公开(公告)号：US20200283119A1

公开(公告)日：2020-09-10

申请号：US16293890

申请日：2019-03-06

Applicant: Bell Helicopter Textron Inc.

Inventor： Pier-Alexandre Pelletier ,  Guillaume Noiseux-Boucher

IPC: B64C1/14 ,  E05B83/40 ,  E05B85/04 ,  E05B85/12 ,  E05B79/12

Abstract: A door structure and method of assembling same. The door structure includes a door frame delimiting a door opening. The door frame has a latch housing portion defining a latch housing cavity extending along a length of the door frame. A door is mounted to the door frame and displaceable between an open position and a closed position. The door has a peripheral portion with an outer wall and an inner wall delimiting a cavity of the peripheral portion. A door latch assembly has a first latch member fixedly mounted to the door, and a door manipulator mounted to one of the door and the fuselage and coupled to a second latch member within the latch housing cavity of the door frame. The door manipulator is configured to be manipulated to displace the second latch member to engage and disengage the first latch member.

公开(公告)号：US11250522B2

公开(公告)日：2022-02-15

申请号：US16701607

申请日：2019-12-03

Applicant: Bell Helicopter Textron Inc.

Inventor： James Corrigan ,  Pier-Alexandre Pelletier

IPC: G06Q50/04 ,  G06Q10/08 ,  G06Q10/00

Abstract: An aircraft component is manufactured from a plurality of separate materials comprising a first material. The first material is physically associated with a tracking device comprising a first storage medium featuring line-of-sight accessible information and a second storage medium featuring non-line-of-sight accessible information. The line-of-sight accessible information and the non-line-of-sight accessible information each comprise information regarding the first material physically associated with the tracking device.

公开(公告)号：US20170116684A1

公开(公告)日：2017-04-27

申请号：US14921064

申请日：2015-10-23

Applicant: Bell Helicopter Textron Inc.

Inventor： James Corrigan ,  Pier-Alexandre Pelletier

IPC: G06Q50/04 ,  B64F5/00 ,  B64C27/12 ,  G06Q10/08 ,  B64C27/04

CPC classification number: G06Q50/04 ,  G06Q10/087 ,  Y02P90/30

Abstract: According to one embodiment, an aircraft component is manufactured from a plurality of separate materials comprising a first material. The first material is physically associated with a tracking device comprising a first storage medium featuring line-of-sight accessible information and a second storage medium featuring non-line-of-sight accessible information. The line-of-sight accessible information and the non-line-of-sight accessible information each comprise information regarding the first material physically associated with the tracking device.