|
gptkbp:instanceOf
|
Patent
|
|
gptkbp:covers
|
Turbine_blade_design
|
|
gptkbp:hasAbstract
|
A method for improving turbine efficiency.
|
|
gptkbp:hasAssignee
|
gptkb:General_Electric_Company
|
|
gptkbp:hasCitations
|
Cited by 15 other patents.
|
|
gptkbp:hasClaim
|
2
1
10
3
4
5
6
7
8
9
|
|
gptkbp:hasDescription
|
This patent describes a novel turbine blade design.
|
|
gptkbp:hasFieldOfUse
|
Aerospace
|
|
gptkbp:hasFilingDate
|
2004-02-06
|
|
gptkbp:hasGoals
|
Active
|
|
gptkbp:hasInventor
|
gptkb:John_Doe
|
|
gptkbp:hasLegalStatus
|
Granted
|
|
gptkbp:hasPatentNumber
|
6,789,090
|
|
gptkbp:hasPriorityDate
|
2024-02-06
2003-02-06
|
|
gptkbp:hasPublications
|
2004-09-14
|
|
gptkbp:hasTechnicalField
|
Mechanical Engineering
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,090 C62 Family
|
|
gptkbp:isCitedBy
|
gptkb:US_7,123,456
|
|
gptkbp:isFiledIn
|
gptkb:United_States
|
|
gptkbp:isFiledUnder
|
Utility Patent
|
|
gptkbp:isMaintainedBy
|
gptkb:USPTO
|
|
gptkbp:isPartOf
|
Patent Cooperation Treaty (PCT)
C62 Patent Family
|
|
gptkbp:isPublishedIn
|
USPTO Database
|
|
gptkbp:isRelatedTo
|
gptkb:US_6,789,091
gptkb:US_6,789,094
gptkb:US_6,789,096
gptkb:US_6,789,100
gptkb:US_6,789,098
gptkb:US_6,789,093
US_6,789,092
US_6,789,095
US_6,789,097
US_6,789,099
|
|
gptkbp:relatedTo
|
Gas turbine engine
|