A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices each having a body. A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacelle from a retracted position to an extended position.
ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET
2018-12-27
Patent
Elektronische Ressource
Englisch
ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN ULTRA-SHORT NACELLE INLET
Europäisches Patentamt | 2019
|ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET
Europäisches Patentamt | 2021
|ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET
Europäisches Patentamt | 2022
|MITIGATION OF ADVERSE FLOW CONDITIONS IN A NACELLE INLET
Europäisches Patentamt | 2024
|MITIGATION OF ADVERSE FLOW CONDITIONS IN A NACELLE INLET
Europäisches Patentamt | 2020
|