公开(公告)号：USD1055824S1

公开(公告)日：2024-12-31

申请号：US29871700

申请日：2023-02-24

Applicant: Textron Aviation Inc.

Designer： Merril Binford Williams ,  Frank Joseph Rowe ,  Zonmong Lor ,  Matthew R. Harrell ,  Karen Tamasi Cooper

公开(公告)号：US20240425183A1

公开(公告)日：2024-12-26

申请号：US18662133

申请日：2024-05-13

Applicant: Textron Aviation Inc.

Inventor： Merril Binford Williams ,  Frank Joseph Rowe

IPC: B64D11/06

Abstract: An aircraft seat includes a support extension with an arm support which extends over an aircraft side ledge. The support extension extends upwardly and outwardly from an aircraft seat bottom. The arm support supports and aligns a user's arm with a side stick controller positioned on the aircraft side ledge.

公开(公告)号：USD1051014S1

公开(公告)日：2024-11-12

申请号：US29875227

申请日：2023-05-01

Applicant: Textron Aviation Inc.

Designer： Zonmong Lor ,  Merril Binford Williams ,  Frank Joseph Rowe

公开(公告)号：US11912414B2

公开(公告)日：2024-02-27

申请号：US17736712

申请日：2022-05-04

Applicant: Textron Aviation Inc.

Inventor： Frank Joseph Rowe ,  Merril Binford Williams ,  Jonathan Lynn Headrick ,  Michael John Seibel

IPC: B64D11/06

CPC classification number: B64D11/0644

Abstract: A cockpit center console armrest includes a base member configured for mounting to a floor, an extending member mechanically coupled to the base member, and an armrest mechanically coupled to the extending member. The extending member includes an inner telescoping member configured for sliding within an outer telescoping member for adjusting a height of the armrest. A lever exposed on an underside of the armrest is configured for actuating a release mechanism. The release mechanism is configured for releasably securing the inner telescoping member to the outer telescoping member. A pivot axis pivotably couples the extending member to the base member such that the extending member is rotatable for rotating the armrest between a deployed orientation and a retracted orientation.

公开(公告)号：US11066173B2

公开(公告)日：2021-07-20

申请号：US15797769

申请日：2017-10-30

Applicant: Textron Aviation Inc.

Inventor： David Wayne Davis ,  Frank Joseph Rowe ,  Jason Michael Decker ,  Matthew Robert Harrell

IPC: B64D11/06 ,  A47B83/00 ,  A47B85/04 ,  A47B85/08 ,  A47B1/05 ,  A47B13/02

Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

公开(公告)号：US20180118349A1

公开(公告)日：2018-05-03

申请号：US15795707

申请日：2017-10-27

Applicant: Textron Aviation Inc.

Inventor： Frank Joseph Rowe ,  Michael Scott Robinson ,  Dave Wayne Davis ,  JoAnn Kimbell ,  Stephen Fagan

IPC: B64D11/04 ,  A47B77/04 ,  A47B95/00 ,  A47B61/02

CPC classification number: B64D11/04 ,  A47B61/02 ,  A47B77/04 ,  A47B95/008

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.