Hybrider Artikulierender/translatorischer Hinterkantenumkehrer

Details

Veröffentlichungs-Nr.

EP3564517

Aktenzeichen

EP19172094

Anmeldetag

1. Mai 2019

Veröffentlichung

30. Juni 2021

Erteilung

30. Juni 2021

Rechtsraum

EP

IPC

F02K1/60F02K1/70F02K1/76

Abstract

A thrust reverser (200) for a gas turbine engine may comprise a frame (210), a first reverser door (202) pivotally mounted to the frame (210) at a first pivot point (280), a second reverser door (204) pivotally mounted to the frame (210) at a second pivot point (282), a first nacelle (206) defining a first trailing edge of the gas turbine engine coupled between the frame (210) and the first reverser door (202), and a second nacelle (208) defining a second trailing edge of the gas turbine engine coupled between the frame (210) and the second reverser door (206). The first nacelle (206) and the second nacelle (208) translate in an aft and radial outward direction (294) relative to the gas turbine engine in response to the thrust reverser (200) moving to a deployed position.

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete