US 6,789,072 G64

GPTKB entity

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber	10/703,198
gptkbp:applicationType	utility
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:claims	20
gptkbp:class	F02C 7/00
gptkbp:country	gptkb:United_States
gptkbp:examiner	gptkb:John_Smith
gptkbp:fieldOfInvention	gas turbine engines
gptkbp:filingCountry	gptkb:US
gptkbp:filingDate	March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,072 G64
gptkbp:internationalClassification	F02C 7/00
gptkbp:inventor	gptkb:Alice_Johnson gptkb:David_A._H._Houghton gptkb:Michael_J._Smith
gptkbp:issuedBy	September 7, 2004
gptkbp:legalStatus	granted
gptkbp:maintenanceFee	paid
gptkbp:patentCitation	gptkb:US_6,123,456_B10 gptkb:US_6,890,123_B7 gptkb:US_6,012,345_B9 gptkb:US_6,678,901_B5 gptkb:US_5,123,456_A gptkb:US_5,678,901_A gptkb:US_6,345,678_B2 gptkb:US_6,890,123_B17 gptkb:US_6,234,567_B1 gptkb:US_6,456,789_B13 gptkb:US_6,123,456_B20 gptkb:US_6,567,890_B4 gptkb:US_6,456,789_B3 gptkb:US_6,789,012_B16 US 6,901,234 B8 US 6,901,234 B18 US_6,012,345_B19 US_6,234,567_B11 US_6,345,678_B12 US_6,567,890_B14 US_6,678,901_B15 US_6,789,012_B6
gptkbp:patentFamily	US_6,789,072_G64_family
gptkbp:patentType	granted patent
gptkbp:priorityDate	March 31, 2003
gptkbp:publicationNumber	US 2004/0200000 A1
gptkbp:relatedTo	gptkb:US_6,123,456_B1
gptkbp:status	active
gptkbp:subclass	F02C_7/10
gptkbp:title	Method and apparatus for controlling a gas turbine engine