Invention Grant
- Patent Title: Aircraft brake torque load reaction through landing gear bogie structure
-
Application No.: US15699682Application Date: 2017-09-08
-
Publication No.: US10598209B2Publication Date: 2020-03-24
- Inventor: Scott Whittle , Richard A. Kipp , Nathaniel J Herrmann
- Applicant: Goodrich Corporation
- Applicant Address: US NC Charlotte
- Assignee: Goodrich Corporation
- Current Assignee: Goodrich Corporation
- Current Assignee Address: US NC Charlotte
- Agency: Snell & Wilmer, L.L.P.
- Main IPC: F16C3/02
- IPC: F16C3/02 ; B64C25/42 ; F16D55/24 ; F16D65/02 ; B64C25/34 ; F16D55/40

Abstract:
An aircraft landing gear arrangement may comprise a landing gear bogie having an axle, a torque tube surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body extending between a first end and a second end. A flange may be disposed at the first end. A mating surface may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
Public/Granted literature
- US20190078608A1 AIRCRAFT BRAKE TORQUE LOAD REACTION THROUGH LANDING GEAR BOGIE STRUCTURE Public/Granted day:2019-03-14
Information query