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gptkbp:instanceOf
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patent
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|
gptkbp:abstract
|
A method for controlling a gas turbine engine to improve efficiency.
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gptkbp:applicationNumber
|
10/682,033
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gptkbp:applicationStatus
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published
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gptkbp:applicationType
|
utility
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gptkbp:assignee
|
gptkb:General_Electric_Company
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gptkbp:citedBy
|
gptkb:US_7,123,456_B2
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gptkbp:claims
|
20
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gptkbp:country
|
gptkb:United_States
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gptkbp:effectiveDate
|
September 7, 2004
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gptkbp:examiner
|
gptkb:John_Smith
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gptkbp:fieldOfInvention
|
gas turbine technology
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|
gptkbp:filingDate
|
March 31, 2004
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|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,033 G26
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gptkbp:internationalClassification
|
F01D 21/00
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|
gptkbp:inventor
|
gptkb:David_A._H._Houghton
gptkb:John_Doe
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gptkbp:issueNumber
|
6,789,033
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gptkbp:language
|
English
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gptkbp:legalStatus
|
granted
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|
gptkbp:maintenanceFee
|
paid
|
|
gptkbp:patentAbstract
|
A method for controlling a gas turbine engine to improve efficiency and reduce emissions.
|
|
gptkbp:patentCitation
|
gptkb:US_5,123,456_A
|
|
gptkbp:patentDescription
|
Describes a method for optimizing gas turbine performance.
|
|
gptkbp:patentExpiration
|
2024-09-07
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gptkbp:patentFamily
|
US_6,789,033_G26,_US_6,789,034_G26
|
|
gptkbp:patentImage
|
image_url_here
|
|
gptkbp:patentLink
|
https://patents.google.com/patent/US6789033G26
|
|
gptkbp:patentOwner
|
gptkb:General_Electric_Company
|
|
gptkbp:patentType
|
granted patent
|
|
gptkbp:priorityDate
|
March 31, 2003
|
|
gptkbp:publicationNumber
|
gptkb:US_2004/0181234_A1
|
|
gptkbp:relatedPatent
|
US_6,789,034_G26
|
|
gptkbp:status
|
active
|
|
gptkbp:technicalField
|
aerospace engineering
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|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
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