CN202244091U - Active target seeking type oil feeding device for airplane air refueling - Google Patents
Active target seeking type oil feeding device for airplane air refueling Download PDFInfo
- Publication number
- CN202244091U CN202244091U CN2011202202194U CN201120220219U CN202244091U CN 202244091 U CN202244091 U CN 202244091U CN 2011202202194 U CN2011202202194 U CN 2011202202194U CN 201120220219 U CN201120220219 U CN 201120220219U CN 202244091 U CN202244091 U CN 202244091U
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- CN
- China
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- oil feeding
- oily
- awarded
- tapered sleeve
- taper sleeve
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Abstract
The utility model discloses an active target seeking type oil feeding device for airplane air refueling. The utility model is characterized in that the oil feeding device comprises a double-layered oil feeding hose, a power supply cable and a control cable are arranged in the double-layered oil feeding hose, one end of the double-layered oil feeding hose is connected with an airplane needing air feeding and the other end of the double-layered oil feeding hose is connected with an oil feeding taper sleeve, a plurality of spoilers are uniformly arranged on the oil feeding taper sleeve and are connected with a transmission mechanism, the transmission mechanism comprises a micro-scale servomotor, a camera is further arranged on the oil feeding taper sleeve, and an oil feeding nozzle is arranged in the center of the oil feeding taper sleeve and is connected and matched with the oil feeding nozzle of the airplane needing air feeding. The oil feeding device has the advantages that a closed control system is adopted, so as to easily realize position shifting of the oil feeding taper sleeve, and further realize active target seeking; through the active target seeking control, the butting for air refueling costs less time, and the difficulty in flying requirements for air refueling is lowered; and by adopting intrinsic safety treatment, air refueling safety is ensured and explosion-protection effect is achieved.
Description
Technical field
The utility model relates to awards oily device field, relates in particular to the active homing formula of a kind of aircraft air refuelling and awards oily device.
Background technology
The control system of closed loop is easy to realize awarding the offset correction of oily tapered sleeve, and manual control requires difficulty high to flight-refueled flight, and air refuelling butt joint difficulty has increased the air refuelling docking time, and air refuelling does not have safety assurance, is easy to generate blast.During to the aircraft air refuelling, awarding oily flexible pipe, when high-speed flight, to wave amplitude big, butt joint difficulty and a solution of proposing.
The utility model content
The purpose of the utility model provides the active homing formula of a kind of aircraft air refuelling and awards oily device.
The technical scheme that the utility model adopts is:
The active homing formula of aircraft air refuelling is awarded oily device, comprises that bilayer awards oily flexible pipe, and said bilayer is awarded oily flexible pipe inside and is provided with feed cable and control cable; Said bilayer is awarded oily flexible pipe one end connection and is awarded oily aircraft; Said bilayer is awarded the other end connection of oily flexible pipe and is awarded oily tapered sleeve, and said awarding evenly is provided with a plurality of spoilers on the oily tapered sleeve, and said spoiler is connected with transmission device; Said transmission device comprises micro servo motor; Said awarding also is provided with video camera on the oily tapered sleeve, the said oily tapered sleeve center of awarding is provided with and awards oil nozzle, saidly awards oil nozzle and awards oily aircraft and award oil nozzle and be connected cooperation.
The utility model has the advantages that: the control system of closed loop is easy to realize awarding the offset of oily tapered sleeve, realizes homing vector; Through active homing control, reduced the air refuelling docking time, reduced that flight-refueled flight is required difficulty; The employing essential safety is handled, and guarantees air refuelling safety, to reach explosion-proof effect.
Description of drawings
Below in conjunction with the accompanying drawing and the specific embodiment the utility model is described in further detail.
Fig. 1 is the structural representation of the utility model.
Fig. 2 awards the structural representation of oily flexible pipe for the utility model bilayer.
Fig. 3 awards the external structure scheme drawing of oily tapered sleeve for the utility model.
Fig. 4 awards the inner structure scheme drawing of oily tapered sleeve for the utility model.
Wherein: 1, bilayer is awarded oily flexible pipe, and 2, feed cable, 3, control cable, 4, award oily tapered sleeve, 5, spoiler, 6, micro servo motor, 7, award oil nozzle, 8, video camera, 9, award oily aircraft and award oil nozzle, 10, award oily aircraft.
The specific embodiment
Shown in Fig. 1 to 4, the active homing formula of aircraft air refuelling of the utility model is awarded oily device, comprises that bilayer awards oily flexible pipe 1; Said bilayer is awarded oily flexible pipe 1 inside and is provided with feed cable 2 and control cable 3, and said bilayer is awarded oily flexible pipe 1 one ends connection and awarded oily aircraft 10, and said bilayer is awarded the other end connection of oily flexible pipe 1 and awarded oily tapered sleeve 4; Said awarding evenly is provided with four spoilers 5 on the oily tapered sleeve 4; Said spoiler 5 is connected with transmission device, and said transmission device comprises micro servo motor 6, and said awarding on the oily tapered sleeve 4 also is provided with video camera 8; Said oily tapered sleeve 4 centers of awarding are provided with and award oil nozzle 7, saidly award oil nozzle 7 and award oily aircraft and award oil nozzle 9 and be connected cooperation.
Principle of work:
During oiling, award oily aircraft 1 and emit bilayer and award oily flexible pipe 1, bilayer is awarded oily flexible pipe 1 and is aloft waved; Awarding miniature high definition video camera 8 on the oily tapered sleeve 4 catches and awards oily aircraft and award oil nozzle 9 backs through awarding oily aircraft 1 airborne computer software locking; Computer is according to awarding oily tapered sleeve 4 and awarding spoiler 5 angles that oily tapered sleeve 4 is awarded in position deviation control that oily aircraft awards oil nozzle 9, the state of flight that oily tapered sleeve 4 is awarded in adjustment.Because in the high-speed flight process, according to aerodynamic principle, the slight change of spoiler 5 can make awards oily tapered sleeve 4 generations very big skew, so the driving of spoiler 5 can adopt micro servo motor 6 to realize.
Utilization is awarded on the oily tapered sleeve 4 subsidiary high definition video camera 8 and is initiatively caught and award oily aircraft and award oil nozzle 9; Through awarding spoiler 5 angles that oily aircraft 10 airborne computer automatic guidances are awarded oily tapered sleeve 4; Utilize the stable state of flight of awarding oily tapered sleeve 4 of aerodynamic principle, thereby reduce the air refuelling docking time.The control system of closed loop is easy to realize awarding the offset of oily tapered sleeve 4, realizes homing vector; Through active homing control, reduced the air refuelling docking time, reduced that flight-refueled flight is required difficulty; The employing essential safety is handled, and guarantees air refuelling safety, to reach explosion-proof effect.
Claims (1)
1. the active homing formula of aircraft air refuelling is awarded oily device, it is characterized in that: comprise that bilayer awards oily flexible pipe, said bilayer is awarded oily flexible pipe inside and is provided with feed cable and control cable; Said bilayer is awarded oily flexible pipe one end connection and is awarded oily aircraft; Said bilayer is awarded the other end connection of oily flexible pipe and is awarded oily tapered sleeve, and said awarding evenly is provided with a plurality of spoilers on the oily tapered sleeve, and said spoiler is connected with transmission device; Said transmission device comprises micro servo motor; Said awarding also is provided with video camera on the oily tapered sleeve, the said oily tapered sleeve center of awarding is provided with and awards oil nozzle, saidly awards oil nozzle and awards oily aircraft and award oil nozzle and be connected cooperation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202202194U CN202244091U (en) | 2011-06-27 | 2011-06-27 | Active target seeking type oil feeding device for airplane air refueling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202202194U CN202244091U (en) | 2011-06-27 | 2011-06-27 | Active target seeking type oil feeding device for airplane air refueling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202244091U true CN202244091U (en) | 2012-05-30 |
Family
ID=46105376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011202202194U Expired - Fee Related CN202244091U (en) | 2011-06-27 | 2011-06-27 | Active target seeking type oil feeding device for airplane air refueling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202244091U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617428A (en) * | 2013-12-16 | 2014-03-05 | 中国科学院自动化研究所 | Target detection method for aerial refueling drogue based on mixed characteristics |
| CN103995538A (en) * | 2014-05-12 | 2014-08-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Air refueling control method based on image identification |
| CN104354871A (en) * | 2014-11-17 | 2015-02-18 | 河南师范大学 | Plane air refueling auxiliary device |
| CN108996459A (en) * | 2018-07-31 | 2018-12-14 | 中冶华天工程技术有限公司 | The automobile-used flexible centering refueling nozzle mechanism of trolley automatic oiling and refueling nozzle |
| CN109747836A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of unmanned plane space base tail portion cable car type recyclable device and recovery method |
| CN110356574A (en) * | 2018-04-11 | 2019-10-22 | 闵杰 | A kind of device improving hose type in-flight refueling rate |
| CN110901876A (en) * | 2019-10-29 | 2020-03-24 | 北京航空航天大学云南创新研究院 | Air supplement system of stratospheric airship |
| CN117922831A (en) * | 2024-03-25 | 2024-04-26 | 中国空气动力研究与发展中心计算空气动力研究所 | Active control aerial refueling taper sleeve based on flexible control surface and control method |
-
2011
- 2011-06-27 CN CN2011202202194U patent/CN202244091U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617428A (en) * | 2013-12-16 | 2014-03-05 | 中国科学院自动化研究所 | Target detection method for aerial refueling drogue based on mixed characteristics |
| CN103617428B (en) * | 2013-12-16 | 2017-03-01 | 中国科学院自动化研究所 | Drogue object detection method based on composite character |
| CN103995538A (en) * | 2014-05-12 | 2014-08-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Air refueling control method based on image identification |
| CN103995538B (en) * | 2014-05-12 | 2017-01-11 | 中国航空工业集团公司沈阳飞机设计研究所 | Air refueling control method based on image identification |
| CN104354871A (en) * | 2014-11-17 | 2015-02-18 | 河南师范大学 | Plane air refueling auxiliary device |
| CN104354871B (en) * | 2014-11-17 | 2016-06-01 | 河南师范大学 | A kind of aircraft air refuelling supplementary unit |
| CN110356574A (en) * | 2018-04-11 | 2019-10-22 | 闵杰 | A kind of device improving hose type in-flight refueling rate |
| CN108996459A (en) * | 2018-07-31 | 2018-12-14 | 中冶华天工程技术有限公司 | The automobile-used flexible centering refueling nozzle mechanism of trolley automatic oiling and refueling nozzle |
| CN109747836A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of unmanned plane space base tail portion cable car type recyclable device and recovery method |
| CN110901876A (en) * | 2019-10-29 | 2020-03-24 | 北京航空航天大学云南创新研究院 | Air supplement system of stratospheric airship |
| CN117922831A (en) * | 2024-03-25 | 2024-04-26 | 中国空气动力研究与发展中心计算空气动力研究所 | Active control aerial refueling taper sleeve based on flexible control surface and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120530 Termination date: 20120627 |