CN206394895U - Oil electric mixed dynamic rotor manned aircraft - Google Patents
Oil electric mixed dynamic rotor manned aircraft Download PDFInfo
- Publication number
- CN206394895U CN206394895U CN201621390318.6U CN201621390318U CN206394895U CN 206394895 U CN206394895 U CN 206394895U CN 201621390318 U CN201621390318 U CN 201621390318U CN 206394895 U CN206394895 U CN 206394895U
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- nacelle
- propeller
- mixed dynamic
- oil electric
- electric mixed
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Abstract
The utility model discloses oil electric mixed dynamic rotor manned aircraft, including nacelle, the bottom of the nacelle is provided with undercarriage, the side of nacelle is provided with opening, hatch door is hinged with opening, the inside of nacelle is provided with the demarcation strip be arrangeding in parallel, the lower section of demarcation strip is provided with seat and control device, seat and control device are installed in the inwall bottom of nacelle, control device is located at the side of seat, the control device includes joystick and control cabinet, joystick is arranged on control cabinet, the inside of control cabinet is provided with circuit board, the top of the demarcation strip is provided with battery, internal combustion engine and fuel tank, internal combustion engine is located between battery and fuel tank, the interstitial fluid stream connection of fuel tank and internal combustion engine, the top of the nacelle is provided with horn and driving box.The utility model both had pure electrodynamic aircraft handling good, the high advantage of stability, had oily power aerial vehicle lifting capacity strong again, long-endurance advantage.
Description
Technical field
The utility model is related to vehicle technology field, more particularly to oil electric mixed dynamic rotor manned aircraft.
Background technology
The mankind have the ideal flown in the air as birds very early, for a long time, and the mankind are most for the fantasy that can fly up into the sky
Various methods, with the continuous development of scientific technology, dream that the mankind fly in the air become reality, existing most of
Aircraft is mainly used in scientific research, and cost is sufficiently expensive, is not particularly suited for masses, with the popularization of aircraft, operation letter
Singly, arisen at the historic moment using flexible manned vehicle, the existing pure electrodynamic aircraft flight time is short, is short of power, holds
Weight ability, and many rotor flying stability of oily power are poor, response speed is slow, it is impossible to meet rapid control rotor manned aircraft
The requirement of flight attitude, is this it is proposed that a kind of oil electric mixed dynamic rotor manned flies.
Utility model content
The purpose of this utility model is and the oil electric mixed dynamic rotation proposed in order to solve shortcoming present in prior art
Wing manned vehicle.
To achieve these goals, the utility model employs following technical scheme：
Oil electric mixed dynamic rotor manned aircraft, including nacelle, the bottom of the nacelle are provided with undercarriage, the one of nacelle
Side is provided with opening, opening and is hinged with hatch door, and the inside of nacelle is provided with the demarcation strip be arrangeding in parallel, and the lower section of demarcation strip is provided with
Seat and control device, seat and control device are installed in the inwall bottom of nacelle, and control device is located at the side of seat, institute
Stating control device includes joystick and control cabinet, and joystick is arranged on control cabinet, and the inside of control cabinet is provided with circuit board,
The top of the demarcation strip is provided with battery, internal combustion engine and fuel tank, and internal combustion engine is located between battery and fuel tank, fuel tank and internal combustion
The interstitial fluid stream connection of machine, the top of the nacelle is provided with horn and driving box, and horn is located at the side of driving box, driving box it is interior
Portion is provided with mechanical coupler and engine, and one end of mechanical coupler is connected with engine, the other end connection of mechanical coupler
There is internal combustion engine, the output shaft of engine is connected with the first propeller, and the two ends of the horn are mounted on motor, and two electronic
Machine is symmetrical arranged, and the output shaft of motor is connected with the second propeller, the output end connection of motor and battery.
It is preferred that, the circuit board is provided with DATA-7311 general purpose controllers, wireless launcher and wireless receiver, stores
The output end of battery is connected with controller, and the output end of control is connected with wireless launcher, engine and motor, controller
Input is connected with wireless receiver.
It is preferred that, the joystick is provided with control button, and control button is connected with controller.
It is preferred that, first propeller is located at the top of the second propeller, and the first propeller and the second propeller phase
It is mutually parallel.
It is preferred that, armorplate glass, armorplate glass and nacelle and hatch door are equipped with the surrounding and hatch door of the nacelle
Junction be equipped with sealing ring and glue.
It is preferred that, the junction of the output shaft of the engine and the first propeller is provided with bearing.
The beneficial effects of the utility model：By the setting of internal combustion engine, engine and the first propeller, provided for aircraft
Power, lifting capacity is strong, and cruising time is long, by the setting of battery, motor and the second propeller, can quickly change winged
The flight attitude of row device, handling good, stability is high, when one of which power breaks down, can also pass through another power
Forced landing is realized, security is improved, the present apparatus both had pure electrodynamic aircraft handling good, the high advantage of stability,
Have oily power aerial vehicle lifting capacity strong again, long-endurance advantage.
Brief description of the drawings
Fig. 1 be the utility model proposes oil electric mixed dynamic rotor manned aircraft structural representation；
Fig. 2 be the utility model proposes oil electric mixed dynamic rotor manned aircraft systematic schematic diagram.
In figure：It is 1 undercarriage, 2 nacelles, 3 control devices, 4 demarcation strips, 5 batteries, 6 mechanical couplers, 7 horns, 8 electronic
Machine, 9 second propellers, 10 first propellers, 11 driving box, 12 engines, 13 fuel tanks, 14 internal combustion engines, 15 hatch doors, 16 seats.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.
Reference picture 1-2, oil electric mixed dynamic rotor manned aircraft, including nacelle 2, the bottom of nacelle 2 are provided with undercarriage
1, the side of nacelle 2, which is provided with opening, opening, is hinged with hatch door 15, and the inside of nacelle 2 is provided with the demarcation strip 4 be arrangeding in parallel,
The lower section of demarcation strip 4 is provided with seat 16 and control device 3, and seat 16 and control device 3 are installed in the inwall bottom of nacelle 2,
Control device 3 is located at the side of seat 16, and the control device 3 includes joystick and control cabinet, and joystick is arranged on control
On case processed, the inside of control cabinet is provided with circuit board, and the top of the demarcation strip 4 is provided with battery 5, internal combustion engine 14 and fuel tank 13,
Internal combustion engine 14 is located between battery 5 and fuel tank 13, the interstitial fluid stream connection of fuel tank 13 and internal combustion engine 14, the top of the nacelle 2
Provided 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 provided with mechanical coupler 6 and hair
Motivation 12, one end of mechanical coupler 6 is connected with engine 12, and the other end of mechanical coupler 6 is connected with internal combustion engine 14, started
The output shaft of machine 12 is connected with the first propeller 10, and the two ends of the horn 7 are mounted on motor 8, and two motor 8 are symmetrical
Set, the output shaft of motor 8 is connected with the second propeller 9, and motor 8 is connected with the output end of battery 5, set on circuit board
There are DATA-7311 general purpose controllers, wireless launcher and wireless receiver, the output end of battery 5 is connected to controller
With motor 8, the output end of control is connected with wireless launcher, engine 12 and motor 8, and the input of controller is connected with
Wireless receiver, joystick is provided with control button, and control button is connected with controller, and the first propeller 10 is located at the second spiral shell
The top of oar 9 is revolved, and the first propeller 10 and the second propeller 9 are parallel to each other, and steel is equipped with the surrounding and hatch door 15 of nacelle 2
Change glass plate, the junction of armorplate glass and nacelle 2 and hatch door 15 is equipped with sealing ring and glue, the surrounding of nacelle 2 and cabin
Armorplate glass is equipped with door 15, the junction of armorplate glass and nacelle 2 and hatch door 15 is equipped with sealing ring and glue, sends out
The junction of the output shaft of motivation 12 and the first propeller 10 is provided with bearing.
Operation principle：Instruction is sent by the button on joystick, controller is received after instruction, controls the band of internal combustion engine 14
The dynamic propeller 10 of engine 12 and first works, and drives aircraft takeoff, and control motor 8 drives the second propeller 9 to work, adjusted
Whole flight attitude, it is ensured that the stability of aircraft, when one of which power breaks down, is realized by another power and compeled
Drop, improves security, can also be manipulated by ground staff, and ground staff sends instruction, and controller is connect by wireless launcher
Instruction is received, aircraft operation is then controlled, while wireless launcher feedback is instructed, realizes remote control.
It is described above, only the utility model preferably embodiment, but protection domain of the present utility model is not
This is confined to, any one skilled in the art is in the technical scope that the utility model is disclosed, according to this practicality
New technical scheme and its utility model design are subject to equivalent substitution or change, should all cover in protection model of the present utility model
Within enclosing.
Claims (7)
1. oil electric mixed dynamic rotor manned aircraft, including nacelle (2), it is characterised in that the bottom of the nacelle (2) is provided with
Undercarriage (1), the side of nacelle (2), which is provided with opening, opening, is hinged with hatch door (15), and the inside of nacelle (2) is provided with parallel
The demarcation strip (4) of setting, the lower section of demarcation strip (4) is provided with seat (16) and control device (3), seat (16) and control device
(3) the inwall bottom of nacelle (2) is installed in, control device (3) is located at the side of seat (16), control device (3) bag
Joystick and control cabinet are included, joystick is arranged on control cabinet, the inside of control cabinet is provided with circuit board, the demarcation strip
(4) top is provided with battery (5), internal combustion engine (14) and fuel tank (13), and internal combustion engine (14) is located at battery (5) and fuel tank (13)
Between, the interstitial fluid stream connection of fuel tank (13) and internal combustion engine (14), the top of the nacelle (2) is provided 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 provided with mechanical coupler (6) and engine
(12), one end of mechanical coupler (6) is connected with engine (12), and the other end of mechanical coupler (6) is connected with internal combustion engine
(14), the output shaft of engine (12) is connected with the first propeller (10), and the two ends of the horn (7) are mounted on motor
(8), two motor (8) are symmetrical arranged, and the output shaft of motor (8) is connected with the second propeller (9), and motor (8) is with storing
The output end connection of battery (5).
2. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that set on the circuit board
There are DATA-7311 general purpose controllers, wireless launcher and wireless receiver, the output end of battery (5) is connected with controller, control
The output end of system is connected with wireless launcher, engine (12) and motor (8), and the input of controller is connected with wireless receiving
Device.
3. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that on the joystick
Provided with control button, control button is connected with controller.
4. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that first propeller
(10) it is located at the top of the second propeller (9), and the first propeller (10) and the second propeller (9) are parallel to each other.
5. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that the nacelle (2)
Armorplate glass is equipped with surrounding and hatch door (15), armorplate glass and the junction of nacelle (2) and hatch door (15) are equipped with
Sealing ring and glue.
6. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that the nacelle (2)
Armorplate glass is equipped with surrounding and hatch door (15), armorplate glass and the junction of nacelle (2) and hatch door (15) are equipped with
Sealing ring and glue.
7. oil electric mixed dynamic rotor manned aircraft according to claim 1, it is characterised in that the engine (12)
Output shaft and the first propeller (10) junction be provided with bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621390318.6U CN206394895U (en) | 2016-12-15 | 2016-12-15 | Oil electric mixed dynamic rotor manned aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621390318.6U CN206394895U (en) | 2016-12-15 | 2016-12-15 | Oil electric mixed dynamic rotor manned aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206394895U true CN206394895U (en) | 2017-08-11 |
Family
ID=59512390
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621390318.6U Active CN206394895U (en) | 2016-12-15 | 2016-12-15 | Oil electric mixed dynamic rotor manned aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206394895U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250081A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of hybrid power helicopter |
-
2016
- 2016-12-15 CN CN201621390318.6U patent/CN206394895U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250081A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of hybrid power helicopter |
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