Properties (12)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:fieldOfTechnology |
aerospace engineering
|
| gptkbp:hasAssignee |
gptkb:General_Electric_Company
|
| gptkbp:hasClaim |
20
|
| gptkbp:hasFilingDate |
2004-02-06
|
| gptkbp:hasPatentNumber |
6,789,635
|
| gptkbp:hasPriorityDate |
2003-02-06
|
| gptkbp:hasPublications |
2004-09-14
|
| gptkbp:hasTitle |
Method for controlling a gas turbine engine
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,635 C70
|
| gptkbp:isFiledIn |
gptkb:United_States
|
| gptkbp:isGranted |
true
|