| CPC F02K 7/10 (2013.01) [B64D 33/02 (2013.01); F02C 7/042 (2013.01); B64D 2033/026 (2013.01)] | 20 Claims |

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1. A hypersonic large internal contraction ratio air inlet channel having a stepless adjustable air release valve, comprising:
an air inlet channel front body;
an air-discharging slit cover plate extending backwards from the air inlet channel front body;
a lip cover disposed on the air-discharging slit cover plate, sidewalls disposed on two sides of the lip cover;
the air inlet channel front body, the air-discharging slit cover plate, the lip cover and the sidewalls on the two sides together form an inner flow channel of the air inlet channel;
wherein a plurality of adjacent air-discharging cavities are arranged from front to back inside the air-discharging slit cover plate, the plurality of adjacent air-discharging cavities are separated by a partition plate, and a plurality of air-discharging slits disposed in the air-discharging slit cover plate connect the plurality of adjacent air-discharging cavities to the inner flow channel;
a lower half of each one of the plurality of adjacent air-discharging cavities has an air-discharging channel laterally penetrating both of the sidewalls; and
the stepless adjustable air release valve comprises:
a driver;
a rotatable shaft extending from the driver; and
a plurality of valve plates with a respective one of the plurality of valve plates disposed in each air-discharging channel, wherein the plurality of valve plates are mounted on the rotatable shaft and are rotated by means of the rotatable shaft between open and closed positions;
when the plurality of valve plates are rotated to the open position, the plurality of adjacent air-discharging cavities are communicated with the outside; and
when the plurality of valve plates are rotated to the closed position, the plurality of adjacent air-discharging cavities are closed by the plurality of valve plates.
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