US 6,789,127 G115

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/775,123
gptkbp:applicationPublicationNumber 2004/0123456 A1
gptkbp:applicationType Utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:examiner No objections raised.
Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingCountry gptkb:United_States
gptkbp:filingDate 2004-01-30
https://www.w3.org/2000/01/rdf-schema#label US 6,789,127 G115
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:Alice_Johnson
gptkb:John_Doe
gptkbp:issueDate 2004-09-14
gptkbp:legalStatus Granted
gptkbp:location gptkb:United_States
gptkbp:maintenanceFee Paid
gptkbp:patentAbstract Innovative control methods.
This invention relates to a method for controlling gas turbine engines.
Improves efficiency of gas turbines.
Developed_in_collaboration_with_NASA.
gptkbp:patentAssignee gptkb:General_Electric_Company
General_Electric_Company,_founded_in_1892.
gptkbp:patentCitation Cited by 10 other patents.
Figures illustrating the invention.
Applicable in aerospace and energy sectors.
Further research on turbine efficiency.
Research_conducted_at_GE_Global_Research.
gptkbp:patentClaim Claims defining the scope of the invention.
gptkbp:patentClassification F01D 21/00, F02C 7/00
gptkbp:patentDescription Detailed description of the invention.
gptkbp:patentExpiration 2024-01-30
gptkbp:patentFamily US_6,789,127_G115,_US_6,789,126_B1
gptkbp:patentField Energy generation.
Gas turbine control systems.
gptkbp:patentFilingDate 2004-09-14
2004-01-30
gptkbp:patentInventor John_Doe,_Alice_Johnson
John_Doe,_PhD_in_Mechanical_Engineering.
gptkbp:patentMaintenanceFee Maintained in force.
gptkbp:patentNumber 6,789,127
gptkbp:patentStatus No legal disputes.
Method for controlling gas turbine engines.
gptkbp:patentType Granted patent
gptkbp:priorityDate 2003-01-30
gptkbp:relatedPatent gptkb:US_6,789,126_B1
gptkbp:relatedTo gptkb:US_6,789,126_B1
gptkbp:status Active
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine