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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 efficiency.
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|
gptkbp:applicationNumber
|
10/123,456
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gptkbp:applicationStatus
|
Granted
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|
gptkbp:applicationType
|
Utility
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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:country
|
gptkb:United_States
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gptkbp:examiner
|
Jane_Smith
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gptkbp:expirationDate
|
February 3, 2024
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|
gptkbp:fieldOfInvention
|
Gas turbine technology
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|
gptkbp:filingDate
|
April 1, 2002
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|
gptkbp:hasFieldOfUse
|
Aerospace
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|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,246 S80
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|
gptkbp:internationalClassification
|
F01D 25/00
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|
gptkbp:inventor
|
gptkb:Alice_Johnson
gptkb:John_Doe
gptkb:Robert_Brown
|
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gptkbp:issueDate
|
February 3, 2004
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|
gptkbp:issuedBy
|
February 3, 2004
|
|
gptkbp:legalStatus
|
Granted
|
|
gptkbp:maintenanceFee
|
Paid
|
|
gptkbp:patentCitation
|
gptkb:US_6,789,257_S80
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gptkb:US_5,123,456_A
gptkb:US_5,987,654_A
gptkb:US_6,123,456_B1
gptkb:US_6,789,248_S80
gptkb:US_6,789,263_S80
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gptkb:US_6,789,253_S80
US_6,789,256_S80
US_6,789,254_S80
|
|
gptkbp:patentFamily
|
US_6,789,246_S80,_US_6,789,245_S80
|
|
gptkbp:patentNumber
|
6,789,246
|
|
gptkbp:patentOffice
|
gptkb:USPTO
|
|
gptkbp:patentType
|
Utility patent
|
|
gptkbp:priorityDate
|
March 15, 2002
|
|
gptkbp:publicationDate
|
August 12, 2004
|
|
gptkbp:relatedPatent
|
gptkb:US_6,789,245_S80
|
|
gptkbp:relatedTo
|
gptkb:US_6,789,245_S80
|
|
gptkbp:status
|
Active
|
|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
|