CN207917151U - Oily electricity mixing VTOL fixed-wing unmanned plane - Google Patents
Oily electricity mixing VTOL fixed-wing unmanned plane Download PDFInfo
- Publication number
- CN207917151U CN207917151U CN201820215966.0U CN201820215966U CN207917151U CN 207917151 U CN207917151 U CN 207917151U CN 201820215966 U CN201820215966 U CN 201820215966U CN 207917151 U CN207917151 U CN 207917151U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- fuselage
- oil
- wing
- tie
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model is related to air vehicle technique fields, specifically, it is related to a kind of oil electricity mixing VTOL fixed-wing unmanned plane, the host wing is symmetrically arranged with the mounting hole through host wing along fuselage, it is respectively equipped with tie-beam in each mounting hole, each tie-beam front and back ends are respectively provided with the elevating screw of control unmanned plane landing, the motor for providing power to elevating screw, and the motor provides power via the battery pack being arranged in fuselage interior；The oil moves engine, motor respectively via the flight control modules control being arranged in fuselage interior, so, using oil electric mixed dynamic VTOL, in unmanned plane landing process, using electric power, cruise process not only solves needs of the fixed-wing unmanned plane landing process to runway using oily power, reduce oil consumption simultaneously, increases cruise duration and the voyage of unmanned plane.
Description
Technical field：
The utility model is related to air vehicle technique fields, and in particular, to it is a kind of oil electricity mixing VTOL fixed-wing without
It is man-machine.
Background technology：
Fixed-wing unmanned plane is widely used in take photo by plane aerial survey, height due to the advantages that speed is fast, voyage is long, flying height is high
The industries such as fields and mapping, geology, oil, agricultural such as empty scouting, traffic monitoring, have a vast market application prospect.
In the prior art, since fixed-wing unmanned plane is higher to site requirements, fixed runway is needed to carry out rising for aircraft
Drop, seriously constrains the use of fixed-wing unmanned plane, thus how to solve fixed-wing unmanned plane take off, the runway that lands and increasing
Add air mileage, endurance problem, is the emphasis of current designer's research.
Utility model content：
The utility model overcomes the deficiencies of existing technologies, and provides a kind of oil electricity mixing VTOL fixed-wing unmanned plane.
Technical problem to be solved in the utility model is realized using following technical scheme：A kind of oil electricity mixing VTOL
Fixed-wing unmanned plane, including fuselage and the host wing in fuselage both sides is symmetrically connected firmly, the fuselage bottom is additionally provided with undercarriage, machine
Behind end be additionally provided with the dynamic engine of oil, be arranged fuselage interior fuel tank and be rotatably arranged on the spiral of the dynamic engine output end of oil
Paddle, the host wing are symmetrically arranged with the mounting hole through host wing along fuselage, tie-beam are respectively equipped in each mounting hole,
Each tie-beam front and back ends are respectively provided with the elevating screw of control unmanned plane landing, for being carried to elevating screw
For the motor of power, the motor provides power via the battery pack being arranged in fuselage interior；The oil is dynamic start it is mechanical, electrical
Motivation is respectively via the flight control modules control being arranged in fuselage interior.
Preferably, the host wing is additionally provided with side aileron and middle aileron close to fuel tank side, and the side aileron is along tie-beam
Side far from fuel tank arranges that the middle aileron is arranged between fuel tank and tie-beam.
Preferably, in back body, the battery pack is arranged in fuel tank upper end position, the lifting spiral shell for the fuel tank setting
Rotation paddle includes upper propeller and lower propeller, and the upper propeller and lower propeller axial line overlap and upper and lower propeller difference
Power is provided via the motor being arranged on tie-beam.
Preferably, each tie-beam rear end extends rearwardly to form holder parallel to each other, and the holder is equipped with empennage,
It is additionally provided with elevator on the empennage.
Preferably, the fuselage is further fixed on airborne equipment inside front end, is additionally provided with below the airborne equipment solid
It is linked to the airborne equipment control module of fuselage lower end.
Preferably, the fuselage is additionally provided with parachute at front end, and the parachute is connected with flight control modules, flies
Row control module controls parachute and opens.
Operation principle：When unmanned plane takes off lift-off, electric motor operation is controlled by flight control modules, at this time by battery pack
Lift is provided for unmanned plane to drive the rotation of upper propeller, lower propeller for motor, when unmanned plane lift-off is arrived
Up to after certain altitude position, flight control modules control motor stall, and the dynamic engine of oil is started to work, and by propeller
Power is provided for unmanned plane；When unmanned plane, which takes off, needs landing, the dynamic engine stop work of flight control modules control oil, weight
It is new to enable electric motor operation, provide required lift for the landing of unmanned plane；When unmanned plane is in flight course, encountering can not be just
When the fortuitous event often to land, the dynamic engine of flight control modules control oil and motor stall, while parachute is enabled,
To ensure unmanned function safe landing.
Compared with prior art, the beneficial effects of the utility model are：
(1) oil electric mixed dynamic VTOL is used, in unmanned plane landing process, using electric power, cruise process uses
Oily power not only solves needs of the fixed-wing unmanned plane landing process to runway, while reducing oil consumption, increases unmanned plane
Cruise duration and voyage；
(2) descending mechanism that hung down uses 4 axis, 8 paddle structure, safe, stability is strong, and use battery for the energy, fortune
Row is at low cost, noise is small, is influenced on the life of ground staff small；
(3) undercarriage uses Sledge type structure, and landing is more stable, be conducive to reduce the impact during landing to body and
The damage of airborne equipment；
(4) use the flight attitude of two-pack wing control unmanned plane, control efficiency high；
(5) UAV Attitude can be adjusted by rotor mechanism under fixed-wing cruise mode, even if the controls such as aileron, elevator
Molding block, which is out of order, can also control unmanned plane, form control module dual redundant, improve the flight safety of unmanned plane.
Description of the drawings：
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model structural front view；
Fig. 3 is the utility model structure top view；
Fig. 4 is the utility model the structure left view；
Fig. 5 is the symmetrical sectional views of Fig. 3；
In figure：1~host wing；2~side aileron；3~elevator；4~empennage；5~tie-beam；The dynamic engine of 6~oil；7
~propeller；8~middle aileron；9~undercarriage；10~fuselage；11~go up propeller；12~motor；13~lower propeller；14
~airborne equipment；15~parachute；16~battery pack；17~flight control modules；18~fuel tank；19~airborne equipment controls mould
Block.
Specific implementation mode：
In order to make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, under
Face combination is specifically illustrating and embodiment, furthers elucidate the utility model.
Embodiment 1：
As shown in Fig. 1,4,5, a kind of oil electricity mixing VTOL fixed-wing unmanned plane, including fuselage 10 and symmetrically connect firmly
The host wing 1 of 10 both sides of fuselage, 10 bottom of fuselage are additionally provided with undercarriage 9, and 10 rear end of fuselage is additionally provided with the dynamic engine 6 of oil, setting
Fuel tank 18 inside fuselage 10 and the propeller 7 for being rotatably arranged on oil 6 output end of dynamic engine, host wing 1 are right along fuselage 10
Claim the mounting hole for being provided through host wing 1, is respectively equipped with tie-beam 5 in each mounting hole, 5 front and back ends of each tie-beam are set respectively
Elevating screw, the motor 12 for providing power to elevating screw for being useful for control unmanned plane landing, motor 12
Power is provided via the battery pack 16 being arranged inside fuselage 10；The dynamic engine 6 of oil, motor 12 are respectively via setting in fuselage
Flight control modules 17 inside 10 control.
In the prior art, since fixed-wing unmanned plane is higher to site requirements, fixed runway is needed to carry out rising for aircraft
Drop, seriously constrains the use of fixed-wing unmanned plane, thus how to solve fixed-wing unmanned plane take off, the runway that lands and increasing
Add air mileage, endurance problem, is the emphasis of current designer's research.A kind of oil electricity mixing provided by the utility model is vertical
Landing fixed-wing unmanned plane was cruised in unmanned plane landing process using electric power using oil electric mixed dynamic VTOL
Cheng Caiyong oil power not only solves needs of the fixed-wing unmanned plane landing process to runway, while reducing oil consumption, increases
The cruise duration of unmanned plane and voyage.
Operation principle：When unmanned plane takes off lift-off, electric motor operation is controlled by flight control modules 17, at this time by battery
Group 16 is powered for motor 12, to drive the rotation of upper propeller 11, lower propeller 13, is provided lift for unmanned plane, is worked as nothing
After man-machine lift-off reaches certain altitude position, flight control modules 17 control motor 12 and are stopped, and the dynamic engine 6 of oil starts
Work, and by propeller 7 power is provided for unmanned plane；When unmanned plane, which takes off, needs landing, flight control modules 17 control oil
Dynamic engine 6 is stopped, and reactivates the work of motor 12, required lift is provided for the landing of unmanned plane；Work as unmanned plane
In flight course, encounter can not regular descent fortuitous event when, flight control modules 17 control the dynamic engine 6 of oil and electronic
Machine 12 is stopped, while enabling parachute 15, to ensure unmanned function safe landing.
As shown in Figure 1, host wing 1 is additionally provided with side aileron 2 and middle aileron 8 close to 18 side of fuel tank, side aileron 2 is along tie-beam
The 5 side arrangements far from fuel tank 18, middle aileron 8 is arranged between fuel tank 18 and tie-beam 5, in this way, controlling nothing using the two-pack wing
Man-machine flight attitude, control efficiency are high；
As shown in Fig. 2,3,5, the setting of fuel tank 18 rises in 10 rear end of fuselage, the setting of battery pack 16 in 18 upper end position of fuel tank
Drop propeller includes upper propeller 11 and lower propeller 13, upper propeller 11 and lower 13 axial line of propeller overlaps and upper and lower spiral shell
Rotation paddle 11,13 provides power via the motor 12 being arranged on tie-beam 5 respectively, in this way, the descending mechanism that hung down uses 4 axis 8
Paddle structure, it is safe, stability is strong, and use battery for the energy, operating cost is low, noise is small, the life to ground staff
Influence living is small.
As shown in Figure 1,5 rear end of each tie-beam extends rearwardly to form holder parallel to each other, holder is equipped with empennage 4, tail
Elevator 3 is additionally provided on the wing 4, fuselage 10 is further fixed on airborne equipment 14 inside front end, and 14 lower section of airborne equipment is additionally provided with
The airborne equipment control module 19 of 10 lower end of fuselage is connected firmly, in this way, rotor mechanism tune can be passed through under fixed-wing cruise mode
Whole UAV Attitude controls unmanned plane the control modules such as aileron, elevator 3 are out of order, and it is double to form control module
Redundancy improves the flight safety of unmanned plane.
Embodiment 2：
As shown in Figure 1, the present embodiment structure and 1 structure of embodiment are essentially identical, something in common no longer repeats, difference
It is：Fuselage 10 is additionally provided with parachute 15 at front end, and parachute 15 and flight control modules 17 connect, flight control modules
17 control parachutes 15 open, in this way, when unmanned plane in flight course, encounter can not regular descent fortuitous event when, fly
Row control module 17 controls the dynamic engine 6 of oil and motor 12 is stopped, while enabling parachute 15, to ensure unmanned plane
It can safe landing.
The characteristics of basic principles and main features and the utility model of the utility model have been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the present utility model is not limited to the above embodiments, described in above embodiments and description
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these changes and improvements are both fallen in claimed the scope of the utility model.This practicality is new
The claimed range of type is defined by the appending claims and its equivalent thereof.
Claims (6)
1. a kind of oil electricity mixing VTOL fixed-wing unmanned plane, including fuselage (10) and symmetrically connect firmly in fuselage (10) both sides
Host wing (1), fuselage (10) bottom are additionally provided with undercarriage (9), and fuselage (10) rear end is additionally provided with the dynamic engine (6) of oil, sets
The propeller (7) of dynamic engine (6) output end of oil is set in the internal fuel tank (18) of fuselage (10) and is rotatably arranged on, feature exists
In,
The host wing (1) is symmetrically arranged with the mounting hole through host wing (1) along fuselage (10), and each mounting hole is interior respectively
Equipped with tie-beam (5), each tie-beam (5) front and back ends are respectively provided with the elevating screw of control unmanned plane landing, use
In the motor (12) for providing power to elevating screw, the motor (12) is via the setting battery internal in fuselage (10)
Group (16) provides power；
The oil moves engine (6), motor (12) respectively via the setting flight control modules (17) internal in fuselage (10)
Control.
2. oil electricity mixing VTOL fixed-wing unmanned plane according to claim 1, which is characterized in that the host wing
(1) it is additionally provided with side aileron (2) and middle aileron (8) close to fuel tank (18) side, the side aileron (2) is along tie-beam (5) far from oil
The side of case (18) arranges that the middle aileron (8) is arranged between fuel tank (18) and tie-beam (5).
3. oil electricity mixing VTOL fixed-wing unmanned plane according to claim 2, which is characterized in that the fuel tank (18)
Setting is arranged in fuselage (10) rear end, the battery pack (16) in fuel tank (18) upper end position, and the elevating screw includes upper
Propeller (11) and lower propeller (13), the upper propeller (11) and lower propeller (13) axial line overlap and upper and lower spiral
Paddle (11,13) provides power via the motor (12) being arranged on tie-beam (5) respectively.
4. oil electricity mixing VTOL fixed-wing unmanned plane according to claim 3, which is characterized in that each tie-beam
(5) rear end extends rearwardly to form holder parallel to each other, and the holder is equipped with empennage (4), liter is additionally provided on the empennage (4)
Rudder (3) drops.
5. oil electricity mixing VTOL fixed-wing unmanned plane according to claim 1, which is characterized in that the fuselage (10)
It is further fixed on airborne equipment (14) inside front end, is additionally provided with below the airborne equipment (14) and connects firmly fuselage (10) lower end
Airborne equipment control module (19).
6. oil electricity mixing VTOL fixed-wing unmanned plane according to claim 5, which is characterized in that the fuselage (10)
Parachute (15), the parachute (15) and flight control modules (19) connection, flight control modules are additionally provided at front end
(19) control parachute (15) is opened.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820215966.0U CN207917151U (en) | 2018-02-07 | 2018-02-07 | Oily electricity mixing VTOL fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820215966.0U CN207917151U (en) | 2018-02-07 | 2018-02-07 | Oily electricity mixing VTOL fixed-wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207917151U true CN207917151U (en) | 2018-09-28 |
Family
ID=63603502
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820215966.0U Active CN207917151U (en) | 2018-02-07 | 2018-02-07 | Oily electricity mixing VTOL fixed-wing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207917151U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109263981A (en) * | 2018-10-30 | 2019-01-25 | 佛山市神风航空科技有限公司 | A kind of manned vehicle |
| CN109484640A (en) * | 2018-12-28 | 2019-03-19 | 河南三和航空工业有限公司 | It is a kind of starting, power generation integrated vertical take-off and landing drone |
| CN109573013A (en) * | 2019-01-24 | 2019-04-05 | 猎鸢科技(厦门)有限公司 | A kind of unmanned plane and its flying method based on multi-composite type dynamical system |
| CN109733620A (en) * | 2018-11-22 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane and its control method |
| CN110091999A (en) * | 2019-06-04 | 2019-08-06 | 南京灵龙旋翼无人机系统研究院有限公司 | A kind of method and structure flying the reduction rotary wings vertical take-off and landing drone main screw lift that electricity rises based on oil |
| CN111452981A (en) * | 2020-04-03 | 2020-07-28 | 厦门大学 | Redundant vertical starting power system of composite vertical take-off and landing aircraft and layout method thereof |
| CN112141329A (en) * | 2019-06-28 | 2020-12-29 | 灵翼飞航（天津）科技有限公司 | Vertical take-off and landing solar unmanned aerial vehicle |
| CN114056561A (en) * | 2021-12-29 | 2022-02-18 | 山东尚飞航空科技有限公司 | Electric vertical take-off and landing aircraft |
-
2018
- 2018-02-07 CN CN201820215966.0U patent/CN207917151U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109263981A (en) * | 2018-10-30 | 2019-01-25 | 佛山市神风航空科技有限公司 | A kind of manned vehicle |
| CN109733620A (en) * | 2018-11-22 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane and its control method |
| CN109484640A (en) * | 2018-12-28 | 2019-03-19 | 河南三和航空工业有限公司 | It is a kind of starting, power generation integrated vertical take-off and landing drone |
| CN109573013A (en) * | 2019-01-24 | 2019-04-05 | 猎鸢科技(厦门)有限公司 | A kind of unmanned plane and its flying method based on multi-composite type dynamical system |
| CN110091999A (en) * | 2019-06-04 | 2019-08-06 | 南京灵龙旋翼无人机系统研究院有限公司 | A kind of method and structure flying the reduction rotary wings vertical take-off and landing drone main screw lift that electricity rises based on oil |
| CN112141329A (en) * | 2019-06-28 | 2020-12-29 | 灵翼飞航（天津）科技有限公司 | Vertical take-off and landing solar unmanned aerial vehicle |
| CN111452981A (en) * | 2020-04-03 | 2020-07-28 | 厦门大学 | Redundant vertical starting power system of composite vertical take-off and landing aircraft and layout method thereof |
| CN114056561A (en) * | 2021-12-29 | 2022-02-18 | 山东尚飞航空科技有限公司 | Electric vertical take-off and landing aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207917151U (en) | Oily electricity mixing VTOL fixed-wing unmanned plane | |
| CN107089328B (en) | Control method of hybrid tail-seat type vertical take-off and landing long-endurance unmanned aerial vehicle | |
| CN108001677B (en) | Falling off tethered vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN214451855U (en) | Duck wing VTOL unmanned aerial vehicle | |
| CN103287576A (en) | Tailless layout single tail seat type vertical take-off and landing aircraft | |
| CN208377055U (en) | A kind of Fixed Wing AirVehicle | |
| CN110949662B (en) | Novel concept layout airplane with double-wing configuration | |
| CN206857002U (en) | Hybrid power tail sitting posture VTOL long endurance unmanned aircraft | |
| CN206141829U (en) | Many rotors of stationary vane combined type aircraft | |
| CN103192981A (en) | Motor-driven low-noise short-distance taking-off and landing wing-connected aircraft | |
| CN110239710A (en) | A kind of electric power unmanned plane for the inspection of natural calamity situation | |
| CN207712292U (en) | A kind of tilting rotor wing unmanned aerial vehicle | |
| CN209176908U (en) | A kind of rotor fixed-wing unmanned plane of composite drive | |
| CN106494614B (en) | Aircraft with Horizontal Take-off and Landing and VTOL function | |
| CN112896499A (en) | Vertical take-off and landing aircraft with combined layout of tilting duct and fixed propeller | |
| CN111498100A (en) | Thrust vector tilting three-rotor unmanned aerial vehicle and control method thereof | |
| CN211281472U (en) | Duct tail sitting posture VTOL unmanned aerial vehicle | |
| CN211253017U (en) | Unmanned aerial vehicle with tandem wings capable of vertically taking off and landing | |
| CN109279007B (en) | Composite driving rotor wing fixed wing unmanned aerial vehicle | |
| CN107284658B (en) | Composite vertical/short-distance take-off and landing aircraft | |
| CN205602117U (en) | Novel high lift VTOL aircraft | |
| CN204822078U (en) | Aircraft during fixed chord of VTOL boat | |
| CN211685619U (en) | Water plane capable of vertically taking off and landing | |
| CN211223827U (en) | Unmanned aerial vehicle capable of taking off and landing vertically | |
| CN208775017U (en) | A kind of distributed-power vertical take-off and landing drone |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |