CN206984353U - A kind of VTOL fixed-wing unmanned plane - Google Patents
A kind of VTOL fixed-wing unmanned plane Download PDFInfo
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- CN206984353U CN206984353U CN201720715781.1U CN201720715781U CN206984353U CN 206984353 U CN206984353 U CN 206984353U CN 201720715781 U CN201720715781 U CN 201720715781U CN 206984353 U CN206984353 U CN 206984353U
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- fuselage
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- unmanned plane
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- 230000003028 elevating effect Effects 0.000 claims description 12
- 230000005611 electricity Effects 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/50—Foldable or collapsible UAVs
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The utility model discloses VTOL fixed-wing unmanned plane, belong to VUAV technical field.VTOL fixed-wing unmanned plane of the present utility model includes fuselage, the wing being fixedly arranged on the fuselage and the empennage for being fixedly arranged on the afterbody, also include 2 pairs of ailerons, 2 pairs of ailerons are rotatably arranged at the side of the fuselage, and 2 pairs of ailerons are respectively arranged on front-end and back-end of the fuselage relative to the wing, aileron described in each pair is symmetricly set in the both sides of the fuselage, the fuselage offers storage tank corresponding to 2 pairs of aileron opening positions, for storing 2 pairs of ailerons in fixed-wing flight.VTOL fixed-wing unmanned plane of the present utility model has the advantages of aileron can easily be stored, deployed, and flying quality is excellent, packed and transported is convenient.
Description
Technical field
The utility model belongs to fixed-wing unmanned air vehicle technique field, more particularly, to a kind of VTOL fixed-wing nobody
Machine.
Background technology
In recent years, with the popularization that unmanned plane is applied, its application field is also continuously available expansion, according to unmanned plane product
Structural form and flight theory, the unmanned plane of in the market are generally divided into fixed-wing unmanned plane and multiaxis unmanned plane.
Fixed-wing unmanned plane has the advantages of efficiency high, load-carrying are big, the hang time is long, flying speed is fast, but it is to rising
It is very strict to drop the requirement in place, causes its application seriously to be limited by place；Requirement of the multiaxis unmanned plane to landing site
The fixed high hovering of not high and easy to control, adjustable point, can VTOL, can be shuttled in narrow space landing, still, its phase
Than in the unmanned engine efficiency of fixed-wing is low, load-carrying is small, flying speed is slow.
A kind of VTOL fixed-wing unmanned plane is proposed in the market, with reference to fixed-wing unmanned plane and multiaxis unmanned plane
The advantages of, the flying quality of unmanned plane is not only ensure that, also solves the problems, such as that it is limited by landing site, but such nobody
Machine often simply by simply by fixed-wing unmanned plane and multiaxis unmanned plane do it is simple be superimposed, utilize the phase of multiaxis unmanned plane
Close structure and carry out VTOL, fixed-wing offline mode is converted into after taking off, in this way, the propeller of its multiaxis is directly exposed, production
Very big flight resistance is given birth to so that the energy consumption substantial increase of unmanned plane, corresponding flight time and highest flying speed
It is obvious to reduce, meanwhile, propeller is exposed to cause its volume to increase, and has a strong impact on that its is attractive in appearance, packaging volume is also bright with cost of transportation
Aobvious increase.
Utility model content
Technical problem to be solved in the utility model is：There is provided a kind of aileron foldable VTOL fixed-wing
Unmanned plane.
Technical scheme is used by the utility model solves above-mentioned technical problem：There is provided a kind of vertical take-off and landing unmanned
Machine, including fuselage, the wing that is fixedly arranged on the fuselage and the empennage for being fixedly arranged on the afterbody, in addition to 2 pairs of auxiliary
The wing, 2 pairs of ailerons are rotatably arranged at the side of the fuselage, and 2 pairs of ailerons are respectively arranged on the fuselage
Relative to the front-end and back-end of the wing, aileron described in each pair is symmetricly set in the both sides of the fuselage, the fuselage pair
2 pairs of aileron opening positions offer storage tank described in Ying Yu, for storing 2 pairs of ailerons in fixed-wing flight.
As the further improvement of above-mentioned technical proposal, the aileron includes horn, retractable frame, motor and lifting
The wing, the retractable frame are fixedly arranged on described horn one end, and the motor is fixedly arranged on the other end of the horn, and the elevating plane is fixed
In on the motor.
As the further improvement of above-mentioned technical proposal, the horn is installed with motor installation corresponding to described motor one end
Seat, the motor are fixedly arranged on the motor mount.
As the further improvement of above-mentioned technical proposal, the quantity of the storage tank is 2, and each storage tank can be same
When storage positioned at the fuselage side two ailerons.
As the further improvement of above-mentioned technical proposal, positioned at a pair of ailerons of the wing nose, it is lifted
The wing is fixedly arranged on the horn upper end or lower end, corresponding, positioned at a pair of ailerons of the rear airfoil end, its described lifting
The wing is fixedly arranged on the lower end or upper end of the horn.
As the further improvement of above-mentioned technical proposal, a pair of connections storage tank is offered on the fuselage side
T-slot, 2 T-slots are respectively arranged on the upper and lower ends of the storage tank, to store 2 ailerons of the wing rear and front end.
As the further improvement of above-mentioned technical proposal, in addition to it is fixedly arranged on the front end fixed-wing aircraft of the front fuselage
Structure.
As the further improvement of above-mentioned technical proposal, the front end fixed-wing mechanism includes front end motor cabinet, front end electricity
Machine and front end fixed-wing, the front end motor cabinet are fixedly arranged on the front fuselage, and the front end motor is fixedly arranged on the front end
On motor cabinet, the front end fixed-wing is connected with the output shaft rotation of the front end motor, to provide the power to flying.
As the further improvement of above-mentioned technical proposal, the empennage includes tailplane and vertical tail, the level
Empennage is flat along water direction and is symmetrically fixedly arranged on the both sides of the tail end of the fuselage, and the vertical tail is vertically fixed to be used for
The tail end of the fuselage.
The beneficial effects of the utility model：
VTOL fixed-wing unmanned plane of the present utility model, 2 pairs of ailerons, 2 pairs of ailerons are installed with fuselage both ends
It can be rotated relative to fuselage, fuselage both ends offer storage tank corresponding to 2 pairs of aileron opening positions, are converted into fixed-wing flight
When, 2 pairs of ailerons can be turned in storage tank with respect to fuselage, so as to solve the exposed caused system of aileron in the prior art
Row technical problem, VTOL fixed-wing unmanned plane of the present utility model have the advantages of aileron can easily be stored, deployed,
Flying quality is good, packed and transported is convenient.
Brief description of the drawings
Fig. 1 is the overall structure diagram of VTOL fixed-wing unmanned plane of the present utility model；
Fig. 2 is VTOL fixed-wing unmanned plane front view of the present utility model；
Fig. 3 is the axis side view of VTOL fixed-wing unmanned plane of the present utility model；
Fig. 4 is the fractionation structural representation of removal fuselage of the present utility model；
Fig. 5 is the structural representation of aileron of the present utility model；
The structural representation of aileron expansion when Fig. 6 is removal fuselage of the present utility model；
The structural representation of aileron storage when Fig. 7 is removal fuselage of the present utility model.
Embodiment
Design, concrete structure and caused technique effect of the present utility model are carried out below with reference to embodiment and accompanying drawing
Clearly and completely describe, to be completely understood by the purpose of this utility model, feature and effect.Obviously, described embodiment
It is part of the embodiment of the present utility model, rather than whole embodiments, based on embodiment of the present utility model, the skill of this area
The other embodiment that art personnel are obtained on the premise of not paying creative work, belong to the model of the utility model protection
Enclose.In addition, all connection/annexations being related in patent, not singly refer to component and directly connect, and refer to can be according to specific
Performance, by adding or reducing couple auxiliary, to form more excellent draw bail.Each skill in the utility model creation
Art feature, can be with combination of interactions on the premise of not conflicting conflict.
Please with reference to Fig. 1 to Fig. 3, VTOL fixed-wing unmanned plane of the present utility model includes fuselage 1, wing 2, tail
The wing and aileron 3.
Wing 2 is fixedly arranged on fuselage 1 at the front position, and empennage is fixedly arranged on the tail end of fuselage 1, fuselage 1, wing 2 with
And empennage constitutes the agent structure of VTOL fixed-wing unmanned plane.
In the present embodiment, the quantity of aileron 3 is 2 pairs, and 2 pairs of ailerons 3 are symmetrical with the both sides of fuselage 1, and wherein one
The front end of wing 1 is arranged to aileron 3, another pair aileron 3 is arranged at the rear end of machine 1, and aileron 3 rotates and is arranged at machine
On body 1,2 pairs of ailerons 3 can be turned on the direction of fuselage 1 with respect to fuselage 1, to carry out VTOL, be converted into
During fixed-wing offline mode, 2 pairs of ailerons 3 turned to respect to fuselage 1 it is parallel with the length direction of fuselage 1, by 2 pairs of ailerons 3
Storage.
During to avoid fixed-wing offline mode, aileron 3 is exposed, and the opening position that the both sides of fuselage 1 correspond to aileron 3 opens up
Have a storage tank 10, when aileron 3 collapses, aileron 3 can be turned in storage tank 10 with respect to fuselage 1, by aileron 3 store to
Inside storage tank 10, the exposed of aileron 3 is avoided.
Preferably, the both ends of storage tank 10 correspond respectively to the position setting of 2 ailerons 3 of the front and rear end of wing 2, from
And 2 ailerons 3 are accommodated in same storage tank 10.
Such as Fig. 4 to Fig. 7, the agent structure of VTOL fixed-wing unmanned plane of the present utility model is a support 4, by
It is the fuselage 1 formed to be added outside support 4 and adapt to aerodynamic shell, and the upper end of support 4 is installed with wing link 40, real
Existing wing 2 is secured to connect, and is installed with aileron link 41 in its two sides, passes through aileron link 41 and aileron
3 are fixedly connected.
To realize the foldable VTOL fixed-wing unmanned plane, aileron 3 includes horn 30, retractable frame 31, motor
32 and elevating plane 33, retractable frame 31 be fixedly arranged on one end of horn 30, the other end of aileron 3 is installed with motor 32, elevating plane
33 are rotatablely connected in the output end of motor 32, and retractable frame 31 is fixedly arranged on the end position of storage tank 10, and with aileron link
41 are fixedly connected, and the rotation of aileron 3 can be controlled by retractable frame 31, aileron 3 is deployed or is accommodated in storage tank 10.
Horn 30 is installed with motor cabinet 34 corresponding to the one end of motor 32, and for installing motor 32, motor 32 is fixedly arranged on motor
On seat 34.
In the present embodiment, 2 ailerons 3 positioned at the front end of wing 2, its elevating plane 33 is set up along the Vertical Square of fuselage 1
Corresponding in the upper end of horn 30 or lower end, 2 ailerons 3 positioned at the rear end of wing 2, its elevating plane 33 is along the Vertical Square of fuselage 1
Set up in the lower end of horn 30 or upper end, in this way, the elevating plane 33 of the front end of wing 2 and rear end is along the Vertical Square of fuselage 1
It is staggered upwards, when aileron 3 is accommodated into storage tank 10, elevating plane 33 is staggered in the same position in storage tank 10
Place is put, effectively saves the space of storage tank 10.
Preferably, in the present embodiment, the T-slot 11 connected with storage tank 10, T-slot 11 are further opened with the side of fuselage 1
The both sides up and down of storage tank 10 are respectively arranged at, when aileron 3 is accommodated in storage tank 10, the T-slot 11 of its upper and lower both sides
It is respectively used to store two elevating planes 33.
In order to improve the flying quality of VTOL fixed-wing unmanned plane, VTOL fixed-wing of the present utility model nobody
Machine also includes the front end fixed-wing mechanism for being fixedly arranged on the front end of fuselage 1, and front end fixed-wing mechanism includes front end fixed-wing 12, front end electricity
Machine 13 and front end motor cabinet 14, front end motor cabinet 14 are fixedly arranged at the front position of fuselage 1, and front end motor 13 is fixedly arranged on front end
On motor cabinet, preceding degree fixed-wing 12 is connected with the output shaft rotation of front end motor, in this way, in VTOL fixed-wing unmanned plane
Front end, there is power source, make its flight efficiency higher.
In the present embodiment, empennage includes vertical tail 15 and tailplane 16, and vertical tail 15 is along in the vertical direction of fuselage 1
The tail end of fuselage 1 is fixedly arranged on, tailplane 16 is symmetrically fixedly arranged on the tail end both sides of fuselage 1 along in the horizontal direction of fuselage 1, by hanging down
Fin 15 makes the VTOL fixed-wing unmanned plane have more preferable balance with tailplane 16.
Above is preferably implement to be illustrated to of the present utility model, but the utility model is created and is not limited to institute
Embodiment is stated, those skilled in the art can also make a variety of be equal on the premise of without prejudice to the utility model spirit
Deformation is replaced, and these equivalent deformations or replacement are all contained in the application claim limited range.
Claims (9)
1. a kind of VTOL fixed-wing unmanned plane, including fuselage, the wing that is fixedly arranged on the fuselage and it is fixedly arranged on described
The empennage of afterbody, it is characterised in that：Also include 2 pairs of ailerons, 2 pairs of ailerons are rotatably arranged at the fuselage
Side, and 2 pairs of ailerons are respectively arranged on front-end and back-end of the fuselage relative to the wing, auxiliary described in each pair
The wing is symmetricly set in the both sides of the fuselage, and the fuselage offers storage tank corresponding to 2 pairs of aileron opening positions, is used for
2 pairs of ailerons are stored in fixed-wing flight.
2. VTOL fixed-wing unmanned plane according to claim 1, it is characterised in that：The aileron include horn,
Retractable frame, motor and elevating plane, the retractable frame are fixedly arranged on described horn one end, and the motor is fixedly arranged on the another of the horn
One end, the elevating plane are fixedly arranged on the motor.
3. VTOL fixed-wing unmanned plane according to claim 2, it is characterised in that：The horn corresponds to the electricity
Machine one end is installed with motor mount, and the motor is fixedly arranged on the motor mount.
4. VTOL fixed-wing unmanned plane according to claim 3, it is characterised in that：The quantity of the storage tank is 2
Individual, each storage tank can store two ailerons positioned at the fuselage side simultaneously.
5. VTOL fixed-wing unmanned plane according to claim 4, it is characterised in that：Positioned at the one of the wing nose
To the aileron, its elevating plane is fixedly arranged on the horn upper end or lower end, corresponding, positioned at a pair of institutes of the rear airfoil end
Aileron is stated, its described elevating plane is fixedly arranged on the lower end or upper end of the horn.
6. VTOL fixed-wing unmanned plane according to claim 5, it is characterised in that：Offered on the fuselage side
The T-slot of a pair of connection storage tanks, 2 T-slots are respectively arranged on the upper and lower ends of the storage tank, to store the wing
2 ailerons of rear and front end.
7. the VTOL fixed-wing unmanned plane according to any one of claim 1-6, it is characterised in that：Also include fixed
In the front end fixed-wing mechanism of the front fuselage.
8. VTOL fixed-wing unmanned plane according to claim 7, it is characterised in that：The front end fixed-wing mechanism bag
Front end motor cabinet, front end motor and front end fixed-wing are included, the front end motor cabinet is fixedly arranged on the front fuselage, the front end
Motor is fixedly arranged on the front end motor cabinet, and the front end fixed-wing is connected with the output shaft rotation of the front end motor, to carry
For the power to flying.
9. VTOL fixed-wing unmanned plane according to claim 8, it is characterised in that：The empennage includes tailplane
With vertical tail, the tailplane is flat along water direction and is symmetrically fixedly arranged on the both sides of the tail end of the fuselage, the vertical end
The vertically fixed tail end for the fuselage of the wing.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720715781.1U CN206984353U (en) | 2017-06-19 | 2017-06-19 | A kind of VTOL fixed-wing unmanned plane |
| PCT/CN2017/091952 WO2018232787A1 (en) | 2017-06-19 | 2017-07-06 | Vertical take-off and landing fixed-wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720715781.1U CN206984353U (en) | 2017-06-19 | 2017-06-19 | A kind of VTOL fixed-wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206984353U true CN206984353U (en) | 2018-02-09 |
Family
ID=61396833
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720715781.1U Active CN206984353U (en) | 2017-06-19 | 2017-06-19 | A kind of VTOL fixed-wing unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN206984353U (en) |
| WO (1) | WO2018232787A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109515705A (en) * | 2018-11-20 | 2019-03-26 | 西安爱生无人机技术有限公司 | A kind of unmanned plane of VTOL |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| EP3771637A1 (en) * | 2019-07-29 | 2021-02-03 | Aurora Flight Sciences Corporation | Retractable propulsor assemblies for vertical take-off and landing (vtol) aircraft |
| WO2022099373A1 (en) * | 2020-11-13 | 2022-05-19 | Innovaero Technologies Pty Ltd | Aerial vehicles |
| CN115520384A (en) * | 2022-11-28 | 2022-12-27 | 成都睿铂科技有限责任公司 | Vertical take-off and landing fixed wing unmanned aerial vehicle |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9120560B1 (en) * | 2011-10-13 | 2015-09-01 | Latitude Engineering, LLC | Vertical take-off and landing aircraft |
| CN106081060B (en) * | 2016-07-05 | 2018-11-09 | 北京航空航天大学 | A kind of VTOL composite layouts unmanned plane rotor draw off gear |
| CN106672232A (en) * | 2017-03-02 | 2017-05-17 | 北京天宇新超航空科技有限公司 | Efficient vertical takeoff and landing aircraft |
| CN106809394A (en) * | 2017-03-10 | 2017-06-09 | 佛山市神风航空科技有限公司 | A kind of landing system and method for aircraft |
-
2017
- 2017-06-19 CN CN201720715781.1U patent/CN206984353U/en active Active
- 2017-07-06 WO PCT/CN2017/091952 patent/WO2018232787A1/en active Application Filing
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109515705A (en) * | 2018-11-20 | 2019-03-26 | 西安爱生无人机技术有限公司 | A kind of unmanned plane of VTOL |
| EP3771637A1 (en) * | 2019-07-29 | 2021-02-03 | Aurora Flight Sciences Corporation | Retractable propulsor assemblies for vertical take-off and landing (vtol) aircraft |
| US11305872B2 (en) * | 2019-07-29 | 2022-04-19 | Aurora Flight Sciences Corporation | Retractable propulsor assemblies for vertical take-off and landing (VTOL) aircraft |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112027075B (en) * | 2020-09-15 | 2022-04-29 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| WO2022099373A1 (en) * | 2020-11-13 | 2022-05-19 | Innovaero Technologies Pty Ltd | Aerial vehicles |
| CN115520384A (en) * | 2022-11-28 | 2022-12-27 | 成都睿铂科技有限责任公司 | Vertical take-off and landing fixed wing unmanned aerial vehicle |
| CN115520384B (en) * | 2022-11-28 | 2023-02-03 | 成都睿铂科技有限责任公司 | Vertical take-off and landing fixed wing unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018232787A1 (en) | 2018-12-27 |
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