US Patent 9011079 Turbine nozzle compartmentalized cooling system
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Patent abstract
The present application provides a compartmentalized cooling system for providing a cooling flow in a turbine with a flow of combustion gases therein. The compartmentalized cooling system may include a turbine nozzle and a cooling baffle. The turbine nozzle may include an airfoil insert and a nozzle outer sidewall. The cooling baffle may include a high pressure cooling passage in communication with the airfoil insert in a first circuit and an impingement plate positioned about the nozzle outer sidewall in a second circuit.
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US Patent 09011079 Turbine nozzle compartmentalized cooling system US Patent 9011079 Turbine nozzle compartmentalized cooling system
Infobox
Patent Number
0901107900
Patent Number
901107900
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Official Website
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Patent Jurisdiction
Patent Number
090110790
Date of Patent
April 21, 2015
0Patent Application Number
133457810
Date Filed
January 9, 2012
0Official Website
Patent Primary Examiner
Edits on 27 Sep, 2022
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Infobox
Is a
Patent Jurisdiction
Patent Number
090110790
Date of Patent
April 21, 2015
0Patent Application Number
133457810
Date Filed
January 9, 2012
0Official Website
Patent Primary Examiner
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US Patent 09011079 Turbine nozzle compartmentalized cooling system
Infobox
Is a
Patent jurisdiction
Patent number
09011079
Date of patent
April 21, 2015
Patent application number
13345781
Date Filed
January 9, 2012
Patent primary examiner
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