Properties (70)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for producing a gas turbine engine component with improved performance.
|
| gptkbp:applicationNumber |
10/646,123
|
| gptkbp:applicationType |
Non-provisional
|
| gptkbp:assignee |
gptkb:General_Electric_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
20
|
| gptkbp:examiner |
Jane_Smith
|
| gptkbp:expirationDate |
September 14, 2024
|
| gptkbp:fieldOfInvention |
Gas turbine technology
|
| gptkbp:filingDate |
February 1, 2003
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,049 F31
|
| gptkbp:internationalClassification |
F01D 21/00
|
| gptkbp:inventor |
gptkb:Alice_Johnson
gptkb:John_Doe |
| gptkbp:issuedOn |
September 14, 2004
|
| gptkbp:legalStatus |
Granted
|
| gptkbp:location |
gptkb:United_States
|
| gptkbp:maintenanceFee |
Paid
|
| gptkbp:patentCitation |
gptkb:US_5,678,901_A
gptkb:US_6,123,456_B1 US 6,789,085 F31 US_6,789,050_F31 US_6,789,051_F31 US_6,789,052_F31 US_6,789,053_F31 US_6,789,054_F31 US_6,789,055_F31 US_6,789,056_F31 US_6,789,057_F31 US_6,789,058_F31 US_6,789,059_F31 US_6,789,060_F31 US_6,789,061_F31 US_6,789,062_F31 US_6,789,063_F31 US_6,789,064_F31 US_6,789,065_F31 US_6,789,066_F31 US_6,789,067_F31 US_6,789,068_F31 US_6,789,069_F31 US_6,789,070_F31 US_6,789,071_F31 US_6,789,072_F31 US_6,789,073_F31 US_6,789,074_F31 US_6,789,075_F31 US_6,789,076_F31 US_6,789,077_F31 US_6,789,078_F31 US_6,789,079_F31 US_6,789,080_F31 US_6,789,081_F31 US_6,789,082_F31 US_6,789,083_F31 US_6,789,084_F31 US_6,789,086_F31 US_6,789,087_F31 US_6,789,088_F31 US_6,789,089_F31 US_6,789,090_F31 |
| gptkbp:patentFamily |
US_6,789,049_F31_family
|
| gptkbp:patentType |
Utility patent
|
| gptkbp:priorityDate |
March 31, 2003
|
| gptkbp:relatedTo |
Gas turbine engines
|
| gptkbp:status |
Active
|
| gptkbp:subclass |
F01D 21/02
|
| gptkbp:technicalField |
Aerospace engineering
|
| gptkbp:title |
Method for producing a gas turbine engine component
|