US 6,789,593 E42

URI: https://gptkb.org/entity/US_6%2C789%2C593_E42

GPTKB entity

Properties (58)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine.
gptkbp:applicationNumber	10/646,123
gptkbp:applicationPublication	gptkb:US_2004/0123456_A1
gptkbp:applicationType	Non-Provisional
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:claims	20
gptkbp:coInventor	gptkb:Alice_Johnson
gptkbp:examiner	Jane_Smith
gptkbp:expirationDate	September 7, 2024
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	February 7, 2003
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,593 E42
gptkbp:internationalClassification	F01D 25/00
gptkbp:inventor	gptkb:John_Doe
gptkbp:inventorCountry	gptkb:USA
gptkbp:issuedOn	September 7, 2004
gptkbp:legalStatus	Granted
gptkbp:location	gptkb:United_States
gptkbp:maintenanceFee	Paid
gptkbp:patentCitation	gptkb:US_10,123,456_B1 gptkb:US_11,234,567_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_B1 gptkb:US_25,678,901_B2 gptkb:US_27,890,123_B2 gptkb:US_29,012,345_B2 gptkb:US_5,123,456_A gptkb:US_5,987,654_A gptkb:US_6,123,456_B1 gptkb:US_7,654,321_B2 gptkb:US_8,123,456_B1 gptkb:US_9,876,543_B2 gptkb:US_30,123,456_B1 gptkb:US_6,789,592_E41 US 18,901,234 B1 US 28,901,234 B1 US_12,345,678_B1 US_14,567,890_B1 US_16,789,012_B1 US_20,123,456_B1 US_21,234,567_B2 US_23,456,789_B2 US_24,567,890_B1 US_26,789,012_B1
gptkbp:patentFamily	US_6,789,593_E42_family
gptkbp:patentNumber	6,789,593
gptkbp:patentOffice	gptkb:USPTO
gptkbp:patentType	Utility
gptkbp:priorityDate	March 31, 2003
gptkbp:relatedTo	gptkb:US_6,789,592_E41
gptkbp:status	Active
gptkbp:technicalField	Aerospace engineering
gptkbp:title	Method and apparatus for controlling a gas turbine engine