CN106904283A - The launching apparatus and mode of a kind of aerodone - Google Patents
The launching apparatus and mode of a kind of aerodone Download PDFInfo
- Publication number
- CN106904283A CN106904283A CN201710139354.8A CN201710139354A CN106904283A CN 106904283 A CN106904283 A CN 106904283A CN 201710139354 A CN201710139354 A CN 201710139354A CN 106904283 A CN106904283 A CN 106904283A
- Authority
- CN
- China
- Prior art keywords
- daughter
- aerodone
- parent
- attachment means
- connection end
- 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.)
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Links
- 238000005183 dynamical system Methods 0.000 claims abstract description 8
- 230000005389 magnetism Effects 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Wind Motors (AREA)
- Toys (AREA)
Abstract
The launching apparatus and mode of a kind of aerodone, belong to technical field of aerospace, more particularly to aerodone mode of taking off；Launching apparatus include daughter and parent, and daughter includes aerodone and connection end；Parent includes multi-rotor aerocraft, attachment means, wind transducer and controller；The folding of the electromagnet power supply of controller control attachment means；Attachment means include pillar and electromagnet.When daughter needs to take off, parent and daughter are connected；Parent starts dynamical system, and parent hangs and hauls daughter lift-off, flight forward after lift-off, and after reaching certain pace, controller makes attachment means depart from the connection end of daughter, and daughter and parent are separated, and are smoothly completed aerodone and are taken off.The present invention is combined using multi-rotor aerocraft with aerodone, allows aerodone to be taken off in the little place of area, simplifies the mode of taking off of aerodone, is conducive to the popularization of aerodone.
Description
Technical field
The launching apparatus and mode of a kind of aerodone, belong to technical field of aerospace, more particularly to aerodone launching apparatus
And mode.
Background technology
Aerodone is that a kind of fixed-wing for overweighting air flown not against certification flight or by smaller power navigates
Pocket, air force is relied primarily on after taking off carries out free flight, and an air transport of a mass character has been turned into some countries.
Aerodone requires height to take-off venue, and mode of taking off is also more numerous and diverse.Have using taking off from by the way of eminence run-up, it is also useful
What the mode that winch truck is pullled was taken off, it is necessary to a frame capstan winch is placed in the place immediately ahead of aerodone farther out during using winch truck
Car, the two ends of a steel cable are separately fixed on winch truck and aerodone, when aerodone will take off, are closed a floodgate and are powered, and make strand
Jiggering quickly rotates, and hawser is rolled, and shorter and shorter, drives aerodone to go at express speed on the ground, this time-consuming consumption of mode of taking off
Power.
The content of the invention
The purpose of the present invention is the above-mentioned deficiency for overcoming traditional aerodone launching apparatus and mode, and the present invention is using many rotations
Rotor aircraft advantage, makes multi-rotor aerocraft be combined with aerodone, is the one aerial runway of manufacture that takes off of aerodone.
A kind of mode of taking off of aerodone, is realized by following launching apparatus, and the launching apparatus include daughter and mother
Body, the daughter includes aerodone and connection end；Connection end is located at aerodone top, and is crossing the plumb line of aerodone center of gravity
On；Parent includes multi-rotor aerocraft, attachment means and controller；The multi-rotor aerocraft includes dynamical system, control system
System, bracing strut, halfpace；The attachment means are located at the halfpace lower section of multi-rotor aerocraft, and attachment means include branch
Post and electromagnet, pillar one end are vertically connected on halfpace lower section, and the other end is connected to electromagnet, electromagnet and controller phase
Even.The controller is located in the halfpace of multi-rotor aerocraft, and the effect of controller is the electromagnet for controlling attachment means
The folding of power supply.When daughter needs to take off, the attachment means of parent are corresponding with the connection end of daughter, controller is opened and connected
The power supply of connection device, attachment means produce magnetic attraction connection end, make parent and daughter connection combination；Parent starts dynamical system
System, parent hangs and hauls daughter lift-off, and after reaching a certain height, parent hangs and hauls daughter acceleration flight forward, before reaching necessarily
After entering speed, controller closes the power supply of attachment means, and the electromagnet of attachment means to lose magnetism and take off the connection end with daughter
From daughter and parent are separated, and daughter continues to fly, and parent is returned, and is smoothly completed aerodone and is taken off.
The aerodone is power glider or unpowered aerodone.
Preferably, the parent also includes wind transducer, and wind transducer is located on halfpace and and control system
It is connected, for detecting the direction of wind, the direction of taking off of aerodone is determined to adjust parent heading.
Preferably, the multi-rotor aerocraft uses four-axle aircraft.
The present invention can be taken off vertically and flexible advantage using multi-rotor aerocraft, using multi-rotor aerocraft with
Aerodone combine, be aerodone take off manufacture one aerial runway, aerodone can also be taken off in the little place of area, simplification
The mode of taking off of aerodone, is conducive to the popularization of aerodone.
Brief description of the drawings
Fig. 1 is daughter structure schematic top plan view；Fig. 2 is daughter and parent connection combination diagram.
In figure, 1- daughters, 2- aerodones, 3- connection ends, 4- parents, 5- four-axle aircrafts, 6- attachment means, 7- pillars,
8- electromagnet, 9- wind transducers, 10- controllers.
Specific embodiment
The present invention is illustrated below in conjunction with the accompanying drawings：A kind of mode of taking off of aerodone, is by the following dress that takes off
Realization is put, the launching apparatus include daughter 1 and parent 4, daughter 1 includes aerodone 2 and connection end 3；Aerodone 2 is using without dynamic
Power aerodone.Connection end 3 is located at the top of aerodone 2, and on the plumb line for crossing the center of gravity of aerodone 2；Parent 4 flies including four axles
Device 5, attachment means 6, wind transducer 9 and controller 10；Four-axle aircraft 5 include dynamical system, control system, bracing strut,
Halfpace；Attachment means 6 are located at the halfpace lower section of four-axle aircraft 5, and attachment means 6 include pillar 7 and electromagnet 8,
The one end of pillar 7 is vertically connected on halfpace lower section, and the other end is connected to electromagnet 8, and electromagnet 8 is connected with controller 10.Wind
It is located on halfpace to sensor 9 and is connected with control system, for detecting the direction of wind, adjusts the heading of parent 4
To determine the direction of taking off of aerodone 2.Controller 10 is located in the halfpace of four-axle aircraft 5, and the effect of controller 10 is
Control the folding of the power supply of electromagnet 8 of attachment means 6.When daughter 1 needs to take off, by the attachment means 6 of parent 4 and daughter 1
Connection end 3 it is corresponding, controller 10 opens the power supply of attachment means 6, and attachment means 6 produce magnetic attraction connection end 3, make mother
Body 4 and the connection combination of daughter 1；Parent 4 starts dynamical system, and parent 4 hangs and hauls daughter 1 and go up to the air, while wind transducer 9 is detected
The direction of wind, the direction of taking off of daughter 1 is adjusted with this；After reaching a certain height, parent 4 hangs and hauls daughter 1 and accelerate windward
Flight forward, after reaching the takeoff speed of aerodone 2, controller 10 closes the power supply of attachment means 6, the electromagnetism of attachment means 6
Iron 8 to be lost magnetism and depart from the connection end 3 with daughter 1, and daughter 1 and parent 4 are separated, and daughter 1 continues to fly, and parent 4 is returned, suitable
Profit completes aerodone 2 and takes off.
Claims (7)
1. a kind of launching apparatus of aerodone, it is characterised in that：Including daughter（1）And parent（4）, the daughter（1）Including cunning
Xiang machine（2）And connection end（3）；Connection end（3）Positioned at aerodone（2）Top；Parent（4）Including multi-rotor aerocraft, connection dress
Put（6）And controller（10）；The multi-rotor aerocraft includes dynamical system, control system, bracing strut, halfpace；It is described
Attachment means（6）Positioned at the halfpace lower section of multi-rotor aerocraft, attachment means（6）Including pillar（7）And electromagnet（8）,
Pillar（7）One end is vertically connected on halfpace lower section, and the other end is connected to electromagnet（8）, electromagnet（8）With controller（10）
It is connected；Controller（10）Effect be control attachment means（6）Electromagnet（8）The folding of power supply.
2. launching apparatus of a kind of aerodone according to claim 1, it is characterised in that：Connection end（3）Crossing aerodone
（2）On the plumb line of center of gravity.
3. launching apparatus of a kind of aerodone according to claim 1, it is characterised in that：Aerodone（2）It is power flide
Machine or unpowered aerodone.
4. launching apparatus of a kind of aerodone according to claim 1, it is characterised in that：The multi-rotor aerocraft is four
Axle aircraft（5）.
5. launching apparatus of a kind of aerodone according to claim 1,2 or 4, it is characterised in that：Parent（4）Also include wind
To sensor（9）, wind transducer（9）It is connected on halfpace and with control system.
6. the mode of taking off of a kind of aerodone, it is characterised in that：It is by any aerodone described in claim 1 ~ 4
Launching apparatus work as daughter come what is realized（1）When needing to take off, by parent（4）Attachment means（6）With daughter（1）Connection end
（3）It is corresponding, controller（10）Open attachment means（6）Power supply, attachment means（6）Produce magnetic attraction connection end（3）, make
Parent（4）And daughter（1）Connection combination；Parent（4）Start dynamical system, parent（4）Hang and haul daughter（1）Lift-off, when reaching
After certain altitude, parent（4）Hang and haul daughter（1）Accelerate flight forward, after reaching certain speed, controller（10）Close connection
Device（6）Power supply, attachment means（6）Electromagnet（8）Losing magnetism will be with daughter（1）Connection end（3）Depart from, daughter
（1）And parent（4）Separate, daughter（1）Continue to fly, parent（4）Return.
7. the mode of taking off of a kind of aerodone, it is characterised in that：It is rising by any aerodone described in claim 5
Winged device works as daughter come what is realized（1）When needing to take off, by parent（4）Attachment means（6）With daughter（1）Connection end（3）
It is corresponding, controller（10）Open attachment means（6）Power supply, attachment means（6）Produce magnetic attraction connection end（3）, make mother
Body（4）And daughter（1）Connection combination；Parent（4）Start dynamical system, parent（4）Hang and haul daughter（1）Lift-off, while wind direction
Sensor（9）The direction of wind is detected, daughter is adjusted with this（1）Direction of taking off；It is female after launching apparatus reach a certain height
Body（4）Hang and haul daughter（1）Accelerate flight forward windward, after reaching certain pace, controller（10）Close attachment means
（6）Power supply, attachment means（6）Electromagnet（8）Losing magnetism will be with daughter（1）Connection end（3）Depart from, daughter（1）With
Parent（4）Separate, daughter（1）Continue to fly, parent（4）Return.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139354.8A CN106904283A (en) | 2017-03-10 | 2017-03-10 | The launching apparatus and mode of a kind of aerodone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139354.8A CN106904283A (en) | 2017-03-10 | 2017-03-10 | The launching apparatus and mode of a kind of aerodone |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106904283A true CN106904283A (en) | 2017-06-30 |
Family
ID=59187776
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139354.8A Withdrawn CN106904283A (en) | 2017-03-10 | 2017-03-10 | The launching apparatus and mode of a kind of aerodone |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106904283A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552635A (en) * | 2018-12-20 | 2019-04-02 | 中国航空工业集团公司西安飞机设计研究所 | A kind of airborne electromagnetic formula unmanned plane recovery method and recyclable device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4267987A (en) * | 1979-03-29 | 1981-05-19 | Mcdonnell William R | Helicopter airborne load systems and composite aircraft configurations |
| CN102183962A (en) * | 2011-03-11 | 2011-09-14 | 中国气象局气象探测中心 | Unmanned aerial vehicle (UAV) dropsonde and method for releasing and controlling same |
| CN105799928A (en) * | 2016-04-14 | 2016-07-27 | 安徽汇金智能科技有限公司 | Fire protection and extinguishing device based on unmanned aerial vehicle |
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
-
2017
- 2017-03-10 CN CN201710139354.8A patent/CN106904283A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4267987A (en) * | 1979-03-29 | 1981-05-19 | Mcdonnell William R | Helicopter airborne load systems and composite aircraft configurations |
| CN102183962A (en) * | 2011-03-11 | 2011-09-14 | 中国气象局气象探测中心 | Unmanned aerial vehicle (UAV) dropsonde and method for releasing and controlling same |
| CN105799928A (en) * | 2016-04-14 | 2016-07-27 | 安徽汇金智能科技有限公司 | Fire protection and extinguishing device based on unmanned aerial vehicle |
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552635A (en) * | 2018-12-20 | 2019-04-02 | 中国航空工业集团公司西安飞机设计研究所 | A kind of airborne electromagnetic formula unmanned plane recovery method and recyclable device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170630 |
|
| WW01 | Invention patent application withdrawn after publication |