A nacelle (12) for a gas turbine jet engine (10) for an aircraft (18) includes plasma actuators (42) that act as flow disruptors to provide boundary layer turbulence when the engine (10) is exposed to air flow that is obtuse or perpendicular to direction of travel of the engine.
申请公布号
EP3090952(A1)
申请公布日期
2016.11.09
申请号
EP20160160912
申请日期
2016.03.17
申请人
ROLLS-ROYCE CORPORATION;ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
