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Combustor liner constructionA combustor liner is fabricated from a plurality of individual segments each containing counter/parallel Finwall material and are arranged circumferentially and axially to define the combustion zone. Each segment is supported by a hook and ring construction to an opened lattice frame with sufficient tolerance between the hook and ring to permit thermal expansion with a minimum of induced stresses.
Document ID
19840016509
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Craig, H. M.
(United Technologies Corp. East Hartford, Conn., United States)
Wagner, W. B.
(United Technologies Corp. East Hartford, Conn., United States)
Strock, W. J.
(United Technologies Corp. East Hartford, Conn., United States)
Date Acquired
September 4, 2013
Publication Date
November 15, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-PATENT-4,414,816
Patent Number: NASA-CASE-LEW-14035-1
Patent Application Number: US-PATENT-APPL-SN-136652
Accession Number
84N24577
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,414,816|NASA-CASE-LEW-14035-1
Patent Application
US-PATENT-APPL-SN-136652
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