US Patent 8240985 Shroud segment arrangement for gas turbine engines
Patent 8240985 was granted and assigned to Pratt & Whitney Canada on August, 2012 by the United States Patent and Trademark Office.
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Patent abstract
The gas turbine engine shroud comprises a plurality of circumferentially-disposed and concentric shroud segments. Each shroud segment has an arc-shaped platform with opposite ends, each end comprising an inter-segment seal slot, at least one slot extending substantially across each corresponding end and having a lengthwise-variable depth.
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Patent Inventor Names
Yves Martin0
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Patent Citations Received
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US Patent 08240985 Shroud segment arrangement for gas turbine engines US Patent 8240985 Shroud segment arrangement for gas turbine engines
Infobox
Patent Number
082409850
Patent Number
82409850
Edits on 29 Apr, 2023
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
082409850
Date of Patent
August 14, 2012
0Patent Application Number
121112230
Date Filed
April 29, 2008
0Patent Primary Examiner
Edits on 15 Dec, 2021
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Infobox (+8 properties)
US Patent 08240985 Shroud segment arrangement for gas turbine engines
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08240985
Date of patent
August 14, 2012
Patent application number
12111223
Date Filed
April 29, 2008
Patent primary examiner
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