US 6,789,129 G40

GPTKB entity

Properties (65)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationDate March 31, 2004
gptkbp:applicationNumber 10/703,174
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:effectiveDate September 7, 2004
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingLocation gptkb:United_States_Patent_and_Trademark_Office
https://www.w3.org/2000/01/rdf-schema#label US 6,789,129 G40
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:Alice_Johnson
gptkb:John_Doe
gptkbp:maintenanceFee Paid
gptkbp:patentCitation gptkb:US_6,789,158_D8
gptkb:US_6,789,135_G5
gptkb:US_6,789,131_C2
gptkb:US_6,789,152_X2
gptkb:US_6,789,142_N2
gptkb:US_6,789,154_Z4
gptkb:US_5,432,109_A
gptkb:US_5,678,901_A
gptkb:US_6,789,132_D1
gptkb:US_6,789,153_Y3
gptkb:US_6,789,155_A5
gptkb:US_6,789,160_F0
gptkb:US_6,789,149_U9
gptkb:US_6,789,162_H2
gptkb:US_6,789,130_B1
gptkb:US_6,789,159_E9
gptkb:US_6,789,157_C7
gptkb:US_6,789,150_V0
gptkb:US_6,789,133_E3
gptkb:US_6,789,143_O3
gptkb:US_6,789,139_K9
gptkb:US_6,789,161_G1
gptkb:US_6,789,138_J8
gptkb:US_6,789,167_M7
gptkb:US_6,789,141_M1
gptkb:US_6,789,165_K5
gptkb:US_6,789,156_B6
gptkb:US_6,789,170_P0
gptkb:US_6,789,144_P4
gptkb:US_6,789,163_I3
gptkb:US_6,789,136_H6
gptkb:US_6,789,164_J4
US 6,789,140 L0
US 6,789,145 Q5
US_6,789,134_F4
US_6,789,137_I7
US_6,789,146_R6
US_6,789,147_S7
US_6,789,148_T8
US_6,789,151_W1
US_6,789,166_L6
US_6,789,168_N8
US_6,789,169_O9
gptkbp:patentFamily US 6,789,129 G40, US 6,123,456 B1
gptkbp:patentType Utility patent
gptkbp:priorityDate March 31, 2003
gptkbp:relatedPatent gptkb:US_6,123,456_B1
gptkbp:status Active
gptkbp:title Method and apparatus for controlling a gas turbine engine