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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 a gas turbine engine to improve efficiency.
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gptkbp:applicationNumber
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10/123,456
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gptkbp:applicationPublication
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gptkb:US_2003/0123456_A1
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gptkbp:applicationStatus
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Published
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gptkbp:applicationType
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Utility
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gptkbp:assignee
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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
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20
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gptkbp:country
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gptkb:United_States
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gptkbp:examiner
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Jane_Smith
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gptkbp:fieldOfInvention
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Gas turbine technology
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gptkbp:filingCountry
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Active
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gptkbp:filingDate
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April 15, 2002
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gptkbp:grantDate
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September 7, 2004
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,027 G25
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gptkbp:internationalClassification
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F01D 21/00
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gptkbp:inventor
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gptkb:Alice_Johnson
gptkb:John_Doe
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gptkbp:issuedOn
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September 7, 2004
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gptkbp:legalStatus
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Granted
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gptkbp:maintenanceFee
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Paid
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gptkbp:patentCitation
|
gptkb:US_5,678,901_A
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gptkbp:patentClassification
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F01D
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gptkbp:patentFamily
|
US_6,789,027_G25,_US_7,123,456_B2
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gptkbp:patentFamilyMembers
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gptkb:US_6,789,042_P1
gptkb:US_6,789,039_M1
gptkb:US_6,789,041_O1
gptkb:US_6,789,046_T1
gptkb:US_6,789,047_U1
gptkb:US_6,789,048_V1
gptkb:US_6,789,033_G1
gptkb:US_6,789,050_X1
gptkb:US_6,789,034_H1
gptkb:US_6,789,030_D1
gptkb:US_6,789,028_B1
gptkb:US_6,789,029_C1
gptkb:US_6,789,038_L1
gptkb:US_6,789,031_E1
gptkb:US_6,789,043_Q1
gptkb:US_6,789,045_S1
gptkb:US_6,789,044_R1
gptkb:US_6,789,049_W1
gptkb:US_6,789,037_K1
gptkb:US_6,789,032_F1
US 6,789,036 J1
US_6,789,040_N1
US_6,789,035_I1
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gptkbp:patentNumber
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6,789,027
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gptkbp:patentOffice
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gptkb:USPTO
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gptkbp:patentType
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Granted patent
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gptkbp:priorityDate
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March 15, 2002
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gptkbp:relatedPatent
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gptkb:US_6,789,028_B1
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gptkbp:relatedTo
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Gas turbine engines
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gptkbp:status
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Active
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gptkbp:technicalField
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Aerospace engineering
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gptkbp:title
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Method and apparatus for controlling a gas turbine engine
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