US 6,789,234 H2

URI: https://gptkb.org/entity/US_6%2C789%2C234_H2

GPTKB entity

Properties (69)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber	10/123,456
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:class	F01D 21/00
gptkbp:country	gptkb:United_States
gptkbp:documentType	Patent
gptkbp:examiner	Jane_Smith
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	April 1, 2002
gptkbp:hasFieldOfUse	Aerospace
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,234 H2
gptkbp:internationalClassification	F01D 21/00
gptkbp:inventor	gptkb:Alice_Johnson gptkb:John_Doe
gptkbp:issueDate	September 7, 2004
gptkbp:issuedBy	September 7, 2004
gptkbp:language	English
gptkbp:legalStatus	Granted
gptkbp:maintenanceFee	Paid
gptkbp:patentCitation	gptkb:US_6,789,255_H2 gptkb:US_6,789,254_H2 gptkb:US_6,789,242_H2 gptkb:US_6,789,243_H2 gptkb:US_6,789,240_H2 gptkb:US_6,789,258_H2 gptkb:US_5,432,109_A gptkb:US_5,678,901_A gptkb:US_6,123,456_B1 gptkb:US_6,789,238_H2 gptkb:US_6,789,241_H2 gptkb:US_6,789,266_H2 gptkb:US_6,789,259_H2 gptkb:US_6,789,245_H2 gptkb:US_6,789,239_H2 gptkb:US_6,789,236_H2 gptkb:US_6,789,244_H2 gptkb:US_6,789,267_H2 gptkb:US_6,789,233_H2 gptkb:US_6,789,250_H2 gptkb:US_6,789,270_H2 gptkb:US_6,789,252_H2 gptkb:US_6,789,247_H2 gptkb:US_6,789,248_H2 gptkb:US_6,789,249_H2 gptkb:US_6,789,246_H2 gptkb:US_6,789,235_H2 gptkb:US_6,789,237_H2 gptkb:US_6,789,251_H2 US_6,789,262_H2 US_6,789,253_H2 US_6,789,256_H2 US_6,789,257_H2 US_6,789,260_H2 US_6,789,261_H2 US_6,789,263_H2 US_6,789,264_H2 US_6,789,265_H2 US_6,789,268_H2 US_6,789,269_H2
gptkbp:patentFamily	US_6,789,234_H2,_US_6,789,235_H2
gptkbp:patentNumber	6,789,234
gptkbp:priorityDate	March 15, 2002
gptkbp:relatedPatent	gptkb:US_6,789,235_H2
gptkbp:status	Active
gptkbp:title	Method for controlling a gas turbine engine