Statements (12)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling the temperature of a gas turbine engine.
|
| gptkbp:applicationNumber |
10/703,174
|
| gptkbp:assignee |
gptkb:The_Boeing_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
20
|
| gptkbp:fieldOfInvention |
aerospace engineering
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,663 C22
|
| gptkbp:issuedOn |
September 14, 2004
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:status |
active
|
| gptkbp:title |
Method and apparatus for controlling the temperature of a gas turbine engine
|