gptkbp:instanceOf
|
patent
|
gptkbp:abstract
|
A method for controlling a gas turbine engine to improve efficiency.
|
gptkbp:applicationNumber
|
10/703,174
|
gptkbp:applicationStatus
|
Granted
|
gptkbp:applicationType
|
Non-Provisional
|
gptkbp:assignee
|
gptkb:General_Electric_Company
|
gptkbp:citedBy
|
gptkb:US_7,123,456_B2
|
gptkbp:claims
|
20
|
gptkbp:country
|
gptkb:United_States
|
gptkbp:examiner
|
Jane_Smith
|
gptkbp:expirationDate
|
September 7, 2024
|
gptkbp:fieldOfInvention
|
Gas turbine technology
|
gptkbp:filingDate
|
March 31, 2004
|
gptkbp:hasFieldOfUse
|
Aerospace
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,038 G43
|
gptkbp:internationalClassification
|
F01D 25/00
|
gptkbp:inventor
|
gptkb:John_Doe
|
gptkbp:issueDate
|
September 7, 2004
|
gptkbp:issuedOn
|
September 7, 2004
|
gptkbp:language
|
English
|
gptkbp:legalStatus
|
Active
|
gptkbp:maintenanceFee
|
Paid
|
gptkbp:numberOfFigures
|
5
|
gptkbp:pageCount
|
12
|
gptkbp:patentCitation
|
gptkb:US_6,789,114_B1
gptkb:US_6,789,119_B2
gptkb:US_6,789,067_B2
gptkb:US_6,789,093_B2
gptkb:US_6,789,115_B2
gptkb:US_6,789,045_B1
gptkb:US_6,789,111_B2
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gptkb:US_6,789,120_B1
gptkb:US_6,789,096_B1
gptkb:US_5,123,456_A
gptkb:US_5,987,654_A
gptkb:US_6,123,456_B1
gptkb:US_6,789,012_B2
gptkb:US_6,789,078_B1
gptkb:US_6,789,102_B1
gptkb:US_6,789,110_B1
gptkb:US_6,789,105_B2
gptkb:US_6,789,101_B2
gptkb:US_6,789,099_B2
gptkb:US_6,789,103_B2
gptkb:US_6,789,109_B2
gptkb:US_6,789,116_B1
gptkb:US_6,789,118_B1
gptkb:US_6,789,113_B2
gptkb:US_6,789,117_B2
gptkb:US_6,789,092_B1
gptkb:US_6,789,098_B1
gptkb:US_6,789,106_B1
gptkb:US_6,789,097_B2
gptkb:US_6,789,104_B1
gptkb:US_6,789,112_B1
gptkb:US_6,789,090_B1
gptkb:US_6,789,095_B2
gptkb:US_6,789,094_B1
gptkb:US_6,789,089_B2
gptkb:US_6,789,107_B2
gptkb:US_6,789,091_B2
gptkb:US_6,789,100_B1
|
gptkbp:patentClassification
|
Utility Patent
|
gptkbp:patentFamily
|
US_6,789,038_G43,_US_6,789,037_G43
|
gptkbp:patentNumber
|
6,789,038
|
gptkbp:patentOffice
|
gptkb:USPTO
|
gptkbp:patentType
|
Utility
|
gptkbp:priorityDate
|
March 31, 2003
|
gptkbp:relatedPatent
|
US_6,789,037_G43
|
gptkbp:relatedTo
|
US_6,789,037_G43
|
gptkbp:status
|
Active
|
gptkbp:subclass
|
F01D 25/00
|
gptkbp:technologyArea
|
Energy conversion
|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
|