公开(公告)号：US20220255175A1

公开(公告)日：2022-08-11

申请号：US17172366

申请日：2021-02-10

Applicant: Bell Textron Inc.

Inventor： William A. Amante ,  Steven Loveland ,  Jessica A. Revere

IPC: H01M50/249 ,  H01M10/613 ,  H01M10/6554 ,  H01M10/625 ,  H01M10/6556 ,  H01M50/244

Abstract: A battery assembly for an aircraft includes a cold plate having an upper planar member, a lower planar member, and at least one fluid channel positioned between the upper and lower planar members and configured to receive a cooling fluid. The battery assembly also includes an upper battery mounted to the upper planar member for transferring heat from the upper battery to the cooling fluid through the upper planar member. The battery assembly further includes a lower battery mounted to the lower planar member for transferring heat from the lower battery to the cooling fluid through the lower planar member.

公开(公告)号：US20200216170A1

公开(公告)日：2020-07-09

申请号：US16733806

申请日：2020-01-03

Applicant: Bell Textron Inc.

Inventor： Steven Loveland ,  Paul Charles Griffiths ,  Allen Brittain

IPC: B64C25/34 ,  B64C25/06 ,  B64C25/52

Abstract: An aircraft landing gear assembly has a longitudinally elongated frame coupled to a lower portion of a fuselage of an aircraft, the frame being capable of supporting at least a portion of the weight of the aircraft. A fairing encloses substantially all of the frame. An optional integrated step can be carried by the frame, and a longitudinally elongated aperture would be formed in the fairing adjacent the step. The step allows a user to place a foot into the aperture and onto the step. An optional door can cover the aperture, and an optional secondary step can be carried by the door.

公开(公告)号：US20200216161A1

公开(公告)日：2020-07-09

申请号：US16733240

申请日：2020-01-03

Applicant: Bell Textron Inc.

Inventor： Paul Charles Griffiths ,  Steven Loveland ,  Allen Brittain

IPC: B64C1/14

Abstract: A modular windshield has a central component and at least one side component. The central component is constructed of polycarbonate and the at least one side component is constructed of acrylic.

公开(公告)号：US11728540B2

公开(公告)日：2023-08-15

申请号：US17172366

申请日：2021-02-10

Applicant: Bell Textron Inc.

Inventor： William A. Amante ,  Steven Loveland ,  Jessica A. Revere

IPC: H01M10/6556 ,  H01M50/244 ,  H01M10/6554 ,  H01M10/625 ,  H01M10/613 ,  H01M50/249 ,  B64D29/04 ,  B64D33/08

CPC classification number: H01M50/249 ,  B64D29/04 ,  B64D33/08 ,  H01M10/613 ,  H01M10/625 ,  H01M10/6554 ,  H01M10/6556 ,  H01M50/244 ,  H01M2220/20

Abstract: A battery assembly for an aircraft includes a cold plate having an upper planar member, a lower planar member, and at least one fluid channel positioned between the upper and lower planar members and configured to receive a cooling fluid. The battery assembly also includes an upper battery mounted to the upper planar member for transferring heat from the upper battery to the cooling fluid through the upper planar member. The battery assembly further includes a lower battery mounted to the lower planar member for transferring heat from the lower battery to the cooling fluid through the lower planar member.

公开(公告)号：US11352130B2

公开(公告)日：2022-06-07

申请号：US16733806

申请日：2020-01-03

Applicant: Bell Textron Inc.

Inventor： Steven Loveland ,  Paul Charles Griffiths ,  Allen Brittain

IPC: B64C25/04 ,  B64C25/34 ,  B64C25/52 ,  B64C25/06 ,  B64C25/32

Abstract: An aircraft landing gear assembly has a longitudinally elongated frame coupled to a lower portion of a fuselage of an aircraft, the frame being capable of supporting at least a portion of the weight of the aircraft. A fairing encloses substantially all of the frame. An optional integrated step can be carried by the frame, and a longitudinally elongated aperture would be formed in the fairing adjacent the step. The step allows a user to place a foot into the aperture and onto the step. An optional door can cover the aperture, and an optional secondary step can be carried by the door.