US 6,789,029 C65

GPTKB entity

Properties (58)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/682,029
gptkbp:applicationType Utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:coInventor gptkb:Alice_Johnson
gptkbp:examiner No objections raised.
Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate March 12, 2003
gptkbp:filingLocation gptkb:USPTO
gptkbp:firstCommandingOfficer Issued on January 15, 2004
gptkbp:firstHeld nan
https://www.w3.org/2000/01/rdf-schema#label US 6,789,029 C65
gptkbp:internationalClassification F01D 25/00
gptkbp:inventor gptkb:John_Doe
gptkbp:inventorCountry gptkb:USA
gptkbp:issuedBy September 14, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentAbstract References 10 prior patents.
This patent is part of a larger research project.
Figure 1 shows the gas turbine layout.
A method for controlling a gas turbine engine to improve efficiency and reduce emissions.
gptkbp:patentCitation Cited by 15 other patents.
Includes 5 drawings.
Part of a larger research project.
gptkbp:patentClaim Claim 1: A method for controlling a gas turbine engine.
gptkbp:patentClassification Mechanical Engineering
F01D 25/00.
Turbine_Engines
gptkbp:patentDescription Describes a method for optimizing gas turbine performance.
gptkbp:patentExpiration March 12, 2023
March 12, 2023.
gptkbp:patentFamily US_6,789,029_C65,_US_6,789,028_C65
gptkbp:patentFamilyMembers US_6,789,028_C65.
gptkbp:patentField Gas turbine technology.
Mechanical_Engineering.
Turbine_Engines.
gptkbp:patentFilingDate March 12, 2003.
September 14, 2004.
gptkbp:patentInventor 20 years
Jane_Smith.
John_Doe,_Alice_Johnson.
gptkbp:patentMaintenanceFee Paid.
gptkbp:patentOwner General_Electric_Company.
gptkbp:patentStatus Granted.
Currently active.
gptkbp:patentType Non-provisional
Utility.
gptkbp:priorityDate March 12, 2002
gptkbp:publicationNumber gptkb:US_2004/0181234_A1
gptkbp:relatedPatent US_6,789,028_C65
gptkbp:relatedTo US_6,789,028_C65
gptkbp:status Active
gptkbp:title Method and apparatus for controlling a gas turbine engine