US 6,789,866 E55

GPTKB entity

Statements (47)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine.
gptkbp:applicationNumber 10/780,123
gptkbp:applicationPublication gptkb:US_2004/0123456_A1
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:description This patent describes a method for optimizing the performance of a gas turbine engine.
gptkbp:drawings Figure 1, Figure 2
gptkbp:examiner Jane_Smith
gptkbp:expirationDate 2024-02-06
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filedWith gptkb:USPTO
gptkbp:filingDate 2004-02-06
https://www.w3.org/2000/01/rdf-schema#label US 6,789,866 E55
gptkbp:internationalClassification F02C 7/00
gptkbp:inventiveStep Yes
gptkbp:inventor gptkb:John_Doe
gptkbp:issueDate 2004-09-14
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
2023-02-06
gptkbp:novelty Yes
gptkbp:patentAbstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:patentAssignee gptkb:General_Electric_Company
gptkbp:patentCitation gptkb:US_5,123,456_A
gptkbp:patentClassification F02C
gptkbp:patentFamily US_6,789,866_E55,_US_6,789,865_E54
gptkbp:patentField Control systems
gptkbp:patentFilingDate 2004-09-14
2004-02-06
gptkbp:patentInventor gptkb:John_Doe
gptkbp:patentLitigation nan
gptkbp:patentNumber 6,789,866
gptkbp:patentOwner gptkb:General_Electric_Company
gptkbp:patentStatus Active
gptkbp:patentType Granted patent
gptkbp:priorityDate 2003-02-06
gptkbp:relatedTo gptkb:US_6,789,865_E54
gptkbp:status Active
gptkbp:subclass F02C_7/10
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine
gptkbp:utility Yes