US 6,789,933 E100

GPTKB entity

Properties (73)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationDate 2004-02-06
gptkbp:applicationNumber 10/780,123
gptkbp:applicationType utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:class F02C 7/00
gptkbp:description The invention relates to a method for controlling a gas turbine engine.
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention gas turbine technology
gptkbp:filedIn gptkb:United_States
gptkbp:filingDate 2004-02-06
https://www.w3.org/2000/01/rdf-schema#label US 6,789,933 E100
gptkbp:internationalClassification F02C 7/00
gptkbp:inventor gptkb:John_Doe
gptkbp:inventorCountry gptkb:USA
gptkbp:issueDate 2004-09-14
gptkbp:legalStatus granted
gptkbp:maintenanceFee paid
gptkbp:patentCitation gptkb:US_6,789,966_E100
gptkb:US_6,789,943_E100
gptkb:US_6,789,968_E100
gptkb:US_6,789,956_E100
gptkb:US_6,789,950_E100
gptkb:US_6,789,960_E100
gptkb:US_6,789,935_E100
gptkb:US_5,123,456_A
gptkb:US_5,654,321_A
gptkb:US_6,789,932_B1
gptkb:US_6,789,938_E100
gptkb:US_6,789,939_E100
gptkb:US_6,789,948_E100
gptkb:US_6,789,941_E100
gptkb:US_6,789,944_E100
gptkb:US_6,789,937_E100
gptkb:US_6,789,952_E100
gptkb:US_6,789,945_E100
gptkb:US_6,789,949_E100
gptkb:US_6,789,953_E100
gptkb:US_6,789,958_E100
gptkb:US_6,789,970_E100
gptkb:US_6,789,957_E100
gptkb:US_6,789,947_E100
gptkb:US_6,789,965_E100
gptkb:US_6,789,936_E100
gptkb:US_6,789,964_E100
gptkb:US_6,789,955_E100
gptkb:US_6,789,946_E100
gptkb:US_6,789,967_E100
gptkb:US_6,789,961_E100
gptkb:US_6,789,959_E100
US_6,789,940_E100
US_6,789,942_E100
US_6,789,951_E100
US_6,789,954_E100
US_6,789,962_E100
US_6,789,963_E100
US_6,789,969_E100
gptkbp:patentExpiration 2024-09-14
gptkbp:patentFamily US_6,789,933_E100,_US_6,789,934_E100
gptkbp:patentNumber 6,789,933
gptkbp:patentOwner gptkb:General_Electric_Company
gptkbp:patentType granted patent
gptkbp:priorityDate 2003-02-06
gptkbp:publicationNumber gptkb:US_2004/0123456_A1
gptkbp:relatedPatent US_6,789,934_E100
gptkbp:relatedTo gas turbine engines
gptkbp:status active
gptkbp:subclass F02C_7/10
gptkbp:technicalField aerospace engineering
gptkbp:title Method for controlling a gas turbine engine