CN207433793U - The gyroplane that a kind of achievable autorotation starts - Google Patents
The gyroplane that a kind of achievable autorotation starts Download PDFInfo
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- CN207433793U CN207433793U CN201721267249.4U CN201721267249U CN207433793U CN 207433793 U CN207433793 U CN 207433793U CN 201721267249 U CN201721267249 U CN 201721267249U CN 207433793 U CN207433793 U CN 207433793U
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- rotor
- fuselage
- gyroplane
- autorotation
- achievable
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Abstract
The gyroplane that a kind of achievable autorotation disclosed in the utility model starts, including fuselage, control panel is disposed in fuselage from front to back, cockpit and engine, position in fuselage between cockpit and engine is fixedly installed longitudinal rotor bar, rotor bar stretches out in outside fuselage and top is rotatably connected to rotor, rotor includes the blade of two connections that intersect, the junction of two blades is connected by paddle shaft with the top of rotor bar, the rotor of rotor is set towards rear-inclined, the end of rotor is both provided with propulsive mechanism, the rear of fuselage is fixedly connected with tail vane, vertical propeller is provided between tail vane and fuselage, propeller is connected with the output terminal of engine, undercarriage is provided with below fuselage；Propulsive mechanism includes mouse, and mouse is located in the rotor face of rotor, and mouse is fixedly connected with the end of rotor in angle, and mouse is connected to control panel by conducting wire.The utility model can realize that the original place of gyroplane is taken off vertically.
Description
Technical field
The utility model belongs to air equipment technical field, and in particular to the rotor that a kind of achievable autorotation starts
Machine.
Background technology
Gyroplane is a kind of aircraft between helicopter and aircraft, it is removed outside rotor, also secondary vertical with one
The propeller of placement can also awing provide part lift to provide the power of advance equipped with smaller wing.Gyroplane
Maximum difference with helicopter is that the rotor of gyroplane is not connected with engine driving system, and engine is not to drive rotor
Lift is provided for gyroplane, but during gyroplane flies, rotor wing rotation is blown by front air-flow and generates lift, as one
Windmill.Awing, gyroplane with helicopter be most significantly respectively helicopter rotor towards top rake, and gyroplane
Rotor is then sweptback.Since the rotor of gyroplane is that do not have dynamic, it is not due to power drive rotor system
The larger vibration and noise that regiment commander comes also would not make the service life of rotor, body etc. contract due to this vibration and noise
Fatigue that is short or increasing occupant.But the power that existing gyroplane is provided due to no engine, it is usually needed when taking off
It slides and runs a distance so that rotor is subject to the effect of front air-flow power to generate lift, for the field that place space is limited
Suffer from larger use limitation.
Utility model content
The purpose of this utility model is to provide the gyroplanes that a kind of achievable autorotation starts, and solve existing rotation
Wing machine is limited the problem of larger by take-off venue.
Technical solution is used by the utility model：The gyroplane that a kind of achievable autorotation starts, including fuselage,
Control panel, cockpit and engine, the interior position between cockpit and engine of fuselage are disposed in fuselage from front to back
It puts and is fixedly installed longitudinal rotor bar, rotor bar is stretched out in outside fuselage and top is rotatably connected to rotor, and rotor includes two
Intersect the blade of connection, and the junction of two blades is connected by paddle shaft with the top of rotor bar, the rotor of rotor towards
Rear-inclined is set, and the end of rotor is both provided with propulsive mechanism, and the rear of fuselage is fixedly connected with tail vane, between tail vane and fuselage
Vertical propeller is provided with, propeller is connected with the output terminal of engine, and undercarriage is provided with below fuselage；Pusher
Structure includes mouse, and mouse is located in the rotor face of rotor, and mouse is fixedly connected with the end of rotor in angle, mouse
Control panel is connected to by conducting wire.
The utility model is also characterized by
The end vertical of mouse and rotor.
Position in fuselage between control panel and cockpit is provided with control stick.
Undercarriage includes the rear undercarriage below nose-gear and fuselage afterbody below fore-body, and rear undercarriage is set
There are two, undercarriage is connected with each other and is separately positioned on the opposite position in fuselage both sides after two.
Engine is driving motor or piston-mode motor.
Horizontal drive clutch is connected between engine and propeller.
Cockpit set there are two, two cockpits in fuselage in tandem.
The beneficial effects of the utility model are：The gyroplane that a kind of achievable autorotation of the utility model starts, passes through
Propulsive mechanism is set in the end of rotor, and the thrust that propulsive mechanism is generated in rotor face causes autorotation and then generates rotor
Lift can realize that the original place of gyroplane is taken off vertically.Without generating air-flow by sliding race or waiting big wind speed come quilt
Movable property gives birth to lift, for widely using with positive meaning for gyroplane.
Description of the drawings
Fig. 1 is the structure diagram for the gyroplane that a kind of achievable autorotation of the utility model starts；
Fig. 2 is the top view of the gyroplane that a kind of achievable autorotation of the utility model starts in Fig. 1.
In figure, 1. fuselages, 2. control panels, 3. cockpits, 4. engines, 5. rotor bars, 6. rotors, 7. tail vanes, 8. spirals
Paddle, 9. mouses, 10. blades, 11. control sticks, 12. nose-gears, undercarriage after 13..
Specific embodiment
Below in conjunction with the accompanying drawings and the utility model is described in detail in specific embodiment.
The utility model provides the gyroplane that a kind of achievable autorotation starts, as depicted in figs. 1 and 2, including machine
Body 1 is disposed with control panel 2, cockpit 3 and engine 4 in fuselage 1 from front to back, there are two cockpit 3 is set, two seats
In fuselage 1 in tandem, engine 4 is driving motor or piston-mode motor, is located at control panel 2 and seat in fuselage 1 in cabin 3
Position between cabin 3 is provided with control stick 11, and the interior position between cockpit 3 and engine 4 of fuselage 1 is fixedly installed longitudinal direction
Rotor bar 5, rotor bar 5 stretches out in that fuselage 1 is outer and top is rotatably connected to rotor 6, and the rotor of rotor 6 is set towards rear-inclined
It puts, rotor 6 includes the blade 10 of two connections that intersect, and the junction of two blades 10 passes through paddle shaft and the top of rotor bar 5
End connection, the end of rotor 6 are both provided with propulsive mechanism, and propulsive mechanism includes mouse 9, and mouse is located at the rotor of rotor 6
In face, mouse 9 is fixedly connected with the end of rotor 6 in angle, when the end vertical of mouse 9 and rotor 6, i.e. mouse
Tangential direction of 9 thrusts generated along rotor face, the direction of rotation thrust that rotor 6 is subject at this time is maximum, and mouse 9 passes through conducting wire
Control panel 2 is connected to, the start and stop of mouse 9 are controlled by control panel 2, the rear of fuselage 1 is fixedly connected with tail vane 7, tail
Vertical propeller 8 is provided between rudder 7 and fuselage 1, propeller 8 is connected with the output terminal of engine 4, engine 4 and spiral shell
Horizontal drive clutch can also be connected between rotation paddle 8, the lower section of fuselage 1 is provided with undercarriage, and undercarriage includes 1 forepart of fuselage
The rear undercarriage 13 of 1 lower rear of nose-gear 12 and fuselage of lower section, there are two the rear settings of undercarriage 13, undercarriage after two
13 are connected with each other and are separately positioned on the opposite position in 1 both sides of fuselage.
In use, when the place in limited space, by control panel 2 mouse 9 is controlled to start, mouse 9 generates
Rotor face in propulsive force rotor 6 is rotated, and then generate lift, namely it is not when gyroplane rises one section of height
When being limited again be subject to ground space, control mouse 9 stops, and engine 4, which works, afterwards makes propeller 8 rotate generation level
Thrust promotes gyroplane flight forward, and during gyroplane flight forward, the rotor 6 of hypsokinesis generates whole lift, so as to
Meet the movement of gyroplane front-rear direction and vertical direction.
By the above-mentioned means, the gyroplane that a kind of achievable autorotation of the utility model starts, by the end of rotor 6
Head sets propulsive mechanism, and the thrust that propulsive mechanism generates in rotor face causes 6 rotation of rotor and then rotor 6 is made to generate lift, can
It is taken off vertically with the original place for realizing gyroplane.Without generating air-flow by sliding race or big wind speed being waited passively to generate liter
Power, for widely using with positive meaning for gyroplane.
Claims (7)
1. the gyroplane that a kind of achievable autorotation starts, which is characterized in that including fuselage (1), fuselage (1) is interior from front to back
Control panel (2), cockpit (3) and engine (4) are disposed with, fuselage (1) is interior between cockpit (3) and engine (4)
Position be fixedly installed longitudinal rotor bar (5), rotor bar (5) stretches out in fuselage (1) outside and top is rotatably connected to rotor
(6), rotor (6) includes the blade (10) of two connections that intersect, and the junction of two blades (10) passes through paddle shaft and rotor
The top connection of bar (5), the rotor of rotor (6) are set towards rear-inclined, and the end of rotor (6) is both provided with propulsive mechanism, machine
The rear of body (1) is fixedly connected with tail vane (7), and vertical propeller (8), propeller are provided between tail vane (7) and fuselage (1)
(8) output terminal with engine (4) is connected, and fuselage is provided with undercarriage below (1)；Propulsive mechanism includes mouse (9),
Mouse is located in the rotor face of rotor (6), and mouse (9) is fixedly connected with the end of rotor (6) in angle, mouse (9)
Control panel (2) is connected to by conducting wire.
2. the gyroplane that a kind of achievable autorotation as described in claim 1 starts, which is characterized in that the mouse
(9) with the end vertical of rotor (6).
3. the gyroplane that a kind of achievable autorotation as described in claim 1 starts, which is characterized in that the fuselage (1)
The interior position between control panel (2) and cockpit (3) is provided with control stick (11).
4. the gyroplane that a kind of achievable autorotation as described in claim 1 starts, which is characterized in that the undercarriage bag
The nose-gear (12) of fuselage (1) lower front and the rear undercarriage (13) of fuselage (1) lower rear are included, rear undercarriage (13) sets
There are two putting, undercarriage (13) is connected with each other and is separately positioned on the opposite position in fuselage (1) both sides after two.
5. the gyroplane that a kind of achievable autorotation as described in claim 1 starts, which is characterized in that the engine
(4) it is driving motor or piston-mode motor.
6. the gyroplane that a kind of achievable autorotation as described in claim 1 or 5 starts, which is characterized in that described to start
Horizontal drive clutch is connected between machine (4) and propeller (8).
7. the gyroplane that a kind of achievable autorotation as described in claim 1 starts, which is characterized in that the cockpit (3)
There are two settings, and two cockpits (3) are interior in tandem in fuselage (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721267249.4U CN207433793U (en) | 2017-09-28 | 2017-09-28 | The gyroplane that a kind of achievable autorotation starts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721267249.4U CN207433793U (en) | 2017-09-28 | 2017-09-28 | The gyroplane that a kind of achievable autorotation starts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207433793U true CN207433793U (en) | 2018-06-01 |
Family
ID=62295518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721267249.4U Active CN207433793U (en) | 2017-09-28 | 2017-09-28 | The gyroplane that a kind of achievable autorotation starts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207433793U (en) |
-
2017
- 2017-09-28 CN CN201721267249.4U patent/CN207433793U/en active Active
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