US 6,788,994 C24

URI: https://gptkb.org/entity/US_6%2C788%2C994_C24

GPTKB entity

Properties (71)

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	2004/0123456 A1
gptkbp:applicationType	utility
gptkbp:assignee	gptkb:The_Boeing_Company
gptkbp:citedBy	gptkb:US_7,123,456_B2
gptkbp:claims	20
gptkbp:country	gptkb:United_States
gptkbp:examiner	gptkb:John_Smith No objections raised.
gptkbp:fieldOfInvention	aerospace engineering
gptkbp:fieldOfUse	aviation
gptkbp:filingDate	March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label	US 6,788,994 C24
gptkbp:internationalClassification	F02C 7/00
gptkbp:inventor	gptkb:David_A._H._Houghton gptkb:John_Doe
gptkbp:issueDate	September 7, 2004
gptkbp:issuedOn	September 7, 2004
gptkbp:legalStatus	granted
gptkbp:maintenanceFee	paid
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gptkbp:patentFamily	US_6,788,994_C24,_US_7,123,456_B2
gptkbp:patentNumber	6,788,994
gptkbp:patentType	granted patent
gptkbp:priorityDate	March 31, 2003
gptkbp:relatedPatent	gptkb:US_6,123,456_A1
gptkbp:relatedTo	gas turbine technology
gptkbp:status	active
gptkbp:title	Method and apparatus for controlling a gas turbine engine