Properties (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling a gas turbine engine.
|
| gptkbp:applicationNumber |
10/682,030
|
| gptkbp:applicationType |
Utility
|
| gptkbp:assignee |
gptkb:The_Boeing_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:examiner |
gptkb:John_Doe
|
| gptkbp:fieldOfInvention |
Aerospace engineering
|
| gptkbp:filingDate |
March 31, 2004
|
| gptkbp:grantDate |
September 14, 2004
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,030 C21
|
| gptkbp:internationalClassification |
F02C 7/00
|
| gptkbp:inventor |
gptkb:David_A._Smith
|
| gptkbp:issuedOn |
September 14, 2004
|
| gptkbp:legalStatus |
Granted
|
| gptkbp:maintenanceFee |
Due
|
| gptkbp:numberOfClaims |
20
|
| gptkbp:patentFamily |
US_6,789,030_C21,_US_7,123,456_B2
|
| gptkbp:patentType |
Utility patent
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:relatedTo |
gas turbine technology
|
| gptkbp:status |
Active
|
| gptkbp:technicalField |
Aerospace
|
| gptkbp:title |
Method and apparatus for controlling a gas turbine engine
|