US 6,789,075 G50

URI: https://gptkb.org/entity/US_6%2C789%2C075_G50

GPTKB entity

Statements (65)

Predicate	Object
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	Utility
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:claims	20
gptkbp:coInventor	gptkb:Bob_Brown
gptkbp:examiner	Jane_Smith
gptkbp:expirationDate	March 31, 2024
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	March 31, 2004
gptkbp:grantDate	September 7, 2004
gptkbp:hasFieldOfUse	Aerospace
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,075 G50
gptkbp:internationalClassification	F01D 21/00
gptkbp:inventor	gptkb:Alice_Johnson gptkb:John_Doe
gptkbp:issuedOn	September 7, 2004
gptkbp:legalStatus	Granted
gptkbp:maintenanceFee	Paid
gptkbp:patentCitation	gptkb:US_6,789,008_B10 gptkb:US_6,789,027_B29 gptkb:US_6,789,003_B5 gptkb:US_6,789,005_B7 gptkb:US_5,123,456_A gptkb:US_5,654,321_A gptkb:US_6,789,000_B2 gptkb:US_6,789,001_B3 gptkb:US_6,789,007_B9 gptkb:US_6,789,009_B11 gptkb:US_6,789,010_B12 gptkb:US_6,789,026_B28 gptkb:US_6,789,004_B6 gptkb:US_6,789,006_B8 gptkb:US_6,789,014_B16 gptkb:US_6,789,015_B17 gptkb:US_6,789,025_B27 gptkb:US_6,789,002_B4 gptkb:US_6,789,019_B21 gptkb:US_6,789,028_B30 US 6,789,024 B26 US_6,789,011_B13 US_6,789,012_B14 US_6,789,013_B15 US_6,789,016_B18 US_6,789,017_B19 US_6,789,018_B20 US_6,789,020_B22 US_6,789,021_B23 US_6,789,022_B24 US_6,789,023_B25 US_6,789,029_B31 US_6,789,030_B32
gptkbp:patentFamily	gptkb:US_6,789,075
gptkbp:patentOffice	gptkb:United_States_Patent_and_Trademark_Office
gptkbp:patentType	Utility patent
gptkbp:priorityDate	March 31, 2003
gptkbp:publicationNumber	gptkb:US_2004/0181234_A1
gptkbp:relatedPatent	gptkb:US_6,789,076_B1
gptkbp:relatedTo	Gas turbine engines
gptkbp:status	Active
gptkbp:technologyArea	Energy generation
gptkbp:title	Method and apparatus for controlling a gas turbine engine