Gestängeanordnung

Details

Veröffentlichungs-Nr.

EP3453901

Aktenzeichen

EP18182320

Anmeldetag

6. Juli 2018

Veröffentlichung

13. Mai 2020

Erteilung

13. Mai 2020

Rechtsraum

EP

IPC

F16C11/06B64D33/04F02K1/12F16C11/02F16C11/04

Abstract

Disclosed is a linkage assembly for a gas turbine engine (20) having a link (102a-102d) having a first end (104a), a second end (104b), and a rod (106) extending therebetween, the first end having a first sliding bearing (108) disposed within a first sliding bearing housing (107), a fastener (118) comprising a first flange (126a) and a second flange (126b), a pin (120) extending between the first flange and the second flange, wherein the first sliding bearing is pivotally connected to the pin; and a biasing member (136a, 136b) secured between the first flange and the sliding bearing housing, the biasing member contacting the sliding bearing housing and biasing the link against rotation about a center axis for the rod of the link.

Anmelder

Firmen

Raytheon Technologies Corporation
United Technologies Corporation

Land

🇺🇸 USA

Fachgebiete