gptkbp:instanceOf
|
patent
|
gptkbp:abstract
|
A method for controlling a gas turbine engine.
|
gptkbp:applicationNumber
|
10/123,456
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gptkbp:applicationStatus
|
published
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gptkbp:applicationType
|
utility
|
gptkbp:assignee
|
gptkb:General_Electric_Company
|
gptkbp:citedBy
|
gptkb:US_7,123,456_B2
|
gptkbp:country
|
gptkb:United_States
|
gptkbp:documentType
|
patent document
|
gptkbp:examiner
|
gptkb:Michael_Johnson
|
gptkbp:family
|
gptkb:US_6,789,959_A1
gptkb:US_6,789,958_C1
gptkb:US_6,789,957_B2
|
gptkbp:fieldOfInvention
|
aerospace engineering
|
gptkbp:filingDate
|
2004-02-06
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,957 C5 family
|
gptkbp:internationalClassification
|
F02C 7/00
|
gptkbp:inventor
|
gptkb:John_Doe
Jane_Smith
|
gptkbp:issueDate
|
2004-09-14
|
gptkbp:language
|
English
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gptkbp:legalStatus
|
granted
|
gptkbp:maintenanceFee
|
paid
|
gptkbp:patentNumber
|
6,789,957
|
gptkbp:patentType
|
granted patent
|
gptkbp:priorityDate
|
2003-02-06
|
gptkbp:publicationNumber
|
2004/0123456 A1
|
gptkbp:relatedPatent
|
gptkb:US_6,789,971_A2
gptkb:US_6,789,983_A1
gptkb:US_6,789,980_A4
gptkb:US_6,789,965_A1
gptkb:US_6,789,990_B4
gptkb:US_6,789,975_B2
gptkb:US_6,789,996_B1
gptkb:US_6,789,963_B4
gptkb:US_6,789,972_B1
gptkb:US_6,789,992_A1
gptkb:US_6,789,984_B2
gptkb:US_6,789,961_C2
gptkb:US_6,789,985_C3
gptkb:US_6,789,977_A3
gptkb:US_6,789,987_B1
gptkb:US_6,789,960_B1
gptkb:US_6,789,988_C2
gptkb:US_6,789,997_C2
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gptkb:US_6,789,974_A1
gptkb:US_6,789,978_B1
gptkb:US_6,789,993_B2
gptkb:US_6,789,962_A3
gptkb:US_6,789,970_C6
gptkb:US_6,789,994_C3
gptkb:US_6,789,967_C3
gptkb:US_6,789,981_B5
gptkb:US_6,789,969_B5
gptkb:US_6,789,976_C4
gptkb:US_6,789,998_A3
gptkb:US_6,789,968_A4
gptkb:US_6,789,964_C5
gptkb:US_6,789,989_A3
US_6,789,973_C3
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US_6,789,986_A4
US_6,789,991_C5
US_6,789,995_A4
|
gptkbp:relatedTo
|
gas turbine technology
|
gptkbp:status
|
active
|
gptkbp:technologyArea
|
energy production
|
gptkbp:title
|
Method for controlling a gas turbine engine
|