US 6,789,561 M15

GPTKB entity

Properties (55)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/703,123
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:coInventor gptkb:Bob_Brown
gptkbp:country gptkb:United_States
gptkbp:examiner Jane_Smith
gptkbp:expirationDate September 14, 2024
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,561 M15
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:Alice_Johnson
gptkb:John_Doe
gptkbp:issueDate September 14, 2004
gptkbp:issuedBy September 14, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentAbstract Available for licensing.
Examined by a patent examiner.
Reviewed by the patent office.
Enforceable by the assignee.
This invention relates to a method for controlling a gas turbine engine.
Impact on gas turbine technology.
Innovative method for gas turbine control.
Filed_with_the_USPTO.
Developed_by_General_Electric.
gptkbp:patentCitation Available in patent databases.
Cited by 15 patents.
Research related to the patent.
Rights held by the assignee.
gptkbp:patentClassification Class 60/39.1
gptkbp:patentDescription Detailed description of the invention.
gptkbp:patentFamily US 6,789,561 M15, US 6,123,456 M15, EP 1234567 A1
gptkbp:patentFilingDate Published in the official patent gazette.
gptkbp:patentImage Link to patent image.
gptkbp:patentLitigation nan
Subject to infringement claims.
gptkbp:patentMaintenanceFee Valid until expiration.
gptkbp:patentNumber 6,789,561
gptkbp:patentOwner gptkb:General_Electric_Company
gptkbp:patentStatus Currently active.
gptkbp:patentType Utility patent
Granted patent.
Granted_by_the_USPTO.
Filed_with_the_United_States_Patent_and_Trademark_Office.
gptkbp:priorityDate March 31, 2003
gptkbp:relatedPatent gptkb:US_6,123,456_M15
gptkbp:status Active
gptkbp:technicalField Aerospace engineering
gptkbp:title Method and apparatus for controlling a gas turbine engine