) inner side, video camera (15) is arranged on aircraft (10) side, described high pressure powder extinguisher (14) comprises jet pipe (1), self-priming blending box (2), electrically-controlled valve (3), limiting valve (4), hand valve (5), compression indicator (6), dry powder can (7), liquid carbon dioxide bottle (8), connection pipe A(11), connection pipe B(12) and T-pipe joint (13), jet pipe (1) is arranged on self-priming blending box (2) right-hand member, self-priming blending box (2) middle part is by connection pipe A(11) be communicated with dry powder can (7), self-priming blending box (2) left end is connected with electrically-controlled valve (3) right-hand member, electrically-controlled valve (3) left end is connected with T-pipe joint (13) right-hand member, T-pipe joint (13) left end is connected with limiting valve (4) right-hand member, T-pipe joint (13) lower end is connected with hand valve (5) upper end, hand valve (5) lower end connects liquid carbonic acid cylinder (8), compression indicator (6) is set between hand valve (5) and liquid carbon dioxide bottle (8), limiting valve (4) left end is by connection pipe B(12) be communicated with dry powder can (7).
2. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described jet pipe (1) front end geometry is taper.
3. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described dry powder can (7) is wheel the form of the foetus metallic steel tank.
4. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described liquid carbon dioxide bottle (8) is arranged on dry powder can (7) inner side.
5. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described aircraft supporting leg (9) is trapezoidal metallic support.
6. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described aircraft (10) is rotor craft.
7. a kind of high pressure dry-chemical fire extinguishing aircraft as claimed in claim 1, is characterized in that: described video camera (15) is thermal infrared imager.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520152239.0U CN204507276U (en) | 2015-03-18 | 2015-03-18 | A kind of high pressure dry-chemical fire extinguishing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520152239.0U CN204507276U (en) | 2015-03-18 | 2015-03-18 | A kind of high pressure dry-chemical fire extinguishing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204507276U true CN204507276U (en) | 2015-07-29 |
Family
ID=53705269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520152239.0U Expired - Fee Related CN204507276U (en) | 2015-03-18 | 2015-03-18 | A kind of high pressure dry-chemical fire extinguishing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204507276U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106864752A (en) * | 2017-03-18 | 2017-06-20 | 芜湖元航空科技有限公司 | Fire extinguisher bomb bomb droping gear is unloaded in a kind of grabbing for fire-fighting unmanned plane |
| CN107308568A (en) * | 2017-07-12 | 2017-11-03 | 重庆国飞通用航空设备制造有限公司 | Flight fire station |
-
2015
- 2015-03-18 CN CN201520152239.0U patent/CN204507276U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106864752A (en) * | 2017-03-18 | 2017-06-20 | 芜湖元航空科技有限公司 | Fire extinguisher bomb bomb droping gear is unloaded in a kind of grabbing for fire-fighting unmanned plane |
| CN107308568A (en) * | 2017-07-12 | 2017-11-03 | 重庆国飞通用航空设备制造有限公司 | Flight fire station |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150729 Termination date: 20170318 |