FIELD: aviation.
SUBSTANCE: system comprises N fuel tanks built into the annular fairing. The tanks are located circumferentially symmetrically relative to the vertical axis of the vehicle. The pipeline supplying fuel to the engine connect the fuel tanks in series with each other, at that each subsequent connected tank is located oppositely or about oppositely relative to the vertical axis of the fairing, to the previous tank. The last tank is connected by the pipeline to the engine.
EFFECT: simplification of the design of the fuel supply system.
7 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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