CN106915445A - One kind combination aircraft and its mode of taking off - Google Patents
One kind combination aircraft and its mode of taking off Download PDFInfo
- Publication number
- CN106915445A CN106915445A CN201710139343.XA CN201710139343A CN106915445A CN 106915445 A CN106915445 A CN 106915445A CN 201710139343 A CN201710139343 A CN 201710139343A CN 106915445 A CN106915445 A CN 106915445A
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- China
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- wing aircraft
- fixed wing
- slot
- rotor aerocraft
- aircraft
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- 230000005484 gravity Effects 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000012544 monitoring process 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
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Abstract
One kind combination aircraft and its mode of taking off, belong to technical field of aerospace, more particularly to a kind of combination aircraft.Including handset and machine tool；Handset includes fixed wing aircraft, T-slot, motor and gate；Machine tool includes multi-rotor aerocraft and T-shaped axle；When fixed wing aircraft needs to take off, T-shaped axle is inserted into T-slot, fixed wing aircraft is in flameout state, vertically gone up to the air by multi-rotor aerocraft and accelerate flight forward to after certain altitude, after the flying speed of multi-rotor aerocraft reaches the takeoff speed of fixed wing aircraft, T-shaped axle is separated with T-slot, fixed wing aircraft is separated with multi-rotor aerocraft, realizes taking off for fixed wing aircraft.The present invention combination aircraft and its mode of taking off, its mode of taking off do not limited by place, it is possible to achieve fixed wing aircraft takes off vertically, simple structure.
Description
Technical field
One kind combination aircraft and its mode of taking off, belong to technical field of aerospace, more particularly to a kind of combination aircraft and
Its mode of taking off.
Background technology
Traditional aviation aircraft can be divided into fixed wing aircraft, helicopter and multi-rotor aerocraft.Wherein, fixed wing aircraft
Flying speed is fast, and mobility is high, and flying radius is big, and security performance coefficient is high, but due to the limitation of itself, to the bar for taking off
Part requirement is harsh, and fixed wing aircraft takes off it is necessary to have sufficiently long runway.Helicopter can be with VTOL, but construction is multiple
It is miscellaneous, and expend larger for the culture of helicopter pilot, the driving technology requirement to driver is high.Multi-rotor aerocraft can be with
Accomplish VTOL, and it is simple to operate, it is workable, some narrow region operations can be entered, but, flying radius is small, continuation of the journey
Ability is low, is used for taking photo by plane, monitoring field, and the scope of application is small, and more seriously, security and stability is low, due to many rotations
Rotor aircraft is that many motors of multiaxis cooperate, as long as one of motor breaks down, certainly will cause to save in the air
Accident.And fixed wing aircraft is directly combined with multi-rotor aerocraft, many rotor structures turn into fixed-wing during flight in the air
Burden, or even influence is produced on the performance of fixed wing aircraft.
The content of the invention
The present invention program is, in order to be directed to the deficiency of above-mentioned aircraft, to invent a kind of combination aircraft that can be taken off vertically
And its mode of taking off, set up aerial runway.
One kind combination aircraft, including handset and machine tool；Handset includes fixed wing aircraft, T-slot, motor and gate；It is T-shaped
Groove is placed in immediately below fixed wing aircraft, is slotted to the position of centre of gravity of fixed wing aircraft from afterbody, T-shaped, T-slot upper surface
Level；On T-slot top backward, there is a groove, groove includes motor and gate, and gate connection motor can be rotated；Gate point
It is closed mode when gate is laid to close and opening two states；It is open mode when gate is vertical；Gate is used to block
T-shaped axle.Machine tool includes multi-rotor aerocraft and T-shaped axle；T-shaped axle is fixed on multi-rotor aerocraft with 3 ° ~ 10 ° inclinations angle, is
Rigid structure, for being embedded into T-slot, be connected wing aircraft.
Described groove is that an a quarter is round, and disc is placed in circle perpendicular to T-slot, radius across T-slot, motor
Heart position, motor parallel to T-slot, perpendicular to disc；Gate is placed in a quarter disc, one end connection machine shaft, energy
Rotate.
It is described combination aircraft the mode of taking off be：When fixed wing aircraft needs to take off, fixed wing aircraft passes through lifting
Equipment is arranged on multi-rotor aerocraft；T-shaped axle reaches T-slot top, closing gate；Now, fixed wing aircraft is in and puts out
Fiery state, multi-rotor aerocraft starts, and vertical lift-off starts fixed wing aircraft engine, multi-rotor aerocraft to certain altitude
Support carries fixed wing aircraft and accelerates flight forward together；After the speed of fixed wing aircraft reaches takeoff speed, electric motor starting, lock
Door is opened, multi-rotor aerocraft decelerating flight, and now the speed due to fixed wing aircraft speed more than multi-rotor aerocraft, T-shaped
Groove is separated with T-shaped axle, and fixed wing aircraft separates with multi-rotor aerocraft and realizes taking off in the air；Multi-rotor aerocraft and fixed-wing
Auto-returned ground after aircraft disengaging.
Combination aircraft and its mode of taking off of the invention, its mode of taking off do not rely on place limitation, it is possible to achieve Gu
Determine taking off vertically for wing aircraft, performance safety reliability, simple structure, while intelligence degree is high, the operation requirement to driver
It is small.
Brief description of the drawings
Fig. 1 is handset schematic rear view；Fig. 2 is gate schematic diagram；Fig. 3 is gate left view schematic diagram；Fig. 4 is combination flight
Device schematic diagram.
In figure, 1-T type grooves, 2-T profile shafts, 3- motors, 4- gates, 5- fixed wing aircrafts, 6- multi-rotor aerocrafts.
Specific embodiment
The present invention is illustrated in conjunction with accompanying drawing, one kind combination aircraft, including handset and machine tool.Including handset
And machine tool.Handset includes fixed wing aircraft 5, T-slot 1, motor 3 and gate 4.Machine tool includes multi-rotor aerocraft 6 and T-shaped axle 2.
Handset includes fixed wing aircraft 5, T-slot 1, motor 3 and gate 4；T-slot 1 is placed in immediately below fixed wing aircraft 5,
Slotted to the position of centre of gravity of fixed wing aircraft 5 from afterbody, T-shaped, the upper surface level of T-slot 1；It is past on the top of T-slot 1
Afterwards, there is an a quarter circular groove, in T-slot 1, across T-slot 1, home position has a motor 3 to radius to texturearunaperpendicular, electricity
Machine 3 parallel to T-slot 1, perpendicular to groove；Gate 4 is placed in a quarter disc, one end connection rotating shaft of motor 3, Ke Yizhuan
It is dynamic, it is divided into closing and opens two states, it is closed mode when gate is laid；It is open mode when gate is vertical.
Machine tool includes multi-rotor aerocraft 6 and T-shaped axle 2；T-shaped axle 2 is fixed on multi-rotor aerocraft 6 with 3 ° ~ 10 ° inclinations angle
On, it is rigid structure, for being embedded in T-slot 1, be connected wing aircraft 5.
When fixed wing aircraft 5 needs to take off, fixed wing aircraft 5 is arranged on multi-rotor aerocraft 6 by crane gear,
T-shaped axle 2 reaches the top of T-slot 1, and gate 4 is closed；Now, fixed wing aircraft 5 is in flameout state, and multi-rotor aerocraft 6 is opened
Dynamic, vertical lift-off starts the engine of fixed wing aircraft 5 to certain altitude, and the support of multi-rotor aerocraft 6 carries fixed wing aircraft 5 one
Rise and accelerate flight forward；After the speed of fixed wing aircraft 5 reaches takeoff speed, motor 3 starts, and gate 4 is opened, and many rotors fly
The decelerating flight of row device 6, the now speed due to the speed of fixed wing aircraft 5 more than multi-rotor aerocraft 6,2 points of T-slot 1 and T-shaped axle
From fixed wing aircraft 5 separates with multi-rotor aerocraft 6 and realizes taking off in the air；Multi-rotor aerocraft 6 takes off with fixed wing aircraft 5
From rear auto-returned ground.
Claims (3)
- It is 1. a kind of to combine aircraft, it is characterised in that：Including handset and machine tool, handset includes fixed wing aircraft（5）, T-slot （1）, motor（3）And gate（4）；Machine tool includes multi-rotor aerocraft（6）With T-shaped axle（2）；The T-slot of handset（1）It is placed in fixation Wing aircraft（5）Underface, slots to fixed wing aircraft from afterbody（5）Position of centre of gravity, T-shaped, T-slot（1）Upper surface Level；In T-slot（1）Backward, there is the semicircle of an a quarter on top, and disc is perpendicular to T-slot（1）, radius is across T-slot （1）, home position has a motor（3）, motor（3）Parallel to T-slot（1）, perpendicular to disc；Gate（4）It is placed in a quarter In disc, one end connection motor（3）Rotating shaft, can rotate, and be divided into closing and open two states, work as gate（4）Lay, to close State；Work as gate（4）Vertically, it is open mode；T-shaped axle（2）Embedded T-slot（1）, multi-rotor aerocraft（6）Be connected the wing Aircraft（5）.
- 2. one kind according to claim 1 combines aircraft, it is characterised in that：T-shaped axle（2）With certain 3 ° ~ 10 ° inclinations angle It is fixed on multi-rotor aerocraft（6）On, T-shaped axle（2）It is rigid structure.
- 3. one kind according to claim 1 and 2 combines aircraft, and its mode of taking off is characterised by：Work as fixed wing aircraft （5）When needing to take off, fixed wing aircraft（5）Multi-rotor aerocraft is arranged on by crane gear（6）On, T-shaped axle（2）Reach T Type groove（1）Top, gate（4）Close, now, fixed wing aircraft（5）In flameout state, multi-rotor aerocraft（6）Start, Vertical lift-off starts fixed wing aircraft to certain altitude（5）Engine, multi-rotor aerocraft（6）Support carries fixed wing aircraft（5） Accelerate flight forward together；Work as fixed wing aircraft（5）Speed reach takeoff speed after, motor（3）Start, gate（4）Open, Multi-rotor aerocraft（6）Decelerating flight, T-slot（1）With T-shaped axle（2）Separate, fixed wing aircraft（5）With multi-rotor aerocraft（6） Separate and realize taking off in the air；Multi-rotor aerocraft（6）With fixed wing aircraft（5）Auto-returned ground after disengaging.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139343.XA CN106915445A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its mode of taking off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139343.XA CN106915445A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its mode of taking off |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106915445A true CN106915445A (en) | 2017-07-04 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139343.XA Withdrawn CN106915445A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its mode of taking off |
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| Country | Link |
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| CN (1) | CN106915445A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107640314A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| CN107640315A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| CN107651178A (en) * | 2017-09-18 | 2018-02-02 | 佛山市神风航空科技有限公司 | One kind combination multi-rotor aerocraft |
| CN109720566A (en) * | 2017-10-31 | 2019-05-07 | 一飞智控(天津)科技有限公司 | The main rotor control system of the unmanned device of manned helicopter |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2843337A (en) * | 1953-09-29 | 1958-07-15 | Hiiler Helicopters | Composite aircraft system and method of flight |
| US4267987A (en) * | 1979-03-29 | 1981-05-19 | Mcdonnell William R | Helicopter airborne load systems and composite aircraft configurations |
| US8950698B1 (en) * | 2012-10-26 | 2015-02-10 | The Boeing Company | Convertible compounded rotorcraft |
| CN105270627A (en) * | 2015-10-27 | 2016-01-27 | 深圳市飞研智能科技有限公司 | Two-unmanned-aircraft system capable of being charged in air and improving endurance capability |
| CN205971844U (en) * | 2016-07-13 | 2017-02-22 | 绵阳空天科技有限公司 | Fixed wing aircraft vertical take -off auxiliary system |
| CN205971845U (en) * | 2016-07-22 | 2017-02-22 | 绵阳空天科技有限公司 | Backpack fixed wing aircraft vertical take -off auxiliary system |
-
2017
- 2017-03-10 CN CN201710139343.XA patent/CN106915445A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2843337A (en) * | 1953-09-29 | 1958-07-15 | Hiiler Helicopters | Composite aircraft system and method of flight |
| US4267987A (en) * | 1979-03-29 | 1981-05-19 | Mcdonnell William R | Helicopter airborne load systems and composite aircraft configurations |
| US8950698B1 (en) * | 2012-10-26 | 2015-02-10 | The Boeing Company | Convertible compounded rotorcraft |
| CN105270627A (en) * | 2015-10-27 | 2016-01-27 | 深圳市飞研智能科技有限公司 | Two-unmanned-aircraft system capable of being charged in air and improving endurance capability |
| CN205971844U (en) * | 2016-07-13 | 2017-02-22 | 绵阳空天科技有限公司 | Fixed wing aircraft vertical take -off auxiliary system |
| CN205971845U (en) * | 2016-07-22 | 2017-02-22 | 绵阳空天科技有限公司 | Backpack fixed wing aircraft vertical take -off auxiliary system |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107640314A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| CN107640315A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| CN107651178A (en) * | 2017-09-18 | 2018-02-02 | 佛山市神风航空科技有限公司 | One kind combination multi-rotor aerocraft |
| CN109720566A (en) * | 2017-10-31 | 2019-05-07 | 一飞智控(天津)科技有限公司 | The main rotor control system of the unmanned device of manned helicopter |
| CN109720566B (en) * | 2017-10-31 | 2024-03-01 | 一飞智控(天津)科技有限公司 | Main rotor control system of unmanned device of manned helicopter |
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| 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: 20170704 |
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| WW01 | Invention patent application withdrawn after publication |