US 6,789,110 E15 Family

URI: https://gptkb.org/entity/US_6%2C789%2C110_E15_Family

GPTKB entity

Statements (64)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber	10/123,456
gptkbp:applicationPublicationNumber	2004/0123456
gptkbp:applicationType	utility
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456
gptkbp:claims	20
gptkbp:country	gptkb:United_States
gptkbp:documentType	patent document
gptkbp:examiner	Jane_Smith
gptkbp:expirationDate	2024-02-06
gptkbp:fieldOfInvention	aerospace engineering
gptkbp:filingDate	2004-02-06
gptkbp:hasFieldOfUse	aviation
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,110 E15 Family
gptkbp:internationalClassification	F02C 7/00
gptkbp:inventor	gptkb:John_Doe
gptkbp:inventorCountry	gptkb:USA
gptkbp:issueDate	2004-09-14
gptkbp:language	English
gptkbp:legalStatus	granted
gptkbp:maintenanceFee	paid
gptkbp:patentCitation	gptkb:US_6,123,456
gptkbp:patentFamily	E15_Family
gptkbp:patentFamilyMembers	gptkb:US_6,789,139 gptkb:US_6,789,135 gptkb:US_6,789,121 gptkb:US_6,789,113 gptkb:US_6,789,131 gptkb:US_6,789,126 gptkb:US_6,789,137 gptkb:US_6,789,128 gptkb:US_6,789,115 gptkb:US_6,789,116 gptkb:US_6,789,122 US 6,789,140 US_6,789,123 US_6,789,112 US_6,789,114 US_6,789,117 US_6,789,118 US_6,789,119 US_6,789,120 US_6,789,130 US_6,789,124 US_6,789,125 US_6,789,127 US_6,789,129 US_6,789,132 US_6,789,133 US_6,789,134 US_6,789,136 US_6,789,138
gptkbp:patentNumber	6,789,110
gptkbp:patentOffice	gptkb:USPTO
gptkbp:patentType	granted patent
gptkbp:priorityDate	2003-02-06
gptkbp:relatedPatent	gptkb:US_6,789,111
gptkbp:relatedTo	gas turbine technology
gptkbp:status	active
gptkbp:subclass	F02C
gptkbp:technologyArea	energy production
gptkbp:title	Method for controlling a gas turbine engine