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US 2026/0296633 A1Published application
Aircraft
AssigneeAirbus Defence and Space GmbH
InventorFranz-Michael Sendner
Life of this patent
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Abstract
An aircraft includes a fuselage, a wing assembly, a propulsion device, and two tail booms, each including a stem and a stabilizing surface, wherein the stabilizing surfaces of the tail booms are each arranged symmetrically with respect to the respective stem of the tail boom, wherein the stabilizing surfaces of the tail booms are arranged at an angle to one another such that upper edges of the stabilizing surfaces have a smaller spacing than lower edges of the stabilizing surfaces, and wherein each of the stabilizing surfaces has a tilting device for controlling the aircraft.
Claims9
An aircraft, comprising:
- a fuselage;
- a wing assembly;
- a propulsion device;
- and
- two tail booms, each comprising a stem and a stabilizing surface;
- wherein the stabilizing surfaces of the tail booms are each arranged symmetrically with respect to a respective stem of the tail boom;
- wherein the stabilizing surfaces of the tail booms are arranged at an angle to one another such that upper edges of the stabilizing surfaces have a smaller spacing than lower edges of the stabilizing surfaces;
- and
- wherein each of the stabilizing surfaces has a tilting device for controlling the aircraft.
6 more elements
Dependencies are inferred from the claim text.