CN106005440A - Hybrid power flying electric vehicle with parasol wing - Google Patents
Hybrid power flying electric vehicle with parasol wing Download PDFInfo
- Publication number
- CN106005440A CN106005440A CN201610340075.3A CN201610340075A CN106005440A CN 106005440 A CN106005440 A CN 106005440A CN 201610340075 A CN201610340075 A CN 201610340075A CN 106005440 A CN106005440 A CN 106005440A
- Authority
- CN
- China
- Prior art keywords
- passenger cabin
- rotor
- hybrid power
- wheel
- cabin
- 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.)
- Pending
Links
- 239000000446 fuel Substances 0.000 claims description 4
- 239000000295 fuel oil Substances 0.000 abstract description 3
- 108010066057 cabin-1 Proteins 0.000 description 13
- 230000033001 locomotion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K7/00—Disposition of motor in, or adjacent to, traction wheel
- B60K7/0007—Disposition of motor in, or adjacent to, traction wheel the motor being electric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention relates to a hybrid power flying electric vehicle with a parasol wing, relates to an air-land dual-use low-altitude flying electric vehicle, and aims at providing the air-land dual-use hybrid power flying electric vehicle with the parasol wing, which is safe and reliable. The hybrid power flying electric vehicle with the parasol wing comprises a cabin (1), wherein a seat (2), an instrument system and a control system are arranged in the cabin; the cabin is streamlined; a first rotary wing (3) is arranged at the tail part of the cabin, and is driven by a fuel oil engine; second rotary wings (4) are respectively arranged on the two sides of the cabin, and are electric rotary wings; a parasol wing (6) is arranged at the top of the cabin; and wheels (7) are mounted at the bottom of the cabin, and are driven by a hub motor.
Description
Technical field
The present invention relates to a kind of electric motor car, particularly relate to the low altitude flight electric motor car that a kind of empty land is dual-purpose.
Background technology
The most domestic wheel driving force umbrella of friend's use that flies is substantially based on frame structure, and great majority are imported product, also have and fly individually
Friend is manual imitated, but all design is simple, technique is coarse, performance is single, there is potential safety hazard.
Summary of the invention
The technical problem to be solved in the present invention is to provide the umbrella wing hybrid power flight electric motor car that a kind of land safe and reliable, empty is dual-purpose.
Umbrella wing hybrid power flight electric motor car of the present invention, including passenger cabin, described passenger cabin is provided with seat, instrument system and manipulation system
System, described passenger cabin is streamlined, and the afterbody of passenger cabin is provided with the first rotor, and the first rotor is driven by fuel engines, passenger cabin
Being respectively provided on two sides with the second rotor, the second rotor is electronic rotor, and the top of described passenger cabin is provided with the umbrella wing, and bottom is provided with car
Wheel, described wheel passes through In-wheel motor driving.
Umbrella wing hybrid power flight electric motor car of the present invention, wherein said seat is ejector seat.
Umbrella wing hybrid power flight electric motor car of the present invention, the quantity of wherein said wheel is 3, and one of them wheel is installed present
The head in cabin, another two wheel is arranged on the two sides of tail of passenger cabin.
Umbrella wing hybrid power flight electric motor car of the present invention, the concrete mode that wherein said second rotor is located on passenger cabin is, the second rotation
The wing is installed on the supporting plate, and passenger cabin is provided with motor, and described gripper shoe is fixed on the output shaft of motor.
The first rotor that umbrella wing hybrid power flight electric motor car difference from prior art of the present invention is in the present invention passes through fuel oil
Electromotor drives, and the second rotor is electronic rotor, and wheel uses In-wheel motor driving, and passenger cabin is airflow design, overall
Structural safety is reliable, it is possible to carry out airflight and land locomotion.
The invention will be further described below in conjunction with the accompanying drawings.
Accompanying drawing explanation
Fig. 1 is the axonometric chart of umbrella wing hybrid power flight electric motor car of the present invention；
Fig. 2 is the front view of umbrella wing hybrid power flight electric motor car of the present invention；
Fig. 3 is the right view of Fig. 2；
Fig. 4 is the upward view of Fig. 2.
Detailed description of the invention
As it is shown in figure 1, also with reference to shown in Fig. 2,3,4, umbrella wing hybrid power flight electric motor car of the present invention includes passenger cabin 1, institute
State passenger cabin 1 in streamlined, so can farthest reduce the air drag in flight or driving process.Described passenger cabin 1 is pacified
Equipped with seat 2, instrument system and steerable system, described seat 2 is ejector seat, and when being in an emergency, electric motor car is driven
The person of sailing can be escaped by this ejector seat, and ejector seat and aforesaid instrument system and steerable system are prior art,
This to its structure not with repeat.
The afterbody of passenger cabin 1 is provided with the first rotor 3, and the first rotor 3 is driven by fuel engines (not shown), fuel oil
Electromotor is arranged on passenger cabin 1.Passenger cabin 1 be respectively provided on two sides with the second rotor 4, the second rotor 4 is electronic rotor.Second
The concrete mode that rotor 4 is located on passenger cabin 1 is: the second rotor 4 is arranged in gripper shoe 5, and passenger cabin 1 is provided with motor (figure
Not shown in), described gripper shoe 5 is fixed on the output shaft of motor.When under electric motor car is in state of flight, the second rotor 4 exists
Starting under cruising condition, i.e. start motor, the output shaft rotation of motor, gripper shoe 5 also rotates, and is arranged on gripper shoe 5
On the second rotor 4 also follow gripper shoe 5 and rotate, when the second rotor 4 turns to level, stop motor, now open
Dynamic second rotor 4 rotates, and maintains the cruising condition of electric motor car.When being again started up motor, make gripper shoe 5 rotate, install
The second rotor 4 in gripper shoe 5 is also followed gripper shoe 5 and is rotated, until the second rotor 4 turns to vertical state, this
Time electric motor car cruising condition terminate.
The top of described passenger cabin 1 is provided with the umbrella wing 6, and when travelling on land, the umbrella wing 6 is not switched on, and is in folded state；When
Aloft during flight, the umbrella wing 6 is in open mode, it is provided that to electric motor car lift.
The bottom of passenger cabin 1 is provided with wheel 7, and described wheel 7 passes through In-wheel motor driving.The quantity of described wheel 7 is 3,
One of them wheel 7 is arranged on the head of passenger cabin 1, and another two wheel 7 is arranged on the two sides of tail of passenger cabin 1, each wheel 7
All by being arranged on the In-wheel motor driving from the most with it, described wheel hub motor is prior art, at this to its structure not with repeat.
The present invention can travel as common electric car on land, the most also can aloft fly, and before flight, opens
The umbrella wing 6, starts the first rotor 3 and quickly moves forward, after the umbrella wing 6 opens completely, it is provided that to electric motor car lift upwards,
When lift is more than the deadweight of electric motor car, electric motor car just leaves ground and flies in the air, be in state of flight.As it was previously stated, when opening
When dynamic second rotor 4 is in level rotation, electric motor car is at cruising condition.
The first rotor 3 in the present invention is driven by fuel engines, and the second rotor 4 is electronic rotor, and wheel 7 uses wheel hub
Motor drives, and passenger cabin 1 is airflow design, and overall structure is safe and reliable, it is possible to carry out airflight and land locomotion.
The feature of umbrella wing hybrid power flight electric motor car of the present invention: 1, easily operate, 2, hybrid power, 3, landing site require low,
4, empty land is dual-purpose, 5, cruise noise low, 6, the cruise time long, 7, safe landing duplicate protection.
The purposes of umbrella wing hybrid power flight electric motor car of the present invention: meaning most important for China is to navigate to vast adolescents with learning
Empty rudimentary knowledge, is striden into three dimensions by two-dimensional space, set up one safe and reliable and be filled with " access bridge " of captivation
" familiarization flight ".The most outstanding pilots and Aero-Space skilled personnel necessarily emerge in large numbers, in such a case for China
Aero-Space and relevant scientific development provide optimal path that is universal and that excite teenager interest.Due to umbrella wing hybrid power electricity
The plurality of advantages of motor-car, enables it to be widely used in multiple low idle job, such as: barton, the monitoring in big forest farm, pesticide spray
Spill, aerotow sets up that high-voltage line, video display are taken photo by plane, advertising, aerial sightseeings, security monitoring, low latitude is searched and the condition of a disaster is supervised
Survey ... etc..
Embodiment described above is only to be described the preferred embodiment of the present invention, not carries out the scope of the present invention
Limiting, on the premise of designing spirit without departing from the present invention, technical scheme is made by those of ordinary skill in the art
Various deformation and improvement, all should fall in the protection domain that claims of the present invention determines.
Claims (4)
1. a umbrella wing hybrid power flight electric motor car, including passenger cabin (1), described passenger cabin is provided with seat (2), instrument system
And steerable system, it is characterised in that: described passenger cabin is streamlined, and the afterbody of passenger cabin is provided with the first rotor (3), and the first rotor leads to
Cross fuel engines drive, passenger cabin be respectively provided on two sides with the second rotor (4), the second rotor is electronic rotor, described passenger cabin
Top is provided with the umbrella wing (6), and bottom is provided with wheel (7), and described wheel passes through In-wheel motor driving.
Umbrella wing hybrid power flight electric motor car the most according to claim 1, it is characterised in that: described seat (2) is bullet
Penetrate seat.
Umbrella wing hybrid power flight electric motor car the most according to claim 2, it is characterised in that: the number of described wheel (7)
Amount is 3, and one of them wheel is arranged on the head of passenger cabin (1), and another two wheel is arranged on the two sides of tail of passenger cabin.
Umbrella wing hybrid power flight electric motor car the most according to claim 3, it is characterised in that: described second rotor (4)
The concrete mode being located on passenger cabin (1) is, the second rotor is arranged in gripper shoe (5), and passenger cabin is provided with motor, described
Gripper shoe is fixed on the output shaft of motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610340075.3A CN106005440A (en) | 2016-05-20 | 2016-05-20 | Hybrid power flying electric vehicle with parasol wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610340075.3A CN106005440A (en) | 2016-05-20 | 2016-05-20 | Hybrid power flying electric vehicle with parasol wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106005440A true CN106005440A (en) | 2016-10-12 |
Family
ID=57095736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610340075.3A Pending CN106005440A (en) | 2016-05-20 | 2016-05-20 | Hybrid power flying electric vehicle with parasol wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106005440A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082500A (en) * | 2018-01-29 | 2018-05-29 | 吉林大学 | A kind of fixed-wing formula hybrid power aircraft driving device and driving method |
| CN109367774A (en) * | 2018-09-29 | 2019-02-22 | 周欢东 | A kind of propeller-parachuting for carrying out aerial multi-mode operation that safety flexibility is high |
| CN109455296A (en) * | 2018-06-20 | 2019-03-12 | 周欢东 | A kind of unmanned transporter of parafoil that air security adaptability height has big load |
| CN109625262A (en) * | 2018-10-12 | 2019-04-16 | 周欢东 | Has the unmanned transporter of the high parafoil of steady air security that lands that takes off that flies |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080040314A (en) * | 2006-11-03 | 2008-05-08 | 김종철 | Watercraft towed by a paraglider |
| TW200940369A (en) * | 2008-03-21 | 2009-10-01 | ming-hui Dong | Sky car structure |
| CN202693818U (en) * | 2012-06-01 | 2013-01-23 | 中色地科矿产勘查股份有限公司 | Low-altitude large scale aviation physical geography collective geological prospecting system |
| CN203567946U (en) * | 2013-11-29 | 2014-04-30 | 航宇救生装备有限公司 | Dual-engine aerofoil unmanned plane |
| CN203958615U (en) * | 2014-07-07 | 2014-11-26 | 宿州同创工程机械销售有限公司 | Double-rotor aerobat |
| CN104723816A (en) * | 2014-07-25 | 2015-06-24 | 李俊兰 | Aerodynamic configuration and power allocation implement plan of air-ground sedan and service car |
| US20160090179A1 (en) * | 2014-09-29 | 2016-03-31 | The Boeing Company | Apparatus, system, and method for flying an aircraft |
-
2016
- 2016-05-20 CN CN201610340075.3A patent/CN106005440A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080040314A (en) * | 2006-11-03 | 2008-05-08 | 김종철 | Watercraft towed by a paraglider |
| TW200940369A (en) * | 2008-03-21 | 2009-10-01 | ming-hui Dong | Sky car structure |
| CN202693818U (en) * | 2012-06-01 | 2013-01-23 | 中色地科矿产勘查股份有限公司 | Low-altitude large scale aviation physical geography collective geological prospecting system |
| CN203567946U (en) * | 2013-11-29 | 2014-04-30 | 航宇救生装备有限公司 | Dual-engine aerofoil unmanned plane |
| CN203958615U (en) * | 2014-07-07 | 2014-11-26 | 宿州同创工程机械销售有限公司 | Double-rotor aerobat |
| CN104723816A (en) * | 2014-07-25 | 2015-06-24 | 李俊兰 | Aerodynamic configuration and power allocation implement plan of air-ground sedan and service car |
| US20160090179A1 (en) * | 2014-09-29 | 2016-03-31 | The Boeing Company | Apparatus, system, and method for flying an aircraft |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082500A (en) * | 2018-01-29 | 2018-05-29 | 吉林大学 | A kind of fixed-wing formula hybrid power aircraft driving device and driving method |
| CN109455296A (en) * | 2018-06-20 | 2019-03-12 | 周欢东 | A kind of unmanned transporter of parafoil that air security adaptability height has big load |
| CN109367774A (en) * | 2018-09-29 | 2019-02-22 | 周欢东 | A kind of propeller-parachuting for carrying out aerial multi-mode operation that safety flexibility is high |
| CN109367774B (en) * | 2018-09-29 | 2024-06-07 | 周欢东 | Power umbrella with high safety and flexibility and capable of performing aerial multi-operation |
| CN109625262A (en) * | 2018-10-12 | 2019-04-16 | 周欢东 | Has the unmanned transporter of the high parafoil of steady air security that lands that takes off that flies |
| CN109625262B (en) * | 2018-10-12 | 2024-05-10 | 周欢东 | Unmanned parachute conveyor with stable flying, taking-off and landing and high air safety |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161012 |
|
| RJ01 | Rejection of invention patent application after publication |