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gptkbp:instanceOf
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patent
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gptkbp:abstract
|
A method for controlling a gas turbine engine to improve performance.
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gptkbp:applicationNumber
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10/682,027
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gptkbp:applicationPublicationNumber
|
2003/0123456 A1
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gptkbp:applicationType
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Non-Provisional
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gptkbp:assignee
|
gptkb:General_Electric_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
|
gptkb:Jane_Doe
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gptkbp:examiner
|
gptkb:John_Smith
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gptkbp:expirationDate
|
March 29, 2023
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gptkbp:fieldOfInvention
|
Gas turbine engines
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gptkbp:fieldOfUse
|
Gas turbine control systems
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gptkbp:filingDate
|
March 29, 2003
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gptkbp:grantDate
|
September 14, 2004
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,027 R17
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gptkbp:internationalClassification
|
F02C 7/00
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gptkbp:inventiveStep
|
Yes
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gptkbp:inventor
|
gptkb:David_A._H._Houghton
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gptkbp:issuedOn
|
September 14, 2004
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gptkbp:legalStatus
|
Granted
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gptkbp:maintenanceFee
|
Paid
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gptkbp:novelty
|
Yes
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gptkbp:patentCitation
|
gptkb:US_5,678,901_A
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gptkbp:patentClassification
|
Class 60
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gptkbp:patentFamily
|
US 6,789,027 R17, US 6,123,456 B1
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gptkbp:patentNumber
|
gptkb:US_6,789,027_R17
6,789,027
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gptkbp:patentOffice
|
gptkb:United_States_Patent_and_Trademark_Office
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gptkbp:patentType
|
Utility
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gptkbp:priorityDate
|
March 29, 2001
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gptkbp:relatedPatent
|
gptkb:US_6,123,456_B1
|
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gptkbp:relatedTo
|
gptkb:US_6,123,456_B1
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gptkbp:status
|
Active
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gptkbp:technologyArea
|
Aerospace Engineering
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gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
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