公开(公告)号：USD1035524S1

公开(公告)日：2024-07-16

申请号：US29811193

申请日：2021-10-12

Applicant: Textron Aviation Inc.

Designer： Jason Michael Decker ,  Emily O'Kelley Pearson ,  Drew Daniel Woodworth

Abstract: FIG. 1 is a perspective view of the cabin divider showing our new design;
FIG. 2 is a front view of the cabin divider of FIG. 1;
FIG. 3 is a rear view of the cabin divider of FIG. 1; and,
FIG. 4 is a left view of the cabin divider of FIG. 1.
In FIGS. 1-4, broken lines showing the interior and seats of a cabin depict environmental structure which forms no part of the claimed design. The broken lines in FIG. 3 show portions of the cabin divider which form no part of the claimed design.

公开(公告)号：US20250091717A1

公开(公告)日：2025-03-20

申请号：US18830543

申请日：2024-09-10

Applicant: Textron Aviation Inc.

Inventor： Michael John Seibel ,  Chad Lee Smith ,  Craig Louis Bothell ,  Emily O'Kelley Pearson

IPC: B64D11/00

Abstract: A repositionable pocket for an aircraft having a rigid pocket wall pivotally attached to the aircraft sidewall and at least one strap assembly connecting the pocket to the sidewall. The strap assembly has a first end fixable to the sidewall and a second end repositionably fastened to the pocket. The strap is preferably made to be elastic and urges the attached pocket into a closed orientation thereby securing any stowed items between the pocket and the aircraft sidewall. Strap adjustability accommodates different sized objects for stowage.

公开(公告)号：US20200148366A1

公开(公告)日：2020-05-14

申请号：US16660192

申请日：2019-10-22

Applicant: Textron Aviation Inc.

Inventor： Stephen Howard Fagan ,  Paul Stokholm Warren ,  Emily O'Kelley Pearson ,  Jeremy Joseph Kneuper ,  Phillip Kendrick

IPC: B64D11/06

Abstract: A seat base includes a plurality of linear actuators each having a first end pivotally mounted to a base member and a second end pivotally mounted to a seat member. A controller is adapted for controlling an extension length of each of the plurality of linear actuators in a coordinated manner for adjusting a position of the seat member with six degrees-of-freedom and for damping vibration of the seat member. An active vibration mitigation method for reducing vibrations of an aircraft seat includes receiving vibration data from one or more accelerometers mounted to the aircraft seat and determining a vibration profile based on the vibration data. When vibration mitigation is warranted, control signals for damping vibration are determined and transmitted to a plurality of linear actuators adapted to support the aircraft seat.