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US 2004/0169110 A1Published application
Aerodynamic component for controlling a landing guide path of an aircraft
AssigneeAirbus Deutschland GmbH
InventorsSusanne Wyrembek, Peter May, Klaus Muthreich
Life of this patent
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Abstract
An aerodynamic including a main body and a control member. The main body is configured to be connected to a wing of an aircraft. The control member is connected to the main body, the control member including a fixed member secured to the main body and a pivotable member configured to increase a drag of the aircraft without substantially changing a lift of the aircraft.
Claims20
An aerodynamic component comprising:
- a main body configured to be connected to a wing of an aircraft;
- and
- a control member connected to the main body, the control member comprising a fixed member secured to the main body and a pivotable member configured to increase a drag of the aircraft without substantially changing a lift of the aircraft.
An aerodynamic component comprising:
- a main body configured to be connected to a wing of an aircraft;
- and
- means for increasing a drag of the aircraft without substantially changing a lift of the aircraft, the means connected to the main body.
Dependencies are inferred from the claim text.