Properties (41)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling a gas turbine engine to improve efficiency.
|
| gptkbp:applicationNumber |
10/780,123
|
| gptkbp:applicationType |
Utility
|
| gptkbp:assignee |
gptkb:General_Electric_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
20
|
| gptkbp:coInventor |
gptkb:Alice_Johnson
|
| gptkbp:examiner |
Jane_Smith
|
| gptkbp:fieldOfInvention |
Gas turbine technology
|
| gptkbp:fieldOfUse |
Aerospace
|
| gptkbp:filingDate |
2004-02-06
|
| gptkbp:firstClaim |
The method of claim 1, wherein the control is automated.
A method for controlling a gas turbine engine. The method of claim 1, wherein the control is based on temperature. The method of claim 1, wherein the control system is digital. The method of claim 1, further comprising monitoring emissions. The method of claim 1, wherein the gas turbine engine is a jet engine. The method of claim 1, wherein the gas turbine engine is used in aircraft. |
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,074 G10
|
| gptkbp:internationalClassification |
F01D 25/00
|
| gptkbp:inventiveStep |
Yes
|
| gptkbp:inventor |
gptkb:John_Doe
|
| gptkbp:issueDate |
2004-09-14
|
| gptkbp:legalStatus |
Granted
|
| gptkbp:location |
gptkb:United_States
|
| gptkbp:maintenanceFee |
Paid
|
| gptkbp:ninthClaim |
The method of claim 1, wherein the control system is user-configurable.
The method of claim 1, wherein the control system includes feedback. The method of claim 1, wherein the control system is networked. |
| gptkbp:novelty |
Yes
|
| gptkbp:patentFamily |
US_6,789,074_G10_family
|
| gptkbp:patentInventor |
20 years
|
| gptkbp:patentNumber |
6,789,074
|
| gptkbp:priorityDate |
2003-02-06
|
| gptkbp:publicationNumber |
2004-0098765 A1
|
| gptkbp:relatedPatent |
gptkb:US_6,789,073_G10
|
| gptkbp:relatedTo |
gptkb:US_6,123,456_A1
|
| gptkbp:status |
Active
|
| gptkbp:technologyDomain |
Energy conversion
|
| gptkbp:title |
Method and apparatus for controlling a gas turbine engine
|