A flow control system on an aircraft engine nacelle incorporates a plurality of translating turning vanes each having a body. An equal plurality of actuators is coupled to a trailing edge of the body of an associated one of the translating turning vanes. The actuator translates the body from a retracted position to an extended position.
TRANSLATING TURNING VANES FOR A NACELLE INET
2018-12-27
Patent
Electronic Resource
English
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