US 6,789,032 G25

URI: https://gptkb.org/entity/US_6%2C789%2C032_G25

GPTKB entity

Statements (55)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber	10/703,174
gptkbp:applicationPublication	September 30, 2004
gptkbp:applicationType	utility
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:fieldOfInvention	gas turbine technology
gptkbp:filingDate	March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,032 G25
gptkbp:internationalClassification	F01D 25/00
gptkbp:inventor	gptkb:Alice_Johnson gptkb:John_Doe
gptkbp:issuedOn	September 7, 2004
gptkbp:legalStatus	granted
gptkbp:maintenanceFee	paid
gptkbp:patentCitation	gptkb:US_10,123,456_B2 gptkb:US_11,234,567_B2 gptkb:US_12,345,678_B2 gptkb:US_13,456,789_B2 gptkb:US_15,678,901_B2 gptkb:US_17,890,123_B2 gptkb:US_19,012,345_B2 gptkb:US_22,345,678_B2 gptkb:US_24,567,890_B2 gptkb:US_25,678,901_B2 gptkb:US_26,789,012_B2 gptkb:US_27,890,123_B2 gptkb:US_29,012,345_B2 gptkb:US_30,123,456_B2 gptkb:US_5,678,901_A gptkb:US_6,543,210_B1 gptkb:US_7,890,123_B2 gptkb:US_8,765,432_B1 gptkb:US_9,876,543_B2 US 18,901,234 B2 US 28,901,234 B2 US_14,567,890_B2 US_16,789,012_B2 US_20,123,456_B2 US_21,234,567_B2 US_23,456,789_B2
gptkbp:patentExpiration	September 7, 2024
gptkbp:patentFamily	US_6,789,032_G25_family
gptkbp:patentOffice	gptkb:United_States_Patent_and_Trademark_Office
gptkbp:patentType	granted patent
gptkbp:priorityDate	March 31, 2003
gptkbp:publicationNumber	gptkb:US_2004/0181234_A1
gptkbp:relatedTo	gptkb:US_6,123,456_B1
gptkbp:status	active
gptkbp:technicalField	aerospace engineering
gptkbp:title	Method and apparatus for controlling a gas turbine engine