Properties (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling the temperature of a gas turbine engine.
|
| gptkbp:applicationDate |
March 31, 2004
|
| gptkbp:applicationNumber |
10/682,444
|
| gptkbp:assignee |
gptkb:The_Boeing_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
20
|
| gptkbp:class |
F02C 7/00
|
| gptkbp:contains |
temperature control system
|
| gptkbp:description |
a method for improving engine efficiency
|
| gptkbp:examiner |
gptkb:John_Smith
|
| gptkbp:fieldOfInvention |
aerospace engineering
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,444 C21
|
| gptkbp:inventor |
gptkb:David_A._H._Houghton
|
| gptkbp:issuedOn |
September 7, 2004
|
| gptkbp:legalStatus |
granted
|
| gptkbp:maintenanceFee |
paid
|
| gptkbp:patentFamily |
US_6,789,444_C21,_US_7,123,456_B2
|
| gptkbp:patentType |
utility
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:relatedTo |
gas turbine technology
|
| gptkbp:status |
active
|
| gptkbp:subclass |
F02C 7/02
|
| gptkbp:title |
Method and apparatus for controlling the temperature of a gas turbine engine
|