US 6,789,065 G93

URI: https://gptkb.org/entity/US_6%2C789%2C065_G93
GPTKB entity
Statements (25)
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 non-provisional
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:examiner gptkb:John_Doe
gptkbp:fieldOfInvention aerospace engineering
gptkbp:filingDate November 6, 2003
gptkbp:filingLocation gptkb:United_States_Patent_and_Trademark_Office
gptkbp:firstClaim A method for controlling a gas turbine engine comprising...
https://www.w3.org/2000/01/rdf-schema#label US 6,789,065 G93
gptkbp:internationalClassification F02C 7/00
gptkbp:inventor Jane_Smith
gptkbp:issuedOn September 7, 2004
gptkbp:legalStatus granted
gptkbp:maintenanceFee paid
gptkbp:numberOfClaims 20
gptkbp:patentFamily US_6,789,065,_US_7,123,456,_US_8,765,432
gptkbp:patentLength 20 years
gptkbp:patentType utility
gptkbp:priorityDate November 6, 2003
gptkbp:relatedTo gas turbine technology
gptkbp:status active
gptkbp:title Method and apparatus for controlling a gas turbine engine