|
gptkbp:instanceOf
|
patent
|
|
gptkbp:abstract
|
A method for controlling a gas turbine engine to improve performance.
|
|
gptkbp:applicationNumber
|
10/703,174
|
|
gptkbp:applicationPublication
|
gptkb:US_2004/0123456_A1
|
|
gptkbp:applicationStatus
|
Published
|
|
gptkbp:applicationType
|
Utility
|
|
gptkbp:assignee
|
gptkb:General_Electric_Company
|
|
gptkbp:citedBy
|
gptkb:US_7,123,456_B2
|
|
gptkbp:claims
|
20
|
|
gptkbp:coInventor
|
gptkb:Jane_Doe
|
|
gptkbp:examiner
|
gptkb:John_Smith
|
|
gptkbp:fieldOfInvention
|
Gas turbine technology
|
|
gptkbp:filingDate
|
March 31, 2004
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 6,789,036 G25
|
|
gptkbp:internationalClassification
|
F01D 21/00
|
|
gptkbp:inventor
|
gptkb:Robert_J._H._Houghton
|
|
gptkbp:inventorResidence
|
gptkb:New_York,_USA
|
|
gptkbp:issueDate
|
September 7, 2004
|
|
gptkbp:issuedOn
|
September 7, 2004
|
|
gptkbp:legalStatus
|
Granted
|
|
gptkbp:maintenanceFee
|
Paid
|
|
gptkbp:patentAbstract
|
A method for controlling a gas turbine engine to improve performance.
|
|
gptkbp:patentCitation
|
gptkb:US_5,123,456_A
|
|
gptkbp:patentClaim
|
4.
3.
20.
5.
13.
15.
19.
2.
6.
16.
1.
11.
12.
14.
7.
8.
10.
9.
17.
18.
|
|
gptkbp:patentExpiration
|
2024-09-07
|
|
gptkbp:patentFamily
|
US_6,789,036_G25_family
|
|
gptkbp:patentNumber
|
6,789,036
|
|
gptkbp:patentOffice
|
gptkb:United_States_Patent_and_Trademark_Office
|
|
gptkbp:patentType
|
Granted patent
|
|
gptkbp:priorityDate
|
March 31, 2003
|
|
gptkbp:relatedPatent
|
gptkb:US_6,789,037_G25
|
|
gptkbp:relatedTo
|
gptkb:US_6,123,456_A1
|
|
gptkbp:status
|
Active
|
|
gptkbp:technicalField
|
Aerospace engineering
|
|
gptkbp:title
|
Method and apparatus for controlling a gas turbine engine
|