Automatically operating mechanism for parasol

An automatic control and parafoil technology, applied in the direction of motor vehicles, manned aircraft, aircraft, etc., can solve the problems of safety accidents, failure to realize, and the danger of operators, to prevent ice inside the fuselage, prevent rain or air pollution, etc. Accurate effects of sand, dust and flight operations

Inactive Publication Date: 2009-09-30
贵州贵航无人机有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, many existing paragliders adopt the manned control mode. When performing high-risk flight tasks, due to the influence of human factors such as the operator's driving skills and emotions, it is easy to cause safety accidents. This makes Operators are at greater risk when flying
In order to overcome this defect, some paragliders have been modified to be piloted remotely by ground personnel, but because the remote control method requires a certain reaction time, the possibility of error during manipulation is relatively high, making it difficult to complete more complex flight tasks ; and the remote control mode limits the distance between the paraglider and the ground personnel, so that this type of remote piloted paraglider cannot complete long-distance precise flight tasks
Like this, in order to fly safely, long-distance and accurately for the paraglider, people expect to install a kind of automatic control mechanism on the paraglider to solve the above problems, but it has not been realized yet.

Method used

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  • Automatically operating mechanism for parasol
  • Automatically operating mechanism for parasol
  • Automatically operating mechanism for parasol

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0018] Embodiment 1 of the present invention: the automatic control mechanism of this umbrella wing aircraft is as figure 1 , 3As shown, it includes the umbrella wing 1 of the existing umbrella wing machine structure, the umbrella rope 2 connected to the two ends of the umbrella wing 1, the hanging umbrella rope 3 connected to the lower end of the umbrella wing rope 2, the umbrella rope 3 connected with the hanging umbrella rope Fuselage 4 and the engine installed on the fuselage 4, the airborne control system that is made up of flight control system, navigation system, flight attitude sensor and radio remote control telemetry and information transmission system is contained on the fuselage 4, to paraglider The flight is carried out calculation control; the parachute control connection mechanism capable of manipulating the parasol 1 and the engine throttle control mechanism capable of manipulating the engine are installed on the fuselage 4, and the output of the flight control...

Embodiment 2

[0021] Embodiment 2 of the present invention: the automatic control mechanism of this umbrella wing aircraft is as figure 2 , 3 As shown, it includes the umbrella wing 1 of the existing umbrella wing machine structure, the umbrella rope 2 connected to the two ends of the umbrella wing 1, the hanging umbrella rope 3 connected to the lower end of the umbrella wing rope 2, the umbrella rope 3 connected with the hanging umbrella rope Fuselage 4 and the engine installed on the fuselage 4, the airborne control system that is made up of flight control system, navigation system, flight attitude sensor and radio remote control telemetry and information transmission system is contained on the fuselage 4, to paraglider The flight is carried out calculation control; the parachute control connection mechanism capable of manipulating the parasol 1 and the engine throttle control mechanism capable of manipulating the engine are installed on the fuselage 4, and the output of the flight contr...

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PUM

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Abstract

The invention discloses an automatic control mechanism for an umbrella wing aircraft, which comprises an umbrella wing, an umbrella wing rope, a hanging umbrella rope, a fuselage, and an engine. The control mechanism, the output command of the flight control system of the airborne control system is used as the control signal of the parawing control connection mechanism and the engine throttle control mechanism. The combination control of the paraglider and the throttle in the present invention realizes the unmanned automatic control of the flying operations such as take-off or landing, level flight or circling of the paraglider, which not only greatly improves the safety of the operator, but also can be achieved by the present invention The programming method automatically flies according to the given route, which makes the flying operation of the paraglider more accurate, the flight time is longer, and the range is longer. Line-of-sight operational flight.

Description

technical field [0001] The invention belongs to the field of air vehicles, in particular to an automatic control mechanism for an umbrella wing aircraft. Background technique [0002] At present, many existing paragliders adopt the manned control method. When performing high-risk flight tasks, due to the influence of human factors such as the operator's driving skills and emotions, it is easy to cause safety accidents. This makes Operators are at greater risk when flying. In order to overcome this defect, some paragliders have been modified to be piloted remotely by ground personnel, but because the remote control method requires a certain reaction time, the possibility of error during manipulation is relatively high, making it difficult to complete more complex flight tasks ; and the remote control mode has limited the distance between the paraglider and the ground personnel, so that the paraglider of this type of remote control can not complete long-distance precise fligh...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C31/04
Inventor 杨绍文王新杰
Owner 贵州贵航无人机有限责任公司
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