US 6,789,630 G27

GPTKB entity

Properties (38)
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:examiner gptkb:John_Doe
No objections.
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingCountry gptkb:United_States
gptkbp:filingDate 2004-02-06
https://www.w3.org/2000/01/rdf-schema#label US 6,789,630 G27
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:John_Smith
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 Mechanical engineering
gptkbp:patentDescription Describes a method for optimizing gas turbine performance.
gptkbp:patentExpiration 2024-09-14
gptkbp:patentFamily US_6,789,630_G27,_US_6,789,629_B2
gptkbp:patentImage image_url_here
gptkbp:patentLink https://patents.google.com/patent/US6789630B2
gptkbp:patentNumber 6,789,630
gptkbp:patentOffice gptkb:USPTO
gptkbp:patentType Utility patent
gptkbp:priorityDate 2003-02-06
gptkbp:relatedTo gptkb:US_6,789,629_B2
gptkbp:status Active
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine