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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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10/682,015
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gptkbp:applicationStatus
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Granted
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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_B2
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gptkbp:claims
|
20
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gptkbp:effectiveDate
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September 7, 2004
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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:filingDate
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March 31, 2004
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gptkbp:firstClaim
|
A method for controlling a gas turbine engine comprising...
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,015 G65
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gptkbp:internationalClassification
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F01D 25/00
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gptkbp:inventor
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gptkb:John_Doe
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gptkbp:inventorCountry
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gptkb:USA
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gptkbp:legalStatus
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Enforceable
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gptkbp:maintenanceFee
|
Paid
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gptkbp:patentCitation
|
gptkb:US_5,123,456_A
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gptkbp:patentClassification
|
Class 60
Subclass 39
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gptkbp:patentExpiration
|
2024-09-07
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gptkbp:patentFamily
|
US,_EP,_JP
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gptkbp:patentOffice
|
gptkb:USPTO
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gptkbp:patentType
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Utility
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gptkbp:priorityDate
|
March 31, 2003
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gptkbp:publicationNumber
|
gptkb:US_2004/0181234_A1
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gptkbp:relatedPatent
|
gptkb:US_6,789,016_G65
|
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gptkbp:status
|
Active
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gptkbp:technicalField
|
Aerospace engineering
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gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
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