US 6,789,059 G29

GPTKB entity

Statements (23)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber 10/703,174
gptkbp:applicationStatus Granted
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,059 G29
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:John_Doe
gptkbp:issuedOn September 7, 2004
gptkbp:legalStatus Active
gptkbp:maintenanceFee Paid
gptkbp:numberOfClaims 20
gptkbp:patentFamily US 6,789,059 G29, US 6,123,456 B1
gptkbp:patentType Utility patent
gptkbp:priorityDate March 31, 2003
gptkbp:relatedPatent gptkb:US_6,123,456_B1
gptkbp:status Active
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine