Fuel measurement sensor layout optimization method for aircraft fuel tank
A technology of measuring sensor and fuel quantity sensor, applied in the field of aircraft fuel tank fuel quantity measuring system, which can solve the problems of troublesome fuel model, unsuitable for wing flat fuel tank structure, lack of sensors, etc.
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[0051] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments, where the schematic embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention.
[0052] The layout optimization method of the aircraft fuel tank fuel measuring sensor of the present invention comprises:
[0053] Step 1) Firstly, generate the bottom initialization arrangable area, that is, the arranging full set.
[0054] In the early stage of fuel system design, usually the pipelines, pumps, valves, openings and other related information in the fuel tank have not been added, and all areas at the bottom can be used as the initial layout area; When the complexity makes it impossible to arrange the sensors, this part of the surface may not be extracted.
[0055] 1.1), first generate discrete points in the feasibility area of the bottom of the fuel tank;
[0056] 1.2)...
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