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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 performance.
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gptkbp:applicationNumber
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10/703,174
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gptkbp:applicationPublication
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gptkb:US_2004/0123456_A1
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gptkbp:applicationType
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Non-provisional
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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_B1
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gptkbp:claims
|
20 claims
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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:expirationDate
|
September 7, 2024
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gptkbp:fieldOfInvention
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Gas turbine technology
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gptkbp:filingDate
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March 31, 2004
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,088 C62
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gptkbp:internationalClassification
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F01D 25/00
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gptkbp:inventor
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gptkb:David_A._H._Houghton
gptkb:Michael_J._Smith
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gptkbp:issuedOn
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September 7, 2004
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gptkbp:legalStatus
|
Granted
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gptkbp:maintenanceFee
|
Paid
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gptkbp:patentCitation
|
gptkb:US_6,789,013_B2
gptkb:US_5,123,456_A
gptkb:US_5,678,901_A
gptkb:US_6,123,456_B2
gptkb:US_6,789,016_B5
gptkb:US_6,789,012_B1
gptkb:US_6,789,019_B8
gptkb:US_6,789,023_B12
gptkb:US_6,789,015_B4
gptkb:US_6,789,017_B6
gptkb:US_6,789,021_B10
gptkb:US_6,789,014_B3
gptkb:US_6,789,018_B7
gptkb:US_6,789,028_B17
gptkb:US_6,789,022_B11
gptkb:US_6,789,027_B16
gptkb:US_6,789,020_B9
US 6,789,024 B13
US_6,789,025_B14
US_6,789,026_B15
US_6,789,029_B18
US_6,789,030_B19
US_6,789,031_B20
|
|
gptkbp:patentFamily
|
US_6,789,088,_US_6,789,087
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|
gptkbp:patentNumber
|
6,789,088
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|
gptkbp:patentType
|
Utility patent
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|
gptkbp:priorityDate
|
March 31, 2003
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|
gptkbp:relatedTo
|
gptkb:US_6,789,087_C62
|
|
gptkbp:status
|
Active
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|
gptkbp:technicalField
|
Aerospace engineering
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gptkbp:title
|
Method for controlling a gas turbine engine
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