CN205311255U - Two duct carplane - Google Patents
Two duct carplane Download PDFInfo
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- CN205311255U CN205311255U CN201521032766.4U CN201521032766U CN205311255U CN 205311255 U CN205311255 U CN 205311255U CN 201521032766 U CN201521032766 U CN 201521032766U CN 205311255 U CN205311255 U CN 205311255U
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- guiding mechanism
- vector wind
- wind guiding
- carplane
- type fan
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Abstract
The utility model discloses a two duct carplane, including the automobile body truss, locate the preceding lift duct formula fan of automobile body truss front end and locate the back lift duct formula fan of automobile body truss rear end, be equipped with between preceding lift duct formula fan and the back lift duct formula fan and be used for preceding lift duct formula fan of separately -driven and back lift duct formula fan moving power unit, the upper portion of preceding lift duct formula fan is equipped with the preceding vector wind guiding mechanism who is used for changing the automobile body direction through the air current that admits air, preceding vector wind guiding mechanism lays along the axletree direction of carplane, the bottom of back lift duct formula fan is equipped with the back vector wind guiding mechanism who is used for changing the automobile body direction through the exhaust air current, and back vector wind guiding mechanism lays along the rear wheel shaft direction of carplane. The problem of equilibrium and gesture adjust is solved, better self regulation still has in the time of can having the perturbed moment in the environment.
Description
Technical field
This utility model relates to hovercar control law technical field, especially, relates to a kind of double; two duct carplane.
Background technology
Carplane is a kind of amphibious Multi-purpose vehicle having flight and driving functions concurrently, and can have certain load-carrying (people or article), the product that domestic market is not correlated with, for carplane concept still in the conception stage. The technical scheme conception that presently, there are has double; two duct aircraft and four duct Gas Turbine Power hovercars, and this technical scheme is primarily present following shortcoming:
1., although pair duct aircraft aircraft when the moment of torsion that two propellers produce is identical will not rotate, when on the line of centres that the center of gravity of aircraft is positioned at front and back propeller, aircraft will not produce rolling. But in practice process, the moment of torsion of two propeller generations is difficult to coupling so as to identical, and the center of aircraft is difficult to overlap with the line of centres of front and back propeller, and in flight course, aircraft rotates in original place; And when on the center of gravity not line between two propellers of aircraft, aircraft can be caused to turn on one's side. Thus, above-mentioned technical though is difficult to try out.
2. four duct Gas Turbine Power hovercars are with gas turbine for power, the problem being difficult to avoid that response time delay length in actual control system designs, and there is, under the small-power states such as level land traveling and downhill path, the problem that electromotor easily stops working.
Utility model content
This utility model provides a kind of double; two duct carplane, there is balance and attitude regulation cannot regulate or regulate the technical problem of difficulty solving existing carplane.
This utility model provides a kind of double; two duct carplane, including car body truss, it is located at the front lift culvert type fan of car body truss front end and is located at the rear lift culvert type fan of car body truss rear end, it is provided with for driving front lift culvert type fan and the actuating unit of rear lift culvert type fan running respectively between front lift culvert type fan and rear lift culvert type fan, the top of front lift culvert type fan is provided with the front vector wind guiding mechanism for being changed car body direction by charge air flow, and front vector wind guiding mechanism is laid along the axial direction of carplane; The bottom of rear lift culvert type fan is provided with the rear vector wind guiding mechanism for being changed car body direction by exhaust airstream, and rear vector wind guiding mechanism is laid along the rear axle direction of carplane.
Further, front vector wind guiding mechanism be connected with for along front vector wind guiding mechanism circumference regulate before vector wind guiding mechanism rotational angle and regulate before vector wind guiding mechanism around the shaft towards the first adjustment structure;And/or after vector wind guiding mechanism be connected with for along rear vector wind guiding mechanism circumference regulate after vector wind guiding mechanism rotational angle and regulate after vector wind guiding mechanism around the shaft towards the second adjustment structure.
Further, the first adjustment structure and/or the second adjustment structure adopt electron speed regulator as actuating mechanism controls vector wind deflector.
Further, front vector wind guiding mechanism and/or rear vector wind guiding mechanism include many group vector wind deflector groups, and often group vector wind deflector group has a pair vector wind deflector.
Further, every piece of vector wind deflector is all connected with one group of electron speed regulator.
Further, front vector wind guiding mechanism and rear vector wind guiding mechanism all include three groups of vector wind deflector groups.
Further, actuating unit adopts for controlling the motor that system quickly responds, and front lift culvert type fan and rear lift culvert type fan are connected with motor one group independent respectively.
Further, car body truss is anterior equipped with one group of front-wheel, and car body truss rear portion is equipped with one group of trailing wheel, and front-wheel and trailing wheel are respectively provided with a running motor.
Further, front lift culvert type fan and rear lift culvert type fan is oppositely oriented.
Further, being provided with controlling organization in the middle part of car body truss, controlling organization is connected by cable and each motor of controlling in car body and each actuator.
This utility model has the advantages that
The double; two duct carplane of the present invention, adopts double; two duct lift structure, by the problem arranging front vector wind guiding mechanism and rear vector wind guiding mechanism solves balance and attitude regulation; Front vector wind guiding mechanism is laid along axial direction and rear vector wind guiding mechanism is laid along wheel direction of principal axis, it is possible to still have good self-regulation when there is disturbance torque in the environment.
Except purpose described above, feature and advantage, this utility model also has other purpose, feature and advantage. Below with reference to figure, this utility model is described in further detail.
Accompanying drawing explanation
The accompanying drawing constituting the part of the application is used for providing being further appreciated by of the present utility model, and schematic description and description of the present utility model is used for explaining this utility model, is not intended that improper restriction of the present utility model. In the accompanying drawings:
Fig. 1 is the structural representation of double; two duct carplane of this utility model preferred embodiment.
Marginal data:
1, car body truss; 2, front lift culvert type fan; 3, rear lift culvert type fan; 4, actuating unit; 5, front vector wind guiding mechanism; 6, rear vector wind guiding mechanism; 7, front-wheel; 8, trailing wheel.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiment of the present utility model is described in detail, but this utility model can be implemented by following the multitude of different ways limiting and covering.
Fig. 1 is the structural representation of double, two duct carplane of this utility model preferred embodiment. as shown in Figure 1, double, two duct carplane of the present embodiment, including car body truss 1, it is located at the front lift culvert type fan 2 of car body truss 1 front end and is located at the rear lift culvert type fan 3 of car body truss 1 rear end, it is provided with for driving front lift culvert type fan 2 and the actuating unit 4 of rear lift culvert type fan 3 operating respectively between front lift culvert type fan 2 and rear lift culvert type fan 3, the top of front lift culvert type fan 2 is provided with the front vector wind guiding mechanism 5 for being changed car body direction by charge air flow, front vector wind guiding mechanism 5 is laid along the axial direction of carplane,The bottom of rear lift culvert type fan 3 is provided with the rear vector wind guiding mechanism 6 for being changed car body direction by exhaust airstream, and rear vector wind guiding mechanism 6 is laid along the rear axle direction of carplane. The double; two duct carplane of the present invention, adopts double; two duct lift structure, by the problem arranging front vector wind guiding mechanism and rear vector wind guiding mechanism solves balance and attitude regulation; Front vector wind guiding mechanism is laid along axial direction and vector wind guiding mechanism is laid along the rear axle direction of carplane afterwards, it is possible to still have good self-regulation when there is disturbance torque in the environment.
As it is shown in figure 1, in the present embodiment, front vector wind guiding mechanism 5 be connected with for vector wind guiding mechanism 5 rotational angle before regulating along front vector wind guiding mechanism 5 circumference and before regulating vector wind guiding mechanism 5 around the shaft towards the first adjustment structure; And/or after vector wind guiding mechanism 6 be connected with for along rear vector wind guiding mechanism 6 circumference regulate after vector wind guiding mechanism 6 rotational angle and regulate after vector wind guiding mechanism 6 around the shaft towards the second adjustment structure.
As it is shown in figure 1, in the present embodiment, the first adjustment structure and/or the second adjustment structure adopt electron speed regulator as actuating mechanism controls vector wind deflector.
As it is shown in figure 1, in the present embodiment, front vector wind guiding mechanism 5 and/or rear vector wind guiding mechanism 6 include many group vector wind deflector groups. Often group vector wind deflector group has a pair vector wind deflector.
As it is shown in figure 1, in the present embodiment, every piece of vector wind deflector is all connected with one group of electron speed regulator.
As it is shown in figure 1, in the present embodiment, front vector wind guiding mechanism 5 and rear vector wind guiding mechanism 6 all include three groups of vector wind deflector groups.
As it is shown in figure 1, in the present embodiment, actuating unit 4 adopts for controlling the motor that system quickly responds, and front lift culvert type fan 2 and rear lift culvert type fan 3 are connected with motor one group independent respectively. The present invention adopts motor as power source, it is possible to solve the problem that the response time delay of control system is longer, it is achieved rapid feedback control accurately.
As it is shown in figure 1, in the present embodiment, car body truss 1 front portion is equipped with one group of front-wheel 7. Car body truss 1 rear portion is equipped with one group of trailing wheel 8. Front-wheel 7 and trailing wheel 8 are respectively provided with a running motor.
As it is shown in figure 1, in the present embodiment, front lift culvert type fan 2 is oppositely oriented with rear lift culvert type fan 3.
As it is shown in figure 1, in the present embodiment, be provided with controlling organization in the middle part of car body truss 1, controlling organization is connected by cable and each motor of controlling in car body and each actuator.
During enforcement, it is provided that a kind of double; two duct carplane, car body (includes car body truss 1), front lift fan (front lift culvert type fan 2), rear lift fan (rear lift culvert type fan 3), vector wind deflector, wheel.
Wherein front lift fan (front lift culvert type fan 2) and rear lift fan (rear lift culvert type fan 3) are culvert type fan, it is oppositely oriented, and is equipped with the vector wind deflector of rotary angle controllable in the duct of front lift fan and rear lift fan. Carplane population structure is shown in Fig. 1.
The front lift fan (front lift culvert type fan 2) of carplane and rear lift fan (rear lift culvert type fan 3) are each by a big motor driving, and general power is between 80～150kW. Two front-wheels are respectively driven by a running motor, and general power is between 7kW～10kW.
Carplane, when ground run, drives front-wheel walking by running motor, and running motor can independently control, and controls motor speed according to driver command by controlling system during turning.Four wheels of carplane are equipped with damping device, can play the effect of undercarriage when carplane landing.
During carplane flight aloft, by independent electron speed regulator as actuating mechanism controls vector wind deflector, car body spin, rollover, rolling can be prevented, but also the carplane direction when flight can be controlled, by regulating the rotating speed of forward and backward lift fan, face upward before scalable vehicle, attitude of swinging back, or realize aerial forward flight, retreat flight.
Under state of flight, by the control to front and back lift fan (front lift culvert type fan 2 and rear lift culvert type fan 3) and vector wind deflector (front vector wind guiding mechanism 5 and rear vector wind guiding mechanism 6), it is achieved to the Equilibrium of hovercar, advance, retreat, the control that turns to and adjustment. Wherein, vector guide plate be divided into some groups (be illustrated as before and after each three groups, often organize a pair vector wind deflector, totally ten two. Vector guide plate is not limited to various layout type, as long as comprising the control mode of spin, rollover, rolling), control the heading of automobile, and spin, rollover, rolling can be prevented; Lift fan lift before reducing, after increase during lift fan lift, vehicle realizes advancing; Lift fan lift before increasing, after reduction during lift fan lift, vehicle realizes slowing down and retreating. The traveling of carplane and the switching of flight are implemented according to driver command by controlling system.
The present invention proposes a kind of brand-new amphibious Multi-purpose vehicle overall plan, and by rationally arranging lift system layout and power configuration scheme, solve the problem that carplane aerial statue is difficult to control to, ground run and airflight power are difficult to coordinate, and scheme easily implements, there is good application prospect. The present invention possesses the critical pieces such as car body, front lift fan, rear lift fan, vector deflector, wheel. Each lift member is connected by car body Truss Design with power, and car body possesses some strength and leaves load space. Control system is positioned at car body centre position, is connected with each motor and actuator by cable.
The foregoing is only preferred embodiment of the present utility model, be not limited to this utility model, for a person skilled in the art, this utility model can have various modifications and variations. All within spirit of the present utility model and principle, any amendment of making, equivalent replacement, improvement etc., should be included within protection domain of the present utility model.
Claims (10)
1. a double; two duct carplane, including car body truss (1), it is located at front lift culvert type fan (2) of described car body truss (1) front end and is located at rear lift culvert type fan (3) of described car body truss (1) rear end
The actuating unit (4) for driving described front lift culvert type fan (2) and described rear lift culvert type fan (3) to operate respectively it is provided with between described front lift culvert type fan (2) and described rear lift culvert type fan (3)
It is characterized in that,
The top of described front lift culvert type fan (2) is provided with the front vector wind guiding mechanism (5) for being changed car body direction by charge air flow, and described front vector wind guiding mechanism (5) is laid along the axial direction of carplane;
The bottom of described rear lift culvert type fan (3) is provided with the rear vector wind guiding mechanism (6) for being changed car body direction by exhaust airstream, and described rear vector wind guiding mechanism (6) is laid along the rear axle direction of carplane.
2. according to claim 1 pair of duct carplane, it is characterised in that
Described front vector wind guiding mechanism (5) be connected with for along described front vector wind guiding mechanism (5) circumference regulate described front vector wind guiding mechanism (5) rotational angle and regulate described front vector wind guiding mechanism (5) around the shaft towards the first adjustment structure;And/or
Described rear vector wind guiding mechanism (6) be connected with for along described rear vector wind guiding mechanism (6) circumference regulate described rear vector wind guiding mechanism (6) rotational angle and regulate described rear vector wind guiding mechanism (6) around the shaft towards the second adjustment structure.
3. according to claim 2 pair of duct carplane, it is characterised in that
Described first adjustment structure and/or described second adjustment structure adopt electron speed regulator as actuating mechanism controls vector wind deflector.
4. according to claim 3 pair of duct carplane, it is characterised in that
Described front vector wind guiding mechanism (5) and/or described rear vector wind guiding mechanism (6) include many group vector wind deflector groups,
Often organize described vector wind deflector group and there is a pair vector wind deflector.
5. according to claim 4 pair of duct carplane, it is characterised in that
Every piece of described vector wind deflector is all connected with one group of electron speed regulator.
6. according to claim 4 pair of duct carplane, it is characterised in that
Described front vector wind guiding mechanism (5) and described rear vector wind guiding mechanism (6) all include three groups of vector wind deflector groups.
7. according to any one of claim 1 to 6 pair of duct carplane, it is characterised in that
Described actuating unit (4) adopts for controlling the motor that system quickly responds, and described front lift culvert type fan (2) and described rear lift culvert type fan (3) are connected with motor one group independent respectively.
8. according to any one of claim 1 to 6 pair of duct carplane, it is characterised in that
Described car body truss (1) is anterior equipped with one group of front-wheel (7),
Described car body truss (1) rear portion equipped with one group of trailing wheel (8),
Described front-wheel (7) and described trailing wheel (8) are respectively provided with a running motor.
9. according to any one of claim 1 to 6 pair of duct carplane, it is characterised in that
Described front lift culvert type fan (2) is oppositely oriented with described rear lift culvert type fan (3).
10. according to any one of claim 1 to 6 pair of duct carplane, it is characterised in that
Described car body truss (1) middle part is provided with controlling organization,
Described controlling organization is connected by cable and each motor of controlling in car body and each actuator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521032766.4U CN205311255U (en) | 2015-12-11 | 2015-12-11 | Two duct carplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521032766.4U CN205311255U (en) | 2015-12-11 | 2015-12-11 | Two duct carplane |
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| Publication Number | Publication Date |
|---|---|
| CN205311255U true CN205311255U (en) | 2016-06-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521032766.4U Active CN205311255U (en) | 2015-12-11 | 2015-12-11 | Two duct carplane |
Country Status (1)
| Country | Link |
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| CN (1) | CN205311255U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106286011A (en) * | 2016-08-11 | 2017-01-04 | 南昌航空大学 | A kind of duct wall and the adjustable ducted fan in blade tip gap |
| CN107042883A (en) * | 2017-03-27 | 2017-08-15 | 上海珞鹏航空科技有限公司成都研发分公司 | Double duct unmanned aerial vehicles that a kind of secondary transmission engine lap siding can generate electricity with loading |
| CN108202568A (en) * | 2016-12-16 | 2018-06-26 | 深圳光启合众科技有限公司 | Hovercar |
| CN108583867A (en) * | 2018-06-27 | 2018-09-28 | 长沙紫宸科技开发有限公司 | A kind of three ducted fan bionic Aircraft of torque self-balancing |
| CN109878282A (en) * | 2019-04-04 | 2019-06-14 | 江苏航空职业技术学院 | A kind of four ducts control VTOL variant hovercar |
| CN110978921A (en) * | 2019-12-22 | 2020-04-10 | 长春工程学院 | Land all-terrain duct cross-domain robot and cross-domain method thereof |
| CN111038193A (en) * | 2020-01-07 | 2020-04-21 | 长春工程学院 | Land-wheel air-propeller type amphibious aircraft and switching method |
| CN114103572A (en) * | 2021-12-30 | 2022-03-01 | 北京国家新能源汽车技术创新中心有限公司 | Double-duct hybrid power device, hovercar and control method |
-
2015
- 2015-12-11 CN CN201521032766.4U patent/CN205311255U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106286011A (en) * | 2016-08-11 | 2017-01-04 | 南昌航空大学 | A kind of duct wall and the adjustable ducted fan in blade tip gap |
| CN108202568A (en) * | 2016-12-16 | 2018-06-26 | 深圳光启合众科技有限公司 | Hovercar |
| CN107042883A (en) * | 2017-03-27 | 2017-08-15 | 上海珞鹏航空科技有限公司成都研发分公司 | Double duct unmanned aerial vehicles that a kind of secondary transmission engine lap siding can generate electricity with loading |
| CN108583867A (en) * | 2018-06-27 | 2018-09-28 | 长沙紫宸科技开发有限公司 | A kind of three ducted fan bionic Aircraft of torque self-balancing |
| CN108583867B (en) * | 2018-06-27 | 2023-10-17 | 长沙紫宸科技开发有限公司 | Torque self-balancing three-duct fan bionic aircraft |
| CN109878282A (en) * | 2019-04-04 | 2019-06-14 | 江苏航空职业技术学院 | A kind of four ducts control VTOL variant hovercar |
| CN110978921A (en) * | 2019-12-22 | 2020-04-10 | 长春工程学院 | Land all-terrain duct cross-domain robot and cross-domain method thereof |
| CN111038193A (en) * | 2020-01-07 | 2020-04-21 | 长春工程学院 | Land-wheel air-propeller type amphibious aircraft and switching method |
| CN114103572A (en) * | 2021-12-30 | 2022-03-01 | 北京国家新能源汽车技术创新中心有限公司 | Double-duct hybrid power device, hovercar and control method |
| CN114103572B (en) * | 2021-12-30 | 2023-08-22 | 北京国家新能源汽车技术创新中心有限公司 | Double-duct hybrid power device, aerocar and control method |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 412002 Dong Jiaduan, Zhuzhou, Hunan Patentee after: China Hangfa South Industrial Co. Ltd. Address before: 412002 Dong Jiaduan, Zhuzhou, Hunan Patentee before: China Southern Airlines Industry (Group) Co., Ltd. |
|
| CP01 | Change in the name or title of a patent holder |