Tiltrotor Aircraft having Rotatable Wing Extensions
First Claim
1. A pylon assembly for a tiltrotor aircraft comprising:
- a fixed pylon having an outboard end;
a rotor assembly rotatably coupled to the fixed pylon and operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode, the rotor assembly including a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode; and
a wing extension rotatably coupled to the outboard end of the fixed pylon, the wing extension having a minimal dimension;
wherein, the wing extension is operable to rotate generally with the rotor assembly such that the minimal dimension of the wing extension remains in the slipstream of the proprotor.
1 Assignment
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Accused Products
Abstract
A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode. The rotor assembly includes a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.
18 Citations
20 Claims
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1. A pylon assembly for a tiltrotor aircraft comprising:
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a fixed pylon having an outboard end; a rotor assembly rotatably coupled to the fixed pylon and operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode, the rotor assembly including a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode; and a wing extension rotatably coupled to the outboard end of the fixed pylon, the wing extension having a minimal dimension; wherein, the wing extension is operable to rotate generally with the rotor assembly such that the minimal dimension of the wing extension remains in the slipstream of the proprotor. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A tiltrotor aircraft comprising:
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a fuselage; first and second wings supported by the fuselage, the first and second wings each having an outboard end; and first and second pylon assemblies positioned, respectively, proximate the outboard ends of the first and second wings, each of the pylon assemblies including; a fixed pylon having an outboard end; a rotor assembly rotatably coupled to the fixed pylon and operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode, the rotor assembly including a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode; and a wing extension rotatably coupled to the outboard end of the fixed pylon, the wing extension having a minimal dimension; wherein, the wing extension is operable to rotate generally with the rotor assembly such that the minimal dimension of the wing extension remains in the slipstream of the proprotor. - View Dependent Claims (17, 18, 19, 20)
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Specification