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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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10/703,174
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gptkbp:applicationPublication
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April 15, 2004
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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
|
20
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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
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Gas turbine technology
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gptkbp:filingDate
|
March 31, 2004
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https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,163 G32
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gptkbp:internationalClassification
|
F01D 25/00
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gptkbp:inventor
|
gptkb:David_A._H._Houghton
gptkb:Michael_J._Smith
gptkb:Sarah_L._Johnson
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gptkbp:issuedOn
|
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_6,890,123_B1
gptkb:US_5,123,456_A
gptkb:US_5,678,901_A
gptkb:US_6,345,678_B2
gptkb:US_6,456,789_C1
gptkb:US_6,789,012_B2
gptkb:US_7,000,000_B2
gptkb:US_7,111,111_B1
gptkb:US_7,444,444_B2
gptkb:US_6,678,901_B1
gptkb:US_7,555,555_B1
gptkb:US_6,234,567_B1
gptkb:US_7,222,222_B2
gptkb:US_7,888,888_B2
gptkb:US_7,999,999_B1
gptkb:US_6,567,890_B2
gptkb:US_7,666,666_B2
gptkb:US_7,777,777_B1
US 7,333,333 B1
|
|
gptkbp:patentExpiration
|
September 7, 2024
|
|
gptkbp:patentFamily
|
US_6,789,163_G32,_US_7,123,456_B2
|
|
gptkbp:patentType
|
Issued patent
|
|
gptkbp:priorityDate
|
March 31, 2003
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|
gptkbp:publicationNumber
|
US_6,789,163
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|
gptkbp:relatedTo
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gptkb:US_6,123,456_B1
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|
gptkbp:status
|
Active
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gptkbp:technicalField
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Aerospace engineering
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gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
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