US 6,789,949 G18

GPTKB entity

Statements (37)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine.
gptkbp:applicationNumber 10/775,123
gptkbp:applicationPublication 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:claims 20
gptkbp:coInventor Jane_Smith
gptkbp:country gptkb:United_States
gptkbp:examiner gptkb:Michael_Johnson
gptkbp:expirationDate 2024-02-06
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate 2004-02-06
https://www.w3.org/2000/01/rdf-schema#label US 6,789,949 G18
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:John_Doe
gptkbp:inventorResidence gptkb:New_York,_USA
gptkbp:issueDate 2004-09-14
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentAbstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:patentCitation gptkb:US_5,123,456_A
gptkbp:patentClassification Class 60
gptkbp:patentDescription Describes a method for optimizing gas turbine performance.
gptkbp:patentFamily US_6,789,949_G18,_US_6,789,948_B1
gptkbp:patentImage image_url_here
gptkbp:patentLink https://patents.google.com/patent/US6789949B2
gptkbp:patentNumber 6,789,949
gptkbp:patentOffice gptkb:USPTO
gptkbp:patentType Granted patent
gptkbp:priorityDate 2003-02-06
gptkbp:relatedTo gptkb:US_6,789,948_B1
gptkbp:status Active
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine