US 6,789,029 G71

URI: https://gptkb.org/entity/US_6%2C789%2C029_G71

GPTKB entity

Statements (63)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber	10/703,174
gptkbp:applicationType	Utility
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:claims	20
gptkbp:coInventor	gptkb:Jane_Doe
gptkbp:country	gptkb:United_States
gptkbp:examiner	gptkb:John_Smith
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,029 G71
gptkbp:internationalClassification	F01D 21/00
gptkbp:inventiveStep	Yes
gptkbp:inventor	gptkb:David_A._H._Houghton
gptkbp:issuedBy	September 7, 2004
gptkbp:legalStatus	Granted
gptkbp:maintenanceFee	Paid
gptkbp:novelty	Yes
gptkbp:patentCitation	gptkb:US_6,012,345_A8 gptkb:US_6,789,012_B5 gptkb:US_6,678,901_B4 gptkb:US_6,123,456_V9 gptkb:US_5,123,456_A gptkb:US_5,678,901_A gptkb:US_6,345,678_B2 gptkb:US_6,456,789_C1 gptkb:US_6,678,901_G4 gptkb:US_6,567,890_F3 gptkb:US_6,234,567_B1 gptkb:US_6,567,890_B3 gptkb:US_6,123,456_B9 gptkb:US_6,345,678_D1 gptkb:US_6,789,012_H5 gptkb:US_6,012,345_K8 gptkb:US_6,456,789_E2 gptkb:US_6,789,012_R5 gptkb:US_6,345,678_N1 gptkb:US_6,890,123_S6 gptkb:US_6,012,345_U8 gptkb:US_6,890,123_B6 US 6,901,234 B7 US 6,567,890 P3 US 6,901,234 J7 US 6,901,234 T7 US_6,234,567_C0 US_6,123,456_L9 US_6,234,567_M0 US_6,456,789_O2 US_6,678,901_Q4 US_6,890,123_I6
gptkbp:patentFamily	US_6,789,029_G71_family
gptkbp:patentNumber	6,789,029
gptkbp:patentOffice	gptkb:USPTO
gptkbp:patentType	Granted patent
gptkbp:priorityDate	March 31, 2003
gptkbp:publicationDate	September 7, 2004
gptkbp:relatedTo	gptkb:US_6,123,456_A1
gptkbp:status	Active
gptkbp:technologyArea	Aerospace engineering
gptkbp:title	Method and apparatus for controlling a gas turbine engine
gptkbp:utility	Yes