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Turbojet engine with fan rotor blades having tip clearance
Turbojet engine with fan rotor blades having tip clearance
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机译:带有叶尖间隙的风扇转子叶片的涡轮喷气发动机
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摘要
In a turbojet engine of the kind having a fan, the face of the radially outer tip of each rotor blade of the fan has a radiussed profile centered at a point R situated in a position displaced on the concavely curved side of the blade relative to its radial axis and beyond the rotational axis of the engine relative to the blade.
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