A fixed-wing UAV air-cooled fuel cell dual-stack integrated power system
A fuel cell stack and power system technology, used in fuel cells, fuel cell additives, fuel cell heat exchange, etc., can solve the problems of low power system efficiency, poor stack heat dissipation, etc., to improve performance consistency, Improve power generation efficiency and drone endurance, and eliminate the effect of energy consumption
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Embodiment 1
[0128] This embodiment provides a fixed-wing UAV air-cooled fuel cell dual-stack integrated power system, such as image 3 As shown, it includes the fuselage U0, the power motor U1 located at the front of the fuselage U0, the high-pressure hydrogen storage tank U4 located at the rear of the fuselage U0, the wings U5 located on both sides of the fuselage U0, and the horizontal plane located at the tail of the fuselage U0. The tail U6 and the vertical tail U7, the task load U100 located between the power motor U1 and the air-cooled fuel cell stack, the first air-cooled fuel cell stack U2 and the second air-cooled fuel cell symmetrically arranged in the middle of the fuselage U0 The stack U3, and a first heat dissipation system and a second heat dissipation system respectively corresponding to the first air-cooled fuel cell stack U2 and the second air-cooled fuel cell stack U3.
[0129] The first air-cooled fuel cell stack U2 and the second air-cooled fuel cell stack U3 both incl...
Embodiment 2
[0146] This embodiment provides a fixed-wing UAV air-cooled fuel cell dual-stack integrated power system, which is used for a fixed-wing UAV equipped with an auxiliary propeller U8 on the wing U5. When the fixed-wing UAV starts or flies, Auxiliary propeller U8 is automatically turned on; if Image 6 As shown, the power system includes a fuselage U0, a power motor U1 located at the front of the fuselage U0, a high-pressure hydrogen storage tank U4 located at the rear of the fuselage U0, wings U5 located on both sides of the fuselage U0, The auxiliary propeller U8 on U5, the horizontal stabilizer U6 and vertical stabilizer U7 located at the tail of the fuselage U0, the task load U100 located between the power motor U1 and the air-cooled fuel cell stack, symmetrically arranged on both sides of the wings U5 The first air-cooled fuel cell stack U2 and the second air-cooled fuel cell stack U3, and the first heat dissipation system and the third air-cooled fuel cell stack correspondi...
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