In-flight auto-ignition control method of engine of unmanned aerial vehicle

An unmanned aerial vehicle and automatic ignition technology, which is applied in the field of unmanned aerial vehicles, can solve the problems of not judging the re-ignition of the aircraft, and the inability to adapt to the start-up control of re-ignition, so as to save flight costs, improve accuracy, and protect the aircraft.

Active Publication Date: 2016-10-26
XIANGYANG HONGWEI AIRCRAFT
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Problems solved by technology

[0006] However, this solution is only applicable to restarting the aeroengine after it is accidentally turned off when the aircraft’s operating conditions are all normal. Its working logic is to turn off and start immediately. Whether the condition of the failure is eliminated or whether the working condition of the aircraft is suitable for re-ignition start, that is, the above scheme cannot adapt to the start-up control of the re-ignition of the unmanned aircraft after the failure

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  • In-flight auto-ignition control method of engine of unmanned aerial vehicle
  • In-flight auto-ignition control method of engine of unmanned aerial vehicle
  • In-flight auto-ignition control method of engine of unmanned aerial vehicle

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[0027] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0028] Such as figure 1 As shown, the automatic ignition system of an unmanned aircraft engine in the air according to an embodiment of the present invention mainly includes an ignition switch 1, an aircraft control module 2, an ignition module 4, a sensor 3, an engine 6, and a signal generator 5 in five parts.

[0029] Such as figure 2 As shown, the aircraft controller only needs to click th...

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Abstract

The invention discloses an in-flight auto-ignition control method of an engine of an unmanned aerial vehicle. The method comprises: (11), detecting whether a ground control station is out of control, or whether the engine of the aerial vehicle is subjected to accidental flameout and shut down; (12), if the ground control station is out of airplane control ability, or the engine of the aerial vehicle is subjected to accidental flameout and shut down, executing the step (13); (13), detecting whether the communication link between the unmanned aerial vehicle and the ground control station is normal, if the communication link between the unmanned aerial vehicle and the ground control station is normal, executing the step (14); (14), detecting whether the engine working condition information and the aerial vehicle flight state meet operation requirements, if the engine working condition information and the aerial vehicle flight state meet the operation requirements, executing the step (15); and (15), detecting whether a throttle servo, an accelerator servo and a task servo of the engine can work normally, if the throttle servo, the accelerator servo and the task servo of the engine can work normally, carrying out an ignition command, and restarting the engine; if the throttle servo, the accelerator servo and the task servo of the engine cannot work normally, stopping sending the ignition command. The method can be applied to reignition and starting of the unmanned aerial vehicle after fault recovery, the aerial vehicle can be effectively protected, and the flight cost is reduced.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a control method for automatic ignition of an unmanned aerial vehicle engine in the air Background technique [0002] An unmanned aerial vehicle is an unmanned aerial vehicle controlled by radio remote control equipment and its own program control device, such as an unmanned aircraft. Unmanned aerial vehicles can generally be divided into unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc. The application range of unmanned aerial vehicles is more and more extensive, including in aerial photography, agriculture, plant protection, selfie, express transportation, disaster rescue, observation of wild animals, monitoring of infectious diseases, surveying and mapping, news reports, power inspection, disaster relief, film and television shooting, manuf...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D31/06F02D17/04B64F1/00B64C39/02
CPCB64C39/024B64D31/06B64F1/00F02D17/04
Inventor 华康薛富利王萌徐杰胡明军薛龙
Owner XIANGYANG HONGWEI AIRCRAFT
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