Airbus Operations Gmbh

Sergej Rajkowski

Ivano Bertolini

Frank Nielsen

Jeff Wee Hong Yap

Michael Höft

Martin Obermaier

A leading edge structure () for a flow control system of an aircraft (), including a leading edge panel () surrounding a plenum () and having a first side portion (), a second side portion (), an inner surface () facing the plenum () and an outer surface () in contact with an ambient flow (), wherein the leading edge panel () includes micro pores (), wherein a first port device () is arranged in the first side portion () fluidly connected to the plenum () via a duct () defined by a duct structure (), and wherein the first port device () comprises a first door () pivotable by a first hinge () about a first hinge axis ().

Leading edge structure for a flow control system of an aircraft

A leading edge structure () for a flow control system of an aircraft (), including a leading edge panel () that surrounds a plenum (), wherein the leading edge panel () has a first side portion (), a second side portion (), an inner surface () and an outer surface (), wherein the leading edge panel () having micro pores () forming a fluid connection between the plenum () and the ambient flow (), wherein a first air inlet/outlet device () is arranged in the first side portion () and a second air inlet outlet/device () is arranged in the second side portion (), fluidly connected to the plenum (), and wherein the first air inlet/outlet device () comprises a pivotable first door () and the second air inlet outlet/device () comprises a pivotable second door ().

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Hamburg, Germany

Sergej Rajkowski