CN207120892U - Mixed dynamic unmanned plane - Google Patents
Mixed dynamic unmanned plane Download PDFInfo
- Publication number
- CN207120892U CN207120892U CN201720396247.9U CN201720396247U CN207120892U CN 207120892 U CN207120892 U CN 207120892U CN 201720396247 U CN201720396247 U CN 201720396247U CN 207120892 U CN207120892 U CN 207120892U
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- CN
- China
- Prior art keywords
- unmanned plane
- fuel engines
- horn
- mixed dynamic
- motor
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- 239000000446 fuel Substances 0.000 claims abstract description 43
- 230000035807 sensation Effects 0.000 claims abstract description 4
- 239000003921 oil Substances 0.000 claims description 29
- 239000000295 fuel oil Substances 0.000 claims description 15
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 8
- 238000005183 dynamical system Methods 0.000 claims description 5
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 4
- 239000004917 carbon fiber Substances 0.000 claims description 4
- 150000001875 compounds Chemical class 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 5
- 239000011120 plywood Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000008450 motivation Effects 0.000 description 2
- 240000000731 Fagus sylvatica Species 0.000 description 1
- 235000010099 Fagus sylvatica Nutrition 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000010223 real-time analysis Methods 0.000 description 1
Abstract
The utility model provides a kind of mixed dynamic unmanned plane, it is characterised in that：Including fuselage, fuel engines and motor, the edge of the fuselage is radially connected horn, the horn at least six roots of sensation, and the end of two horns of fuselage opposite side is each provided with fuel engines, and the end of remaining horn is respectively provided with motor；The fuel engines is respectively connected with lifting rotor, on the contrary, the motor is respectively connected with posture rotor, the direction of rotation of adjacent posture rotor is opposite for the direction of rotation of two lifting rotors.The beneficial effects of the utility model are：A kind of six axle unmanned planes are provided, it is provided for providing the fuel engines of lift in the relative both sides of fuselage, it is provided for providing the motor of flight attitude adjustment on remaining four axle, combine long the characteristics of continuing a journey of the efficient quick control ability of electric propulsion system and oil burning power system, while ensureing unmanned plane operating characteristics, the cruising time of unmanned plane is greatly improved.
Description
Technical field
Unmanned plane field is the utility model is related to, refers in particular to a kind of mixed dynamic unmanned plane.
Background technology
With the progress of unmanned air vehicle technique, unmanned air vehicle technique is more and more perfect, and the application to unmanned plane in the industry enters
Stage of technology deep ploughing.Existing pure oily power unmanned plane throttle has delay, and reaction is slowly；Pure electronic unmanned plane endurance is short,
Voyage is limited, and these limitations have limited to unmanned plane stable performance, easy operation, intelligence degree height, landing without place limit significantly
Many advantageous features such as system, also made troubles to the production and living work that unmanned plane participates in, it is therefore necessary to long endurance, oceangoing voyage
Journey unmanned air vehicle technique is developed, and is used with expanding the multi-field high-performance of unmanned plane.
Utility model content
Technical problem to be solved in the utility model is：A kind of unmanned plane of oil electric mixed dynamic is provided.
In order to solve the above-mentioned technical problem, the technical solution adopted in the utility model is：The mixed dynamic unmanned plane of one kind, including machine
Body, fuel engines and motor, the edge of the fuselage is radially connected horn, the horn at least six roots of sensation, fuselage phase
The end of two horns of offside is each provided with fuel engines, and the end of remaining horn is respectively provided with motor；The fuel oil hair
Motivation is respectively connected with lifting rotor, and the direction of rotation of two lifting rotors is on the contrary, the motor is respectively connected with posture rotor, phase
The direction of rotation of adjacent posture rotor is opposite.
Further, be connected with support bar on the downside of the horn end provided with fuel engines, the support bar it is another
End is connected with the foot stool of the underbelly of unmanned plane, and the support bar is set horizontal by angle.
Further, the oily dynamical system includes fuel oil supply unit, and the fuel oil supply unit is fixed on support bar.
Further, the fuel oil supply unit includes oil can, oil pump and oil pipe, and the oil pump is built in oil can, and oil can passes through
Oil pipe is connected with fuel engines.
Further, it is provided with the length for being shorter in length than the horn for being provided with motor of the horn of fuel engines.
Further, the fuel engines is two reciprocating piston engines.
Further, the fuel engines includes throttle, and the throttle is connected with steering wheel, the steering wheel and flight control system
Connection.
Further, the lifting rotor is wooden aviation blade, and the posture rotor is compound carbon fiber blade.
Further, the fuel engines is connected with generator.
The beneficial effects of the utility model are：A kind of six axle unmanned planes are provided, are provided in the relative both sides of fuselage
The fuel engines of lift is provided, is provided for providing the motor of flight attitude adjustment on remaining four axle, combines electricity
The characteristics of long continuation of the journey of the efficient quick control ability of dynamical system and oil burning power system, ensure the same of unmanned plane operating characteristics
When, greatly improve cruising time of unmanned plane.
Brief description of the drawings
Concrete structure of the present utility model is described in detail below in conjunction with the accompanying drawings：
Fig. 1 is the overall structure diagram of mixed dynamic unmanned plane of the present utility model；
Fig. 2 is the fuselage roof structural representation of mixed dynamic unmanned plane of the present utility model；
Fig. 3 is the fuselage bottom structure schematic diagram of mixed dynamic unmanned plane of the present utility model；
1- fuselages；11- top plates；12- lower plywoods；15- batteries；16- camera cradle heads；17- cameras；18- carries portion；
2- fuel engines；21- lifting rotors；3- motor；31- posture rotors；
4- support bars；5- fuel oil supply units；6- foot stools；7- horns.
Embodiment
To describe technology contents of the present utility model, construction feature, the objects and the effects in detail, below in conjunction with implementation
Mode simultaneously coordinates accompanying drawing to be explained in detail.
Refer to Fig. 1 to Fig. 3, the mixed dynamic unmanned plane of one kind, including fuselage 1, fuel engines 2 and motor 3, the fuselage
1 edge is radially connected horn 7, and the horn 7 at least six roots of sensation, the end of two horns 7 of the opposite side of fuselage 1 is respectively set
There is fuel engines 2, the end of remaining horn 7 is respectively provided with motor 3；The fuel engines 2 is respectively connected with lifting rotor 21,
The direction of rotation of two lifting rotors 21 on the contrary, the motor 3 is respectively connected with posture rotor 31, adjacent posture rotor 31
Direction of rotation is opposite.
Fuselage 1 includes top plate 11 and lower plywood 12, the connecting portion of horn 7 and fuselage 1 in fuselage top plate 11 and
Between lower plywood 12, it is in " * " shape that fuselage 1 is overall with horn 7, and wherein fuel engines 2 is arranged at the horn of the left and right sides of fuselage 1
7 ends, the fuselage 1 of unmanned plane it is left front, right before, it is left back, right after the end of horn 7 be provided with motor 3, this structure is set
In respect of beneficial to the overall center of gravity of control unmanned plane, pose adjustment difficulty is reduced；
The top plate 11 and lower plywood 12 of fuselage 1 are correspondingly arranged on cavern part, for placing battery 15, under lower plywood 12
Face is provided with carry portion 18, and for carry weapon, unmanned plane front portion is provided with camera cradle head 16, for real-time image acquisition information, nothing
People's motor spindle is provided with camera 17, for aiding in aiming at.
Unmanned plane also includes flight control system, and flight control system can be carried out by the sensor of fuel engines 2 and motor 3
In real time analysis, make be advantageous to unmanned plane current power output adjustment, wherein fuel engines 2 for UAS provide to
Few 70% lift, motor 3 then provide the torque and part lift needed for pose adjustment for UAS, and flight control system connects
Communication module is connected to, unmanned plane is carried out data transmission by communication module and operating personnel.
It was found from foregoing description, the beneficial effects of the utility model are：A kind of six axle unmanned planes are provided, it is relative in fuselage
Both sides be provided for provide lift fuel engines, be provided on remaining four axle provide flight attitude adjustment electricity
Motivation, long the characteristics of continuing a journey of the efficient quick control ability of electric propulsion system and oil burning power system is combined, ensures nobody
While machine operating characteristics, the cruising time of unmanned plane is greatly improved.
Embodiment 1
Support bar 4, the other end and nothing of the support bar 4 are connected with the downside of the end of horn 7 provided with fuel engines 2
The foot stool 6 of the man-machine bottom of fuselage 1 is connected, and the support bar 4 is set horizontal by angle.
Horn, support bar and foot stool form triangular frame structure, are advantageous to the stability of unmanned plane structure, the present embodiment
In, using the horn of double supporting rods structural support fuel engines.
Embodiment 2
The oily dynamical system includes fuel oil supply unit 5, and the fuel oil supply unit 5 is fixed on support bar 4.
Support bar is set horizontal by angle, and fuel oil supply unit is fixed on support bar, and tilting fuel oil supply unit is easy to supply
Oil, in addition, oil can is arranged at into fuselage both sides, be advantageous to balance the center of gravity of unmanned plane.
In the present embodiment, between fuel oil supply unit is placed in into two support bars, be advantageous to simplify fuel oil supply unit and support bar
Attachment structure.
Embodiment 3
The fuel oil supply unit 5 includes oil can, oil pump and oil pipe, and the oil pump is built in oil can, and oil can passes through oil pipe and combustion
Oil turbine connects.
Oil pump is built in oil can, advantageously reduces complex degree of structure, reduces fault rate.
Embodiment 4
It is provided with the length for being shorter in length than the horn 7 for being provided with motor 3 of the horn 7 of fuel engines 2.
Fuel engines is responsible for lift, therefore sets the horn stress of fuel engines larger, can be reduced using short horn
The wheelbase of fuel engines, accordingly reduce its horn stress, reduce the interference to UAV Attitude adjustment, be advantageous to unmanned plane appearance
The control of state, it is preferred that the horn of fuel engines uses cantilever beam structure.
Embodiment 5
The fuel engines 2 is two reciprocating piston engines.
The structure of two reciprocating piston engines is simple, and from heavy and light, power is big, is advantageous to increase the continuation of the journey of unmanned plane.
Embodiment 6
The fuel engines 2 includes throttle, and the throttle is connected with steering wheel, and the steering wheel is connected with flight control system.
Throttle is used for the power output for controlling fuel engines, distant by ground here using the depth of servos control throttle
Control signal connects the flight control system of unmanned plane in real time, and steering wheel is operated by flight control system.
Embodiment 7
The lifting rotor 21 is wooden aviation blade, and the posture rotor 31 is compound carbon fiber blade.
The wing loading capability of wooden aviation blade is stronger, possesses preferable structural strength, can undertake caused by fuel engines
Lift load, it is preferred that using the blade of beech matter；Posture blade load is little, and the lighter compound carbon fiber blade of use has
Conduct oneself with dignity beneficial to unmanned plane is reduced.
Embodiment 8
The fuel engines 2 is connected with generator.
Generator is connected with power supply module, and the energy as caused by fuel engines is converted into electrical power storage into battery,
Aid in unmanned plane power supply.
Embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, it is every
The equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or be directly or indirectly used in
Other related technical areas, similarly it is included in scope of patent protection of the present utility model.
Claims (9)
1. the mixed dynamic unmanned plane of one kind, it is characterised in that：Including fuselage, fuel engines and motor, the edge footpath of the fuselage
To horn, the horn at least six roots of sensation is connected with, the end of two horns of fuselage opposite side is each provided with fuel engines,
The end of remaining horn is respectively provided with motor；
The fuel engines is respectively connected with lifting rotor, and the direction of rotation of two lifting rotors is on the contrary, the motor respectively connects
Posture rotor is connected to, the direction of rotation of adjacent posture rotor is opposite.
2. mixed dynamic unmanned plane as claimed in claim 1, it is characterised in that：Connect on the downside of horn end provided with fuel engines
Support bar is connected to, the other end of the support bar is connected with the foot stool of the underbelly of unmanned plane, the support bar and horizontal plane
Angled setting.
3. mixed dynamic unmanned plane as claimed in claim 2, it is characterised in that：Also include oily dynamical system, the oily dynamical system
Including fuel oil supply unit, the fuel oil supply unit is fixed on support bar.
4. mixed dynamic unmanned plane as claimed in claim 3, it is characterised in that：The fuel oil supply unit includes oil can, oil pump and oil pipe,
The oil pump is built in oil can, and oil can is connected by oil pipe with fuel engines.
5. mixed dynamic unmanned plane as claimed in claim 4, it is characterised in that：It is provided with being shorter in length than for the horn of fuel engines
It is provided with the length of the horn of motor.
6. the mixed dynamic unmanned plane as described in claim 1-5 any one, it is characterised in that：The fuel engines is two strokes
Piston engine.
7. mixed dynamic unmanned plane as claimed in claim 6, it is characterised in that：The fuel engines includes throttle, the throttle
It is connected with steering wheel, the steering wheel is connected with flight control system.
8. mixed dynamic unmanned plane as claimed in claim 7, it is characterised in that：The lifting rotor is wooden aviation blade, described
Posture rotor is compound carbon fiber blade.
9. mixed dynamic unmanned plane as claimed in claim 8, it is characterised in that：The fuel engines is connected with generator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720396247.9U CN207120892U (en) | 2017-04-14 | 2017-04-14 | Mixed dynamic unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720396247.9U CN207120892U (en) | 2017-04-14 | 2017-04-14 | Mixed dynamic unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207120892U true CN207120892U (en) | 2018-03-20 |
Family
ID=61614987
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720396247.9U Expired - Fee Related CN207120892U (en) | 2017-04-14 | 2017-04-14 | Mixed dynamic unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207120892U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106915469A (en) * | 2017-04-14 | 2017-07-04 | 深圳市轻准科技有限公司 | Mixed dynamic unmanned plane |
| CN109343553A (en) * | 2018-10-30 | 2019-02-15 | 佛山市神风航空科技有限公司 | A kind of no medicine makes a return voyage unmanned plane automatically |
| WO2020180374A1 (en) | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects Inc. | Distributed propulsion configurations for aircraft having mixed drive systems |
| FR3128200A1 (en) * | 2021-10-20 | 2023-04-21 | Zipair | Hybrid flying device |
-
2017
- 2017-04-14 CN CN201720396247.9U patent/CN207120892U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106915469A (en) * | 2017-04-14 | 2017-07-04 | 深圳市轻准科技有限公司 | Mixed dynamic unmanned plane |
| CN109343553A (en) * | 2018-10-30 | 2019-02-15 | 佛山市神风航空科技有限公司 | A kind of no medicine makes a return voyage unmanned plane automatically |
| WO2020180374A1 (en) | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects Inc. | Distributed propulsion configurations for aircraft having mixed drive systems |
| EP3931091A4 (en) * | 2019-03-01 | 2023-01-11 | Pratt & Whitney Canada Corp. | Distributed propulsion configurations for aircraft having mixed drive systems |
| FR3128200A1 (en) * | 2021-10-20 | 2023-04-21 | Zipair | Hybrid flying device |
| WO2023067253A1 (en) * | 2021-10-20 | 2023-04-27 | Zipair | Hybrid flying device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180320 |