US 6,789,031 R32

URI: https://gptkb.org/entity/US_6%2C789%2C031_R32
GPTKB entity
Properties (29)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber 10/703,155
gptkbp:applicationType Non-Provisional
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:coInventor gptkb:Jane_Doe
gptkbp:examiner gptkb:John_Smith
gptkbp:expirationDate September 7, 2024
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,031 R32
gptkbp:internationalClassification F01D 21/00
gptkbp:inventiveStep Yes
gptkbp:inventor gptkb:David_A._H._Houghton
gptkbp:issuedOn September 7, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:novelty Yes
gptkbp:patentFamily US_6,789,031_R32,_US_7,123,456_B2
gptkbp:patentNumber 6,789,031
gptkbp:patentOffice gptkb:United_States_Patent_and_Trademark_Office
gptkbp:patentType Utility
gptkbp:priorityDate March 31, 2003
gptkbp:relatedTo gptkb:US_6,123,456_B1
gptkbp:status Active
gptkbp:technicalField Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine