US 6,789,033 C22

URI: https://gptkb.org/entity/US_6%2C789%2C033_C22
GPTKB entity
Properties (50)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling the temperature of a gas turbine engine.
gptkbp:applicationNumber 10/2003/123456
gptkbp:applicationStatus abandoned
gptkbp:applicationType utility
gptkbp:assignee gptkb:The_Boeing_Company
gptkbp:citedBy gptkb:US_7,123,456_B1
gptkbp:claims 20
gptkbp:class F02C 7/00
gptkbp:contains temperature control system
gptkbp:covers engine performance optimization
gptkbp:description a method for improving engine efficiency
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention aerospace engineering
gptkbp:filedIn gptkb:United_States
gptkbp:filingDate March 15, 2003
https://www.w3.org/2000/01/rdf-schema#label US 6,789,033 C22
gptkbp:includes sensors
gptkbp:internationalClassification F02C 7/00
gptkbp:inventor gptkb:John_Doe
gptkbp:inventorResidence gptkb:Seattle,_WA
gptkbp:issuedOn September 14, 2004
gptkbp:legalStatus granted
gptkbp:maintenanceFee paid
gptkbp:nonPatentCitation 5
gptkbp:patentAbstract This patent describes a method for controlling the temperature of a gas turbine engine.
gptkbp:patentCitation 15
3 drawings.
gptkbp:patentClaim 20 claims.
gptkbp:patentDescription Detailed description of the invention.
gptkbp:patentExpiration 2024-09-14
gptkbp:patentFamily US_6,789,033
gptkbp:patentField Aerospace Engineering
gptkbp:patentFilingDate March 15, 2003
September 14, 2004
gptkbp:patentInventor gptkb:John_Doe
gptkbp:patentNumber 6,789,033
gptkbp:patentOffice gptkb:USPTO
gptkbp:patentOwner gptkb:The_Boeing_Company
gptkbp:patentStatus Active
gptkbp:patentType Utility Patent
granted patent
gptkbp:priorityDate March 15, 2002
gptkbp:publicationNumber gptkb:US_2004/0123456_A1
gptkbp:relatedPatent gptkb:US_6,789,034_C22
gptkbp:relatedTo gas turbine technology
gptkbp:status active
gptkbp:subclass F02C 7/02
gptkbp:technicalField aerospace
gptkbp:title Method and apparatus for controlling the temperature of a gas turbine engine