CN201094819Y - Fighter fire extinguisher - Google Patents
Fighter fire extinguisher Download PDFInfo
- Publication number
- CN201094819Y CN201094819Y CNU2007200158006U CN200720015800U CN201094819Y CN 201094819 Y CN201094819 Y CN 201094819Y CN U2007200158006 U CNU2007200158006 U CN U2007200158006U CN 200720015800 U CN200720015800 U CN 200720015800U CN 201094819 Y CN201094819 Y CN 201094819Y
- Authority
- CN
- China
- Prior art keywords
- fire extinguisher
- control valve
- fuselage
- nozzle
- fire
- 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.)
- Expired - Fee Related
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
A battleplane fire extinguisher is provided with a fire extinguisher on a machine body. The nozzle of the fire extinguisher is arranged on the outer surface of the machine body. The control valve of the fire extinguisher is an electric control valve. The control valve is connected with a control meter in a cockpit. The battleplane extinguisher has the advantages that as the machine body is provided with the fire extinguisher, one oil box catches fire caused by being shot by bombs, the fire extinguisher can be instantly started to lead extinguishing agent to be sprayed on the machine body in a sector, thus reaching the goal of extinguishing fire and ensuring the security of a pilot, leading the pilot to be able to drive the plane to escape a war zone and reducing the loss of the plane as possible.
Description
Technical field:
The utility model is particularly related to a kind of fighter plane extinguishing device.
Background technology:
Existing fighter plane all is not provided with extinguishing device, in case in actual combat fuel tank be hit by a bullet catch fire the back mid-air explosion just took place in very short time, cause the fatal crass.
Summary of the invention:
The purpose of this utility model is to solve the problems referred to above that prior art exists, and provides a kind of and can carry out quick extinguishing after fuel tanker is hit by a bullet, and guarantees pilot's life security, reduces the fighter plane extinguishing device of opportunity of combat loss.
The utility model is achieved in that it is provided with fire extinguisher on fuselage, and described fire extinguisher nozzle is positioned at the fuselage outer surface, and the fire extinguisher control valve is an electrically-controlled valve, and control valve is connected with the controller dial plate that is positioned at driving cabin.
Above-mentioned fighter plane extinguishing device, described nozzle are two and lay respectively at the upper and lower surface of fuselage that nozzle form is flat duckbill.
Above-mentioned fighter plane extinguishing device, described nozzle are two groups, and two groups of nozzles lay respectively at the upper and lower surface of fuselage.
The utility model has the advantages that: owing on fuselage, be provided with fire extinguisher, catch fire, can start fire extinguisher immediately in case fuel tank is hit by a bullet, make extinguishing chemical be fan-shaped spray to fuselage, reach the fire extinguishing purpose, guarantee pilot's safety, the pilot can be driven an airplane break away from the region of war, reduce the aircraft loss as far as possible.
Description of drawings:
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is nozzle distribution schematic sectional view among Fig. 1 (corresponding embodiment 1);
Fig. 3 is nozzle distribution schematic sectional view among Fig. 1 (corresponding embodiment 2);
Among the figure: fuselage 1, controller dial plate 2, driving cabin 3, fire extinguisher 4, control valve 5, nozzle 6.
The specific embodiment
As shown in Figure 1 and Figure 2, be provided with fire extinguisher 4 at fuselage 1, the nozzle 6 of described fire extinguisher 4 lays respectively at fuselage 1 upper and lower surface and towards the fuel tank position, nozzle 6 is flat duckbill.The control valve 5 of fire extinguisher 4 is an electrically-controlled valve, and control valve 5 is connected with the controller dial plate 2 that is positioned at driving cabin 3.
In actual combat, when fuel tank was hit and catches fire, the pilot opened control valve 5 by the control button on the controller dial plate 3, started fire extinguisher 4, and the extinguishing chemical in the fire extinguisher 4 is fan-shaped spray to fuselage by nozzle 6, plays the fire extinguishing purpose.
As Fig. 1, shown in Figure 3, be provided with fire extinguisher 4 at fuselage 1, the nozzle 6 of described fire extinguisher 4 is two groups, and every group of nozzle 6 is at least three, and present embodiment is an example with three.Two groups of nozzles 6 lay respectively at the upper and lower surface of fuselage and towards the fuel tank position.The control valve 5 of fire extinguisher 4 is an electrically-controlled valve, and control valve 5 is connected with the controller dial plate 2 that is positioned at driving cabin 3.
In actual combat, when fuel tank was hit and catches fire, the pilot opened control valve 5 by the control button on the controller dial plate 2, started fire extinguisher 4, and the extinguishing chemical in the fire extinguisher 4 is by nozzle 6 and intersects fan-shaped spray to fuselage, plays the fire extinguishing purpose.
Claims (3)
1, a kind of fighter plane extinguishing device is characterized in that: be provided with fire extinguisher on fuselage, described fire extinguisher nozzle is positioned at the fuselage outer surface, and the fire extinguisher control valve is an electrically-controlled valve, and control valve is connected with the controller dial plate that is positioned at driving cabin.
2, fighter plane extinguishing device according to claim 1 is characterized in that: described nozzle is two and lays respectively at the upper and lower surface of fuselage that nozzle form is flat duckbill.
3, fighter plane extinguishing device according to claim 1 is characterized in that: described nozzle is two groups, and two groups of nozzles lay respectively at the upper and lower surface of fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200158006U CN201094819Y (en) | 2007-11-08 | 2007-11-08 | Fighter fire extinguisher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200158006U CN201094819Y (en) | 2007-11-08 | 2007-11-08 | Fighter fire extinguisher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201094819Y true CN201094819Y (en) | 2008-08-06 |
Family
ID=39921877
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200158006U Expired - Fee Related CN201094819Y (en) | 2007-11-08 | 2007-11-08 | Fighter fire extinguisher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201094819Y (en) |
-
2007
- 2007-11-08 CN CNU2007200158006U patent/CN201094819Y/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080806 Termination date: 20101108 |