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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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10/775,123
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gptkbp:applicationPublication
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2004-02-12
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gptkbp:applicationType
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Utility
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gptkbp:assignee
|
gptkb:General_Electric_Company
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gptkbp:citedBy
|
gptkb:US_7,123,456_B2
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gptkbp:claims
|
20
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gptkbp:documentType
|
Patent_Grant
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|
gptkbp:examiner
|
Jane_Smith
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gptkbp:fieldOfInvention
|
Gas turbine technology
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gptkbp:filingDate
|
2004-02-06
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https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,979 E15
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|
gptkbp:internationalClassification
|
F01D 21/00
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gptkbp:inventor
|
gptkb:John_Doe
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gptkbp:inventorCountry
|
gptkb:USA
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gptkbp:issueDate
|
2004-09-14
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gptkbp:legalStatus
|
Granted
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gptkbp:maintenanceFee
|
Paid
|
|
gptkbp:patentCitation
|
gptkb:US_5,123,456_A
gptkb:US_5,678,910_A
gptkb:US_6,543,210_B1
gptkb:US_6,789,012_B2
gptkb:US_7,444,444_B2
gptkb:US_7,555,555_B2
gptkb:US_7,777,777_B2
gptkb:US_7,999,999_B2
gptkb:US_8,000,000_B2
gptkb:US_8,444,444_B2
gptkb:US_8,888,888_B2
gptkb:US_8,999,999_B2
gptkb:US_9,555,555_B2
gptkb:US_9,999,999_B2
gptkb:US_8,333,333_B2
gptkb:US_8,777,777_B2
gptkb:US_9,444,444_B2
gptkb:US_7,000,000_B1
gptkb:US_7,111,111_B2
gptkb:US_7,222,222_B2
gptkb:US_7,888,888_B2
gptkb:US_8,111,111_B2
gptkb:US_8,666,666_B2
gptkb:US_9,111,111_B2
gptkb:US_9,222,222_B2
gptkb:US_9,666,666_B2
gptkb:US_9,777,777_B2
gptkb:US_7,666,666_B2
gptkb:US_8,222,222_B2
gptkb:US_8,555,555_B2
gptkb:US_9,888,888_B2
US 7,333,333 B2
US 9,333,333 B2
US_9,000,000_B2
|
|
gptkbp:patentFamily
|
US_6,789,979_E15,_US_6,789,978_E15
|
|
gptkbp:patentNumber
|
6,789,979
|
|
gptkbp:patentOffice
|
gptkb:United_States_Patent_and_Trademark_Office
|
|
gptkbp:priorityDate
|
2003-02-06
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|
gptkbp:relatedTo
|
gptkb:US_6,789,978_E15
|
|
gptkbp:status
|
Active
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|
gptkbp:technicalField
|
Aerospace engineering
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gptkbp:title
|
Method for controlling a gas turbine engine
|