Properties (65)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling a gas turbine engine to improve efficiency.
The invention relates to a method for controlling a gas turbine engine. |
| gptkbp:applicationNumber |
10/682,038
|
| gptkbp:applicationStatus |
Published
|
| gptkbp:applicationType |
Utility
|
| gptkbp:assignee |
gptkb:General_Electric_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B1
|
| gptkbp:claims |
20
|
| gptkbp:country |
gptkb:United_States
|
| gptkbp:documentType |
Patent document
|
| gptkbp:examiner |
gptkb:Robert_Brown
Jane_Smith |
| gptkbp:fieldOfInvention |
Gas turbine technology
|
| gptkbp:filingDate |
March 29, 2002
|
| gptkbp:grantDate |
September 7, 2004
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,038 C62
|
| gptkbp:internationalClassification |
F01D 25/00
|
| gptkbp:inventor |
gptkb:Alice_Johnson
gptkb:John_Doe |
| gptkbp:issuedOn |
September 7, 2004
|
| gptkbp:language |
English
|
| gptkbp:legalStatus |
Granted
|
| gptkbp:maintenanceFee |
Paid
|
| gptkbp:patentAbstract |
English.
Method for controlling gas turbine engines. Filed_with_the_USPTO. |
| gptkbp:patentAssignee |
General_Electric.
General_Electric_Company. |
| gptkbp:patentCitation |
Cited by 10 other patents.
Cited by 10 patents. |
| gptkbp:patentClaim |
20 claims.
|
| gptkbp:patentClassification |
F01D 25/00
|
| gptkbp:patentExpiration |
2024-09-07
|
| gptkbp:patentFamily |
US 6,789,038 C62, US 6,123,456 B2
|
| gptkbp:patentField |
Aerospace engineering.
Energy production. Gas turbine technology. |
| gptkbp:patentFilingDate |
March 29, 2002.
September 7, 2004. March 29, 2001. |
| gptkbp:patentInventor |
Jane_Smith.
John_Doe,_Alice_Johnson. John_Doe. United_States. |
| gptkbp:patentMaintenanceFee |
Paid.
|
| gptkbp:patentNumber |
6,789,038
6,789,038. |
| gptkbp:patentOwner |
gptkb:General_Electric_Company
|
| gptkbp:patentStatus |
Active.
Granted. |
| gptkbp:patentType |
Utility patent.
Granted patent Patent document. Filed under 35 U.S.C. 111. Granted_by_the_USPTO. US_6,123,456_B2. Related_to_US_6,123,456_B2. |
| gptkbp:priorityDate |
March 29, 2001
|
| gptkbp:publicationNumber |
gptkb:US_2004/0181234_A1
|
| gptkbp:relatedPatent |
gptkb:US_6,123,456_B2
|
| gptkbp:relatedTo |
gptkb:US_6,123,456_B2
|
| gptkbp:status |
Active
|
| gptkbp:technicalField |
Aerospace engineering
|
| gptkbp:title |
Method for controlling a gas turbine engine
|