US 6,789,065 K6

GPTKB entity

Properties (52)
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 non-provisional
gptkbp:assignee gptkb:K6_Technologies,_Inc.
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:examiner No objections raised.
Jane_Smith
gptkbp:fieldOfInvention aerospace engineering
gptkbp:filingDate March 5, 2004
https://www.w3.org/2000/01/rdf-schema#label US 6,789,065 K6
gptkbp:internationalClassification F02C 7/00
gptkbp:inventor gptkb:Alice_Johnson
gptkb:John_Doe
gptkbp:issueDate September 7, 2004
gptkbp:issuedBy September 7, 2004
gptkbp:legalStatus granted
gptkbp:location gptkb:United_States
gptkbp:maintenanceFee paid
gptkbp:patentAbstract gptkb:US_6,123,456_A1
March 5, 2004
This patent describes a method for optimizing gas turbine performance.
gptkbp:patentAssignee gptkb:K6_Technologies,_Inc.
gptkb:Alice_Johnson
gptkbp:patentCitation gptkb:US_5,678,901_A
gptkbp:patentClassification mechanical engineering
F02C 7/00
gptkbp:patentExpiration 2024-09-07
gptkbp:patentFamily gptkb:K6_family
Method for controlling gas turbine engine.
gptkbp:patentFamilyMembers gptkb:US_6,123,456_A1
gptkbp:patentField aerospace applications
gas turbine technology
gptkbp:patentFilingDate March 5, 2004
September 7, 2004
gptkbp:patentInventor gptkb:John_Doe
gptkbp:patentNumber 6,789,065
6,789,065 K6
gptkbp:patentOwner gptkb:K6_Technologies,_Inc.
gptkbp:patentStatus active
active patent
gptkbp:patentType utility
September 7, 2004
granted patent
10/703,123
gptkbp:priorityDate March 5, 2003
gptkbp:relatedPatent gptkb:US_6,123,456_A1
gptkbp:status active
gptkbp:technicalField energy conversion
gptkbp:title Method and apparatus for controlling a gas turbine engine