公开(公告)号：US20230257100A1

公开(公告)日：2023-08-17

申请号：US18137000

申请日：2023-04-20

Applicant: Textron Innovations 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.

公开(公告)号：US09199732B2

公开(公告)日：2015-12-01

申请号：US14101953

申请日：2013-12-10

Applicant: TEXTRON INNOVATIONS INC.

Inventor： Mark L. Isaac ,  David A. Elliott ,  Brent C. Ross

IPC: B64C27/22 ,  B64C29/00 ,  B64D35/04 ,  B64D35/08 ,  B64D29/00 ,  B64D35/00

CPC classification number: B64C29/0033 ,  B64D29/00 ,  B64D35/00 ,  B64D35/04 ,  B64D35/08

Abstract: The system of the present application includes an engine and pylon arrangement for a tilt rotor aircraft in which the engine is fixed in relation to a wing portion of the aircraft, while the pylon is rotatable. The pylon supports a rotor hub having a plurality of rotor blades. Rotation of the pylon allows the aircraft to selectively fly in a helicopter mode and an airplane mode, as well as any combination thereof.

Abstract translation: 本申请的系统包括用于倾斜转子飞机的发动机和塔架布置，其中发动机相对于飞行器的翼部分固定，而塔架可旋转。 塔架支撑具有多个转子叶片的转子轮毂。 塔架的旋转允许飞机选择性地以直升机模式和飞行模式飞行，以及它们的任何组合。