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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:applicationNumber
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10/682,984
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gptkbp:applicationPublication
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US 2003/0201234 A1
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gptkbp:applicationType
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Non-provisional
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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
|
20
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gptkbp:coInventor
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gptkb:Michael_J._Smith
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gptkbp:country
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gptkb:United_States
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gptkbp:examiner
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gptkb:John_Smith
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gptkbp:fieldOfInvention
|
Gas turbine engines
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gptkbp:filingDate
|
March 29, 2002
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gptkbp:firstClaim
|
A method for controlling the temperature of a gas turbine engine comprising...
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gptkbp:grantDate
|
September 7, 2004
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,788,984 C23
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gptkbp:internationalClassification
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F02C 7/00
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gptkbp:inventor
|
gptkb:David_A._H._Houghton
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gptkbp:issuedOn
|
September 7, 2004
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gptkbp:legalStatus
|
Granted
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gptkbp:maintenanceFee
|
Required
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|
gptkbp:patentExpiration
|
2024-09-07
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gptkbp:patentFamily
|
Boeing_gas_turbine_patents
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gptkbp:patentNumber
|
6,788,984
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gptkbp:patentType
|
Utility patent
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gptkbp:priorityDate
|
March 29, 2001
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gptkbp:relatedTo
|
gptkb:US_6,123,456_B1
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gptkbp:status
|
Active
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gptkbp:title
|
Method and apparatus for controlling the temperature of a gas turbine engine
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