US 6,789,031 C23

URI: https://gptkb.org/entity/US_6%2C789%2C031_C23
GPTKB entity
Properties (25)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling the temperature of a gas turbine engine.
gptkbp:applicationNumber 10/682,031
gptkbp:applicationType Non-provisional
gptkbp:assignee gptkb:The_Boeing_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:country gptkb:United_States
gptkbp:examiner gptkb:John_Smith
gptkbp:expirationDate September 7, 2024
gptkbp:fieldOfInvention Gas turbine engines
gptkbp:filingDate March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,031 C23
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:David_A._H._Houghton
gptkbp:issuedOn September 7, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentFamily US_6,789,031_C23,_US_7,123,456_B2
gptkbp:patentType Utility patent
gptkbp:priorityDate March 31, 2003
gptkbp:relatedTo Gas turbine technology
gptkbp:status Active
gptkbp:technicalField Aerospace engineering
gptkbp:title Method and apparatus for controlling the temperature of a gas turbine engine