Cross-medium flight vehicle power device based on air-water runner compact layout
A power device and cross-medium technology, applied in the field of cross-medium aircraft power devices
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[0021] The present disclosure will be further described in detail below with reference to the drawings and embodiments. It can be understood that the specific implementation manners described here are only used to explain relevant content, rather than to limit the present disclosure. It should also be noted that, for ease of description, only parts related to the present disclosure are shown in the drawings.
[0022] It should be noted that, in the case of no conflict, the implementation modes and the features in the implementation modes in the present disclosure can be combined with each other. The present disclosure will be described in detail below with reference to the drawings and embodiments.
[0023] This disclosure proposes a trans-medium aircraft power plant scheme, which introduces the main combustion chamber mode selection valve 3, sealing mechanism, volute water inlet 8, etc. on the basis of the traditional turbojet propulsion system and turbowater jet propulsion ...
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