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Large freight unmanned aerial vehicle fuel system and control method thereof

A fuel system and unmanned aerial vehicle technology, applied in the field of unmanned aerial vehicles, can solve problems such as engine parking, affecting the flight safety of unmanned aerial vehicles, fluctuations in fuel supply pressure, etc., and achieve the effect of improving safety and reliability

Inactive Publication Date: 2020-05-12
AEROSPACE TIMES FEIHONG TECH CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] With the continuous increase of drone flight time, the aviation piston engine used in it is changed to an electronically controlled fuel injection system (hereinafter referred to as the electronic injection aviation piston engine). The electronic injection aviation piston engine is very sensitive to the fuel supply pressure. Fuel supply pressure fluctuations will cause the engine to work abnormally, and even cause the engine to stop, seriously affecting the flight safety of the drone

Method used

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  • Large freight unmanned aerial vehicle fuel system and control method thereof
  • Large freight unmanned aerial vehicle fuel system and control method thereof
  • Large freight unmanned aerial vehicle fuel system and control method thereof

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Embodiment

[0044] Such as figure 1As shown, the technical solution adopted in the present invention is composed of fuel tank, fuel supply conduit, fuel tank selection solenoid valve, fuel master switch, fuel return tank, fuel filter, electric booster pump, check valve, oil pressure sensor, tee and pass Composed of air pipes, the number of the fuel tanks is two, respectively the first fuel tank (left wing fuel tank) 3-1, the second fuel tank (right wing fuel tank) 3-2, the fuel tank selection solenoid valve is Two, respectively the first fuel tank selection solenoid valve (left wing fuel tank selection solenoid valve) 6-1 and the second fuel tank selection solenoid valve (right wing fuel tank selection solenoid valve) 6-2, the fuel supply conduit includes the first One oil supply conduit 5-1, second oil supply conduit 5-2, third oil supply conduit 5-3, fourth oil supply conduit 5-4, fifth oil supply conduit 5-5, the first oil supply conduit The conduit 5-1 is connected between the left w...

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Abstract

The invention, which relates to the technical field of unmanned aerial vehicles, discloses a large freight transport unmanned aerial vehicle fuel system. A first oil supply system comprises a first oil tank, a fuel tank selection electromagnetic valve, a fuel main switch, a fuel filter, an electric booster oil pump, a second one-way valve, an oil pressure sensor, an oil pressure regulator, an oilreturn guide pipe and an oil return tank, and is formed by combining an oil supply guide pipe and a three-way joint. A second oil supply system comprises a second oil tank, a fuel tank selection electromagnetic valve, a fuel main switch, a fuel filter, a mechanical booster oil pump, a first one-way valve, an oil pressure sensor, an oil pressure regulator, an oil return guide pipe and an oil returntank, and is formed by combining an oil supply guide pipe and a three-way joint. According to the technical scheme, the oil supply pressure can be actively adjusted, a redundant backup oil supply andtransportation system is provided, the design is reasonable, the service life is long, the safety performance is excellent, and the working requirement of the electronic injection type aviation piston engine is met.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a large-scale cargo unmanned aerial vehicle fuel system and a control method thereof. Background technique [0002] At present, the UAV fuel system is mainly used to store the fuel required for flight, and continuously supply fuel to the engine during the flight of the UAV to ensure the safe and reliable continuous operation of the engine and provide power for the UAV. The aviation piston engines generally used by UAVs use mechanical carburetors to control and adjust the fuel supply of the engines. The carburetor-supplied aviation piston engines have simple requirements for the UAV fuel system and have no special requirements for the fuel supply pressure. Its fuel system usually consists of a fuel tank, an oil supply pipeline and a ventilation pipeline. [0003] With the continuous increase of drone flight time, the aviation piston engine used in it is changed t...

Claims

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Application Information

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IPC IPC(8): B64D37/02B64D37/32B64D37/00
CPCB64D37/00B64D37/02B64D37/32
Inventor 陈建国王振宇于敬欢龚毅姜楠
Owner AEROSPACE TIMES FEIHONG TECH CO LTD
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