CN207913048U - A kind of aviation main cabin fast fire-extinguishing apparatus - Google Patents
A kind of aviation main cabin fast fire-extinguishing apparatus Download PDFInfo
- Publication number
- CN207913048U CN207913048U CN201721736540.1U CN201721736540U CN207913048U CN 207913048 U CN207913048 U CN 207913048U CN 201721736540 U CN201721736540 U CN 201721736540U CN 207913048 U CN207913048 U CN 207913048U
- Authority
- CN
- China
- Prior art keywords
- tank body
- screw
- pedestal
- main cabin
- extinguishing apparatus
- 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
Links
Abstract
The utility model discloses a kind of aviation main cabin fast fire-extinguishing apparatus,Including temperature-sensitive glass nozzle,Pressure display unit,Tank body,Screw hole,Upper spray,Screw,Vitreum,Dry powder is equipped in the tank body,The tank body top is equipped with can,The tank body is mutually fixedly connected with can,Pressure display unit is equipped on the right side of the can,The can is detachably connected with pressure display unit,Temperature-sensitive glass nozzle is equipped with above the pressure display unit,Screw hole is equipped at the top of the temperature-sensitive glass nozzle,The screw hole is equipped with upper spray,The upper spray has screw,The screw is mutually fixedly connected with screw hole,The screw has vitreum,The vitreum is mutually fixedly connected by mounting seat with pedestal,The pedestal both sides are equipped with arm support,The arm support is mutually welded with pedestal,The pedestal has screwed pipe,The screwed pipe and can phase dismantling connection,Mainly solve the self-extinguishing of aviation main cabin fast fire-extinguishing apparatus,It is simple in structure,It is easily achieved.
Description
Technical field
The utility model is related to gear pump technical fields, specially high-pressure gear pump and high-pressure gear motor axle sleeve.
Background technology
Extinguishing device：Extinguishing device is another saying of extinguishment product, now people to the title of extinguishment product in addition to
Outside extinguishing device, also：Fire distinguisher, fire extinguishing system, fire-extinguishing apparatus, fire extinguisher, extinguishing medium, extinguishing chemical.The visitor of aviation at present
Cabin extinguishing device, mostly using the mode put out a fire manually, such fire-fighting mode is often put out a fire too late when encountering fire behavior
When, unnecessary loss is caused, while can cause centainly to destroy to atmospheric ozone layer, generates greenhouse effects.
Utility model content
The purpose of this utility model is to provide a kind of aviation main cabin fast fire-extinguishing apparatus, solve in background technology and are carried
The problem of going out.
To achieve the above object, the utility model provides the following technical solutions：A kind of aviation main cabin fast fire-extinguishing apparatus, packet
Temperature-sensitive glass nozzle, pressure display unit, tank body, screw hole, upper spray, screw, vitreum are included, dry powder, institute are equipped in the tank body
It states tank body top and is equipped with can, the tank body is mutually fixedly connected with can, and pressure display unit, the tank are equipped on the right side of the can
Head is detachably connected with pressure display unit, and temperature-sensitive glass nozzle, the temperature-sensitive glass nozzle are equipped with above the pressure display unit
Top is equipped with screw hole, and the screw hole is equipped with upper spray, and the upper spray has screw, and the screw is mutually fixed with screw hole
Connection, the screw have vitreum, and the vitreum is mutually fixedly connected by mounting seat with pedestal, the pedestal both sides
Equipped with arm support, the arm support is mutually welded with pedestal, and the pedestal has a screwed pipe, the screwed pipe and the can mutually company of dismounting
It connects.
As a kind of preferred embodiment of the utility model, the temperature-sensitive glass nozzle be both temperature-sensitive releasing member and
It is watering element.
As a kind of preferred embodiment of the utility model, dry powder is housed in the tank body, dry powder is ultra-fine ABC dry powder
Go out pulvis.
As a kind of preferred embodiment of the utility model, the tank is filled with nitrogen as driving gas.
As a kind of preferred embodiment of the utility model, the tank body is externally provided with baking vanish.
Compared with prior art, the beneficial effects of the utility model：This kind of aviation main cabin fast fire-extinguishing apparatus, using
The mode of quick self-extinguishing, while what tank body used instead is on-land type design, facilitates placements, is conducive to put out a fire, be equipped in tank body
Dry powder and gas, ozone layer will not be damaged, mainly solve the self-extinguishing of aviation main cabin fast fire-extinguishing apparatus, knot
Structure is simple, it is easy to accomplish.
Description of the drawings
Fig. 1 is a kind of whole structural schematic diagram of aviation main cabin fast fire-extinguishing apparatus of the utility model；
Fig. 2 is a kind of structure chart of the temperature-sensitive glass nozzle of aviation main cabin fast fire-extinguishing apparatus of the utility model；
In figure:1 temperature-sensitive glass nozzle, 2 pressure display units, 3 tank bodies, 4 screw holes, spray, 6 screws, 7 vitreums, 8 peaces on 5
Fill pedestal, 9 arm supports, 10 pedestals, 11 screwed pipes, 12 dry powder, 13 cans.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of aviation main cabin fast fire-extinguishing apparatus, including
Temperature-sensitive glass nozzle 1, pressure display unit 2, tank body 3, screw hole 4, upper spray 5, screw 6, vitreum 7, interior be equipped with of the tank body 3 are done
Powder 12,3 top of the tank body are equipped with can 13, and the tank body 3 is fixedly connected with 13 phase of can, and 13 right side of the can is equipped with pressure
Power display 2, the can 13 are detachably connected with pressure display unit 2, and the pressure display unit 2 is equipped with temperature-sensitive glass and sprays above
First 1,1 top of the temperature-sensitive glass nozzle is equipped with screw hole 4, and the screw hole 4 is equipped with upper spray 5, and the upper spray 5 has spiral shell
Nail 6, the screw 6 is fixedly connected with 4 phase of screw hole, and the screw 6 has vitreum 7, and the vitreum 7 is by installing bottom
Seat 8 is fixedly connected with 10 phase of pedestal, and 10 both sides of the pedestal are equipped with arm support 9, and the arm support 9 is welded with 10 phase of pedestal, the bottom
Seat 10 has screwed pipe 11, the screwed pipe 11 and 13 phase dismantling connection of can.
As a kind of preferred technical solution in the present embodiment, the temperature-sensitive glass nozzle 1 be both temperature-sensitive releasing member and
It is watering element, is conducive to the uniform sprinkling of large area, dry powder 12 is housed in the tank body 3, dry powder 12 is ultra-fine ABC dry powder
Go out pulvis, and the fire-fighting efficiency of unit area is higher, will not be made to ozone layer as driving gas filled with nitrogen in the tank body 3
At destruction, the tank body 3 is externally provided with baking vanish, is effectively protected tank body 3.
The improvement of the utility model is：It is equipped with using temperature-sensitive glass on this kind of aviation main cabin fast fire-extinguishing apparatus
Nozzle 1 can quick self-extinguishing, while what tank body 3 used instead is on-land type design, facilitates placements, is conducive to put out a fire, in tank body 3
The dry powder 12 and gas being equipped with, dry powder 12 are that ultra-fine ABC dry powder goes out pulvis, and the fire-fighting efficiency of unit area is higher, and gas is nitrogen
Gas will not damage ozone layer.
Finally it should be noted that：The above descriptions are merely preferred embodiments of the present invention, is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it still can be with technical scheme described in the above embodiments is modified, or to which part technical characteristic
Carry out equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (5)
1. a kind of aviation main cabin fast fire-extinguishing apparatus, including temperature-sensitive glass nozzle（1）, pressure display unit（2）, tank body（3）, screw
Hole（4）, upper spray（5）, screw（6）, vitreum（7）, it is characterised in that：The tank body（3）It is interior to be equipped with dry powder（12）, the tank body
（3）Top is equipped with can（13）, the tank body（3）With can（13）It is mutually fixedly connected, the can（13）Right side is equipped with pressure
Display（2）, the can（13）With pressure display unit（2）It is detachably connected, the pressure display unit（2）It is equipped with temperature-sensitive above
Glass nozzle（1）, the temperature-sensitive glass nozzle（1）Top is equipped with screw hole（4）, the screw hole（4）It is equipped with upper spray（5）,
The upper spray（5）Have screw（6）, the screw（6）With screw hole（4）It is mutually fixedly connected, the screw（6）Have glass
Glass body（7）, the vitreum（7）Pass through mounting seat（8）With pedestal（10）It is mutually fixedly connected, the pedestal（10）Both sides are equipped with
Arm support（9）, the arm support（9）With pedestal（10）It mutually welds, the pedestal（10）Have screwed pipe（11）, the screwed pipe
（11）With can（13）Phase dismantling connection.
2. a kind of aviation main cabin fast fire-extinguishing apparatus according to claim 1, it is characterised in that：The temperature-sensitive glass nozzle
（1）It is both temperature-sensitive releasing member and watering element.
3. a kind of aviation main cabin fast fire-extinguishing apparatus according to claim 1, it is characterised in that：The tank body（3）It is built-in
There is dry powder（12）, dry powder is that ultra-fine ABC dry powder goes out pulvis.
4. a kind of aviation main cabin fast fire-extinguishing apparatus according to claim 1, it is characterised in that：The tank body（3）Inside fill
There is nitrogen as driving gas.
5. a kind of aviation main cabin fast fire-extinguishing apparatus according to claim 1, it is characterised in that：The tank body（3）Peripheral hardware
There is baking vanish.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721736540.1U CN207913048U (en) | 2017-12-13 | 2017-12-13 | A kind of aviation main cabin fast fire-extinguishing apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721736540.1U CN207913048U (en) | 2017-12-13 | 2017-12-13 | A kind of aviation main cabin fast fire-extinguishing apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207913048U true CN207913048U (en) | 2018-09-28 |
Family
ID=63606232
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721736540.1U Expired - Fee Related CN207913048U (en) | 2017-12-13 | 2017-12-13 | A kind of aviation main cabin fast fire-extinguishing apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207913048U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109364396A (en) * | 2018-11-17 | 2019-02-22 | 景德镇兴航科技开发有限公司 | A kind of airline extinguishment component |
-
2017
- 2017-12-13 CN CN201721736540.1U patent/CN207913048U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109364396A (en) * | 2018-11-17 | 2019-02-22 | 景德镇兴航科技开发有限公司 | A kind of airline extinguishment component |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20180928 Termination date: 20181213 |