METHOD OF MANUFACTURING FAIRING SEAL WITH INTEGRATED SEAL

PROBLEM TO BE SOLVED: To provide a method of manufacturing a fairing and an integrated seal in the fairing used in a gas turbine engine. SOLUTION: This method of manufacturing the integrated seal includes the steps of: supplying a component having an edge portion; forming a profile on the edge porti...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	GARTEN SCOTT ALAN, MEHTA SAMIR MAHENDRA, KALAANI ELI B, DINSER STEVEN EDWARD, TUDOR COURTNEY JAMES
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a method of manufacturing a fairing and an integrated seal in the fairing used in a gas turbine engine. SOLUTION: This method of manufacturing the integrated seal includes the steps of: supplying a component having an edge portion; forming a profile on the edge portion; supplying a seal; applying a bond preparation on a surface on the edge portion; applying a bonding material on the seal; mounting the seal to the edge portion; and curing bond. A method of assembling a stator assembly includes the steps of: providing a vane; providing a first fairing; providing a second fairing located near the second side of the vane, the second fairing having a second seal coupled to the second edge portion of the second fairing; and engaging a portion of the first seal with a portion of the second seal. COPYRIGHT: (C)2011,JPO&INPIT