CN205396560U - Hose formula flight refuelling receptacle that can dock automatically - Google Patents
Hose formula flight refuelling receptacle that can dock automatically Download PDFInfo
- Publication number
- CN205396560U CN205396560U CN201620156940.4U CN201620156940U CN205396560U CN 205396560 U CN205396560 U CN 205396560U CN 201620156940 U CN201620156940 U CN 201620156940U CN 205396560 U CN205396560 U CN 205396560U
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- China
- Prior art keywords
- movable wing
- oil filler
- floating anchor
- oil pipe
- metal outer
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Abstract
The utility model discloses a hose formula flight refuelling receptacle that can dock automatically relates to air refuelling technical field, the scalable oil pipe of receiving, sea anchor formula oil filler hole that include and receive oily quick -witted fixed connection, add oil pipe, it stretches out front end fixed connection from the tanker aircraft lower extreme to add oil pipe sea anchor formula oil filler hole, sea anchor formula oil filler hole sets up a plurality of movable wing along the metal outer lane of umbelliform structure is equidistant, movable wing with the metal outer lane is through the round pin hub connection, movable wing follows inside and outside the opening of round pin axle is closed for arouse that the air current changes, guide sea anchor formula oil filler hole carries out the azimuth shift. The utility model discloses a automatically move of sea anchor formula oil filler hole aims at and receives oil pipe, greatly alleviates the working strength who receives oily quick -witted driver, has reduced the technical requirement to the driver, shortens the butt joint time simultaneously, provides more tanker aircraft meetings.
Description
Technical field
This utility model relates to air refuelling technical field, especially a kind of can the hose type flight refuelling receptacle of automatic butt.
Background technology
Hose type flight refueling installation is also known as flexible pipe-floating anchor type (Probe&Drogue) fuel loading system and came out in 1949.Adopting this kind of mode to carry out air refuelling, the equipment of refueled aircraft is very simple, if prow or the leading edge of a wing fill one fixing or telescopic by oil pipe；The fuel-servicing equipment of fuel charger is then made up of the long flexible pipe of capstan winch, 22-30 rice and a funneling drogue, and drogue is funnel-form and lightweight, is fitted with mechanical automatic locking mechanism.After being put in drogue by oil pipe, the mechanical automatic locking mechanism auto lock on drogue is by oil pipe mouth so as to be connected mutually with oil hose, and flexible pipe is then released by winch control and reclaims.But air-flow is changed rdativery sensitive by this kind of oiling mode, relatively difficult during linking, the manipulation technology of pilot is required height.
Utility model content
For the problems referred to above, this utility model provide a kind of can the hose type flight refuelling receptacle of automatic butt.
In order to solve above-mentioned technical problem, the technical solution of the utility model is:
Can the hose type flight refuelling receptacle of automatic butt, including fixing be connected scalable by oil pipe, floating anchor type oil filler, oil filling pipe with refueled aircraft, described oil filling pipe stretches out from fuel charger lower end, front end is fixing connects described floating anchor type oil filler, described floating anchor type oil filler arranges multiple movable wing at equal intervals along the metal outer ring of umbrella-shaped structure, described movable wing is connected by bearing pin with described metal outer ring, described movable wing is along opening and closing inside and outside described bearing pin, for causing air-flow to change, floating anchor type oil filler is guided to carry out azimuth shift；Described laser or infrared transmitting device are installed by the oil pipe mouth of pipe；Described floating anchor type oil filler is provided with laser or infrared receiver；Described laser or infrared receiver are connected to position controller, and described position controller is for controlling the inside and outside opening and closing of movable wing.
Further, described movable wing arranges six at equal intervals along the metal outer ring of umbrella-shaped structure.
Further, described position controller includes signal input interface, signal processor and control signal output interface, and described signal input interface connects described laser or infrared receiver, and described control signal output interface connects described movable wing.
This utility model is directed at by oil pipe by automatically moving of floating anchor type oil filler, greatly alleviates the working strength of refueled aircraft driver, reduces the technology requirement to driver, shortens docking time simultaneously, it is provided that more fuel charger meeting.
Accompanying drawing explanation
Fig. 1 of the present utility model faces structural representation；
Fig. 2 is side-looking structural representation of the present utility model.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, this utility model is described in further detail.Embodiment of the present utility model provides for example with for the purpose of describing, and is not exhaustively or this utility model is limited to disclosed form.Many modifications and variations are apparent from for the ordinary skill in the art.Selecting and describing embodiment is in order to principle of the present utility model and practical application are better described, and makes those of ordinary skill in the art it will be appreciated that this utility model is thus design is suitable to the various embodiments with various amendments of special-purpose.
Embodiment
Can the hose type flight refuelling receptacle of automatic butt, such as Fig. 1, shown in 2, including fixing be connected scalable by oil pipe with refueled aircraft, floating anchor type oil filler 101, oil filling pipe 102, described oil filling pipe 102 stretches out from fuel charger lower end, front end is fixing connects described floating anchor type oil filler 101, described floating anchor type oil filler 101 arranges six movable wings 103 at equal intervals along the metal outer ring 1011 of umbrella-shaped structure, described movable wing 103 is connected by bearing pin with described metal outer ring 1011, described movable wing 103 is along opening and closing inside and outside described bearing pin, for causing air-flow to change, floating anchor type oil filler 101 is guided to carry out azimuth shift；Described laser or infrared transmitting device are installed by the oil pipe mouth of pipe；Described floating anchor type oil filler is provided with laser or infrared receiver；Described laser or infrared receiver are connected to position controller, and described position controller is for controlling the inside and outside opening and closing of movable wing 103.Concrete, described position controller includes signal input interface, signal processor and control signal output interface, and described signal input interface connects described laser or infrared receiver, and described control signal output interface connects described movable wing 103.The signal that described signal processor receives according to laser or infrared receiver, analyze the orientation by oil pipe, be subject to oil pipe orientation further according to what analyze, control different movable wing 103 folding activity, the agitating of movable wing 103 causes air-flow to change, and promotes floating anchor type oil filler 101 Orientation differences.
When by oil pipe close to floating anchor type oil filler 101, laser or infrared receiver detect by the signal that oil pipe sends, position controller is according to the bearing signal by oil pipe, control different movable wings 103 and carry out folding, air-flow is caused to change, thus adjusting the position of floating anchor type oil filler so that it is alignment is by oil pipe.This utility model is directed at by oil pipe by automatically moving of floating anchor type oil filler, greatly alleviates the working strength of refueled aircraft driver, reduces the technology requirement to driver, shortens docking time simultaneously, it is provided that more fuel charger meeting.
Obviously, described embodiment is only a part of embodiment of the present utility model, rather than whole embodiments.The every other embodiment obtained under the premise not making creative work based on the embodiment in this utility model, this area and those of ordinary skill in the related art, all should belong to the scope of this utility model protection.
Claims (3)
1. can the hose type flight refuelling receptacle of automatic butt, including fix with refueled aircraft be connected scalable by oil pipe, floating anchor type oil filler, oil filling pipe, described oil filling pipe stretches out from fuel charger lower end, front end is fixing connects described floating anchor type oil filler, it is characterised in that:
Described floating anchor type oil filler arranges multiple movable wing at equal intervals along the metal outer ring of umbrella-shaped structure, described movable wing is connected by bearing pin with described metal outer ring, described movable wing, along opening and closing inside and outside described bearing pin, is used for causing air-flow to change, and guides floating anchor type oil filler to carry out azimuth shift；
Described laser or infrared transmitting device are installed by the oil pipe mouth of pipe；Described floating anchor type oil filler is provided with laser or infrared receiver；Described laser or infrared receiver are connected to position controller, and described position controller is for controlling the inside and outside opening and closing of movable wing.
2. according to claim 1 can the hose type flight refuelling receptacle of automatic butt, it is characterised in that: described movable wing arranges six at equal intervals along the metal outer ring of umbrella-shaped structure.
3. according to claim 1 can the hose type flight refuelling receptacle of automatic butt, it is characterized in that: described position controller includes signal input interface, signal processor and control signal output interface, described signal input interface connects described laser or infrared receiver, and described control signal output interface connects described movable wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620156940.4U CN205396560U (en) | 2016-03-02 | 2016-03-02 | Hose formula flight refuelling receptacle that can dock automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620156940.4U CN205396560U (en) | 2016-03-02 | 2016-03-02 | Hose formula flight refuelling receptacle that can dock automatically |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205396560U true CN205396560U (en) | 2016-07-27 |
Family
ID=56947572
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620156940.4U Expired - Fee Related CN205396560U (en) | 2016-03-02 | 2016-03-02 | Hose formula flight refuelling receptacle that can dock automatically |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205396560U (en) |
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2016
- 2016-03-02 CN CN201620156940.4U patent/CN205396560U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160727 Termination date: 20190302 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |