gptkbp:instanceOf
|
patent
|
gptkbp:abstract
|
A method for producing a gas turbine engine component with improved performance.
|
gptkbp:applicationNumber
|
10/703,174
|
gptkbp:applicationStatus
|
Published
|
gptkbp:applicationType
|
Utility
|
gptkbp:assignee
|
gptkb:General_Electric_Company
|
gptkbp:citedBy
|
gptkb:US_7,123,456_B2
|
gptkbp:claims
|
20
|
gptkbp:class
|
F01D 21/00
|
gptkbp:country
|
gptkb:United_States
|
gptkbp:examiner
|
No objections raised.
Jane_Smith
|
gptkbp:fieldOfInvention
|
Gas turbine technology
|
gptkbp:filedIn
|
gptkb:General_Electric_Company
|
gptkbp:filingDate
|
March 15, 2004
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,072 F26
|
gptkbp:internationalClassification
|
F01D 21/00
|
gptkbp:inventor
|
gptkb:Alice_Johnson
gptkb:Bob_Brown
gptkb:John_Doe
|
gptkbp:issueDate
|
September 14, 2004
|
gptkbp:issuedBy
|
September 14, 2004
|
gptkbp:legalStatus
|
Granted
|
gptkbp:patentCitation
|
gptkb:US_6,789,071_F25
gptkb:US_5,123,456_A
gptkb:US_5,654,321_A
gptkb:US_6,789,070_B1
US_6,789,073_F27
|
gptkbp:patentFamily
|
US_6,789,072_F26,_US_7,123,456_B2
|
gptkbp:patentNumber
|
6,789,072
|
gptkbp:patentOffice
|
gptkb:United_States_Patent_and_Trademark_Office
|
gptkbp:patentType
|
Granted patent
|
gptkbp:priorityDate
|
March 15, 2002
|
gptkbp:publicationDate
|
September 14, 2004
|
gptkbp:relatedTo
|
gptkb:US_6,789,071_F25
|
gptkbp:status
|
Active
|
gptkbp:subclass
|
F01D 21/02
|
gptkbp:title
|
Method for producing a gas turbine engine component
|