US 6,790,009 W63

URI: https://gptkb.org/entity/US_6%2C790%2C009_W63
GPTKB entity
Properties (26)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber 10/682,198
gptkbp:applicationPublicationNumber gptkb:US_2004/0123456_A1
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:effectiveDate September 14, 2004
gptkbp:examiner gptkb:John_Smith
gptkbp:fieldOfInvention gas turbine technology
gptkbp:filingDate October 7, 2003
https://www.w3.org/2000/01/rdf-schema#label US 6,790,009 W63
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:Robert_J._H._Houghton
gptkbp:legalStatus granted
gptkbp:maintenanceFee paid
gptkbp:patentFamily US_6,790,009_W63,_US_7,123,456_B2
gptkbp:patentNumber 6,790,009
gptkbp:patentType granted patent
gptkbp:priorityDate March 29, 2001
gptkbp:relatedPatent gptkb:US_6,123,456_B1
gptkbp:status active
gptkbp:technicalField aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine