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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 performance.
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gptkbp:applicationNumber
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10/780,123
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gptkbp:applicationType
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Utility
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gptkbp:assignee
|
J79_Technologies,_Inc.
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gptkbp:citedBy
|
gptkb:US_7,123,456_B2
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gptkbp:claims
|
20
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gptkbp:coInventor
|
gptkb:Bob_Brown
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gptkbp:examiner
|
Jane_Smith
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gptkbp:fieldOfInvention
|
Gas turbine technology
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gptkbp:filingDate
|
2004-02-06
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https://www.w3.org/2000/01/rdf-schema#label
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US 6,789,219 J79
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gptkbp:internationalClassification
|
F02C 7/00
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gptkbp:inventor
|
gptkb:Alice_Johnson
gptkb:John_Doe
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gptkbp:issueDate
|
2004-09-14
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gptkbp:legalStatus
|
Granted
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gptkbp:maintenanceFee
|
Paid
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gptkbp:patentCitation
|
gptkb:US_5,123,456_A
gptkb:US_5,678,901_A
gptkb:US_6,789,012_B2
gptkb:US_7,444,444_B2
gptkb:US_7,555,555_B2
gptkb:US_7,777,777_B2
gptkb:US_7,999,999_B2
gptkb:US_8,000,000_B2
gptkb:US_8,444,444_B2
gptkb:US_8,888,888_B2
gptkb:US_8,999,999_B2
gptkb:US_9,555,555_B2
gptkb:US_9,999,999_B2
gptkb:US_8,333,333_B2
gptkb:US_8,777,777_B2
gptkb:US_9,444,444_B2
gptkb:US_6,234,567_B1
gptkb:US_7,000,000_B1
gptkb:US_7,111,111_B2
gptkb:US_7,222,222_B2
gptkb:US_7,888,888_B2
gptkb:US_8,111,111_B2
gptkb:US_8,666,666_B2
gptkb:US_9,111,111_B2
gptkb:US_9,222,222_B2
gptkb:US_9,666,666_B2
gptkb:US_9,777,777_B2
gptkb:US_7,666,666_B2
gptkb:US_8,222,222_B2
gptkb:US_8,555,555_B2
gptkb:US_9,888,888_B2
US 7,333,333 B2
US 9,333,333 B2
US_9,000,000_B2
|
|
gptkbp:patentInventor
|
20 years
|
|
gptkbp:patentNumber
|
6,789,219
|
|
gptkbp:priorityDate
|
2003-02-06
|
|
gptkbp:relatedPatent
|
gptkb:US_6,500,000_B1
|
|
gptkbp:status
|
Active
|
|
gptkbp:technologyArea
|
Aerospace engineering
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|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
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