公开(公告)号：US20220204154A1

公开(公告)日：2022-06-30

申请号：US17139049

申请日：2020-12-31

Applicant: Bell Textron Inc.

Inventor： Robert W. Roe ,  Mark L. Isaac

IPC: B64C3/32 ,  B64C3/18 ,  B64C3/26

Abstract: A wing for an aircraft includes a first end, a second end, and a skin extending longitudinally from the first end to the second end. The wing also includes at least one channel positioned within the skin and extending longitudinally between the first and second ends. The at least one channel defines a longitudinal translation path for translating at least one electrical power source longitudinally between the first and second ends.

公开(公告)号：US11661172B2

公开(公告)日：2023-05-30

申请号：US17139049

申请日：2020-12-31

Applicant: Bell Textron Inc.

Inventor： Robert W. Roe ,  Mark L. Isaac

IPC: B64C3/32 ,  B64C29/00

CPC classification number: B64C3/32 ,  B64C29/0033

Abstract: A wing for an aircraft includes a first end, a second end, and a skin extending longitudinally from the first end to the second end. The wing also includes at least one channel positioned within the skin and extending longitudinally between the first and second ends. The at least one channel defines a longitudinal translation path for translating at least one electrical power source longitudinally between the first and second ends.