Schubumkehrfächerdüse mit Veränderbarem Strömungsquerschnitt

Details

Veröffentlichungs-Nr.

EP2987991

Aktenzeichen

EP15181071

Anmeldetag

14. August 2015

Veröffentlichung

31. März 2021

Erteilung

31. März 2021

Rechtsraum

EP

IPC

F02K1/12F02K1/70F02K1/76

Abstract

A thrust reverse variable area nozzle system for a nacelle of an aircraft engine system may include a reverse thrust opening disposed in the nacelle, and a thrust reverser door pivotally movable relative to the nacelle for selectively covering the reverse thrust opening, wherein the thrust reverser door is pivotally movable between a first position for completely covering the reverse thrust opening, a second position for partially uncovering a forward portion of the reverse thrust opening and discharging a bypass airflow through the forward portion of the reverse thrust opening in a forward direction, and a third position for partially uncovering an aft portion of the reverse thrust opening and discharging the bypass airflow through the aft portion of the reverse thrust opening in an aft direction.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete