CN211584982U - Fixed wing aircraft fire-extinguishing bottle installation device - Google Patents
Fixed wing aircraft fire-extinguishing bottle installation device Download PDFInfo
- Publication number
- CN211584982U CN211584982U CN201921668047.XU CN201921668047U CN211584982U CN 211584982 U CN211584982 U CN 211584982U CN 201921668047 U CN201921668047 U CN 201921668047U CN 211584982 U CN211584982 U CN 211584982U
- Authority
- CN
- China
- Prior art keywords
- belt
- fixed
- fire
- quick
- wing aircraft
- 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.)
- Active
Links
Images
Landscapes
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The utility model relates to a fire-extinguishing bottle installation device, in particular to a fire-extinguishing bottle installation device used on a fixed-wing aircraft. A fixed wing aircraft fire-extinguishing bottle mounting device comprises a fixing piece, a belt-shaped piece and a quick-release device; the fixing piece is used for installing and fixing the belt-shaped piece on the airplane frame; the belt-shaped piece is used for containing a fire extinguishing bottle; the quick release device is arranged at the free end of the belt and used for opening or tightening the belt. Compared with the prior art, the utility model has the advantages of as follows: 1. the problem of the installation of fire-extinguishing bottle under the narrow and small space is fixed and satisfy convenient quick installation and dismouting requirement, this band form has light in weight's advantage simultaneously. 2. Manpower and time are saved for maintenance of the aircraft.
Description
Technical Field
The utility model relates to a fire-extinguishing bottle installation device, in particular to a fire-extinguishing bottle installation device used on a fixed-wing aircraft.
Background
A power system of a certain type of tandem double-seat fixed wing aircraft is provided with two full-authority digital control engines, the two engines are arranged in a left engine compartment and a right engine compartment in parallel, a set of independent fire alarm detection device is respectively arranged in the left engine compartment and the right engine compartment to detect the fire condition of the left engine compartment and the right engine compartment, and when the fire condition occurs, a fire extinguishing button is pressed, so that the fire extinguishing agent in a fire extinguishing bottle can be sprayed into a corresponding ignition area to extinguish the fire. Because the space of the fixed-wing aircraft is narrow, the installation of the fire extinguishing bottle needs to meet the problems of installation space and disassembly and assembly at the same time.
Disclosure of Invention
The utility model aims at providing a can solve the fixed problem of installation and easy dismounting's of fire-extinguishing bottle under narrow and small space stationary vane aircraft fire-extinguishing bottle installation device.
In order to achieve the above purpose, the utility model adopts the following technical scheme: a fixed wing aircraft fire-extinguishing bottle mounting device comprises a fixing piece, a belt-shaped piece and a quick-release device; the fixing piece is used for installing and fixing the belt-shaped piece on the airplane frame; the belt-shaped piece is used for containing a fire extinguishing bottle; the quick release device is arranged at the free end of the belt and used for opening or tightening the belt.
Preferably, the fixing piece is a bracket and a rivet; the support is fixed on the airplane frame through a rivet.
Preferably, the belt-shaped members are a plurality of belt straps connected through triangular rings and are connected and fixed with the support through rivets.
Preferably, the quick-release device comprises a connecting piece, a quick-release nut and a screw rod; the connecting piece is fixed at the free end part of the belt-shaped piece and is provided with a through hole for the screw rod to pass through, and the quick-release nut is matched with the screw rod and is screwed at the end part of the screw rod.
Preferably, the quick-release nut is a butterfly nut.
Preferably, the free ends are two pairs and are adjacently arranged.
The working principle is as follows: adopt the area of band to take the lock form of unloading soon to fix circular fire-extinguishing bottle on the aircraft frame outside the fire district reliable and stable, when the fire-extinguishing bottle was dismantled, only need to twist off the quick-release nut on the band, the fire-extinguishing bottle just can down be dismantled, when the fire-extinguishing bottle was installed, only need open the band, the fire-extinguishing bottle just can be installed toward the aircraft, can solve the fixed problem of installation of fire-extinguishing bottle under the narrow and small space and satisfy convenient quick installation and dismouting requirement, this band form has light in weight's advantage simultaneously.
Compared with the prior art, the utility model has the advantages of as follows:
1. the problem of the installation of fire-extinguishing bottle under the narrow and small space is fixed and satisfy convenient quick installation and dismouting requirement, this band form has light in weight's advantage simultaneously.
2. Manpower and time are saved for maintenance of the aircraft.
Drawings
FIG. 1 is a schematic structural diagram of an embodiment of the present invention;
in the figure, 1, a bracket; 2. wrapping belts; 3. a triangular ring; 4. quickly disassembling the nut; 5. a screw.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawing 1: as shown in fig. 1, the fixed-wing aircraft fire-extinguishing bottle mounting device comprises a bracket 1, a belt 2, a triangular ring 3, a quick-release nut 4 and a screw rod 5; the support 1 is fixed on the airplane frame through rivets; the belt 2 is provided with a plurality of belts, which are connected and fixed through the triangular rings 3 to form a circle for containing a round fire-extinguishing bottle, the free ends of the belt 2 are connected and fixed through a quick-release device so as to be convenient for the installation and the disassembly of the fire-extinguishing bottle, and the round structure formed by the belt 2 is fixed on the bracket 1 through rivets; the quick-release device is used for opening or tightening the wrapping tape 2 and comprises a connecting piece, a quick-release nut 4 and a screw rod 5; the connecting piece is fixed at the free end of the belting 2 and is provided with a through hole for the screw rod 5 to pass through, the through hole is arranged oppositely, and the quick-release nut 4 is matched with the screw rod 5 and is screwed at the end part of the screw rod.
In order to facilitate the installation and the disassembly of the fire extinguishing bottle, the free ends of the wrapping belts 2 are arranged into two pairs, the two pairs are arranged adjacently and are close to the lower part, and the opening is larger, so that the fire extinguishing bottle is more favorable for the installation from bottom to top and the downward disassembly.
The installation process of the fire extinguishing bottle of the certain tandem double-seat fixed wing aircraft is as follows:
(1) fixing the bracket 1 on an airplane frame through rivets;
(2) connecting the bag belt 2 with the bracket 1 through a rivet;
(3) unscrewing the quick-release nut 4, opening the screw rod 5 and opening the wrapping belt 2;
(4) and (3) assembling the fire extinguishing bottle from bottom to top, combining the belt 2, combining the screw rods 5, and screwing the quick-release nut 4 to finish the installation.
The disassembly process of the fire extinguishing bottle of the certain type of tandem double-seat fixed wing aircraft is the reverse process of the process.
The long-time use of above-mentioned installation form shows, can solve the fixed problem of installation of fire-extinguishing bottle under the narrow and small space and satisfy convenient quick installation and dismouting requirement according to this scheme, and this band form has light in weight's advantage simultaneously, has practiced thrift manpower and time for the maintenance of aircraft.
The above embodiments are merely illustrative of the present invention and should not be construed as limiting the present invention. Other alternatives to straps may also be used, for example: other soft materials with toughness. Of course, the structural shape formed by the belt can also be other structural shapes according to the actual shape requirement of the fire extinguishing bottle, and is not limited to the circular shape of the utility model. It should be understood by those skilled in the art that any extension and modification made without departing from the present invention are within the scope of the present invention.
Claims (6)
1. The utility model provides a fixed wing aircraft fire-extinguishing bottle installation device which characterized in that: comprises a fixing piece, a belt-shaped piece and a quick release device; the fixing piece is used for installing and fixing the belt-shaped piece on the airplane frame; the belt-shaped piece is used for containing a fire extinguishing bottle; the quick release device is arranged at the free end of the belt and used for opening or tightening the belt.
2. A fixed-wing aircraft fire suppression bottle mounting apparatus as defined in claim 1, wherein: the fixing piece is a bracket and a rivet; the support is fixed on the airplane frame through a rivet.
3. A fixed-wing aircraft fire suppression bottle mounting apparatus as defined in claim 2, wherein: the belt-shaped parts are a plurality of belt belts connected through triangular rings and are fixedly connected with the support through rivets.
4. A fixed-wing aircraft fire suppression bottle mounting apparatus as defined in claim 1, wherein: the quick-release device comprises a connecting piece, a quick-release nut and a screw rod; the connecting piece is fixed at the free end part of the belt-shaped piece and is provided with a through hole for the screw rod to pass through, and the quick-release nut is matched with the screw rod and is screwed at the end part of the screw rod.
5. A fixed-wing aircraft fire suppression bottle mounting apparatus as defined in claim 4, wherein: the quick-release nut is a butterfly nut.
6. A fixed-wing aircraft fire suppression bottle mounting apparatus as defined in claim 1, wherein: the two pairs of free ends are arranged adjacently.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921668047.XU CN211584982U (en) | 2019-10-08 | 2019-10-08 | Fixed wing aircraft fire-extinguishing bottle installation device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921668047.XU CN211584982U (en) | 2019-10-08 | 2019-10-08 | Fixed wing aircraft fire-extinguishing bottle installation device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN211584982U true CN211584982U (en) | 2020-09-29 |
Family
ID=72585403
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201921668047.XU Active CN211584982U (en) | 2019-10-08 | 2019-10-08 | Fixed wing aircraft fire-extinguishing bottle installation device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN211584982U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4112129A1 (en) * | 2021-07-02 | 2023-01-04 | Airbus Operations (S.A.S.) | Assembly comprising a structure and a tank attached to the structure and containing a fire extinguishing fluid |
FR3132080A1 (en) * | 2022-01-25 | 2023-07-28 | Airbus Operations (S.A.S.) | ASSEMBLY OF AT LEAST ONE EXTINGUISHING AGENT TANK INSIDE AN AIRCRAFT MAST |
-
2019
- 2019-10-08 CN CN201921668047.XU patent/CN211584982U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4112129A1 (en) * | 2021-07-02 | 2023-01-04 | Airbus Operations (S.A.S.) | Assembly comprising a structure and a tank attached to the structure and containing a fire extinguishing fluid |
FR3124793A1 (en) * | 2021-07-02 | 2023-01-06 | Airbus Operations | ASSEMBLY COMPRISING A STRUCTURE AND A TANK FIXED TO THE STRUCTURE AND CONTAINING AN EXTINGUISHING FLUID |
FR3132080A1 (en) * | 2022-01-25 | 2023-07-28 | Airbus Operations (S.A.S.) | ASSEMBLY OF AT LEAST ONE EXTINGUISHING AGENT TANK INSIDE AN AIRCRAFT MAST |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN211584982U (en) | Fixed wing aircraft fire-extinguishing bottle installation device | |
US4037809A (en) | Device for mounting a turboreactor on an aeroplane | |
US10494113B2 (en) | Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box | |
RU2565129C2 (en) | Double-flow turbojet engine assembly and double-flow turbojet engine | |
WO2010007226A3 (en) | Aircraft propulsion system | |
CA2898818C (en) | Rear mount assembly for gas turbine engine | |
CN109250154A (en) | A kind of secondary parachute-opening safety landing system in side | |
CN104029828A (en) | Thermal insulation device for engine of detector | |
CN105944268A (en) | Deluge gun head and deluge gun | |
CN106394937B (en) | A kind of Vehicle nose's insulated hold of repeatable disassembly assembling | |
CN109367790B (en) | Aircraft oxygen cylinder mounting structure | |
CN110439707A (en) | A kind of airplane tail group elastic piece component | |
CN204096089U (en) | Helicopter escape system and escape employment are with rushing umbrella big gun and helicopter with rushing umbrella big gun | |
Gal-Or | Civilizing military thrust vectoring flight control | |
CN106507762B (en) | Airborne wing tip smog ejecting device | |
CN103029823A (en) | Mounting structure of airplane container | |
CN109305319A (en) | Split type unmanned plane | |
CN210049100U (en) | Damper structure for bridge stay cable | |
US10106266B2 (en) | Suspension structure for suspending a turboprop having two unducted propellers from a structural element of an aircraft with rigid fastening of the air intake structure | |
CN202708423U (en) | Clamp structure capable of being dismantled quickly | |
CN207027343U (en) | A kind of fastener anti-dropout installation tool | |
CN202987522U (en) | Mounting structure of airplane container | |
CN208453248U (en) | A kind of series connection TBCC engine pod structure | |
CN210240231U (en) | Integrated fastening device | |
RU2814557C1 (en) | Flying laboratory for flight tests of aircraft engines and other objects of aviation equipment suspended from engine pylon of aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CP02 | Change in the address of a patent holder |
Address after: Nanchang high tech Industrial Development Zone, Jiangxi Province Patentee after: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd. Address before: 330000 Jiangxi city in Nanchang Province, the new bridge box 460 box 5001 Patentee before: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd. |
|
CP02 | Change in the address of a patent holder |