CN206942276U - Aircraft moves integrally hangar - Google Patents
Aircraft moves integrally hangar Download PDFInfo
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- CN206942276U CN206942276U CN201720838740.1U CN201720838740U CN206942276U CN 206942276 U CN206942276 U CN 206942276U CN 201720838740 U CN201720838740 U CN 201720838740U CN 206942276 U CN206942276 U CN 206942276U
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- hangar
- aircraft
- moves integrally
- air bag
- air
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Abstract
The utility model, which belongs to Aircraft Hangar technical field and discloses aircraft, moves integrally hangar, including wear-resistant pad on the ground is set and the PVC coated polyester fibers that are arranged on wear-resistant pad made of integral structure air bag；The bottom of the air bag is provided with hook, and the sandbag for counterweight is provided with hook.The utility model uses air sac type structure, and air pressure is sufficient, securely and reliably；Arch design, hangar monolithic stability, the bad weathers such as violent storm, accumulated snow, high/low temperature can be resisted；Aircraft moves integrally hangar and carries out modularized design, builds and acts freely, convenient transportation, has portability；Hangar inflation is intelligent, safe；In hangar folding and unfolding, quickly the gas in hangar can be drained by air pump, it is convenient to fold；During gas leakage will not total Collapse, and can Rapid-Repair, aircraft will not be damaged.
Description
Technical field
The utility model moves integrally hangar more particularly to aircraft, belongs to Aircraft Hangar technical field.
Background technology
With the fast development of CAAC, fleet scale Rapid Expansion, aircraft maintenance task is increasingly heavy, according to aircraft
The needs of maintenance work, these aircraft maintenances work must hangar lijin's rows.The seat in the plane of current domestic permanent hangar is at full stretch,
The investment of newly-built permanent hangar is big, cycle length.When aircraft needs emergency maintenance, it may appear that permanent hangar does not have vacant seat in the plane
And delay, cause very big loss.Mobile hangar currently used in the market is built a framework one layer of cloth of outer cover using inside, this
Kind structure builds time length, unstable, and easily aircraft is damaged；Also a kind of mobile hangar is to use inflatable, monoblock
Change design, using domestic membrane material, this structure bulky, folding and unfolding is difficult, does not possess portability, air pressure is low in addition, and stability compares
Difference.
Utility model content
The technical problems to be solved in the utility model overcomes the defects of existing, there is provided aircraft moves integrally hangar, using gas
Bellows structure, air pressure is sufficient, securely and reliably；Arch design, hangar monolithic stability, violent storm, accumulated snow, high/low temperature etc. can be resisted
Bad weather；Aircraft moves integrally hangar and carries out modularized design, builds and acts freely, convenient transportation, has portability；Hangar
Inflation is intelligent, safe；In hangar folding and unfolding, quickly the gas in hangar can be drained by air pump, it is convenient to fold；Gas leakage
Shi Buhui total Collapses, and can Rapid-Repair, aircraft will not be damaged, can effectively solve asking in background technology
Topic.
In order to solve the above-mentioned technical problem, the utility model provides following technical scheme：
The utility model provides aircraft and moves integrally hangar, including sets wear-resistant pad on the ground and be arranged on wear-resisting
The air bag of integral structure made of PVC coated polyester fibers on pad；The bottom of the air bag is provided with hook, and
The sandbag for counterweight is provided with hook, the bottom of the air bag is connected with air pump, and in the air pump and switch board
The pressure monitor unit PCU in portion is connected in a manner of being electrically connected with, and the pressure monitor unit PCU inside the switch board and hair
Motor and mains supply are electrically connected with.
As a kind of optimal technical scheme of the present utility model, the air bag is domes.
As a kind of optimal technical scheme of the present utility model, the air pump is provided with four, and in parallel between each other.
As a kind of optimal technical scheme of the present utility model, the sandbag is provided with two rows and with the air bag
The heart is symmetrical arranged.
As a kind of optimal technical scheme of the present utility model, the junction of the air pump and the air bag is provided with pressure
Force snesor, and pressure sensor is used to monitor the pressure inside the air bag, and by the pressure value of monitoring with electric signal
Form be delivered to pressure monitor unit PCU inside the switch board.
As a kind of optimal technical scheme of the present utility model, the pressure sensor is the pressure sensing of PX409 series
Device.
The beneficial effect that the utility model is reached is：Using air sac type structure, air pressure is sufficient, securely and reliably；Arch is set
Meter, hangar monolithic stability, can resist the bad weathers such as violent storm, accumulated snow, high/low temperature；Aircraft moves integrally hangar and carries out module
Change design, build and act freely, convenient transportation, there is portability；Hangar inflation is intelligent, safe；In hangar folding and unfolding,
Quickly the gas in hangar can be drained by air pump, it is convenient to fold；During gas leakage will not total Collapse, and can Rapid-Repair, no
Aircraft can be damaged.
Brief description of the drawings
Accompanying drawing is used for providing further understanding to of the present utility model, and a part for constitution instruction, with this practicality
New embodiment is used to explain the utility model together, does not form to limitation of the present utility model.
In the accompanying drawings：
Fig. 1 is that the aircraft described in the utility model embodiment moves integrally hangar top view；
Fig. 2 is that the aircraft described in the utility model embodiment moves integrally hangar stereogram a；
Fig. 3 is that the aircraft described in the utility model embodiment moves integrally hangar rearview；
Fig. 4 is that the aircraft described in the utility model embodiment moves integrally hangar right view；
Fig. 5 is that the aircraft described in the utility model embodiment moves integrally hangar stereogram b；
Label in figure：1st, wear-resistant pad；2nd, generator；3rd, mains supply；4th, switch board；5th, air pump；6th, sandbag；7th, inflating air
Capsule.
Embodiment
Preferred embodiment of the present utility model is illustrated below in conjunction with accompanying drawing, it will be appreciated that described herein excellent
Select embodiment to be merely to illustrate and explain the utility model, be not used to limit the utility model.
Embodiment：Refer to Fig. 1-5, the utility model aircraft moves integrally hangar, including sets on the ground wear-resisting
The air bag 7 of integral structure made of pad 1 and the PVC coated polyester fibers being arranged on wear-resistant pad 1；Wear-resistant pad 1 exists
Designed when building air bag 7 for the prevention coarse scratch air bag 7 in ground, the bottom of the air bag 7 is reserved with extension
Hook, and be provided with hook the sandbag 6 for counterweight, the bottom of the air bag 7 is connected with air pump 5, and the air pump 5 and
Pressure monitor unit PCU inside switch board 4 is connected in a manner of being electrically connected with, and the pressure monitor inside the switch board 4
Unit PCU is electrically connected with generator 2 and mains supply 3, and power supply mode can also use mains supply 3 with generator, because
During emergency maintenance, the airplane parking area at place does not have mains supply 3, can only use generator powered；The air bag 7 is arch knot
Structure, monolithic stability, the bad weathers such as violent storm, accumulated snow, high/low temperature can be resisted；The air pump 5 is provided with four, and between each other
It parallel connection, can quickly be evacuated, when there is one of damage, but also not influence other work；The sandbag 6 is provided with
Two rows and with the center symmetric setting of the air bag 7, make the load-bearing of air bag 7 uniform；The air pump 5 and the inflation
The junction of air bag 7 is provided with pressure sensor, and pressure sensor is used to monitor the pressure inside the air bag 7, and will
The pressure value of monitoring is delivered to the pressure monitor unit PCU inside the switch board 4, the pressure sensing as electronic signals
Device is the pressure sensor of PX409 series, and pressure monitor unit PCU nominal pressure is 150KPa；Low pressure is 90KPa, is generated electricity
Machine 2 is air pump, pressure monitor unit PCU and pressure sensor provide electric power, ensures filling inside normal monitoring air bag 7
Atmospheric pressure, the air pressure inside air bag 7 is set to be maintained in the range of stable 90KPa-150KPa, and pressure monitor unit
PCU is connected with the siren inside switch board and not drawn in figure, and controls siren to work, and has security alarm function, safety
Property it is high；In hangar folding and unfolding, quickly the gas in air bag 7 can be drained by air pump work, it is convenient to fold；Other generator
Electric power mainly is provided to air pump, pressure monitor unit PCU and pressure sensor, is also supplied in addition to other external light unitses
Electricity：Such as illumination, air-conditioned coach, air exhauster, heating equipment.
It should be noted that the utility model, which is aircraft, moves integrally hangar, during work, using air sac type structure, air pressure
Abundance, securely and reliably；Arch design, hangar monolithic stability, the bad weathers such as violent storm, accumulated snow, high/low temperature can be resisted；Aircraft
Move integrally hangar and carry out modularized design, build and act freely, convenient transportation, there is portability；Hangar inflation is intelligent, peace
Quan Xinggao；In hangar folding and unfolding, quickly the gas in hangar can be drained by air pump, it is convenient to fold；Will not integrally it be fallen during gas leakage
Collapse, and can Rapid-Repair, aircraft will not be damaged.
Finally it should be noted that：Preferred embodiment of the present utility model is the foregoing is only, 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 can still modify to the technical scheme described in foregoing embodiments, or to which part technical characteristic
Carry out equivalent substitution.All any modification, equivalent substitution and improvements within the spirit and principles of the utility model, made etc.,
It should be included within the scope of protection of the utility model.
Claims (6)
1. aircraft moves integrally hangar, including sets wear-resistant pad on the ground（1）And it is arranged on wear-resistant pad（1）On PVC
The air bag of integral structure made of coated polyester fiber（7）；Characterized in that, the air bag（7）Bottom set
There is hook, and the sandbag for counterweight is provided with hook（6）, the air bag（7）Bottom and air pump（5）Connection, and
The air pump（5）With switch board（4）Connected in a manner of electric connection, and the switch board（4）With generator（2）With civil power electricity
Source（3）It is electrically connected with.
2. aircraft according to claim 1 moves integrally hangar, it is characterised in that the air bag（7）For arch knot
Structure.
3. aircraft according to claim 1 moves integrally hangar, it is characterised in that the air pump（5）Provided with four, and phase
It is in parallel between mutually.
4. aircraft according to claim 1 moves integrally hangar, it is characterised in that the sandbag（6）Provided with two rows and with
The air bag（7）Center symmetric setting.
5. aircraft according to claim 1 moves integrally hangar, it is characterised in that the air pump（5）With the inflating air
Capsule（7）Junction be provided with pressure sensor, and pressure sensor is used to monitor the air bag（7）Internal pressure, and
The pressure value of monitoring is delivered to the switch board as electronic signals（4）Internal pressure monitor unit PCU.
6. aircraft according to claim 5 moves integrally hangar, it is characterised in that the pressure sensor is PX409 systems
The pressure sensor of row.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720838740.1U CN206942276U (en) | 2017-07-12 | 2017-07-12 | Aircraft moves integrally hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720838740.1U CN206942276U (en) | 2017-07-12 | 2017-07-12 | Aircraft moves integrally hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206942276U true CN206942276U (en) | 2018-01-30 |
Family
ID=61368545
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720838740.1U Active CN206942276U (en) | 2017-07-12 | 2017-07-12 | Aircraft moves integrally hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206942276U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109736629A (en) * | 2018-12-29 | 2019-05-10 | 湖北航特装备制造股份有限公司 | A kind of intelligent work inflation hangar control system |
| CN110409910A (en) * | 2019-08-09 | 2019-11-05 | 蚌埠市建金智能科技有限公司 | A kind of desert inflatable house |
-
2017
- 2017-07-12 CN CN201720838740.1U patent/CN206942276U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109736629A (en) * | 2018-12-29 | 2019-05-10 | 湖北航特装备制造股份有限公司 | A kind of intelligent work inflation hangar control system |
| CN110409910A (en) * | 2019-08-09 | 2019-11-05 | 蚌埠市建金智能科技有限公司 | A kind of desert inflatable house |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 510470 Room 201, No. 2, Lane 2, Fenghe feng'an street, Renhe Town, Baiyun District, Guangzhou City, Guangdong Province (Airport Baiyun) Patentee after: Guangzhou Jianghong Technology Co.,Ltd. Address before: 510440 room 918, Tower B, No. 88, Airport Avenue, Jiahe street, Baiyun District, Guangzhou, Guangdong Province Patentee before: PILOT AIRCRAFT Corp. |