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US 2025/0115346 A1Published application
Apparatus and methods for transonic truss-braced wing aircraft
AssigneeThe Boeing Company
InventorsNeal A. Harrison, Paul W. Dees, Donald Thomas Powell
Life of this patent
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Abstract
Apparatus and methods for transonic truss-braced wing aircraft are disclosed herein. An example aircraft disclosed herein includes a fuselage and a wing supported by a truss. The truss includes a pylon coupled to and extending from the fuselage and a strut attached to the wing. An engine is coupled to the pylon.
Claims29
An aircraft comprising:
- a fuselage;
- a wing supported by a truss, the truss including:
- a pylon coupled to and extending from the fuselage;
- and
- a strut attached to the wing;
- and
- an engine coupled to the pylon.
4 more elements
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A method of attaching an engine to an aircraft comprising:
- coupling a truss to a wing, the truss having a strut coupled to the wing and a pylon;
- coupling the pylon to a fuselage of the aircraft;
- and
- coupling an engine nacelle to the pylon of the truss.
1 more element
An aircraft comprising:
- a fuselage;
- a wing having a first end coupled to the fuselage at a first location and a second end extending from the fuselage;
- a truss to support the wing, the truss including:
- a pylon having a third end coupled to the fuselage at a second location and a fourth end extending from the fuselage, the second location different from the first location;
- and
- a strut extending between the wing and the pylon, the strut having a fifth end attached to the wing and a sixth end opposite the first end attached to the pylon;
- and
- an engine coupled to the truss.
5 more elements
Dependencies are inferred from the claim text.