公开(公告)号：USD1031338S1

公开(公告)日：2024-06-18

申请号：US29811196

申请日：2021-10-12

Applicant: Textron Aviation Inc.

Designer： Nathan Earl Esau ,  Craig Louis Bothell ,  Jason Eric Francis ,  Matthew R. Harrell ,  Shelby Nicole Page

Abstract: FIG. 1 is a perspective view of the drip edge on galley work surface showing our new design;
FIG. 2 is a front view of the drip edge on galley work surface of FIG. 1;
FIG. 3 is a back view of the drip edge on galley work surface of FIG. 1;
FIG. 4 is a left view of the drip edge on galley work surface of FIG. 1;
FIG. 5 is a right view of the drip edge on galley work surface of FIG. 1;
FIG. 6 is a top view of the drip edge on galley work surface of FIG. 1;
FIG. 7 is a bottom view of the drip edge on galley work surface of FIG. 1;
FIG. 8 is a perspective view of the drip edge on galley work surface of FIG. 1 in a stowed configuration;
FIG. 9 is a front view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 10 is a left view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 11 is a right view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 12 is a perspective view of the drip edge on galley work surface of FIG. 1 in a deployed configuration;
FIG. 13 is a front view of the drip edge on galley work surface of FIG. 1 in the deployed configuration;
FIG. 14 is a left view of the drip edge on galley work surface of FIG. 1 in the deployed configuration; and,
FIG. 15 is a right view of the drip edge on galley work surface of FIG. 1 in the deployed configuration.
In FIGS. 1-15, broken lines indicate environmental structure that forms 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.