公开(公告)号：US20250145271A1

公开(公告)日：2025-05-08

申请号：US18934165

申请日：2024-10-31

Applicant: Textron Aviation Inc.

Inventor： Gonzalo Eduardo Mendoza ,  Corey Wailes Hagemeister ,  Steven Michael Klausmeyer

IPC: B64C1/14 ,  B64D27/33 ,  B64D27/355 ,  B64D27/357

Abstract: An aircraft having unobstructed cabin door access includes a hybrid power drive with a combustion engine connected to an electricity generating machine. Components of the hybrid power drive are positioned throughout the aircraft to provide a weight distribution having an aft bias. The aircraft further includes a forward swept wing and a cabin door positioned forward of the forward swept wing, such that access into a fuselage of the aircraft via the cabin door is unobstructed by the forward swept wing.

公开(公告)号：US20240132212A1

公开(公告)日：2024-04-25

申请号：US18483338

申请日：2023-10-08

Applicant: Textron Aviation Inc.

Inventor： Gonzalo Eduardo Mendoza ,  Corey Wailes Hagemeister ,  Steven Michael Klausmeyer

IPC: B64C39/08 ,  B64D27/02

CPC classification number: B64C39/08 ,  B64D27/02

Abstract: An electric aircraft includes a forward wing and an aft wing both located on a top side of a fuselage and both having an upward dihedral angle. The forward wing has a straight or slightly forward-swept leading edge. The aft wing has a swept leading edge. A plurality of propeller engines are located on a leading-edge side of the forward wing. A single propeller engine may be located on a top side of an aft end of the fuselage; alternatively, a plurality of propeller engines are located on the aft wing on either its leading or trailing edge. The propeller engines are each powered by an electric motor. An unobstructed cargo door is located on a side of the fuselage, aft of the forward wing.

公开(公告)号：US20240228036A9

公开(公告)日：2024-07-11

申请号：US18483338

申请日：2023-10-09

Applicant: Textron Aviation Inc.

Inventor： Gonzalo Eduardo Mendoza ,  Corey Wailes Hagemeister ,  Steven Michael Klausmeyer

IPC: B64C39/08 ,  B64D27/02

CPC classification number: B64C39/08 ,  B64D27/02

Abstract: An electric aircraft includes a forward wing and an aft wing both located on a top side of a fuselage and both having an upward dihedral angle. The forward wing has a straight or slightly forward-swept leading edge. The aft wing has a swept leading edge. A plurality of propeller engines are located on a leading-edge side of the forward wing. A single propeller engine may be located on a top side of an aft end of the fuselage; alternatively, a plurality of propeller engines are located on the aft wing on either its leading or trailing edge. The propeller engines are each powered by an electric motor. An unobstructed cargo door is located on a side of the fuselage, aft of the forward wing.