MOTION RESTRICTOR SYSTEM FOR AN AIRCRAFT ENGINE

A method and apparatus comprising a first wall (122) and a plurality of longitudinal members (120). The first wall is for an inlet (110) of an aircraft engine (108). The plurality of longitudinal members connects the first wall to a structure for the aircraft engine. The plurality of longitudinal me...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	STANESCU, Adrian, MAHANIAN, Saba
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A method and apparatus comprising a first wall (122) and a plurality of longitudinal members (120). The first wall is for an inlet (110) of an aircraft engine (108). The plurality of longitudinal members connects the first wall to a structure for the aircraft engine. The plurality of longitudinal members has an orientation configured to reduce motion in the inlet.