US Patent 9982541 Gas turbine engine flow path member
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Patent abstract
A gas turbine engine flow path member is disclosed which includes an extending end portion capable of contacting a surface of the turbine engine. The flow path member includes openings to pass a cooling fluid to cool the extending end portion. The flow path member, furthermore, can be made using a variety of approaches. To set forth just two non-limiting examples, the flow path member can be cast and it can be a laminated construction.
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Patent Inventor Names
Jeffrey F. Rhodes0
Okey Kwon0
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US Patent 09982541 Gas turbine engine flow path member US Patent 9982541 Gas turbine engine flow path member
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Patent Number
099825410
Patent Number
99825410
Edits on 31 Mar, 2023
Golden AI
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Patent Jurisdiction
Patent Number
099825410
Date of Patent
May 29, 2018
0Patent Application Number
147321530
Date Filed
June 5, 2015
0Patent Primary Examiner
Edits on 20 Jan, 2022
Golden AI
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US Patent 09982541 Gas turbine engine flow path member
Infobox
Is a
Patent jurisdiction
Patent number
09982541
Date of patent
May 29, 2018
Patent application number
14732153
Date Filed
June 5, 2015
Patent primary examiner
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