BOSS FOR GAS TURBINE ENGINE
A gas turbine engine (10), has: a case (32) extending circumferentially around a central axis (11) of the gas turbine engine (10); a boss (140) protruding from the case (32) away from the central axis (11), the boss (140) defining an internal passage (142c); a tubular member (162) received within th...
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | A gas turbine engine (10), has: a case (32) extending circumferentially around a central axis (11) of the gas turbine engine (10); a boss (140) protruding from the case (32) away from the central axis (11), the boss (140) defining an internal passage (142c); a tubular member (162) received within the internal passage (142c) of the boss (140) and secured to the boss (140); an annular gap (164) extending all around the tubular member (162) and located between the tubular member (162) and the boss (40, 140); and a fitting (56) hydraulically connecting a fluid source to the tubular member (162), the fitting (56) having a portion received within the tubular member (162) and encircled by both of the annular gap (164) and the tubular member (162), the fitting (56) sealingly engaged to the tubular member (162). |
---|