CN109250126A - A kind of oil electric mixed dynamic manned vehicle - Google Patents
A kind of oil electric mixed dynamic manned vehicle Download PDFInfo
- Publication number
- CN109250126A CN109250126A CN201811274934.9A CN201811274934A CN109250126A CN 109250126 A CN109250126 A CN 109250126A CN 201811274934 A CN201811274934 A CN 201811274934A CN 109250126 A CN109250126 A CN 109250126A
- Authority
- CN
- China
- Prior art keywords
- cabin
- propeller
- manned vehicle
- mixed dynamic
- motor
- 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.)
- Withdrawn
Links
- 238000002485 combustion reaction Methods 0.000 claims description 18
- 238000004519 manufacturing process Methods 0.000 claims description 16
- 239000000126 substance Substances 0.000 claims description 9
- 230000008961 swelling Effects 0.000 claims description 9
- 239000002828 fuel tank Substances 0.000 claims description 8
- 239000011521 glass Substances 0.000 claims description 7
- PXIPVTKHYLBLMZ-UHFFFAOYSA-N Sodium azide Chemical compound [Na+].[N-]=[N+]=[N-] PXIPVTKHYLBLMZ-UHFFFAOYSA-N 0.000 claims description 5
- IDCPFAYURAQKDZ-UHFFFAOYSA-N 1-nitroguanidine Chemical compound NC(=N)N[N+]([O-])=O IDCPFAYURAQKDZ-UHFFFAOYSA-N 0.000 claims description 3
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 claims description 3
- 238000005273 aeration Methods 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims description 3
- 238000003860 storage Methods 0.000 claims description 3
- ULRPISSMEBPJLN-UHFFFAOYSA-N 2h-tetrazol-5-amine Chemical compound NC1=NN=NN1 ULRPISSMEBPJLN-UHFFFAOYSA-N 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims description 2
- 238000006243 chemical reaction Methods 0.000 claims 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 4
- 230000000903 blocking effect Effects 0.000 abstract description 4
- 229910052799 carbon Inorganic materials 0.000 abstract description 4
- 230000006698 induction Effects 0.000 abstract 1
- 108010066114 cabin-2 Proteins 0.000 description 13
- 238000000034 method Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000003915 air pollution Methods 0.000 description 1
- 210000004712 air sac Anatomy 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-N ammonia Natural products N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 125000003831 tetrazolyl group Chemical group 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- B64D27/026—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Abstract
The invention discloses a kind of oil electric mixed dynamic manned vehicles, including body and cockpit, body is equipped with air bag, there are four horns for tool on body, a motor is equipped on each horn, motor is bolted on horn head end, shaft is arranged in motor center, one rotor is installed in each shaft, rotor is bolted on motor, it is driven and is rotated by corresponding motor, the center of body is arranged in cockpit, manned seat and operation display are installed in cockpit, operation display controls the movement of entire aircraft, cockpit bottom is equipped with landing bracket, battery and reserve battery are additionally provided between body and cockpit；High comprehensive performance of the present invention is provided simultaneously with preferable flying quality and security performance；Urban traffic blocking can be alleviated, carbon emission is reduced and can be realized rapid delivery passenger；When crashing, the safety of personnel in cockpit is protected in the meeting automatic inflating expansion of induction type air bag to greatest extent.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to a kind of oil electric mixed dynamic manned vehicle.
Background technique
In actual life, the trip of people relies on the vehicles mostly, but most cities are congested in traffic serious at present,
In the case where poor for the trip especially pavement behavior of short distance, conventional vehicles trip is inconvenient, while a large amount of friendships
The discharge of logical tool tail gas causes air pollution serious.
As traffic above-ground congestion problems are on the rise, the demand to transatmospheric vehicle is come into being.However, personal fly
The technical maturity of row device is lower, parks the problems such as space occupied is big, flight efficiency is low, speed is slow, the space requirement that takes off is big
It can not be ignored, in practical applications, additional inconvenience and puzzlement may be brought to traffic above-ground and driver.
The aircraft flight time of existing pure electric vehicle power is short, is short of power, and load-bearing capacity is poor, and the oily more rotors of power fly
Row stability is poor, and response speed is slow, is unable to satisfy the requirement of control rotor manned aircraft flight posture rapidly
And existing manned vehicle is all largely low-latitude flying, and parachute is unable to fully open when failure, is played
Effect, so current manned vehicle security performance is poor, therefore the security performance for improving manned vehicle seems especially heavy
It wants.
Therefore, a kind of flight stability how is provided, the oil electric mixed dynamic that cruising ability is strong, security performance is high is manned
The problem of device is those skilled in the art's urgent need to resolve.
Summary of the invention
In view of this, the present invention provides a kind of oil electric mixed dynamic manned vehicle, high comprehensive performance has preferably
Flying quality and security performance, urban traffic blocking can be alleviated, carbon emission is reduced and can be realized rapid delivery and multiply
Visitor.
In order to achieve the above object, invention adopts the following technical scheme that
A kind of oil electric mixed dynamic manned vehicle, including fuselage body and cabin, which is characterized in that the cabin is spherical in shape,
It is rotatably arranged on the fuselage body, the cabin and the fuselage body junction are provided with cabin rotating electric machine, are used for
The cabin rotation is driven to realize that the cabin is verted when VTOL state is converted to flat winged state；The cabin periphery
It is provided with swelling gasbag, the aeration aperture of the swelling gasbag is connected to by check valve with the gas outlet that gas manufactures box, the gas
Body manufacture box is located in the cabin, and storage generates the substance of gas in the gas manufacture box；
The bottom end of the cabin is equipped with undercarriage, and the side of cabin is equipped with opening, and opening is hinged with hatch door, the inside peace of cabin
Equipped with demarcation plate disposed in parallel, the lower section of demarcation plate is equipped with seat and control device, and seat and control device are installed in cabin
The inner wall bottom end of body, control device are located at the side of seat, and the control device includes control handle and control cabinet, control handle
It is mounted on control cabinet, the inside of control cabinet is equipped with circuit board, and the top of the demarcation plate is equipped with battery, internal combustion engine and oil
Case, internal combustion engine is between battery and fuel tank, and liquid stream connects between fuel tank and internal combustion engine, and the top of the cabin is equipped with horn
And driving box, horn are located at the side of driving box, the inside of driving box is equipped with mechanical coupler and gearbox, mechanical coupler
One end is connected with gearbox, and the other end of mechanical coupler is connected with internal combustion engine, and the output shaft of gearbox is connected with the first spiral
Paddle, the both ends of the horn are mounted on motor, and two motor are symmetrical arranged, and the output shaft of motor is connected with the second spiral shell
Revolve paddle, the output end connection of motor, cabin rotating electric machine and battery；
The control device is electrically connected with laser ranging controller, the second propeller synchronizing speed distributor, center dynamic balancing
System and control system for internal combustion engine.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the circuit board is equipped with the general control of DATA-7311
Device, wireless transmitter and wireless receiver processed, the output end of battery are connected with controller, the output end connection of the controller
The wireless transmitter, the gearbox and the motor, the input terminal of controller are connected with wireless receiver.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the control handle is equipped with control button, control
Button and control device are electrically connected.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, first propeller is located at the second propeller
Top, and the first propeller and the second propeller are parallel to each other, the electricity that first propeller and the second propeller are correspondingly arranged
Motivation is electrically connected with the second propeller synchronizing speed distributor.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, steel is equipped in the surrounding and hatch door of the cabin
The junction for changing glass plate, armorplate glass and cabin and hatch door is equipped with sealing ring.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the output shaft of the gearbox and the first propeller
Junction be equipped with bearing.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the substance for generating gas includes: Azide
Sodium, ammonium nitrate, 5- Aminotetrazole, nitroguanidine.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the gas manufacture box further includes ignition control list
Member, the ignition control unit control gas manufacture box electric appliance igniting；When aircraft generation flame-out in flight accident, and setting
Time in when unmanned plane can not be made to restore regular flight condition, ignition control unit control gas manufactures box electric appliance point
Fire；Substance, which can decompose rapidly to react, when the ignition control unit executes ignition order, in the gas manufacture box produces
Raw a large amount of N2 gas, gas are filled in air bag rapidly through metal mesh filter, cooling.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, discouraged safety valve is provided on the air bag.
Preferably, in above-mentioned oil electric mixed dynamic manned vehicle, the seat is adjustable height seat.
It can be seen via above technical scheme that compared with prior art, the present disclosure provides a kind of oil electricity mixing is dynamic
Power manned vehicle, high comprehensive performance have preferable flying quality and security performance, can alleviate urban traffic blocking,
It reduces carbon emission and can be realized rapid delivery passenger.Laser ranging controller awing will not for controlling aircraft
Higher than safe altitude, and then improve the safety coefficient of aircraft；Second propeller synchronizing speed distributor ensure that in operating
Two the second propeller speeds are consistent, improve dynamic balancing ability；Center dynamic balance system adjustable lower load-bearing is always maintained at
Center improves dynamic balancing ability of the aircraft in running, further increases safety coefficient；The control system for internal combustion engine can root
Carry out the revolving speed of adjusting internal combustion engine according to power demand；
Cabin rotating electric machine can drive cabin to rotate, and by spherical cabin of verting, can keep in any state of flight
Pilot's line of vision is horizontal, and comfortable stable, meets mankind's driving habit.
By the setting of internal combustion engine and the first propeller, power is provided for aircraft, lifting capacity is strong, and cruise duration is long,
By the setting of battery, motor and the second propeller, it is capable of the flight attitude of quick change of flight device, it is handling good, surely
Qualitative height can also be realized by another power and be force-landed, improve safety, this dress when one of power breaks down
It is good to set both aircraft handlings with pure electric vehicle power, the high advantage of stability, and there is oily power aerial vehicle lifting capacity
By force, long-endurance advantage；
Simultaneously when crashing, swelling gasbag meeting inflation protects the safety of personnel in cabin to greatest extent, due to
Air sac type structure is used, is fallen in lake or rivers even if air crash occurs, air bag is capable of providing enough buoyancy, it is ensured that personnel
The arrival waited for rescue.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawing is overall structure diagram of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The embodiment of the invention discloses a kind of oil electric mixed dynamic manned vehicle, high comprehensive performance has preferable
Flying quality and security performance can alleviate urban traffic blocking, reduce carbon emission and can be realized rapid delivery passenger.
In conjunction with attached drawing 1, the invention discloses a kind of oil electric mixed dynamic manned vehicles, including fuselage body 101 and cabin
Body 2, cabin 2 is spherical in shape, is rotatably arranged on fuselage body 101, and cabin 2 and 101 junction of fuselage body are provided with cabin rotation
Rotating motor 102, for driving the rotation of cabin 2 to realize that cabin 2 is verted when VTOL state is converted to flat winged state；Cabin
2 peripheries are provided with swelling gasbag 103, and the aeration aperture of swelling gasbag 103 is connected by the gas outlet that check valve and gas manufacture box 104
Logical, gas manufacture box 104 is located in cabin 2, and gas manufactures the substance that storage in box 104 generates gas；
The bottom end of cabin 2 is equipped with undercarriage 1, and the side of cabin 2 is equipped with opening, and opening is hinged with hatch door, the inside peace of cabin 2
Equipped with demarcation plate 4 disposed in parallel, the lower section of demarcation plate 4 is equipped with seat 16 and control device 3, and seat 16 and control device 3 are equal
It is mounted on the inner wall bottom end of cabin 2, control device 3 is located at the side of seat 16, and control device 3 includes control handle and control
Case, control handle are mounted on control cabinet, and the inside of control cabinet is equipped with circuit board, and the top of demarcation plate 4 is equipped with battery 5, interior
Combustion engine 14 and fuel tank 13, internal combustion engine 14 is between battery 5 and fuel tank 13, and liquid stream connects between fuel tank 13 and internal combustion engine 14,
The top of cabin 2 is equipped with horn 7 and driving box 11, and horn 7 is located at the side of driving box 11, and the inside of driving box 11 is equipped with machinery
Coupler 6 and gearbox 12, one end of mechanical coupler 6 are connected with gearbox 12, and the other end of mechanical coupler 6 is connected with interior
Combustion engine 14, the output shaft of gearbox 12 are connected with the first propeller 10, and the both ends of horn 7 are mounted on motor 8, and two electronic
Machine 8 is symmetrical arranged, and the output shaft of motor 8 is connected with the second propeller 9, motor 8, cabin rotating electric machine 102 and battery 5
Output end connection；
Control device 3 is electrically connected with laser ranging controller, the second propeller synchronizing speed distributor, center dynamic balance system
And control system for internal combustion engine.
In order to further optimize the above technical scheme, circuit board is equipped with DATA-7311 general purpose controller, wireless transmitter
And wireless receiver, the output end of battery 5 are connected with controller, the output end of controller connects wireless transmitter, gearbox
12 and motor 8, the input terminal of controller be connected with wireless receiver.
In order to further optimize the above technical scheme, control handle is equipped with control button, control button and control device 3
It is electrically connected.
In order to further optimize the above technical scheme, the first propeller 10 is located at the top of the second propeller 9, and the first spiral shell
Rotation paddle 10 and the second propeller 9 are parallel to each other, and the motor 8 that the first propeller 10 and the second propeller 9 are correspondingly arranged is with the
Two propeller synchronizing speed distributors are electrically connected.
In order to further optimize the above technical scheme, armorplate glass, tempering glass are equipped on the surrounding of cabin 2 and hatch door
The junction of glass plate and cabin 2 and hatch door is equipped with sealing ring.
In order to further optimize the above technical scheme, the output shaft of gearbox 12 and the junction of the first propeller 10 are equipped with
Bearing.
In order to further optimize the above technical scheme, the substance for generating gas includes: sodium azide, ammonium nitrate, 5- ammonia
Base tetrazolium, nitroguanidine.
In order to further optimize the above technical scheme, gas manufacture box 104 further includes ignition control unit, ignition control list
Member control gas manufacture box electric appliance igniting；When aircraft generation flame-out in flight accident, and nothing can not be made within the set time
When man-machine recovery regular flight condition, ignition control unit controls gas manufacture box electric appliance igniting；When ignition control unit executes
Substance, which can decompose rapidly to react, when ignition order, in gas manufacture box generates a large amount of N2 gas, and gas is through metal mesh filter, drop
Temperature is filled in air bag rapidly.
In order to further optimize the above technical scheme, discouraged safety valve is provided on swelling gasbag 103.
In order to further optimize the above technical scheme, seat 16 is adjustable height seat.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (10)
1. a kind of oil electric mixed dynamic manned vehicle, including fuselage body (101) and cabin (2), which is characterized in that the cabin
Body (2) is spherical in shape, is rotatably arranged on the fuselage body (101), and the cabin (2) connect with the fuselage body (101)
Place is provided with cabin rotating electric machine (102), for driving the cabin (2) rotation to realize the cabin (2) in VTOL
State is verted when converting to flat winged state；Cabin (2) periphery is provided with swelling gasbag (103), the swelling gasbag (103)
Aeration aperture be connected to by the gas outlet of check valve and gas manufacture box (104), the gas manufactures box (104) and is located at the cabin
In body (2), storage generates the substance of gas in gas manufacture box (104)；
The bottom end of the cabin (2) is equipped with undercarriage (1), and the side of cabin (2) is equipped with opening, and opening is hinged with hatch door
(15), the inside of cabin (2) is equipped with demarcation plate disposed in parallel (4), and the lower section of demarcation plate (4) is equipped with seat (16) and controls
Device (3), seat (16) and control device (3) are installed in the inner wall bottom end of cabin (2), and control device (3) is located at seat
(16) side, the control device (3) include control handle and control cabinet, and control handle is mounted on control cabinet, control cabinet
Inside be equipped with circuit board, the top of the demarcation plate (4) is equipped with battery (5), internal combustion engine (14) and fuel tank (13), internal combustion engine
(14) between battery (5) and fuel tank (13), liquid stream is connected between fuel tank (13) and internal combustion engine (14), the cabin (2)
Top be equipped with horn (7) and driving box (11), horn (7) is located at the side of driving box (11), and the inside of driving box (11) is set
There are mechanical coupler (6) and gearbox (12), one end of mechanical coupler (6) is connected with gearbox (12), mechanical coupler (6)
The other end be connected with internal combustion engine (14), the output shaft of gearbox (12) is connected with the first propeller (10), the horn (7)
Both ends are mounted on motor (8), and two motor (8) are symmetrical arranged, and the output shaft of motor (8) is connected with the second propeller
(9), motor (8), cabin rotating electric machine (102) are connect with the output end of battery (5)；
The control device (3) be electrically connected with laser ranging controller, the second propeller synchronizing speed distributor, in it is aroused in interest flat
Balance system and control system for internal combustion engine.
2. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the circuit board is equipped with
The output end of DATA-7311 general purpose controller, wireless transmitter and wireless receiver, battery (5) is connected with controller, described
The output end of controller connects the wireless transmitter, the gearbox (12) and the motor (8), the input terminal of controller
It is connected with wireless receiver.
3. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the control handle is equipped with
Control button, control button and control device (3) are electrically connected.
4. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that first propeller (10)
Positioned at the top of the second propeller (9), and the first propeller (10) and the second propeller (9) are parallel to each other, first spiral
The motor (8) that paddle (10) and the second propeller (9) are correspondingly arranged is electrically connected with the second propeller synchronizing speed distributor.
5. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the surrounding of the cabin (2)
Be equipped with armorplate glass on hatch door (15), armorplate glass and cabin (2) and the junction of hatch door (15) are equipped with sealing
Circle.
6. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the gearbox (12) it is defeated
The junction of shaft and the first propeller (10) is equipped with bearing.
7. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the substance for generating gas
Include: sodium azide, ammonium nitrate, 5- Aminotetrazole, nitroguanidine.
8. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the gas manufactures box
It (104) further include ignition control unit, the ignition control unit control gas manufacture box electric appliance igniting；When sky occurs for aircraft
Middle parking accident, and can not make within the set time unmanned plane restore regular flight condition when, the ignition control unit
Control gas manufacture box electric appliance igniting；When the ignition control unit executes ignition order, substance in the gas manufacture box
The reaction that can decompose rapidly generates a large amount of N2 gas, and gas is filled in air bag rapidly through metal mesh filter, cooling.
9. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the swelling gasbag (103)
On be provided with discouraged safety valve.
10. oil electric mixed dynamic manned vehicle according to claim 1, which is characterized in that the seat (16) is height
Spend seat chair with adjustable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274934.9A CN109250126A (en) | 2018-10-30 | 2018-10-30 | A kind of oil electric mixed dynamic manned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274934.9A CN109250126A (en) | 2018-10-30 | 2018-10-30 | A kind of oil electric mixed dynamic manned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109250126A true CN109250126A (en) | 2019-01-22 |
Family
ID=65043013
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274934.9A Withdrawn CN109250126A (en) | 2018-10-30 | 2018-10-30 | A kind of oil electric mixed dynamic manned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109250126A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
-
2018
- 2018-10-30 CN CN201811274934.9A patent/CN109250126A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190122 |
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| WW01 | Invention patent application withdrawn after publication |