Statements (42)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling a gas turbine engine to improve efficiency.
|
| gptkbp:applicationNumber |
10/703,155
|
| 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:country |
gptkb:United_States
|
| gptkbp:examiner |
Jane_Smith
|
| gptkbp:fieldOfInvention |
Gas turbine technology
|
| gptkbp:filingDate |
March 31, 2004
|
| 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 system is adaptive. The method of claim 1, wherein the control is based on temperature. 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 power generation. |
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,090 G92
|
| gptkbp:internationalClassification |
F01D 21/00
|
| gptkbp:inventiveStep |
Yes
|
| gptkbp:inventor |
gptkb:John_Doe
|
| gptkbp:issuedBy |
September 14, 2004
|
| gptkbp:language |
English
|
| gptkbp:legalStatus |
Granted
|
| gptkbp:maintenanceFee |
Paid
|
| gptkbp:ninthClaim |
The method of claim 1, wherein the control system is integrated.
The method of claim 1, wherein the control is based on real-time data. The method of claim 1, wherein the gas turbine engine is used in aviation. |
| gptkbp:novelty |
Yes
|
| gptkbp:patentFamily |
US_6,789,090_G92_family
|
| gptkbp:patentNumber |
6,789,090
|
| gptkbp:patentOffice |
gptkb:USPTO
|
| gptkbp:patentType |
Granted patent
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:publicationDate |
September 14, 2004
|
| gptkbp:relatedTo |
gptkb:US_6,789,091_G93
|
| gptkbp:status |
Active
|
| gptkbp:technologyArea |
Aerospace engineering
|
| gptkbp:title |
Method and apparatus for controlling a gas turbine engine
|
| gptkbp:utility |
Yes
|