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US 2023/0406489 A1Published application
Hybrid aircraft and landing launch/recovery system
AssigneeLeigh Aerosystems Corporation
InventorsGORDON L. HARRIS, Stephen L. Harris
Life of this patent
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Abstract
An aircraft includes a fuselage extending along a first x-axis and a wing assembly including a first wing an a second wing. A first power assembly of the aircraft includes a first propulsion element and a first electric motor while a second power assembly includes a second propulsion element and a second electric motor. The aircraft further includes a third power assembly positioned aft of the first power assembly and the second power assembly. The third power assembly includes a third propulsion element and an internal combustion engine.
Claims12
An aircraft, comprising:
- a fuselage extending along a first x-axis;
- a wing assembly including a first wing an a second wing;
- a first power assembly that includes a first propulsion element and a first electric motor coupled to the first propulsion element;
- a second power assembly that includes a second propulsion element and a second electric motor coupled to the second propulsion element;
- a third power assembly positioned aft of the first power assembly and the second power assembly, wherein the third power assembly includes a third propulsion element and an internal combustion engine coupled to the third propulsion element.
2 more elements
Dependencies are inferred from the claim text.