CN202863052U - Multifunctional flying vehicle - Google Patents
Multifunctional flying vehicle Download PDFInfo
- Publication number
- CN202863052U CN202863052U CN2012205955087U CN201220595508U CN202863052U CN 202863052 U CN202863052 U CN 202863052U CN 2012205955087 U CN2012205955087 U CN 2012205955087U CN 201220595508 U CN201220595508 U CN 201220595508U CN 202863052 U CN202863052 U CN 202863052U
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- hovercar
- rotor
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- chassis
- vehicle
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Abstract
The utility model discloses a multifunctional flying vehicle which comprises a vehicle body and vehicle wheels. Main rotors are arranged at the front end and the back end of an underpan of the vehicle body. Auxiliary rotors are arranged on the left side and the right side of the underpan of the vehicle body. The main rotors and the auxiliary rotors are connected with an engine arranged inside the vehicle body and a rotor controller. A flying program is arranged inside the rotor controller. Overall skin is coated outside the vehicle body. Grids corresponding to the positions of the main rotors and the auxiliary rotors of the underpan are arranged at the bottom of the overall skin. The multifunctional flying vehicle can take off and land vertically, the limitation that take-off and landing of a flying vehicle need a wide smooth runway is solved, take-off and landing of the flying vehicle is not limited by ground conditions, and the multifunctional flying vehicle can successfully take off and land almost at any occasions.
Description
Technical field
The utility model belongs to mechanical device and transportation (B) technical field, is specifically related to a kind of multi-functional hovercar, can be used for cross-country car or El Airplane.
Background technology
Hovercar has been reported in the world, and the hovercar of finding report has all adopted the fixed-wing mode, and both hovercar was run at high speed at runway or highway, after reaching certain speed, the lift that fixed-wing produces can overcome himself gravity, automobile built on stilts, aloft flight.When hovercar lands, need equally smooth runway.The hovercar of this mode all needs runway or highway just to take off and land, and the take-off venue is required harshness, has therefore limited its popularization.
The utility model content
The utility model is intended to overcome the deficiencies in the prior art, and a kind of multi-functional hovercar is provided.
In order to achieve the above object, the technical scheme that provides of the utility model is:
A kind of multi-functional hovercar comprises body shell and wheel, and rear and front end, described body shell chassis is provided with main rotor; The left and right sides, body shell chassis is provided with auxiliary rotor; Main rotor is connected with rotor controller with the driving engine of being located at body shell inside with auxiliary rotor, the built-in mission program of rotor controller; Body shell is wrapped with whole covering, and described whole covering bottom is provided with the grid corresponding with chassis main rotor and auxiliary rotor position.
Wherein, two main rotor hand of rotation of rear and front end, described chassis are opposite; Two auxiliary rotor hand of rotation of the left and right sides, described chassis are opposite; Described driving engine is the fuel oil type driving engine; Described whole covering adopts sheet steel to make, and is provided with rib in it; Described body shell inside also is provided with a plurality of attitude sensors that are connected with rotor controller, and attitude sensor is sent to mission program with the automobile attitude signal, and the mission program output command makes rotor controller control rotor attitude.
The utility model is described in further detail below in conjunction with principle of design:
In the utility model, the Lightweight high-rigidity design is adopted on the auto body chassis, is the main framework of multi-functional hovercar.Driving engine provides power for multi-purpose vehicle(MPV), and power-transmission system to rotor and wheel, and can switch transmission power by arrangement of clutch the power transmission of driving engine between wheel and rotor.Whole covering adopts sheet steel to make, and in order to improve the rigidity of covering, increases reinforced rib in inside, guarantees car conour, the resistance when reducing automotive operation simultaneously.Automotive wheel is the inflated rubber wheel, and hovercar relies on wheel to run at high speed on land, and during landing, wheel especially plays the effect of buffering as the alighting gear of hovercar when hovercar lands, reduce impulsive force.The hand of rotation of former and later two main rotors is opposite, about the hand of rotation of two auxiliary rotors opposite, rotor relies on the power High Rotation Speed of driving engine transmission, required most of lift when main rotor is used for providing multi-purpose vehicle(MPV) flight, balance when auxiliary rotor aloft flies for the assurance multi-purpose vehicle(MPV) provides a part of lift simultaneously.In addition, whole covering bottom can rely on electric multi-stage control to close or open with the grid of main rotor and auxiliary rotor correspondence position, and when automobile during at land locomotion, grid is closed, and guarantees the automobile smooth contour, the air resistance when reducing running car; When automobile flew, grid was opened, and guaranteed that air circulates smoothly.Attitude sensor in the automobile is used for providing the real-time attitude information of multi-functional hovercar, and it comprises in electronic compass, micromechanical gyro, micro-mechanical accelerometer, global positioning system (GPS) receptor two or more at least; Attitude sensor can accurately be exported the attitude information of hovercar by specific correction algorithm, supplies with mission program, and as the reference information of control hovercar, with the stabilized flight of control hovercar, GPS then provides the location information of hovercar.Attitude sensor output hovercar attitude information is to the mission program of rotor controller inside, through the mission program computing, produce control signal, instruction rotor controller control rotor state, thereby the attitude of control hovercar makes the hovercar stable suspersion in aerial or do maneuvering flight.
Compared with prior art, the beneficial effects of the utility model are:
The creationary screw propeller mode that adopted of hovercar of the present utility model relies on the screw propeller of High Rotation Speed that lift is provided, and overcomes the hovercar self gravitation.Hovercar of the present utility model adopts the mode of vertical takeoff and landing, and the adjustable point suspension is aerial, to the take-off venue no requirement (NR), almost can take off or land in any place.
Multi-functional hovercar can be realized on the ground high-speed motion, when running into obstacle, can fly clear an obstacle aloft.Multi-functional hovercar adopts the mode of vertical takeoff and landing, therefore landing site has been reduced requirement, and on ground with stronger maneuverability arranged in the air.Can be used as powerful cross-country car at civil area, carry weapon in military domain and can be used as El Airplane and use, gather around and hold out broad prospects.
In addition, the technical index that reaches of the utility model is as follows:
(1) maximum take-off weight: 100Kg
(2) maximum ceiling: 50m
(3) maximum power consumption: 20KW.
Description of drawings
Fig. 1 is the utility model structural representation.
Among the figure: 1, body shell; 2, wheel; 3, main rotor; 4, auxiliary rotor.
The specific embodiment
Embodiment 1
The applicant has successfully developed a multi-functional hovercar according to such scheme, 3.7 rice long, 1.5 meters wide, and successfully fly: referring to Fig. 1, described multi-functional hovercar comprises body shell 1 and wheel 2, and rear and front end, described body shell 1 chassis is provided with main rotor 3; The left and right sides, body shell 1 chassis is provided with auxiliary rotor 4; Main rotor 3 is connected with auxiliary rotor and is connected with rotor controller with the driving engine of being located at body shell 1 inside; Body shell 1 is wrapped with whole covering, and described whole covering bottom is provided with the grid 5 corresponding with chassis main rotor 3 and auxiliary rotor 4 positions.
Wherein, two main rotor 3 hand of rotation of rear and front end, described chassis are opposite; Two auxiliary rotor 4 hand of rotation of the left and right sides, described chassis are opposite; Described driving engine is the fuel oil type driving engine; Be provided with rib in the described whole covering; Described body shell 1 inside also is provided with a plurality of attitude sensors that are connected with rotor controller.
Claims (6)
1. a multi-functional hovercar comprises body shell (1) and wheel (2), it is characterized in that, described body shell (1) rear and front end, chassis is provided with main rotor (3); Body shell (1) left and right sides, chassis is provided with auxiliary rotor (4); Main rotor (3) is connected 4 with auxiliary rotor) be connected with rotor controller with the driving engine of being located at body shell (1) inside; Body shell (1) is wrapped with whole covering, and described whole covering bottom is provided with the grid (5) corresponding with chassis main rotor (3) and auxiliary rotor (4) position.
2. hovercar as claimed in claim 1 is characterized in that, two main rotors (3) hand of rotation of rear and front end, described chassis is opposite.
3. hovercar as claimed in claim 1 is characterized in that, two auxiliary rotors (4) hand of rotation of the left and right sides, described chassis is opposite.
4. hovercar as claimed in claim 1 is characterized in that, described driving engine is the fuel oil type driving engine.
5. hovercar as claimed in claim 1 is characterized in that, is provided with rib in the described whole covering.
6. hovercar as claimed in claim 1 is characterized in that, described body shell (1) inside also is provided with a plurality of attitude sensors that are connected with rotor controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012205955087U CN202863052U (en) | 2012-11-13 | 2012-11-13 | Multifunctional flying vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012205955087U CN202863052U (en) | 2012-11-13 | 2012-11-13 | Multifunctional flying vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202863052U true CN202863052U (en) | 2013-04-10 |
Family
ID=48029800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012205955087U Expired - Lifetime CN202863052U (en) | 2012-11-13 | 2012-11-13 | Multifunctional flying vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202863052U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104773043A (en) * | 2015-04-27 | 2015-07-15 | 朱沫 | Vector water jet propulsion type amphibious device and working method thereof |
| CN107175999A (en) * | 2017-06-21 | 2017-09-19 | 江阴市翔诺电子科技有限公司 | Hovercar |
| CN108556579A (en) * | 2018-07-04 | 2018-09-21 | 天津超算科技有限公司 | Automobile aerocraft |
| CN108944307A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
| CN108944306A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
-
2012
- 2012-11-13 CN CN2012205955087U patent/CN202863052U/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104773043A (en) * | 2015-04-27 | 2015-07-15 | 朱沫 | Vector water jet propulsion type amphibious device and working method thereof |
| CN107175999A (en) * | 2017-06-21 | 2017-09-19 | 江阴市翔诺电子科技有限公司 | Hovercar |
| CN108556579A (en) * | 2018-07-04 | 2018-09-21 | 天津超算科技有限公司 | Automobile aerocraft |
| CN108944307A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
| CN108944306A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130410 |
|
| CX01 | Expiry of patent term |