CN201592782U - Helicopter refueling platform - Google Patents
Helicopter refueling platform Download PDFInfo
- Publication number
- CN201592782U CN201592782U CN2009200470622U CN200920047062U CN201592782U CN 201592782 U CN201592782 U CN 201592782U CN 2009200470622 U CN2009200470622 U CN 2009200470622U CN 200920047062 U CN200920047062 U CN 200920047062U CN 201592782 U CN201592782 U CN 201592782U
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- CN
- China
- Prior art keywords
- helicopter
- platform
- support
- hollow material
- refuelling
- 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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- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The utility model relates to the technical field of avigation, in particular to a refueling platform used for a helicopter, which comprises a support and a refueling platform disposed on the support, a stand column is disposed below the support, the platform is put together by a hollow profile, a hydraulic power unit and an oil filling port are disposed on the platform, and helicopter fuel is filled in the hollow profile. The utility model greatly reduces potential safety hazards by using the refueling platform to fuel up the helicopter, and blocking explosion-proof material is filled in the platform, so as to prevent flammable and explodable liquids from accidents of naked fire, static electricity, impact, shooting and the like which cause explosion.
Description
Technical field
The utility model relates to the aeronautical technology field, especially a kind of refuelling platform that is used for helicopter.
Background technology
Helicopter refuels and generally is divided into air refuelling and bottom surface oiling dual mode, the helicopter that possesses the air refuelling function all has a long fuel filler pipe, its length must exceed the rotor scope, and helicopter inflight refueling, can only adopt flexible pipe to refuel, the hose type flight refueling installation also is called flexible pipe-floating anchor type (Probe ﹠amp; Drogue) fuel loading system is that Britain's air refuelling Co., Ltd is developed on the basis of inheriting forefathers' experience, comes out in 1949.Adopt this kind mode to carry out air refuelling, the equipment of refueled aircraft is very simple, as long as adorn a fixing or telescopic oil pipe that is subjected at the prow or the leading edge of a wing.The bunkering facilities of fuel charger then is made up of capstan winch, 22 to 30 meters long flexible pipes and a funneling drogue.Drogue is funnel-form, and in light weight, and mechanical self-latching mechanism is housed above.After being subjected to oil pipe to put in drogue, the mechanism's auto lock on the drogue is subjected to the oil pipe mouth to make it to be connected mutually with oil hose, and flexible pipe is then emitted and reclaimed by winch control, and this mode operation requirements is very strict, careless slightlyly promptly can cause a serious accident.
And ground refueling generally adopts special-purpose fuel feeding car to refuel to helicopter, and according to the rules, fuel feeding spacing helicopter is no less than 50 meters at least, therefore needs very long fuel filler pipe, and is dangerous when refueling equally.
The utility model content
The utility model provides a kind of helicopter refuelling platform, to solve dangerous this technical matters of original helicopter oiling.
The technical scheme that its technical matters that solves the utility model adopts is: a kind of helicopter refuelling platform, have support and the refuelling platform that is arranged on the support, the support below is provided with column, described platform is assembled by hollow material, platform is provided with hydraulic power unit and oil filling port, is filled with helicopter fuel in the described hollow material.
Further: safer in order to use, be filled with block blast-proof materials in the hollow material.
In order to separate block blast-proof materials, further: be provided with baffle plate in the hollow material, rectangular distribution is useful on the micropore of liquid communication on the baffle plate.
The loading and unloading and the cleaning of block blast-proof materials for convenience, further: hollow material has the lid of flexible connection.
For safety, further: flat-bed is shaped as equilateral polygon, and the length between its each corresponding both sides is all greater than the twice of lifting airscrew diameter.
The utility model refuels to helicopter by refuelling platform, greatly reduces potential safety hazard, and is filled with block blast-proof materials in the platform, and it is explosion caused to prevent that inflammable-explosive liquid is subjected to contingencies such as naked light, static, collision, gunslinging.
Description of drawings
Below in conjunction with accompanying drawing the utility model is further specified.
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the utility model platform plane structural representation;
Fig. 3 is the structural representation of the utility model hollow material;
Fig. 4 is the structural representation of the utility model hollow material Internal baffle;
Wherein: 1, hollow material, 1-1, baffle plate, 1-2, micropore, 1-3, lid, 2, support, 3, column, 4, block blast-proof materials.
The specific embodiment
In conjunction with the accompanying drawings the utility model is described in further detail now.These accompanying drawings are the scheme drawing of simplification, basic structure of the present utility model only is described in a schematic way, so it only show the formation relevant with the utility model.
As Fig. 1, shown in 2, a kind of helicopter refuelling platform, have support and the refuelling platform that is arranged on the support, the support below is provided with column, described platform is assembled by hollow material, platform is provided with hydraulic power unit and oil filling port, be filled with helicopter fuel in the described hollow material, safer in order to use, be filled with block blast-proof materials in the hollow material, in order to separate block blast-proof materials, be provided with baffle plate in the hollow material, rectangular distribution is useful on the micropore of liquid communication on the baffle plate, the loading and unloading and the cleaning of block blast-proof materials for convenience, hollow material has the lid of flexible connection, platform be shaped as equilateral polygon, the length between its each corresponding both sides is all greater than the twice of lifting airscrew diameter.
After helicopter drops on the platform, can the fuel in the platform be added in the helicopter by oil filling port.
The aluminum alloy block blast-proof materials of mentioning in the utility model maintains the leading position in national like product, product has been obtained the important breakthrough of explosion-proof technology, solved and intercepted the wretched insufficiency that explosion-proof technology exists in earlier stage, emphasis solved explosion-proof lamp long-term use meeting produce broken, seriously stop up the difficult problem of various oil circuits.Meanwhile reasonable price is moderate, and cost performance is high.
This aluminum alloy block blast-proof materials product engineering has passed through the assessment of result of national province-level and ministry-level up-to-date technology science and technology, and every index meets the every standard of AQ3001-2005 by economizing the check of quality supervision research institute.
This aluminum alloy block blast-proof materials product is a kind of netted mechanism material that adopts particular aluminum alloy series material and special processing technology manufacturing to form, be filled in it in container that has inflammable, explosive liquid by certain density mode, when air and corresponding liquid vapor mixing reach the explosive limits scope in this container, the accident of when running into naked light, static, bump, thunderbolt and accident and clash accident, can not blasting.Fuel tank such as it can be widely used in the fuel transport car, the filling car that flows, aircraft gas refueller, military-designed vehicle, aircraft, naval vessels and oil tank are explosion-proof; Also can be used for the explosion-proof of containers such as various storage gasoline, diesel oil, banana oil, acetone and tank body.
This aluminium alloy block blast-proof materials has following characteristic:
1, can restrain gasoline, methane, propane, diesel oil, acetone, toluene, ethane, oil equal solvent and similar material and blast.
2, the metal that material is housed can be eliminated static effectively.
3, when the container leakage of this material is housed, can be directly use gas being with under the oily mode, repair welding is carried out in electric welding.
4, the tank truck of this material is housed in transportation, can reduce the shaking degree of liquid.
5, this material container inner wall that do not wear and tear, material itself does not pollute oil, and is indeformable in container, not loss of burn in the oil plant equal solvent, not broken, can not stop up various oil circuits, once pack into and can use for a long time.
6, this material only account for be filled with container cylindrical≤1.0%, spherical≤1.0%, addition is 28～32kg/m3。
Claims (5)
1. helicopter refuelling platform, it is characterized in that: have support (2) and be arranged on refuelling platform on the support (2), the support below is provided with column (3), described platform is assembled by hollow material (1), platform is provided with hydraulic power unit and oil filling port, and described hollow material is filled with helicopter fuel in (1).
2. helicopter refuelling platform according to claim 1 is characterized in that: be filled with block blast-proof materials (4) in the described hollow material (1).
3. helicopter refuelling platform according to claim 1, it is characterized in that: be provided with the stiffening profile effect in the described hollow material (1) and separated the baffle plate (1-1) of block blast-proof materials (4) effect, baffle plate (1-1) is gone up the micropore (1-2) that rectangular distribution is useful on liquid communication.
4. helicopter refuelling platform according to claim 1 is characterized in that: described hollow material (1) has the lid (1-3) of flexible connection.
5. helicopter refuelling platform according to claim 1 is characterized in that: described flat-bed is shaped as octagon, and the length between its each corresponding both sides is all greater than the twice of lifting airscrew diameter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200470622U CN201592782U (en) | 2009-07-08 | 2009-07-08 | Helicopter refueling platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200470622U CN201592782U (en) | 2009-07-08 | 2009-07-08 | Helicopter refueling platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201592782U true CN201592782U (en) | 2010-09-29 |
Family
ID=42774846
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009200470622U Expired - Fee Related CN201592782U (en) | 2009-07-08 | 2009-07-08 | Helicopter refueling platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201592782U (en) |
-
2009
- 2009-07-08 CN CN2009200470622U patent/CN201592782U/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 | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Jiangsu Ampute Explosion Prevention Technology Co., Ltd. Assignor: Mo Suping Contract record no.: 2011320000691 Denomination of utility model: Helicopter refueling platform Granted publication date: 20100929 License type: Exclusive License Record date: 20110505 |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100929 Termination date: 20130708 |