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：US11071391B2

公开(公告)日：2021-07-27

申请号：US16142742

申请日：2018-09-26

Applicant: Textron Aviation Inc.

Inventor： Jason Michael Decker ,  Nathan Earl Esau ,  Michael Scott Robinson ,  Christopher Adair Pinkerton ,  David Michael Kuhn

IPC: A47C17/213 ,  A47C17/16 ,  A47C7/62 ,  A47C17/175 ,  A47C21/00

Abstract: A convertible couch with concealed storage includes an upper seat back, a seat bottom adapted for sliding inwardly for a first mode and sliding outwardly for a second mode, and an articulating seat section between the upper seat back and the seat bottom. The articulating seat section converts between a lower seat back in the first mode and an inner seat bottom in the second mode. The first mode is adapted for seating and the second mode is adapted for lying and reclining. A storage location housing convenience features is located behind the articulating section, such that the storage location and convenience features are concealed in the first mode and accessible in the second mode.

公开(公告)号：US20190099005A1

公开(公告)日：2019-04-04

申请号：US16142742

申请日：2018-09-26

Applicant: Textron Aviation Inc.

Inventor： Jason Michael Decker ,  Nathan Earl Esau ,  Michael Scott Robinson ,  Christopher Adair Pinkerton ,  David Michael Kuhn

IPC: A47C17/213 ,  A47C21/00 ,  A47C7/62 ,  A47C17/16

Abstract: A convertible couch with concealed storage includes an upper seat back, a seat bottom adapted for sliding inwardly for a first mode and sliding outwardly for a second mode, and an articulating seat section between the upper seat back and the seat bottom. The articulating seat section converts between a lower seat back in the first mode and an inner seat bottom in the second mode. The first mode is adapted for seating and the second mode is adapted for lying and reclining. A storage location housing convenience features is located behind the articulating section, such that the storage location and convenience features are concealed in the first mode and accessible in the second mode.

公开(公告)号：US12263946B2

公开(公告)日：2025-04-01

申请号：US18056892

申请日：2022-11-18

Applicant: Textron Aviation Inc.

Inventor： Nathan Earl Esau ,  Jonathan Lynn Headrick

IPC: B64D11/00 ,  B64C1/06

Abstract: An overhead bin in an aircraft includes a liner disposed on an underside of a cabin ceiling and a receptacle that protrudes through an opening in the liner. A bin has a top side with at least one attachment point that includes: a stud mechanically coupled to the top side and a screw disposed within the stud. The stud includes a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner. An installation method for an overhead bin in an aircraft includes raising the overhead bin to engage the stud with the receptacle, sliding the overhead bin outboard for inserting the stud into the receptacle, and turning a screw within the stud for tightening the stud within the receptacle for securing the overhead bin beneath the ceiling.

公开(公告)号：US20230159170A1

公开(公告)日：2023-05-25

申请号：US18056892

申请日：2022-11-18

Applicant: Textron Aviation Inc.

Inventor： Nathan Earl Esau ,  Jonathan Lynn Headrick

IPC: B64D11/00 ,  B64F5/10

CPC classification number: B64D11/003 ,  B64F5/10

Abstract: An overhead bin in an aircraft includes a liner disposed on an underside of a cabin ceiling and a receptacle that protrudes through an opening in the liner. A bin has a top side with at least one attachment point that includes: a stud mechanically coupled to the top side and a screw disposed within the stud. The stud includes a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner. An installation method for an overhead bin in an aircraft includes raising the overhead bin to engage the stud with the receptacle, sliding the overhead bin outboard for inserting the stud into the receptacle, and turning a screw within the stud for tightening the stud within the receptacle for securing the overhead bin beneath the ceiling.