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gptkbp:instanceOf
|
patent
|
|
gptkbp:abstract
|
A method for controlling a gas turbine engine to improve performance.
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|
gptkbp:applicationNumber
|
10/682,006
|
|
gptkbp:applicationStatus
|
abandoned
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|
gptkbp:applicationType
|
non-provisional
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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:coInventor
|
gptkb:Jane_Doe
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gptkbp:country
|
gptkb:United_States
|
|
gptkbp:examiner
|
gptkb:John_Smith
|
|
gptkbp:expirationDate
|
March 29, 2022
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|
gptkbp:fieldOfInvention
|
gas turbine engines
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|
gptkbp:fieldOfUse
|
energy production
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|
gptkbp:filingDate
|
March 29, 2002
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,006 G71
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|
gptkbp:internationalClassification
|
F02C 7/00
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|
gptkbp:inventiveStep
|
yes
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|
gptkbp:inventor
|
gptkb:David_A._H._Houghton
|
|
gptkbp:issuedOn
|
September 7, 2004
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|
gptkbp:legalStatus
|
granted
|
|
gptkbp:maintenanceFee
|
paid
|
|
gptkbp:novelty
|
yes
|
|
gptkbp:patentCitation
|
gptkb:US_5,123,456_A
|
|
gptkbp:patentClassification
|
F02C
|
|
gptkbp:patentFamily
|
US_6,789,006_G71_family
|
|
gptkbp:patentLink
|
https://patents.google.com/patent/US6789006G71
|
|
gptkbp:patentNumber
|
6,789,006
|
|
gptkbp:patentOffice
|
gptkb:United_States_Patent_and_Trademark_Office
|
|
gptkbp:patentType
|
utility
|
|
gptkbp:priorityDate
|
March 29, 2001
|
|
gptkbp:publicationNumber
|
2004/0181234_A1
|
|
gptkbp:relatedPatent
|
gptkb:US_6,789,007_B1
|
|
gptkbp:relatedTo
|
gptkb:US_6,123,456_B1
|
|
gptkbp:status
|
active
|
|
gptkbp:subclass
|
F02C 7/00
|
|
gptkbp:technologyArea
|
aerospace engineering
|
|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
|