Schubumkehrereinheit

Details

Veröffentlichungs-Nr.

EP2837810

Aktenzeichen

EP14178856

Anmeldetag

29. Juli 2014

Veröffentlichung

1. November 2017

Erteilung

1. November 2017

Rechtsraum

EP

IPC

F02K1/72

Abstract

A thrust reverser unit (TRU) 100 for a gas turbine engine 10 is provided that has first and second cascade elements 110, 120. In a stowed configuration, both the first and second cascade elements, and the operating mechanism, are located inside the nacelle 40, meaning that the TRU has no detrimental impact on the flow through the bypass duct 22. In the deployed configuration, the first cascade element 110 extends across the bypass duct 22. The first cascade element 110 has flow passages 112 that allow the flow to pass through, redirecting the flow towards the second cascade element 120. The second cascade element 120 further turns the flow so as to provide decelerating reverse thrust.

Anmelder

Firma

Rolls-Royce Deutschland Ltd & Co KG

Land

🇩🇪 Deutschland

Fachgebiete