公开(公告)号：US11072419B2

公开(公告)日：2021-07-27

申请号：US16532347

申请日：2019-08-05

Applicant: Textron Innovations Inc.

Inventor： Mark Loring Isaac ,  James Everett Kooiman ,  Charles David Hogue

IPC: B64C25/12 ,  B64C25/34 ,  B64C25/20 ,  B64C27/82 ,  B64C29/00 ,  B64C27/06

Abstract: A retractable landing gear system configured to contour an aircraft fuselage includes a landing wheel having an axle, a wheel rotation strut assembly coupling the landing wheel to the aircraft fuselage and an actuation strut assembly configured to move the wheel rotation strut assembly between various positions including a deployed position and a stowed position. The axle of the landing wheel is pivotably coupled to a distal end of the wheel rotation strut assembly and configured to pivot relative to the wheel rotation strut assembly as the actuation strut assembly moves the wheel rotation strut assembly between the deployed and stowed positions such that the landing wheel generally contours the aircraft fuselage when the wheel rotation strut assembly is in the stowed position.

公开(公告)号：US12214857B2

公开(公告)日：2025-02-04

申请号：US18188132

申请日：2023-03-22

Applicant: Textron Innovations Inc.

Inventor： Charles David Hogue ,  James Everett Kooiman ,  Joseph Richard Carpenter, Jr. ,  David G. Carlson ,  Jonathan Alexander Freeman

IPC: B64C1/06 ,  B64C27/26

Abstract: An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.

公开(公告)号：US20250121926A1

公开(公告)日：2025-04-17

申请号：US19002889

申请日：2024-12-27

Applicant: Textron Innovations Inc.

Inventor： Charles David Hogue ,  James Everett Kooiman ,  Joseph Richard Carpenter, JR. ,  David G. Carlson ,  Jonathan Alexander Freeman

IPC: B64C1/06 ,  B64C27/26

Abstract: An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith. The plurality of stiffening beads may be integrated with the side panel and extend parallel to one another.

公开(公告)号：US20240317382A1

公开(公告)日：2024-09-26

申请号：US18188132

申请日：2023-03-22

Applicant: Textron Innovations Inc.

Inventor： Charles David Hogue ,  James Everett Kooiman ,  Joseph Richard Carpenter, JR. ,  David G. Carlson ,  Jonathan Alexander Freeman

IPC: B64C1/06

CPC classification number: B64C1/061 ,  B64C27/26

Abstract: An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.