US Patent 9016695 Gas turbine exhaust nozzle divergent flap seal
Patent 9016695 was granted and assigned to United Technologies on April, 2015 by the United States Patent and Trademark Office.
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Patent abstract
A seal assembly for a nozzle in a gas turbine engine includes a connector having a first hinge portion for attaching to the nozzle, a flat portion for sealing against a wall of the engine; and a first hinge for attaching the connector to the flat portion wherein the connector is adapted to rotate relative to the nozzle and the flat portion is adapted to rotate relative to the connector.
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US Patent 09016695 Gas turbine exhaust nozzle divergent flap seal US Patent 9016695 Gas turbine exhaust nozzle divergent flap seal
Infobox
Patent Number
0901669500
Patent Number
901669500
Edits on 4 Apr, 2023
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
090166950
Date of Patent
April 28, 2015
0Patent Application Number
131960740
Date Filed
August 2, 2011
0Official Website
Patent Primary Examiner
Edits on 24 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
090166950
Date of Patent
April 28, 2015
0Patent Application Number
131960740
Date Filed
August 2, 2011
0Official Website
Patent Primary Examiner
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US Patent 09016695 Gas turbine exhaust nozzle divergent flap seal
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
09016695
Date of patent
April 28, 2015
Patent application number
13196074
Date Filed
August 2, 2011
Patent primary examiner
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