US 6,789,059 G40

URI: https://gptkb.org/entity/US_6%2C789%2C059_G40

GPTKB entity

Statements (57)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve performance.
gptkbp:applicationNumber	10/703,174
gptkbp:applicationPublicationNumber	gptkb:US_2004/0123456_A1
gptkbp:applicationStatus	Published
gptkbp:applicationType	Utility
gptkbp:assignee	gptkb:General_Electric_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:country	gptkb:United_States
gptkbp:effectiveDate	2004-09-14
gptkbp:examiner	gptkb:John_Smith
gptkbp:expirationDate	2024-09-14
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	2003-11-12
gptkbp:grantDate	2004-09-14
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,059 G40
gptkbp:internationalClassification	F01D 21/00
gptkbp:inventor	gptkb:David_A._H._Houghton gptkb:Jane_Doe gptkb:Michael_Johnson
gptkbp:legalStatus	Granted
gptkbp:maintenanceFee	Paid
gptkbp:numberOfClaims	20
gptkbp:patentCitation	gptkb:US_6,789,069_G50 gptkb:US_6,789,071_G52 gptkb:US_6,789,074_G55 gptkb:US_5,432,109_A gptkb:US_5,678,901_A gptkb:US_6,789,062_G43 gptkb:US_6,789,078_G59 gptkb:US_6,789,060_G41 gptkb:US_6,789,064_G45 gptkb:US_6,789,077_G58 gptkb:US_6,789,079_G60 gptkb:US_6,789,073_G54 gptkb:US_6,789,070_G51 gptkb:US_6,789,058_B1 gptkb:US_6,789,061_G42 US_6,789,063_G44 US_6,789,065_G46 US_6,789,066_G47 US_6,789,067_G48 US_6,789,068_G49 US_6,789,072_G53 US_6,789,075_G56 US_6,789,076_G57
gptkbp:patentClassification	F01D 21/00
gptkbp:patentFamily	US 6,789,059 G40, US 6,123,456 A1, US 7,123,456 B2
gptkbp:patentNumber	6,789,059
gptkbp:patentOffice	gptkb:USPTO
gptkbp:patentType	Utility patent
gptkbp:priorityDate	2001-12-14
gptkbp:relatedApplication	US_10/703,174
gptkbp:relatedPatent	gptkb:US_6,123,456_A1
gptkbp:status	Active
gptkbp:technologyArea	Aerospace engineering
gptkbp:title	Method and apparatus for controlling a gas turbine engine