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AssigneePla Air Force Engineering Universit
InventorsFeilong SONG, Yun WU, Huimin SONG, Min JIA, Shanguang GUO, Xin CHEN, Di JIN, Zhao YANG
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The application relates to an anti-back-transfer intake structure of a rotating detonation combustion chamber including a Tesla valve communicating with the rotating detonation combustion chamber and arranged at an inlet of the rotating detonation combustion chamber. The Tesla valve includes a casing and a flow passage, the casing is coaxially connected with an outer wall of the rotating detonation combustion chamber, the flow passage is arranged in the casing, and the flow passage has an inlet end for introducing air, and an outlet end connected with an annular passage of the rotating detonation combustion chamber.
An anti-back-transfer intake structure for a rotating detonation combustion chamber, comprising a Tesla valve communicating with the rotating detonation combustion chamber and arranged at an inlet of the rotating detonation combustion chamber, wherein the Tesla valve comprises a casing and a flow passage, the casing is coaxially connected with an outer wall of the rotating detonation combustion chamber, the flow passage is arranged in the casing, and the flow passage has an inlet end for introducing air and an outlet end connected with an annular passage of the rotating detonation combustion chamber.
Dependencies are inferred from the claim text.