Statements (14)
| 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 |
Gas turbine engines
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,026 C24
|
| gptkbp:inventor |
gptkb:David_A._H._Houghton
|
| gptkbp:issuedBy |
September 7, 2004
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:relatedTo |
US_6,789,025_C24
|
| gptkbp:status |
Active
|
| gptkbp:title |
Method and apparatus for controlling the temperature of a gas turbine engine
|