US 6,789,031 F26

GPTKB entity

Properties (25)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/123,456
gptkbp:applicationType Utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:class F01D 21/00
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate April 15, 2003
https://www.w3.org/2000/01/rdf-schema#label US 6,789,031 F26
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:John_Doe
gptkbp:issueDate February 3, 2004
gptkbp:issuedBy February 3, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentFamily US_6,789,031_F26,_US_7,123,456_B2
gptkbp:patentOffice gptkb:United_States_Patent_and_Trademark_Office
gptkbp:priorityDate March 15, 2002
gptkbp:relatedTo gptkb:US_6,789,030_F26
gptkbp:status Active
gptkbp:technologyDomain Aerospace engineering
gptkbp:title Method for controlling a gas turbine engine