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gptkbp:instanceOf
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patent
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gptkbp:abstract
|
A method for controlling the temperature of a gas turbine engine.
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gptkbp:applicationNumber
|
10/682,427
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gptkbp:applicationPublication
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October 7, 2004
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gptkbp:applicationStatus
|
Granted
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gptkbp:applicationType
|
Utility
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|
gptkbp:assignee
|
gptkb:The_Boeing_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:examiner
|
gptkb:John_Smith
|
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gptkbp:expirationDate
|
March 31, 2023
|
|
gptkbp:fieldOfInvention
|
Gas turbine engines
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|
gptkbp:fieldOfUse
|
Aerospace
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gptkbp:filingDate
|
March 31, 2003
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|
gptkbp:grantDate
|
September 14, 2004
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|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,427 C21
|
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gptkbp:internationalClassification
|
F02C 7/00
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|
gptkbp:inventor
|
gptkb:David_A._H._Houghton
gptkb:Michael_J._Smith
gptkb:James_T._Brown
|
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gptkbp:issuedOn
|
September 14, 2004
|
|
gptkbp:legalStatus
|
Patent_Law_Group
|
|
gptkbp:maintenanceFee
|
Paid
|
|
gptkbp:patentCitation
|
gptkb:US_6,789,049_B1
gptkb:US_6,789,037_B1
gptkb:US_6,789,040_B1
gptkb:US_6,789,050_B1
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gptkb:US_6,789,046_B1
gptkb:US_5,123,456_A
gptkb:US_5,678,901_A
gptkb:US_6,123,456_B1
gptkb:US_6,789,000_B2
gptkb:US_6,789,005_B1
gptkb:US_6,789,006_B1
gptkb:US_6,789,007_B1
gptkb:US_6,789,008_B1
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gptkb:US_6,789,042_B1
gptkb:US_6,789,010_B1
gptkb:US_6,789,019_B1
gptkb:US_6,789,035_B1
gptkb:US_6,789,039_B1
gptkb:US_6,789,047_B1
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gptkb:US_6,789,018_B1
gptkb:US_6,789,022_B1
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gptkb:US_6,789,028_B1
gptkb:US_6,789,029_B1
gptkb:US_6,789,036_B1
gptkb:US_6,789,038_B1
gptkb:US_6,789,041_B1
gptkb:US_6,789,048_B1
gptkb:US_6,789,002_B1
gptkb:US_6,789,032_B1
gptkb:US_6,789,034_B1
gptkb:US_6,789,043_B1
US 6,789,024 B1
|
|
gptkbp:patentFamily
|
US_6,789,427_C21,_US_6,789,426_B1
|
|
gptkbp:patentNumber
|
6,789,427
|
|
gptkbp:patentType
|
Utility Patent
|
|
gptkbp:priorityDate
|
March 31, 2003
|
|
gptkbp:publicationNumber
|
gptkb:US_2004/0191234_A1
|
|
gptkbp:relatedPatent
|
gptkb:US_6,789,426_B1
|
|
gptkbp:relatedTo
|
gptkb:US_6,789,426_B1
|
|
gptkbp:status
|
Active
|
|
gptkbp:technology
|
Thermal control systems
|
|
gptkbp:title
|
Method and apparatus for controlling the temperature of a gas turbine engine
|