公开(公告)号：US20240140604A1

公开(公告)日：2024-05-02

申请号：US18409901

申请日：2024-01-11

Applicant: THE BOEING COMPANY

Inventor： Keith A. Etling ,  Hilary G. Knight

IPC: B64C39/12 ,  B64U20/20

CPC classification number: B64C39/12 ,  B64U20/20 ,  B64C2001/0045

Abstract: An aerial vehicle including a main body having a leading edge. An inlet is recessed aft from the leading edge. Forward protrusions extend from the main body on opposite sides of the inlet. An outlet nozzle is proximate to an aft end. The inlet is in fluid communication with the outlet nozzle. Wings extend from the main body.

公开(公告)号：US20220348326A1

公开(公告)日：2022-11-03

申请号：US17320357

申请日：2021-05-14

Applicant: THE BOEING COMPANY

Inventor： Keith A. Etling ,  Hilary G. Knight

IPC: B64C39/12 ,  B64C1/00 ,  B64C39/02

Abstract: An aerial vehicle including a main body having a leading edge. An inlet is recessed aft from the leading edge. Forward protrusions extend from the main body on opposite sides of the inlet. An outlet nozzle is proximate to an aft end. The inlet is in fluid communication with the outlet nozzle. Wings extend from the main body.

公开(公告)号：US12246831B2

公开(公告)日：2025-03-11

申请号：US18409901

申请日：2024-01-11

Applicant: THE BOEING COMPANY

Inventor： Keith A Etling ,  Hilary G. Knight

IPC: B64C39/12 ,  B64C1/00 ,  B64U10/25 ,  B64U20/20

Abstract: An aerial vehicle including a main body having a leading edge. An inlet is recessed aft from the leading edge. Forward protrusions extend from the main body on opposite sides of the inlet. An outlet nozzle is proximate to an aft end. The inlet is in fluid communication with the outlet nozzle. Wings extend from the main body.

公开(公告)号：US11897610B2

公开(公告)日：2024-02-13

申请号：US17320357

申请日：2021-05-14

Applicant: THE BOEING COMPANY

Inventor： Keith A. Etling ,  Hilary G. Knight

IPC: B64C39/12 ,  B64U20/20 ,  B64C1/00 ,  B64U10/25

CPC classification number: B64C39/12 ,  B64U20/20 ,  B64C2001/0045 ,  B64U10/25

Abstract: An aerial vehicle including a main body having a leading edge. An inlet is recessed aft from the leading edge. Forward protrusions extend from the main body on opposite sides of the inlet. An outlet nozzle is proximate to an aft end. The inlet is in fluid communication with the outlet nozzle. Wings extend from the main body.

公开(公告)号：USD985426S1

公开(公告)日：2023-05-09

申请号：US29749405

申请日：2020-09-04

Applicant: THE BOEING COMPANY

Designer： Hilary G. Knight ,  Keith A. Etling

Abstract: FIG. 1 is a perspective front top view of an aerial vehicle, showing our new design.
FIG. 2 is a top view thereof.
FIG. 3 is a bottom view thereof
FIG. 4 is a left view thereof.
FIG. 5 is a right view thereof
FIG. 6 is a front view thereof; and,
FIG. 7 is a rear view thereof.
The broken lines illustrate portions of the aerial vehicle that form no part of the claimed design.