CN106915442A - A kind of air rescue device and mode - Google Patents
A kind of air rescue device and mode Download PDFInfo
- Publication number
- CN106915442A CN106915442A CN201710139331.7A CN201710139331A CN106915442A CN 106915442 A CN106915442 A CN 106915442A CN 201710139331 A CN201710139331 A CN 201710139331A CN 106915442 A CN106915442 A CN 106915442A
- Authority
- CN
- China
- Prior art keywords
- wing aircraft
- fixed wing
- fixed
- plain stage
- succor plain
- 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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- 210000001015 abdomen Anatomy 0.000 claims abstract description 12
- 230000001771 impaired effect Effects 0.000 claims abstract description 4
- 238000001514 detection method Methods 0.000 claims description 6
- 230000009429 distress Effects 0.000 claims description 4
- 238000003032 molecular docking Methods 0.000 claims description 3
- 238000007689 inspection Methods 0.000 claims 1
- 230000005611 electricity Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000010338 mechanical breakdown Methods 0.000 description 1
Classifications
-
- 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
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The air rescue device and its mode of a kind of air rescue device and its mode, category vehicle technology field, more particularly to aircraft.The device includes that a Succor plain stage, controller, level detecting apparatus, support, motor, propeller, left fixed mount, platform rotating shaft and machine shaft are constituted.Air rescue mode：When fixed wing aircraft because engine failure or wing because bird collisions is impaired cannot normal flight or during landing, multi-rotor aerocraft carries Succor plain stage and flies to the belly of failure fixed wing aircraft, and Succor plain stage is fixed on the belly of fixed wing aircraft by fixed mount.A kind of undercarriage that can be flown of the present invention passes through air rescue device, complete to realize automatic butt with the fixed wing aircraft of failure in the air, can solve the problem that because engine failure is unable to normal flight and wing failure problems, implement emergency relief in the air, for fixed wing aircraft provides interim power, guiding fixed wing aircraft realizes forced landing.
Description
Technical field
A kind of air rescue device of air rescue device and mode, category vehicle technology field, more particularly to aircraft and
Mode.
Background technology
When aircraft engine runs in the air, if there is pilot operator error, mechanical breakdown, electronic system malfunction,
The problems such as bird strike, engine stop can be caused to work, this is referred to as " flame-out in flight " on aviation field, works as fixation
Wing aircraft engine failure, loses flying power even crash out of control, can cause fatal crass.Commercial aircraft is dynamic equipped with auxiliary
Power unit（APU）, generally in afterbody.If engine engine breaks down, APU can provide electric power and compressed air for aircraft,
Also having a small amount of APU can provide additional thrust to aircraft.In the dual misfire event that can not possibly extremely occur, can generally protect
Aircraft balanced is held, until landing in an emergency.Also aircraft belly built with " ram air turbine（RAT）" draw when aircraft
When holding up failure, this turbine can decline and from as a kind of airborne wind mill equipment from belly, aircraft below by sky
The energy that aerodynamic force is produced provides emergence power and emergent hydraulic pressure, but these deliverance apparatus complex structures for aircraft, and volume is larger,
Cannot be used on small-sized fixed wing aircraft.
The content of the invention
The purpose of the present invention is run out of steam and the flight of wing failure and landing to solve fixed wing aircraft engine failure
Problem, invents a kind of air rescue device and its mode, by a multi-rotor aerocraft carry Succor plain stage be raised in the air, with
Fixed wing aircraft and be arranged on failure fixed wing aircraft bottom, as interim power, fixed wing aircraft is can continue to forward
Flight and uneventful landing.
A kind of air rescue mode, is realized by following device, and the deliverance apparatus include a Succor plain stage, control
Device processed, prelocalization detection means, rear locating and detecting device, support, motor, propeller, left fixed mount, right fixed mount, platform turn
Axle and machine shaft, air rescue device is constituted by combining, and is docked with Fixed Wing AirVehicle, carries out air rescue.Institute
State Succor plain stage middle part and controller is installed, it is right for controlling whole air rescue device flight and Fixed Wing AirVehicle to carry out
Connect, locating and detecting device has been respectively mounted before and after the Succor plain stage top, the position for detecting fixed wing aircraft, guiding is empty
Middle deliverance apparatus fly to the fixed wing aircraft lower section of failure, and positioning action when playing docking；Four angles of the Succor plain stage
Four supports are connected to by four platformses rotating shaft, four ends of support are connected by machine shaft with four motors, four
Propeller is assembled with motor；Controller can be turned an angle with control platform rotating shaft and machine shaft, and then adjust empty
Middle deliverance apparatus flight attitude；The both sides of the Succor plain stage are provided with left fixed mount and right fixed mount, are flown with fixed-wing
Stretched out after device docking, Succor plain stage is fixed under the belly of fixed wing aircraft.A kind of air rescue mode：It is by one
Multi-rotor aerocraft carries Succor plain stage is sued and laboured, when fixed wing aircraft because of engine failure or wing because bird collisions is impaired
Cannot normal flight or landing when, earthward airport boat station send an SOS, airport boat station be connected to distress signal after, at once send
It has multi-rotor aerocraft and carries the lower section that Succor plain stage flies to failure fixed wing aircraft, controller is received by locating and detecting device
The information for arriving, guiding Succor plain stage is consolidated Succor plain stage by left fixed mount and right fixed mount near the belly of fixed wing aircraft
It is scheduled on the belly of fixed wing aircraft.After the completion of the Succor plain stage is docked with fixed wing aircraft, four supports are by flat
Platform rotating shaft is made horizontal direction and is rotated around Succor plain stage, and, four motors pass through with two wings of fixed wing aircraft horizontally
Machine shaft rotates around support, makes motor and propeller identical with fixed wing aircraft heading holding, now four motors and
Propeller can allow fixed wing aircraft to continue to neighbouring aerodrome flight as temporary flight power；When the wing of fixed wing aircraft is received
When damage is in stays or slides in the air, controller can control to be arranged on four supports of Succor plain stage and four motors are rotated
To adjust the flight attitude of fixed wing aircraft, the balance and certain flying speed of whole fuselage are kept, it is to avoid aircraft is because of stall
And crash, then switch to vertical landing state so that the fixed wing aircraft of failure can in a short time forced landing on ground
On face.
The support can make horizontal direction and rotate around Succor plain stage.
The motor can rotate around machine shaft.
A kind of undercarriage that can be flown of the present invention completes the fixed wing aircraft with failure in the air by air rescue device
Automatic butt is realized, be can solve the problem that because engine failure is unable to normal flight and wing failure problems, implement promptly to rescue in the air
Help, for fixed wing aircraft provides interim power, guiding fixed wing aircraft realizes forced landing.
Brief description of the drawings
Fig. 1 is the schematic diagram of fixed wing aircraft and air rescue device combination flight forward；Fig. 2 is fixed wing aircraft and sky
The schematic diagram of middle deliverance apparatus combination flight attitude adjustment；Fig. 3 is the structural representation of air rescue device.
In figure, 1- Succor plain stages, 2- controllers, 31- prelocalization detection means, locating and detecting device after 32-, 4- supports,
5- motors, 6- propellers, the left fixed mounts of 71-, the right fixed mounts of 72-, 8- platform rotating shafts, 9- machine shafts, 10- fixed wing aircrafts.
Specific embodiment
The present invention is illustrated in conjunction with accompanying drawing：A kind of air rescue device, including a Succor plain stage 1, control
Device processed 2, prelocalization detection means 31, rear locating and detecting device 32, support 4, motor 5, propeller 6, left fixed mount 71, right fixation
Frame 72, platform rotating shaft 8 and machine shaft 9 are constituted, and air rescue device is constituted by combining, and it is right to be carried out with fixed wing aircraft 10
Connect, carry out air rescue.
The Succor plain stage 1 is specifically made using aviation aluminum alloy material, and the middle part of Succor plain stage 1 is provided with controller 2, uses
In controlling whole air rescue device flight and Fixed Wing AirVehicle 10 to be docked, before and after the top of the Succor plain stage 1 respectively
Prelocalization detection means 31 and rear locating and detecting device 32 are mounted with, the position for detecting fixed wing aircraft 10, guiding is aerial
Deliverance apparatus fly to the lower section of fixed wing aircraft 10 of failure and interfaced；Put down at used four of four angles of the Succor plain stage 1
Platform rotating shaft 8 is connected to four supports 4, and support 4 can make horizontal direction and rotate 90 ° ~ 135 ° around Succor plain stage 1, four supports 4
End is connected by machine shaft 9 with four motors 5, and motor 5 specifically uses high-tension motor, and motor 5 can be around motor turn
Axle 9 rotates 0 ° ~ 90 °, and propeller 6 is assembled with four motors 5；Controller 2 can be with control platform rotating shaft 8 and machine shaft 9
Turn an angle, air rescue device flight attitude can be adjusted；The both sides of the Succor plain stage 1 are provided with the He of left fixed mount 71
Right fixed mount 72, is stretched out after being docked with Fixed Wing AirVehicle 10, and Succor plain stage 1 is fixed on the belly bottom of fixed wing aircraft
Under.
The air rescue mode is sued and laboured by a multi-rotor aerocraft carrying Succor plain stage, specially works as fixation
Wing aircraft 10 because engine failure or wing because bird collisions is impaired cannot normal flight or during landing, earthward airport boat station hair
Go out distress signal, after airport boat station is connected to distress signal, send air rescue device to fly to failure fixed wing aircraft 10 at once
Lower section, the information that controller 2 is received by prelocalization detection means 31 and rear locating and detecting device 32 guides Succor plain stage 1
Near the belly of fixed wing aircraft 10, Succor plain stage 1 is fixed on by fixed wing aircraft 10 by left fixed mount 71 and right fixed mount 72
Belly.
Specifically after the completion of the Succor plain stage 1 is docked with fixed wing aircraft 10, four supports 4 pass through platform rotating shaft 8
Make horizontal direction around Succor plain stage 1 to rotate, four motors 5 are by electricity with two wings of fixed wing aircraft 10 horizontally
Machine rotating shaft 9 rotates around support 4, motor 5 and propeller 6 is consistent with the heading of fixed wing aircraft 10, now four electricity
Machine 5 and propeller 6 allow fixed wing aircraft 10 to continue to prepare to force-land to neighbouring aerodrome flight as temporary flight power；Work as fixation
The wing of wing aircraft 10 is damaged in stays or when sliding in the air, and controller 2 can control to be arranged on four of Succor plain stage 1
Support 4 and four motors 5 rotate to adjust the flight attitude of fixed wing aircraft 10, for the flight of fixed wing aircraft 10 provides power,
Keep the balance and certain flying speed of whole fuselage, it is to avoid aircraft crashes because of stall；Then four supports 4 and four electricity
Machine 5 deflects certain angle, allows motor 5 and propeller 6 upward, air rescue platform 1 is switched to vertical landing attitude so that
The fixed wing aircraft 10 of failure can forced landing be on the ground in the short time.
Claims (4)
1. a kind of air rescue device, it is characterised in that：Including Succor plain stage（1）And controller（2）；Controller（2）It is arranged on
Succor plain stage（1）Middle part, the Succor plain stage（1）Prelocalization detection means has been respectively mounted before and after top（31）With rear positioning inspection
Survey device（32）；The Succor plain stage（1）Four angles pass through four platformses rotating shaft（8）It is connected to four supports（4）, four branch
Frame（4）End pass through machine shaft（9）With four motors（5）It is connected, four motors（5）On be assembled with propeller（6）；Institute
State Succor plain stage（1）Both sides left fixed mount is installed（71）With right fixed mount（72）.
2. a kind of air rescue device according to claim 1, it is characterised in that：The support（4）Can be around Succor plain stage
（1）Make horizontal direction rotation.
3. a kind of air rescue device according to claim 1 and 2, it is characterised in that：The motor（5）Can be around motor
Rotating shaft（9）Rotation.
4. a kind of air rescue mode, it is characterised in that：It is to be rescued in the air by any according to claims 1 to 3
Shaking apparatus works as fixed wing aircraft come what is implemented（10）Because engine failure or wing because bird collisions it is impaired cannot normal flight or
During landing, earthward boat station in airport sends an SOS, and after airport boat station is connected to distress signal, air rescue device is sent at once
Fly to failure fixed wing aircraft（10）Lower section, controller（2）The information received by locating and detecting device, guiding rescue is flat
Platform（1）Near fixed wing aircraft（10）Belly, by left fixed mount（71）With right fixed mount（72）By Succor plain stage（1）It is fixed
In fixed wing aircraft（10）Belly；When the Succor plain stage（1）With fixed wing aircraft（10）After the completion of docking, four branch
Frame（4）By platform rotating shaft（8）Around Succor plain stage（1）Make horizontal direction rotation, with fixed wing aircraft（10）Two wings into
Horizontal direction, four motors（5）By machine shaft（9）Around support（4）Rotation, makes motor（5）And propeller（6）With fixed-wing
Aircraft（10）Heading keeps identical, now four motors（5）And propeller（6）Fixation can be allowed as temporary flight power
Wing aircraft（10）Continue to neighbouring aerodrome flight；Work as fixed wing aircraft（10）Wing be damaged in stays or slide in the air
When, controller（2）Can control to be arranged on Succor plain stage（1）Four supports（4）And four motors（5）Rotate to adjust fixation
Wing aircraft（10）Flight attitude, keep the balance and certain flying speed of whole fuselage, it is to avoid aircraft crashes because of stall,
Then switch to vertical landing state so that the fixed wing aircraft of failure（10）Can in a short time forced landing on ground
On.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139331.7A CN106915442A (en) | 2017-03-10 | 2017-03-10 | A kind of air rescue device and mode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139331.7A CN106915442A (en) | 2017-03-10 | 2017-03-10 | A kind of air rescue device and mode |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106915442A true CN106915442A (en) | 2017-07-04 |
Family
ID=59461061
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139331.7A Withdrawn CN106915442A (en) | 2017-03-10 | 2017-03-10 | A kind of air rescue device and mode |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106915442A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972859A (en) * | 2017-12-11 | 2018-05-01 | 王美航 | A kind of two-way aircraft |
| CN107992077A (en) * | 2017-12-13 | 2018-05-04 | 北京小米移动软件有限公司 | Aircraft fault rescue method and device |
| CN111936388A (en) * | 2020-07-10 | 2020-11-13 | 曹庆恒 | Separated airplane protection device, method and system |
| CN112224417A (en) * | 2020-09-22 | 2021-01-15 | 南京航空航天大学 | An aircraft equipped with a modular embedded landing gear and its application method |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101274668A (en) * | 2007-03-26 | 2008-10-01 | 黄金富 | Safe landing system and method for rescuing airplane out of action in flight |
| CN205044987U (en) * | 2015-09-28 | 2016-02-24 | 邱祥康 | Aircraft goes up and down to assist flying platform |
| CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
| CN106043696A (en) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | Flying system for unmanned aerial vehicle |
| CN106275434A (en) * | 2016-08-28 | 2017-01-04 | 张玉华 | A kind of aircraft rescue unmanned plane |
| US20170036762A1 (en) * | 2015-08-03 | 2017-02-09 | Dustin Gamble | Release and Capture of a Fixed-Wing Aircraft |
| CN206885358U (en) * | 2017-03-10 | 2018-01-16 | 佛山市神风航空科技有限公司 | A kind of air rescue device |
-
2017
- 2017-03-10 CN CN201710139331.7A patent/CN106915442A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101274668A (en) * | 2007-03-26 | 2008-10-01 | 黄金富 | Safe landing system and method for rescuing airplane out of action in flight |
| US20170036762A1 (en) * | 2015-08-03 | 2017-02-09 | Dustin Gamble | Release and Capture of a Fixed-Wing Aircraft |
| CN205044987U (en) * | 2015-09-28 | 2016-02-24 | 邱祥康 | Aircraft goes up and down to assist flying platform |
| CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
| CN106043696A (en) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | Flying system for unmanned aerial vehicle |
| CN106275434A (en) * | 2016-08-28 | 2017-01-04 | 张玉华 | A kind of aircraft rescue unmanned plane |
| CN206885358U (en) * | 2017-03-10 | 2018-01-16 | 佛山市神风航空科技有限公司 | A kind of air rescue device |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972859A (en) * | 2017-12-11 | 2018-05-01 | 王美航 | A kind of two-way aircraft |
| CN107992077A (en) * | 2017-12-13 | 2018-05-04 | 北京小米移动软件有限公司 | Aircraft fault rescue method and device |
| CN111936388A (en) * | 2020-07-10 | 2020-11-13 | 曹庆恒 | Separated airplane protection device, method and system |
| WO2022006905A1 (en) * | 2020-07-10 | 2022-01-13 | 曹庆恒 | Separable aircraft protection device, method and system |
| CN112224417A (en) * | 2020-09-22 | 2021-01-15 | 南京航空航天大学 | An aircraft equipped with a modular embedded landing gear and its application method |
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| 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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170704 |