US 6,789,033 R17

GPTKB entity

Properties (59)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/682,033
gptkbp:applicationPublicationNumber gptkb:US_2003/0123456_A1
gptkbp:applicationType utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:country gptkb:United_States
gptkbp:documentType patent document
gptkbp:effectiveDate September 14, 2004
gptkbp:examiner Jane_Smith
gptkbp:expirationDate September 14, 2024
gptkbp:fieldOfInvention gas turbine technology
gptkbp:filingDate March 29, 2002
gptkbp:grantDate September 14, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,033 R17
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:Alice_Johnson
gptkb:John_Doe
gptkbp:language English
gptkbp:legalStatus active
gptkbp:maintenanceFee paid
gptkbp:nonPatentCitation 5
gptkbp:patentAbstract aerospace engineering.
A method for controlling a gas turbine engine.
This invention relates to a method for controlling a gas turbine engine.
gptkbp:patentAssignee General_Electric.
gptkbp:patentCitation 15
gptkbp:patentClaim 20 claims.
gptkbp:patentClassification mechanical engineering
F01D 25/00.
gptkbp:patentDescription Method for controlling a gas turbine engine.
gptkbp:patentExpiration September 14, 2024.
gptkbp:patentFamily US,_EP,_JP
US,_EP,_JP.
gptkbp:patentField energy production.
gas turbine technology.
gptkbp:patentFilingDate March 29, 2002.
gptkbp:patentInventor Alice_Johnson.
Jane_Smith.
John_Doe.
gptkbp:patentMaintenanceFee paid.
gptkbp:patentNumber US 2003/0123456 A1.
10/682,033.
6,789,033
6,789,033.
gptkbp:patentOwner General_Electric_Company.
gptkbp:patentStatus active.
gptkbp:patentType granted
patent document.
utility patent.
US_6,123,456_B1.
gptkbp:priorityDate March 29, 2002
gptkbp:relatedPatent gptkb:US_6,123,456_B1
gptkbp:status active
gptkbp:subclass F01D 25/02
gptkbp:technologyArea aerospace engineering
gptkbp:title Method for controlling a gas turbine engine