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gptkbp:instanceOf
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patent
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gptkbp:abstract
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A method for controlling the temperature of a gas turbine engine.
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gptkbp:analyzes
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gptkb:USPTO
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gptkbp:applicationDate
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March 31, 2004
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gptkbp:applicationNumber
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10/703,174
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gptkbp:applicationType
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utility
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gptkbp:assignee
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gptkb:The_Boeing_Company
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gptkbp:citedBy
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gptkb:US_7,123,456_B2
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gptkbp:claims
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20
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gptkbp:contains
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temperature control system
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gptkbp:description
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a method for optimizing engine performance
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gptkbp:examiner
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gptkb:John_Smith
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gptkbp:fieldOfInvention
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aerospace engineering
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gptkbp:filedIn
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gptkb:The_Boeing_Company
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,029 C22
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gptkbp:internationalClassification
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F02C 7/00
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gptkbp:inventor
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gptkb:David_A._H._Houghton
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gptkbp:issuedOn
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September 14, 2004
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gptkbp:legalStatus
|
granted
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gptkbp:patentFamily
|
US_6,789,029_C22,_US_7,123,456_B2
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gptkbp:patentNumber
|
6,789,029
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gptkbp:patentType
|
granted patent
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gptkbp:priorityDate
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March 31, 2003
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gptkbp:relatedTo
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gas turbine technology
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gptkbp:status
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active
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gptkbp:title
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Method and apparatus for controlling the temperature of a gas turbine engine
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