CN207860452U - It is a kind of can VTOL connection wing unmanned plane - Google Patents
It is a kind of can VTOL connection wing unmanned plane Download PDFInfo
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- CN207860452U CN207860452U CN201820094579.6U CN201820094579U CN207860452U CN 207860452 U CN207860452 U CN 207860452U CN 201820094579 U CN201820094579 U CN 201820094579U CN 207860452 U CN207860452 U CN 207860452U
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- wing
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- unmanned plane
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Abstract
The utility model be it is a kind of can VTOL connection wing unmanned plane, including fuselage, it is equipped with a pair of of swept-back wing in waist, the wing of swept-back wing is slightly equipped with the end wing upwardly extended, it is equipped with vertical tail in fuselage afterbody, a pair of of buzzard-type wing is equipped with above vertical tail, it is fixedly connected at the top of the wing root and vertical tail of buzzard-type wing, the wing of buzzard-type wing slightly connects with end wing top, lower section is arranged with thrust propeller in the middle part of buzzard-type wing, it is arranged with pulling force propeller in fuselage head both sides, pulling force propeller is connected by cantilever with swept-back wing, tail is installed in afterbody and pushes away propeller.The utility model realizes VTOL, saves the starting process before connection wing unmanned plane takes off, effectively solves the problems, such as that flight is limited, the scope of application is wider, and two sets of independent dynamical systems are equipped with, realization optimizes energy utilization rate to the full extent, effectively extends flight duration and distance.
Description
Technical field
The utility model is related to air vehicle technique field, especially it is a kind of can VTOL connection wing unmanned plane.
Background technology
The wing of unmanned plane directly determines the gas of aircraft as most important component in load plane system, its aerodynamic characteristic
Dynamic characteristic and main performance.Usually there is the lift that wing generates to account for 70% or more of full machine lift, the resistance of generation accounts for zero liter of full machine
30% or so of resistance.In addition to this, induced drag is substantially also to be generated by wing.Therefore, in order to improve unmanned plane liter
Power reduces unmanned plane overall dimensions, the connection wing unmanned plane that buzzard-type wing and swept-back wing are combined occurs.But connection wing unmanned plane category
In fixed-wing unmanned plane, landing of taking off is required for the runway of certain length, and flight is limited under specific circumstances, and the item that takes off is not achieved
Part limits the use scope of unmanned plane.This just needs to design a kind of novel connection wing unmanned plane, and to solve, flight is limited to ask
Topic, and further solve the problems, such as that unmanned plane during flying duration and distance are shorter.
Invention content
The technical problems to be solved in the utility model is in view of the deficiencies of the prior art, to propose that a kind of applicability is wide, extend
Flight duration and distance can VTOL connection wing unmanned plane.
The technical problems to be solved in the utility model is achieved through the following technical solutions, it is a kind of can VTOL connection
Wing unmanned plane, including fuselage are equipped with a pair of of swept-back wing in waist, and the wing of the swept-back wing is slightly equipped with the end upwardly extended
The wing is equipped with vertical tail in fuselage afterbody, a pair of of buzzard-type wing, the wing root and vertical tail of buzzard-type wing is equipped with above vertical tail
Top be fixedly connected, the wing of buzzard-type wing slightly connects with end wing top, its main feature is that, be equipped with the thrust propeller rotated horizontally and
Pulling force propeller, the thrust propeller are symmetrically mounted on the lower section in the middle part of buzzard-type wing, and the pulling force propeller is symmetricly set on
Fuselage head both sides, the thrust propeller and pulling force propeller drive unmanned plane VTOL jointly；Equipped with cantilever, the drawing
Wrench of a force system paddle is mounted on the top of cantilever front end, and cantilever rear end is fixedly connected with swept-back wing；Propeller is pushed away equipped with tail, is installed
In afterbody, push it flat winged after being risen for unmanned plane.
The technical problems to be solved in the utility model can also further realize by the following technical programs, be located at fuselage
The projection join line of the thrust propeller of the same side and the center of pulling force propeller in the horizontal plane is parallel with fuselage center line.
The technical problems to be solved in the utility model can also further realize by the following technical programs, in fuselage
Equipped with the dynamical system I for providing power for thrust propeller and pulling force propeller, and pushes away propeller for tail and the dynamic of power is provided
Force system II.
The technical problems to be solved in the utility model can also further realize by the following technical programs, the power
System I is set as cell power systems.
The technical problems to be solved in the utility model can also further realize by the following technical programs, the power
System II is set as the dynamic engine system of oil.
Compared with prior art, the utility model by thrust propeller and pulling force propeller are set with drive the connection wing nobody
Machine VTOL saves the starting process before connection wing unmanned plane takes off, effectively solves the problems, such as that flight is limited, makes the suitable of unmanned plane
It is wider with range；Propeller is pushed away to push unmanned plane is flat to fly by the way that tail is arranged；It is flown over by being set as VTOL process peace
Journey provides two sets of independent dynamical systems of power respectively, optimizes energy utilization rate to the full extent to realize, and effectively prolong
The flight duration and distance of long connection wing unmanned plane.
Description of the drawings
Fig. 1 is the stereoscopic schematic diagram of the utility model；
Fig. 2 indicates the front view of the utility model in Fig. 1；
Fig. 3 indicates the vertical view of the utility model in Fig. 1.
Specific implementation mode
The specific technical solution for further describing the utility model, in order to which those skilled in the art is further understood that
The utility model, without constituting the limitation to its right.
Embodiment 1, referring to Fig.1-3, it is a kind of can VTOL connection wing unmanned plane, including fuselage 1 sets at 1 middle part of fuselage
There are a pair of of swept-back wing 7, the wing of the swept-back wing 7 to be slightly equipped with the end wing 6 upwardly extended, vertical tail 2 be equipped at 1 rear portion of fuselage,
A pair of of buzzard-type wing 4 is equipped with above vertical tail 2, the top of the wing root and vertical tail 2 of buzzard-type wing 4 is fixedly connected, buzzard-type wing 4
The wing slightly connect with the end wing 6 top；
Thrust propeller 5 equipped with horizontal rotation and pulling force propeller 9, the thrust propeller 5 are symmetrically mounted on sweepforward
The lower section at 4 middle part of the wing, the pulling force propeller 9 are symmetricly set on 1 head on both sides of fuselage, the thrust propeller 5 and pulling force spiral shell
It revolves paddle 9 and drives unmanned plane VTOL jointly；
Equipped with cantilever 8, the pulling force propeller 9 is mounted on the top of 8 front end of cantilever, 8 rear end of cantilever and swept-back wing 7
It is fixedly connected, the wheelbase between thrust propeller and pulling force propeller is increased by cantilever, to increase efficiency；
Propeller 3 is pushed away equipped with tail, is mounted on 1 tail portion of fuselage, pushes it flat winged after being risen for unmanned plane；
Positioned at the thrust propeller of 1 the same side of fuselage and the center projection join line in the horizontal plane and machine of pulling force propeller
Body center line is parallel；
It is equipped in fuselage 1 and provides the dynamical system I of power for thrust propeller and pulling force propeller, and be that tail pushes away spiral shell
Revolve the dynamical system II that paddle provides power；
The dynamical system I is set as cell power systems；
The dynamical system II is set as the dynamic engine system of oil.
In vertical and landing takeoff, tail pushes away propeller and does not work unmanned plane, cell power systems be thrust propeller and
Pulling force propeller provides power；When flat winged, thrust propeller and pulling force propeller are stopped, and are tail by the dynamic engine system of oil
It pushes away propeller and power is provided.By the way that two sets of independent dynamical systems are arranged, energy utilization rate can be optimized to the full extent, increased
Unmanned plane during flying duration and distance.
Claims (5)
1. it is a kind of can VTOL connection wing unmanned plane, including fuselage is equipped with a pair of of swept-back wing, the swept-back wing in waist
The wing be slightly equipped with the end wing that upwardly extends, be equipped with vertical tail in fuselage afterbody, a pair of of buzzard-type wing be equipped with above vertical tail,
It is fixedly connected at the top of the wing root and vertical tail of buzzard-type wing, the wing of buzzard-type wing slightly connects with end wing top, it is characterised in that：
Thrust propeller equipped with horizontal rotation and pulling force propeller, the thrust propeller are symmetrically mounted in the middle part of buzzard-type wing
Lower section, the pulling force propeller are symmetricly set on fuselage head both sides, and the thrust propeller and pulling force propeller drive jointly
Unmanned plane VTOL；
Equipped with cantilever, the pulling force propeller is mounted on the top of cantilever front end, and cantilever rear end is fixedly connected with swept-back wing；
Propeller is pushed away equipped with tail, is mounted on afterbody, pushes it flat winged after being risen for unmanned plane.
2. it is according to claim 1 it is a kind of can VTOL connection wing unmanned plane, it is characterised in that：Positioned at fuselage the same side
Thrust propeller and pulling force propeller center projection join line in the horizontal plane it is parallel with fuselage center line.
3. it is according to claim 1 it is a kind of can VTOL connection wing unmanned plane, it is characterised in that：It is equipped in fuselage and is
Thrust propeller and pulling force propeller provide the dynamical system I of power, and push away the dynamical system that propeller provides power for tail
Ⅱ。
4. it is according to claim 3 it is a kind of can VTOL connection wing unmanned plane, it is characterised in that：The dynamical system I
It is set as cell power systems.
5. it is according to claim 3 it is a kind of can VTOL connection wing unmanned plane, it is characterised in that：The dynamical system II
It is set as the dynamic engine system of oil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820094579.6U CN207860452U (en) | 2018-01-20 | 2018-01-20 | It is a kind of can VTOL connection wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820094579.6U CN207860452U (en) | 2018-01-20 | 2018-01-20 | It is a kind of can VTOL connection wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207860452U true CN207860452U (en) | 2018-09-14 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820094579.6U Active CN207860452U (en) | 2018-01-20 | 2018-01-20 | It is a kind of can VTOL connection wing unmanned plane |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109987223A (en) * | 2019-04-02 | 2019-07-09 | 夏季风 | A kind of new vertical landing unmanned plane coupling wing configuration |
| CN110127047A (en) * | 2019-05-31 | 2019-08-16 | 深圳创壹通航科技有限公司 | The VTOL Fixed Wing AirVehicle and its control method of four-vector control |
| CN111619795A (en) * | 2019-02-27 | 2020-09-04 | 空客直升机德国有限公司 | Multi-rotor aircraft with connecting wings capable of vertically taking off and landing |
| CN111619785A (en) * | 2019-02-27 | 2020-09-04 | 空客直升机德国有限公司 | Multi-rotor aircraft suitable for vertical take-off and landing |
| CN113264181A (en) * | 2020-02-17 | 2021-08-17 | 空客直升机德国有限公司 | Tailless composite helicopter |
| CN114126966A (en) * | 2019-05-29 | 2022-03-01 | 工艺航空航天技术股份有限公司 | Novel aircraft design using tandem wings and distributed propulsion system |
-
2018
- 2018-01-20 CN CN201820094579.6U patent/CN207860452U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111619795A (en) * | 2019-02-27 | 2020-09-04 | 空客直升机德国有限公司 | Multi-rotor aircraft with connecting wings capable of vertically taking off and landing |
| CN111619785A (en) * | 2019-02-27 | 2020-09-04 | 空客直升机德国有限公司 | Multi-rotor aircraft suitable for vertical take-off and landing |
| US11691722B2 (en) | 2019-02-27 | 2023-07-04 | Airbus Urban Mobility Gmbh | Multirotor aircraft that is adapted for vertical take-off and landing |
| CN111619785B (en) * | 2019-02-27 | 2023-10-10 | 空客城市移动有限公司 | Multi-rotor aircraft suitable for vertical take-off and landing |
| CN109987223A (en) * | 2019-04-02 | 2019-07-09 | 夏季风 | A kind of new vertical landing unmanned plane coupling wing configuration |
| CN109987223B (en) * | 2019-04-02 | 2023-03-10 | 夏季风 | Novel VTOL unmanned aerial vehicle of hookup wing configuration |
| CN114126966A (en) * | 2019-05-29 | 2022-03-01 | 工艺航空航天技术股份有限公司 | Novel aircraft design using tandem wings and distributed propulsion system |
| CN110127047A (en) * | 2019-05-31 | 2019-08-16 | 深圳创壹通航科技有限公司 | The VTOL Fixed Wing AirVehicle and its control method of four-vector control |
| CN113264181A (en) * | 2020-02-17 | 2021-08-17 | 空客直升机德国有限公司 | Tailless composite helicopter |
| CN113264181B (en) * | 2020-02-17 | 2022-05-06 | 空客直升机德国有限公司 | Tailless composite helicopter |
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