CN104691771A - Fuel giving machine active search type aerial refueling auxiliary device for aircrafts - Google Patents
Fuel giving machine active search type aerial refueling auxiliary device for aircrafts Download PDFInfo
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- CN104691771A CN104691771A CN201510123755.5A CN201510123755A CN104691771A CN 104691771 A CN104691771 A CN 104691771A CN 201510123755 A CN201510123755 A CN 201510123755A CN 104691771 A CN104691771 A CN 104691771A
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- electric pushrod
- oil machine
- taper shank
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Abstract
The invention discloses a fuel giving machine active search type aerial refueling auxiliary device for aircrafts. The fuel giving machine active search type aerial refueling auxiliary device comprises a double-layer fuel giving hose, a fuel giving machine taper sleeve, a triangular turbulence device, a camera device, a control desk and a circuit control module. The double-layer fuel giving hose comprises an outer-layer protective sleeve and an inner-layer fuel delivery pipe, the fuel giving machine taper sleeve comprises a taper shank and an umbrella sleeve which are fixedly connected with each other, the camera device is arranged on the taper shank on the inner side of the umbrella sleeve, an axial fuel giving hole is formed in the middle of the taper shank, the outer-layer protective sleeve is connected with an outer ring of the taper shank, the inner-layer fuel delivery pipe is connected with the fuel giving hole in the middle of the taper shank, and electric flexible flat cables are arranged between the outer-layer protective sleeve and the inner-layer fuel delivery pipe and are connected with the camera device on the taper shank and electric push rods in the triangular turbulence device. The fuel giving machine active search type aerial refueling auxiliary device has the advantages that the fuel giving machine active search type aerial refueling auxiliary device is controlled by fuel giving machine operators in an active search mode, accordingly, the aerial refueling butting time can be shortened, and aerial refueling flight requirement difficulty can be lowered.
Description
Technical field
The invention belongs to Aircraft Air refuel technical field, be specifically related to one award oil machine master seek formula Aircraft Air refuel auxiliary device.
Background technology
In prior art, when Aircraft Air refuels, awarding oil machine releases outside machine by flexible pipe, oil machine tapered sleeve is awarded to be put into by fuel filler pipe in the position that the aviator of refueled aircraft adjusts refueled aircraft, because refueled aircraft and the velocity contrast and diff-H awarding oil machine have serious regulation, therefore the control action of receiver pilot must be very accurately stable, and this skill set requirements for receiver pilot is high, operates and also has very large difficulty.In addition, due to award oil machine tapered sleeve aloft air-flow impact under very unstable, some are mainly sought to formula Aircraft Air to refuel auxiliary device adjustment stability of getting up not ideal enough.
Summary of the invention
The technical matters that the present invention solves there is provided a kind of easy to use and simple to operate oil machine master that awards and seeks formula Aircraft Air oiling auxiliary device, this auxiliary device is controlled by the operating personal awarding oil machine and regulates the direction of awarding oil machine tapered sleeve, and then complete air refuelling process, refueled aircraft fuel filler pipe with award in the docking operation of oil machine tapered sleeve, triangle spoiler is made to produce an angle relative to horizontal direction by regulating the relative position of three electric pushrods, be referred to as the angle of attack, change the size of the triangle spoiler angle of attack, according to the parallelogram law of vector calculus, change and award the stressed of oil machine tapered sleeve thus adjust the position of awarding oil machine tapered sleeve, complete and award docking of oil machine tapered sleeve and refueled aircraft fuel filler pipe.According to actual conditions, by controlling the lifting of three electric pushrods, changing the size of the angle of attack thus realizing awarding the adjustment in oil machine tapered sleeve direction up and down.
The present invention adopts following technical scheme for solving the problems of the technologies described above, one is awarded oil machine master and is sought formula Aircraft Air oiling auxiliary device, it is characterized in that comprising bilayer awards oily flexible pipe, award oil machine tapered sleeve, triangle disturbing flow device, cam device, control desk and circuit control module, wherein bilayer is awarded oily flexible pipe and is made up of outer layer protective sleeve and internal layer transport pipe, award oil machine tapered sleeve to be made up of the taper shank umbrella cover that is connected, taper shank inside umbrella cover is provided with cam device, the middle part of this taper shank is provided with axially awards oilhole, outer layer protective sleeve is connected with taper shank outer shroud, internal layer transport pipe is connected with the oilhole of awarding in the middle part of taper shank, cable arrange-line is provided with between outer layer protective sleeve and internal layer transport pipe, wherein cable arrange-line is connected with the electric pushrod in triangle disturbing flow device with the cam device be arranged on taper shank, the electric pushrod that described triangle disturbing flow device comprises triangle spoiler and objective table and is arranged between triangle spoiler and objective table, wherein the upper end of electric pushrod is articulated with three angles place of triangle spoiler by coupler, the bottom of electric pushrod is connected with objective table, the motor of electric pushrod is arranged at the inside of objective table respectively, this objective table be nested in award oil machine tapered sleeve taper shank on, described control desk is provided with telltale, master cock, control button and the circuit control module being arranged at control desk inside, circuit control module is primarily of power circuit block, circuit control module, electric pushrod control module and display circuit module are formed, power circuit block comprises power supply and power supply adaptor, power supply is connected with power supply adaptor, power supply adaptor respectively with circuit control module, electric pushrod control module is connected with display circuit module, circuit control module comprises control button, control button circuit, micro controller system and SCM peripheral circuit, control button is connected with control button circuit, control button circuit is connected with micro controller system, micro controller system is connected with the cam device circuit in display circuit module with the electric pushrod control circuit in electric pushrod control module respectively, electric pushrod control module comprises electric pushrod control circuit and electric pushrod, electric pushrod is connected with electric pushrod control circuit, display circuit module comprises cam device, cam device circuit, display circuit and telltale, cam device is connected with cam device circuit, cam device circuit is connected with display circuit, display circuit is connected with telltale.
Work process of the present invention is: in whole air refuelling process, when awarding oil machine tapered sleeve and docking with refueled aircraft fuel filler pipe, award oil machine and refueled aircraft keeps geo-stationary, awarded the position of oil machine tapered sleeve according to the real-time video adjustment being arranged on the high-definition camera head unit awarded on oil machine tapered sleeve and transferring back to telltale by the operating personal awarding oil machine, regulate the electric pushrod be arranged on objective table to stretch to change the stressed of triangle spoiler by pressing corresponding control button on control desk, the drive of triangle spoiler is awarded oil machine tapered sleeve and is moved, until again reach stress balance, realize refueled aircraft fuel filler pipe and award docking of oil machine tapered sleeve, complete Aircraft Air to refuel, after oiling terminates, award oil machine tapered sleeve and refueled aircraft fuel filler pipe departs from, oil machine tapered sleeve is awarded in withdrawal.
The present invention compared with prior art has following beneficial effect: (1) awards the position of oil machine tapered sleeve by awarding the control of oil machine operating personal, by the size regulating the relative position of electric pushrod to change the triangle spoiler angle of attack, and then change is awarded the stressed of oil machine tapered sleeve thus adjusts the position of awarding oil machine tapered sleeve, realize the skew of awarding oil machine tapered sleeve position, compared to the convenient safety in position of the operating personal adjustment aircraft of refueled aircraft; (2) controlling by awarding oil machine operating personal master formula of seeking, decreasing flight-refueled docking time, reducing and difficulty is required to flight-refueled flight.
Accompanying drawing explanation
Fig. 1 is oil pipeline connection structure schematic diagram in the present invention, Fig. 2 is the structural representation of taper shank in the present invention, Fig. 3 is the structural representation of control desk in the present invention, Fig. 4 is the structural representation of intermediate cam spoiler of the present invention and electric pushrod junction, and Fig. 5 is the circuit connection diagram of circuit control module in the present invention.
Drawing illustrates: 1, bilayer awards oily flexible pipe, 2, award oil machine tapered sleeve, 3, triangle disturbing flow device; 4, cam device, 5, control desk, 6, outer layer protective sleeve; 7, internal layer transport pipe, 8, taper shank, 9, umbrella cover; 10, oilhole is awarded, 11, electric pushrod, 12, triangle spoiler; 13, objective table, 14, coupler, 15, telltale; 16, master cock, 17, control button.
Detailed description of the invention
Describe particular content of the present invention by reference to the accompanying drawings in detail.One is awarded oil machine master and is sought formula Aircraft Air oiling auxiliary device, comprise bilayer and award oily flexible pipe 1, award oil machine tapered sleeve 2, triangle disturbing flow device 3, cam device 4, control desk 5 and circuit control module, wherein bilayer is awarded oily flexible pipe 1 and is made up of outer layer protective sleeve 6 and internal layer transport pipe 7, award oil machine tapered sleeve 2 to be made up of taper shank 8 umbrella cover 9 that is connected, taper shank 8 inside umbrella cover 9 is provided with cam device 4, the middle part of this taper shank 8 is provided with axially awards oilhole 10, described outer layer protective sleeve 6 is connected with taper shank 8 outer shroud, internal layer transport pipe 7 is connected with the oilhole 10 of awarding in the middle part of taper shank 8, cable arrange-line is provided with between outer layer protective sleeve 6 and internal layer transport pipe 7, wherein cable arrange-line is connected with the electric pushrod 11 in triangle disturbing flow device 3 with the cam device 4 be arranged on taper shank 8, the electric pushrod 11 that described triangle disturbing flow device 3 comprises triangle spoiler 12 and objective table 13 and is arranged between triangle spoiler 12 and objective table 13, wherein the upper end of electric pushrod 11 is articulated with three angles place of triangle spoiler 12 by coupler 14, the bottom of electric pushrod 11 is connected with objective table 13, the motor of electric pushrod 11 is arranged at the inside of objective table 13 respectively, this objective table 13 is nested in be awarded on the taper shank 8 of oil machine tapered sleeve 2, described control desk 5 is provided with telltale 15, master cock 16, control button 17 and the circuit control module being arranged at control desk 5 inside, circuit control module is primarily of power circuit block, circuit control module, electric pushrod control module and display circuit module are formed, power circuit block comprises power supply and power supply adaptor, power supply is connected with power supply adaptor, power supply adaptor respectively with circuit control module, electric pushrod control module is connected with display circuit module, circuit control module comprises control button, control button circuit, micro controller system and SCM peripheral circuit, control button is connected with control button circuit, control button circuit is connected with micro controller system, micro controller system is connected with the cam device circuit in display circuit module with the electric pushrod control circuit in electric pushrod control module respectively, electric pushrod control module comprises electric pushrod control circuit and electric pushrod, electric pushrod is connected with electric pushrod control circuit, display circuit module comprises cam device, cam device circuit, display circuit and telltale, cam device is connected with cam device circuit, cam device circuit is connected with display circuit, display circuit is connected with telltale.
Power circuit block: power circuit block comprises power supply and power supply adaptor, aircraft is furnished with low pressure stabilized current supply, low pressure stabilized current supply is transformed into the power supply of 5V and 24V after power supply adaptor, the voltage of 5V is powered to circuit control module and display circuit module, and the voltage of 24V is powered to electric pushrod control module.
Circuit control module: be provided with three groups of control buttons and a telltale on control desk, often organize in control button and have two control keys, control key can select the film button switch of 4mm*4mm*0.8mm, press energising, loose one's grip power-off, I/O mouths different from micro controller system is respectively connected, and each control key has two feelers, a feeler is connected with micro controller system, other end ground connection.When control key is not pressed, single-chip processor i/o mouth is high level, I/O mouth corresponding when pressing becomes low level, micro controller system is according to the low and high level signal control electric pushrod control circuit of control button, elongation and the shortening of electric pushrod is driven by electric pushrod control circuit, thus change the stressed of triangle spoiler, realize the change in location of awarding oil machine tapered sleeve.Often organize control button corresponding control electric pushrod, when operating personal is by corresponding control button next time, will issue micro controller system signal impulse, micro controller system will send a signal to electric pushrod control circuit, and electric pushrod control circuit drives electric pushrod.Micro controller system can choose the micro controller system of 51 series, and the program of micro controller system can write realization by assembly language or C language.SCM peripheral circuit is that external crystal and electric capacity are formed, and the optional frequency of crystal oscillator is taken as 12MHz.
Triangle disturbing flow device is by three electric pushrods, a triangle spoiler and an objective table composition, electric pushrod is articulated with three angles place of triangle spoiler by coupler, electric pushrod is connected with objective table, objective table be nested in award oil machine tapered sleeve taper shank on, electric pushrod is chosen for operating voltage and is chosen for 24V, maximum load is within the scope of 50-60kg, the DTZ push rod of installation dimension in the scope of 30-50cm, DTZ push rod uses POM material in miniature electromotive handspike, noise is little, weigh large, wherein the motor of DTZ and expansion link direction are vertical configuration, adopt the installation method of turbine and worm drive mechanism.The alloy of high temperature high voltage resistant all chosen by the material of triangle spoiler and objective table, and the equicrural triangle that triangle spoiler is about 50cm by waist length is formed.
Cam device chooses small-sized high-definition camera, the operating voltage of camera is direct current 5V, press the arbitrary control button of control desk, can open camera by micro controller system through cam device circuit, camera can be passed through video data above the band cross scale telltale that RCA video line is sent to control desk in real time.Taper shank front end, then by inlay, taper shank is suited mutually with taper shank front end arc, in order to avoid make troubles when refueling.
More than show and describe groundwork of the present invention, principal character and advantage, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these changes and improvements all fall into claimed scope of the present invention.
Claims (2)
1. one kind award oil machine master seek formula Aircraft Air refuel auxiliary device, it is characterized in that comprising bilayer awards oily flexible pipe, award oil machine tapered sleeve, triangle disturbing flow device, cam device, control desk and circuit control module, wherein bilayer is awarded oily flexible pipe and is made up of outer layer protective sleeve and internal layer transport pipe, award oil machine tapered sleeve to be made up of the taper shank umbrella cover that is connected, taper shank inside umbrella cover is provided with cam device, the middle part of this taper shank is provided with axially awards oilhole, outer layer protective sleeve is connected with taper shank outer shroud, internal layer transport pipe is connected with the oilhole of awarding in the middle part of taper shank, cable arrange-line is provided with between outer layer protective sleeve and internal layer transport pipe, wherein cable arrange-line is connected with the electric pushrod in triangle disturbing flow device with the cam device be arranged on taper shank, the electric pushrod that described triangle disturbing flow device comprises triangle spoiler and objective table and is arranged between triangle spoiler and objective table, wherein the upper end of electric pushrod is articulated with three angles place of triangle spoiler by coupler, the bottom of electric pushrod is connected with objective table, the motor of electric pushrod is arranged at the inside of objective table respectively, this objective table be nested in award oil machine tapered sleeve taper shank on, described control desk is provided with telltale, master cock, control button and the circuit control module being arranged at control desk inside, circuit control module is primarily of power circuit block, circuit control module, electric pushrod control module and display circuit module are formed, power circuit block comprises power supply and power supply adaptor, power supply is connected with power supply adaptor, power supply adaptor respectively with circuit control module, electric pushrod control module is connected with display circuit module, circuit control module comprises control button, control button circuit, micro controller system and SCM peripheral circuit, control button is connected with control button circuit, control button circuit is connected with micro controller system, micro controller system is connected with the cam device circuit in display circuit module with the electric pushrod control circuit in electric pushrod control module respectively, electric pushrod control module comprises electric pushrod control circuit and electric pushrod, electric pushrod is connected with electric pushrod control circuit, display circuit module comprises cam device, cam device circuit, display circuit and telltale, cam device is connected with cam device circuit, cam device circuit is connected with display circuit, display circuit is connected with telltale.
2. according to claim 1 award oil machine master seek formula Aircraft Air refuel auxiliary device, it is characterized in that: in whole air refuelling process, when awarding oil machine tapered sleeve and docking with refueled aircraft fuel filler pipe, award oil machine and refueled aircraft keeps geo-stationary, awarded the position of oil machine tapered sleeve according to the real-time video adjustment being arranged on the high-definition camera head unit awarded on oil machine tapered sleeve and transferring back to telltale by the operating personal awarding oil machine, regulate the electric pushrod be arranged on objective table to stretch to change the stressed of triangle spoiler by pressing corresponding control button on control desk, the drive of triangle spoiler is awarded oil machine tapered sleeve and is moved, until again reach stress balance, realize refueled aircraft fuel filler pipe and award docking of oil machine tapered sleeve, complete Aircraft Air to refuel, after oiling terminates, award oil machine tapered sleeve and refueled aircraft fuel filler pipe departs from, oil machine tapered sleeve is awarded in withdrawal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510123755.5A CN104691771A (en) | 2015-03-20 | 2015-03-20 | Fuel giving machine active search type aerial refueling auxiliary device for aircrafts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510123755.5A CN104691771A (en) | 2015-03-20 | 2015-03-20 | Fuel giving machine active search type aerial refueling auxiliary device for aircrafts |
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| Publication Number | Publication Date |
|---|---|
| CN104691771A true CN104691771A (en) | 2015-06-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510123755.5A Pending CN104691771A (en) | 2015-03-20 | 2015-03-20 | Fuel giving machine active search type aerial refueling auxiliary device for aircrafts |
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| CN (1) | CN104691771A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552649A (en) * | 2017-09-26 | 2019-04-02 | 波音公司 | Telescopic oiling arm control system and method |
| CN110304262A (en) * | 2019-06-21 | 2019-10-08 | 西北工业大学 | A kind of autonomous motor-driven tapered sleeve and control method of unmanned plane air refuelling |
| CN111216907A (en) * | 2020-01-15 | 2020-06-02 | 西北工业大学 | Autonomous mobile taper sleeve for soft air refueling |
| CN112660398A (en) * | 2020-12-29 | 2021-04-16 | 中国航空工业集团公司西安飞机设计研究所 | Device for soft type air active refueling butt joint |
| CN113002786A (en) * | 2021-04-02 | 2021-06-22 | 哈尔滨工业大学 | Air refueling hose with carbon fiber pipe sleeved outside |
| 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 |
Citations (3)
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| US20060065785A1 (en) * | 2002-08-23 | 2006-03-30 | Enig Eric N | Hose-and-drogue in-flight refueling system |
| CN204210738U (en) * | 2014-11-17 | 2015-03-18 | 河南师范大学 | A kind of Aircraft Air oiling auxiliary device |
| CN204473150U (en) * | 2015-03-20 | 2015-07-15 | 河南师范大学 | One is awarded oil machine master and is sought formula Aircraft Air oiling auxiliary device |
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2015
- 2015-03-20 CN CN201510123755.5A patent/CN104691771A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060065785A1 (en) * | 2002-08-23 | 2006-03-30 | Enig Eric N | Hose-and-drogue in-flight refueling system |
| CN204210738U (en) * | 2014-11-17 | 2015-03-18 | 河南师范大学 | A kind of Aircraft Air oiling auxiliary device |
| CN204473150U (en) * | 2015-03-20 | 2015-07-15 | 河南师范大学 | One is awarded oil machine master and is sought formula Aircraft Air oiling auxiliary device |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552649A (en) * | 2017-09-26 | 2019-04-02 | 波音公司 | Telescopic oiling arm control system and method |
| CN109552649B (en) * | 2017-09-26 | 2022-11-29 | 波音公司 | Telescopic refueling arm control system and method |
| CN110304262A (en) * | 2019-06-21 | 2019-10-08 | 西北工业大学 | A kind of autonomous motor-driven tapered sleeve and control method of unmanned plane air refuelling |
| CN111216907A (en) * | 2020-01-15 | 2020-06-02 | 西北工业大学 | Autonomous mobile taper sleeve for soft air refueling |
| CN112660398A (en) * | 2020-12-29 | 2021-04-16 | 中国航空工业集团公司西安飞机设计研究所 | Device for soft type air active refueling butt joint |
| CN113002786A (en) * | 2021-04-02 | 2021-06-22 | 哈尔滨工业大学 | Air refueling hose with carbon fiber pipe sleeved outside |
| 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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Application publication date: 20150610 |
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