| 7222488 |
Fabricated cowl for double annular combustor of a gas turbine engine |
Steven C. Vise, Walter Byron Houchens, III, Craig Douglas Young |
2007-05-29 |
$81,931,000 |
| 7216485 |
Adjusting airflow in turbine component by depositing overlay metallic coating |
James M. Caldwell, Thomas John Tomlinson, Robert George Zimmerman, Jr., Raymond W. Heidorn |
2007-05-15 |
$35,333,000 |
| 7022940 |
Combustor linear and method for making thereof |
James Groeschen, Ronald Redden, Shaun DeVane |
2006-04-04 |
$32,265,000 |
| 6931728 |
Test model for a gas turbine combustor dome and method of fabricating |
Edward Lee Howard, James Hollice Poynter, Ronald L. Sheranko, John Robert Staker, Thomas Carl Mills +1 more |
2005-08-23 |
$20,161,000 |
| 6908657 |
Coated component with through-hole having improved surface finish |
Jeffrey Fehrenbach |
2005-06-21 |
$35,071,000 |
| 6779268 |
Outer and inner cowl-wire wrap to one piece cowl conversion |
— |
2004-08-24 |
$38,400,000 |
| 6729940 |
Apparatus for stripping coating |
Jeffrey Fehrenbach, William Lee Imhoff, David Allen Kastrup |
2004-05-04 |
$54,354,000 |
| 6725667 |
Combustor dome for gas turbine engine |
James Groeschen |
2004-04-27 |
$51,799,000 |
| 6672067 |
Corrugated cowl for combustor of a gas turbine engine and method for configuring same |
Ronald Redden, Balena B. Shorter, James Groeschen, Mehmet Dede, Daniel Lee Durstock |
2004-01-06 |
$53,549,000 |
| 6663919 |
Process of removing a coating deposit from a through-hole in a component and component processed thereby |
Jeffrey Fehrenbach |
2003-12-16 |
$60,770,000 |
| 6655149 |
Preferential multihole combustor liner |
Daniel Dale Brown, Myron Edward Rutherford |
2003-12-02 |
$42,474,000 |
| 6655147 |
Annular one-piece corrugated liner for combustor of a gas turbine engine |
Shaun DeVane, John Lawrence Vandike |
2003-12-02 |
$42,474,000 |
| 6655146 |
Hybrid film cooled combustor liner |
Ella Christine Kutter, Marwan Al-Roub, Thomas Leen, Daniel Dale Brown, Craig Douglas Young +1 more |
2003-12-02 |
$42,474,000 |
| 6651437 |
Combustor liner and method for making thereof |
James Groeschen, Ronald Redden, Shaun DeVane |
2003-11-25 |
$41,541,000 |
| 6629415 |
Methods and apparatus for modeling gas turbine engine combustor liners |
Edward Lee Howard, James Hollice Poynter, Ronald L. Sheranko, Gregory Lucas |
2003-10-07 |
$51,954,000 |
| 6620457 |
Method for thermal barrier coating and a liner made using said method |
Thomas John Tomlinson, Raymond W. Heidorn, Jeffrey Fehrenbach, William Lee Imhoff, Myron Edward Rutherford |
2003-09-16 |
$54,496,000 |
| 6592287 |
Self-fixtured joint assembly and its preparation |
Michael P. Hagle |
2003-07-15 |
$52,334,000 |
| 6568079 |
Methods for replacing combustor liner panels |
David Bruce Patterson, Steven Allen Stiverson, James M. Caldwell, Edward John Emilianowicz, Jeffrey Michael Martini |
2003-05-27 |
$63,628,000 |
| 6561872 |
Method and apparatus for stripping coating |
Jeffrey Fehrenbach, William Lee Imhoff, David Allen Kastrup |
2003-05-13 |
$55,705,000 |
| 6557350 |
Method and apparatus for cooling gas turbine engine igniter tubes |
Ella Christine Kutter, Steven C. Vise, John Robert Staker, Marwan Al-Roub, Tariq Kay Harris |
2003-05-06 |
$48,116,000 |
| 6553767 |
Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form |
Daniel Dale Brown, Myron Edward Rutherford, Steven C. Vise, Jeffrey Michael Martini |
2003-04-29 |
$55,961,000 |
| 6513331 |
Preferential multihole combustor liner |
Daniel Dale Brown, Myron Edward Rutherford |
2003-02-04 |
$73,993,000 |
| 6408610 |
Method of adjusting gas turbine component cooling air flow |
James M. Caldwell, Karl S. Fessenden, Xuenan Wang, Jerald M. Kauffman |
2002-06-25 |
$56,960,000 |
| 6345441 |
Method of repairing combustion chamber liners |
James M. Caldwell, Steven Allen Stiverson, David Bruce Patterson, Edward John Emilianowicz |
2002-02-12 |
$127,630,000 |
| 6286302 |
Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein |
James Groeschen, Mark Gerard Rettig |
2001-09-11 |
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