US Patent 9151166 Composite gas turbine engine component
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Patent abstract
A gas turbine engine component is disclosed having a composite construction. In one embodiment the gas turbine engine component is a blade that includes a shroud. A fiber ply of the composite construction extends from an airfoil part of the blade to the shroud. The shroud can include multiple plies that can be stitched together. In one form a sealing knife is formed and coupled to the shroud. The sealing knife can be coupled to the shroud by stitching. Filler material can be used in the composite construction of the gas turbine engine component.
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US Patent 09151166 Composite gas turbine engine component US Patent 9151166 Composite gas turbine engine component
Infobox
Patent Number
0915116600
Patent Number
915116600
Edits on 6 Apr, 2023
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Infobox
Is a
Patent Jurisdiction
Patent Number
091511660
Date of Patent
October 6, 2015
0Patent Application Number
127953910
Date Filed
June 7, 2010
0Official Website
Patent Primary Examiner
Edits on 24 Sep, 2022
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Infobox
Is a
Patent Jurisdiction
Patent Number
091511660
Date of Patent
October 6, 2015
0Patent Application Number
127953910
Date Filed
June 7, 2010
0Official Website
Patent Primary Examiner
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US Patent 09151166 Composite gas turbine engine component
Infobox
Is a
Patent jurisdiction
Patent number
09151166
Date of patent
October 6, 2015
Patent application number
12795391
Date Filed
June 7, 2010
Patent primary examiner
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