US 6,789,921 E100

URI: https://gptkb.org/entity/US_6%2C789%2C921_E100

GPTKB entity

Properties (65)

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:coInventor	gptkb:Alice_Johnson
gptkbp:examiner	Jane_Smith
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filedWith	gptkb:USPTO
gptkbp:filingDate	2004-02-06
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,921 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_10,123,456_B2 gptkb:US_14,123,456_B2 gptkb:US_5,678,901_A gptkb:US_6,123,456_B1 gptkb:US_7,000,000_B2 gptkb:US_7,123,456_B2 gptkb:US_7,654,321_B1 gptkb:US_8,000,000_B2 gptkb:US_8,123,456_B2 gptkb:US_9,123,456_B2 gptkb:US_13,123,456_B2 gptkb:US_15,123,456_B2 gptkb:US_19,123,456_B2 gptkb:US_11,123,456_B2 gptkb:US_18,123,456_B2 gptkb:US_6,789,920_E100 US_10,000,000_B2 US_11,000,000_B2 US_20,000,000_B2 US_9,000,000_B2 US_12,000,000_B2 US_12,123,456_B2 US_13,000,000_B2 US_14,000,000_B2 US_15,000,000_B2 US_16,000,000_B2 US_17,000,000_B2 US_17,123,456_B2 US_18,000,000_B2 US_19,000,000_B2 US_20,123,456_B2 US_16,123,456_B2
gptkbp:patentExpiration	2024-09-14
gptkbp:patentFamily	US_6,789,921_E100_family
gptkbp:patentNumber	6,789,921
gptkbp:patentType	Granted patent
gptkbp:priorityDate	2003-02-06
gptkbp:publicationNumber	gptkb:US_2004/0123456_A1
gptkbp:relatedPatent	gptkb:US_6,789,920_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