CN205524948U - Unmanned autogyro - Google Patents
Unmanned autogyro Download PDFInfo
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- CN205524948U CN205524948U CN201620255375.7U CN201620255375U CN205524948U CN 205524948 U CN205524948 U CN 205524948U CN 201620255375 U CN201620255375 U CN 201620255375U CN 205524948 U CN205524948 U CN 205524948U
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- steering wheel
- control
- rotor
- autogyro
- control steering
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Abstract
The utility model relates to an unmanned autogyro, the rotor head is connected to frame (1) of gyroplane upper end, and the overhead side of rotor installs complete machine parachute (15), and rotor (4) are installed on rotor head both sides, and engine (3) are located between tail vane (6) and fuselage (2), still is provided with screw (5) in the one end of engine, is provided with throttle control steering wheel (7) at the perpendicular roof beam intermediate position of frame (1), throttle control steering wheel (7) lower extreme is provided with a pair of every single move roll control steering engine (8), is provided with undercarriage (14) in the bottom of fuselage (2) the inside of fuselage (2) leans on every single move roll control steering engine's (8) one end to be provided with flight control (11) the bottom end rail front end of frame (1) is provided with brake control steering engine (10) brake control steering engine's (10) rear end is provided with direction control steering engine (9) directional control steering wheel (9) are used for controlling the direction of front wheel and tail vane, the front wheel and for the tail vane steel cable link to each other, receive directional control steering wheel (9) control simultaneously.
Description
Technical field
This utility model relates to field of aviation flight, particularly relates to unmanned autogyro.
Background technology
Along with the appearance of the progressive internal combustion engine of industrial technology, machine enhances the physical ability of people, and we fly to from ground in the air.
After the appearance of computer, information technology enhances again the intelligence of people so that aircraft is from having people to unmanned conversion.The appearance of unmanned plane,
Being exactly the development of technology, let us returns to ground from the air again, and machine is stayed in the air, goes the past to have man-machine completing
Mission.Therefore, " unmanned plane " is not genuine " unmanned ", but people is in the loop, by people's supervision, manages direct remote control and flies
Machine.The unmanned autogyro of my company's development and design, belongs to the world and initiates, open the new page of unmanned autogyro.
Unmanned autogyro is that relative wind blows autorotation to produce the rotor class of lift when flying before a kind of utilization
Airborne vehicle, including frame, fuselage, electromotor, rotor, complete machine parachute, propeller, tail vane, steering engine actuator, flight controls
System, undercarriage, frame upper end connects rotor, and electromotor, between tail vane and control cabinet, is provided with flight control in control cabinet
System, performs steering wheel and is connected with rotor head by controlling connecting rod, and electromotor is connected with propeller, under frame by change gear box
Side is provided with undercarriage, and described rotor is for be made up of two or more rotary blades, and rotary blade is fixed on the rotor head of frame upper end
On, rotor head top is provided with complete machine parachute.Unmanned autogyro safety is high, landing apart from short, stability is high, wind resistance
Property strong, load is big, be prone to dispose, have a highest cost performance simultaneously.
Summary of the invention
The purpose of this utility model is to overcome the deficiency of existing unmanned plane, it is provided that a kind of good stability, work safety system
Number height, load is big, boat duration, and wind resistance is strong, have the unmanned autogyro of relatively high performance-price ratio, and its total take-off weight 400 is public
More than Jin, mission payload more than 150 kilograms, during boat more than 4 hours.
A kind of unmanned autogyro, frame (1) upper end of described gyroplane connects rotor head, and rotor head is arranged above
Complete machine parachute (15), rotor head both sides are provided with rotor (4), and electromotor (3) is positioned between tail vane (6) and fuselage (2), are sending out
One end of motivation is additionally provided with propeller (5), is provided with Throttle Opening Control steering wheel (7) in the vertical beam centre position of frame (1), described
Throttle Opening Control steering wheel (7) lower end is provided with a pair pitching control of sideward roll steering wheel (8), and the bottom of fuselage (2) is provided with undercarriage
(14), in the inside of described fuselage (2), the one end by pitching control of sideward roll steering wheel (8) is provided with flight control system (11),
The sill front end of described frame (1) is provided with brake and controls steering wheel (10), and the rear end controlling steering wheel (10) in described brake sets
It is equipped with direction controlling steering wheel (9) described direction controlling steering wheel (9) and is used for controlling the direction of front-wheel and tail vane, front-wheel and tail vane steel
Cable is connected, and is controlled by direction control flaps machine (9) simultaneously.
Described flight control system is including gyro, accelerometer, pressure-altitude sensor, airspeed sensor and GPS
Unmanned plane whole process self-control system.
Described unmanned gyroplane sends control signals to data radio station by ground control computer, and data radio station leads to again
Crossing antenna and send a signal to airborne antenna again, airborne antenna sends signal to airborne data radio station, and airborne data radio station is again
Sending a signal to flight control system, controlled Throttle Opening Control steering wheel by flight control system respectively, brake controls steering wheel,
Pitching control of sideward roll steering wheel, direction controlling steering wheel and multiple mission payload control steering wheel.
Autogyro be a kind of using autorotating rotor as lifting surface, propeller as onward impulse rotor class fly
Device.Autogyro is actually a kind of aircraft between helicopter and fixed wing airplane, and it removes outside rotor, also carries
There is a secondary propeller to provide the power advanced.Autogyro with the maximum difference of helicopter is, the rotor of autogyro
Not being connected with engine driving system, electromotor simply drives propeller to provide forward thrust for aircraft, but flies at gyroplane
During row, front air-flow blow the raw lift of rotor wing rotation movable property.And the rotor of helicopter and engine driving system phase
Even, lift can be produced, be provided that again the power of flight.Owing to the rotor of autogyro is rotation type, it is delivered on fuselage
Moment of torsion the least, therefore autogyro is without tail-rotor as helicopter, but is generally equipped with tail vane, to control flight appearance
State.
Have the beneficial effect that
1, safety is high
Owing to the rotor head of gyroplane is arranged above complete machine parachute, awing stop if there is in engine air
Car, or other mechanical breakdowns, flight control system automatically detects and enters emergency flight control pattern, sending instruction unpack parachute
Aircraft safety is made to land.
2, landing is apart from short
Autogyro has individual distinguishing feature, it is simply that its distance of landing run is substantially shorter than takeoff distance, very
To handling well and can not slide race landing on the spot.
3, stability is high, and wind resistance is strong
The gyroplane flight training handbook of the U.S. is said: " stability of gyroplane is the highest in all airborne vehicles ".It can be certainly
Dynamic regulation, makes fuselage have good pitching stability, roll stability and speed stability.
It is that wind loading rating is high that autogyro is different from the great advantage of other class aircraft, and when taking off, it is also
Like there is wind.For autogyro, wind is conducive to the starting of rotor and accelerates to rotate, and can shorten the distance of sliding race,
When reaching sufficiently large wind speed, general autogyro can also need not sliding race standing start.
4, there is the highest cost performance
Owing to autogyro is simple relative to helicopter structure, there is no tail-rotor drive system, decelerator, auto-bank unit
With main-rotor drive system, so not only price is low, and fault rate is the lowest.In addition working service is simple and convenient, required expense
The lowest.Its handy, safe and convenient feature of autogyro so that it is will occupy in following airborne vehicle family seat it
Ground.
Accompanying drawing explanation
Fig. 1 is unmanned autogyro structure chart；
Fig. 2 is control station system structure.
1, frame, 2, casing, 3, electromotor, 4, rotary blade, 5, propeller, 6, rudder,
7, Throttle Opening Control steering wheel, 8, pitching control of sideward roll steering wheel,
9, direction controlling steering wheel, 10, brake control steering wheel, 11, flight control system, 12, airborne station, 13, sky, radio station
Line, 14, undercarriage, 15, complete machine parachute, 16, ground control computer；17, for data radio station；18 pass antenna for number.
Detailed description of the invention
The utility model will be further described below in conjunction with the accompanying drawings.
Unmanned autogyro, frame (1) upper end of described gyroplane connects rotor head, and rotor head is arranged above complete machine
Parachute (15), rotor head both sides are provided with rotor (4), and electromotor (3) is positioned between tail vane (6) and fuselage (2), at electromotor
One end be additionally provided with propeller (5), be provided with in the vertical beam centre position of frame (1) Throttle Opening Control steering wheel (7) be used for control
The accelerator open degree of electromotor, described Throttle Opening Control steering wheel (7) lower end is provided with a pair pitching control of sideward roll steering wheel (8), oar dish control
Steering wheel processed is two, and the both sides controlling rotor head respectively control connecting rod, is responsible for controlling rotor disk pitching and roll action, at machine
The bottom of body (2) is provided with undercarriage (14), and in the inside of described fuselage (2), the one end by pitching control of sideward roll steering wheel (8) sets
It is equipped with flight control system (11), is provided with brake in the sill front end of described frame (1) and controls steering wheel (10), be used for controlling
The rear wheel brake installed on rear undercarriage, the rear end controlling steering wheel (10) in described brake is provided with direction controlling steering wheel (9) institute
Stating direction controlling steering wheel (9) and be used for controlling the direction of front-wheel and tail vane, front-wheel is connected with tail vane wirerope, simultaneously by direction controlling
Steering wheel (9) controls.
Described flight control system is including gyro, accelerometer, pressure-altitude sensor, airspeed sensor and GPS
Unmanned plane whole process self-control system.
Described unmanned gyroplane sends control signals to data radio station by ground control computer, and data radio station leads to again
Crossing antenna and send a signal to airborne antenna again, airborne antenna sends signal to airborne data radio station, and airborne data radio station is again
Sending a signal to flight control system, controlled Throttle Opening Control steering wheel by flight control system respectively, brake controls steering wheel,
Pitching control of sideward roll steering wheel, direction controlling steering wheel and multiple mission payload control steering wheel.
Unmanned autogyro is a kind of to fly as the rotor class of onward impulse using autorotating rotor as lifting surface, propeller
Row device.Autogyro is actually a kind of aircraft between helicopter and fixed wing airplane, and it removes outside rotor, also
With a secondary propeller to provide the power advanced.Autogyro with the maximum difference of helicopter is, the rotation of autogyro
The wing is not connected with engine driving system, and electromotor simply drives propeller to provide forward thrust for aircraft, but at gyroplane
During flight, front air-flow blow the raw lift of rotor wing rotation movable property.And the rotor of helicopter and engine driving system
It is connected, lift can be produced, be provided that again the power of flight.Owing to the rotor of autogyro is rotation type, it is delivered to fuselage
On moment of torsion the least, therefore autogyro is without tail-rotor as helicopter, but is generally equipped with tail vane, to control flight appearance
State.
It is last that it is noted that obviously above-described embodiment is only for clearly demonstrating the application example, and also
The non-restriction to embodiment.For those of ordinary skill in the field, can also do on the basis of the above description
Go out change or the variation of other multi-form.Here without also cannot all of embodiment be given exhaustive.And thus drawn
What Shen went out obviously changes or among the variation protection domain still in the application type.
Claims (4)
- The most unmanned autogyro, it is characterised in that: frame (1) upper end of described gyroplane connects rotor head, above rotor head Being provided with complete machine parachute (15), rotor head both sides are provided with rotor (4), electromotor (3) be positioned at tail vane (6) and fuselage (2) it Between, it is additionally provided with propeller (5) in one end of electromotor, the vertical beam centre position of frame (1) is provided with Throttle Opening Control steering wheel (7), described Throttle Opening Control steering wheel (7) lower end is provided with a pair pitching control of sideward roll steering wheel (8), arranges in the bottom of fuselage (2) Having undercarriage (14), in the inside of described fuselage (2), the one end by pitching control of sideward roll steering wheel (8) is provided with flight control system (11), it is provided with brake in the sill front end of described frame (1) and controls steering wheel (10), control steering wheel (10) in described brake Rear end is provided with direction controlling steering wheel (9) described direction controlling steering wheel (9) and is used for controlling the direction of front-wheel and tail vane, front-wheel and tail Rudder wirerope is connected, and is controlled by direction control flaps machine (9) simultaneously.
- Unmanned autogyro the most according to claim 1, it is characterised in that: described flight control system include gyro, Accelerometer, pressure-altitude sensor, airspeed sensor and GPS.
- Unmanned autogyro the most according to claim 1, it is characterised in that: described gyroplane controls to calculate by ground Machine sends control signals to data radio station, and data radio station sends a signal to airborne antenna, airborne antenna again by antenna again Sending signal to airborne data radio station, airborne data radio station sends a signal to flight control system again, by flight control System controls Throttle Opening Control steering wheel respectively, and brake controls steering wheel, pitching control of sideward roll steering wheel, direction controlling steering wheel and multiple Mission payload controls steering wheel.
- Unmanned autogyro the most according to claim 1, it is characterised in that: this unmanned autogyro is always to play fly weight Amount is more than 400 kilograms, mission payload more than 150 kilograms, the technical grade of more than 4 hours large-scale unmanned plane during boat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620255375.7U CN205524948U (en) | 2016-03-30 | 2016-03-30 | Unmanned autogyro |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620255375.7U CN205524948U (en) | 2016-03-30 | 2016-03-30 | Unmanned autogyro |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205524948U true CN205524948U (en) | 2016-08-31 |
Family
ID=56786724
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620255375.7U Expired - Fee Related CN205524948U (en) | 2016-03-30 | 2016-03-30 | Unmanned autogyro |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205524948U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818971A (en) * | 2016-03-30 | 2016-08-03 | 河南三和航空工业有限公司 | Unmanned gyroplane |
| CN109703747A (en) * | 2018-12-29 | 2019-05-03 | 东北农业大学 | Small-sized oil moves unmanned autorotating rotor flight instruments |
-
2016
- 2016-03-30 CN CN201620255375.7U patent/CN205524948U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818971A (en) * | 2016-03-30 | 2016-08-03 | 河南三和航空工业有限公司 | Unmanned gyroplane |
| CN109703747A (en) * | 2018-12-29 | 2019-05-03 | 东北农业大学 | Small-sized oil moves unmanned autorotating rotor flight instruments |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160831 Termination date: 20210330 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |