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Combustor liner support assemblyA support assembly for a gas turbine engine combustor includes an annular frame having a plurality of circumferentially spaced apart tenons, and an annular combustor liner disposed coaxially with the frame and including a plurality of circumferentially spaced apart tenons circumferentially adjoining respective ones of the frame tenons for radially and tangentially supporting the liner to the frame while allowing unrestrained differential thermal radial movement therebetween.
Document ID
20080004005
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Halila, Ely E.
Date Acquired
August 24, 2013
Publication Date
March 8, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-014886
Patent Number: US-PATENT-5,291,732
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,291,732
Patent Application
US-PATENT-APPL-SN-014886

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