FS

Friedrich Soechting

RTX (Raytheon): 17 patents #543 of 15,912Top 4%
Mitsubishi Electric: 9 patents #3,275 of 25,717Top 15%
MI Mitsuibshi Heavy Industries: 1 patents #4 of 121Top 4%
Overall (All Time): #147,727 of 4,157,543Top 4%
27
Patents All Time

Issued Patents All Time

Showing 25 most recent of 27 patents

Patent #TitleCo-InventorsDate
7552647 Turbine blade fatigue life evaluating method Charles Ellis, Yasuoki Tomita, Yugo Tokunaga 2009-06-30
7033138 Ring segment of gas turbine Yasuoki Tomita, Osamu Isumi, Shinichi Inoue, Vincent P. Laurello, Hiroshige Matsuoka 2006-04-25
6994514 Turbine blade and gas turbine Yasuoki Tomita, Shunsuke Torii 2006-02-07
6988872 Turbine moving blade and gas turbine Charles Ellis, Yasuoki Tomita, Shunsuke Torii 2006-01-24
6983659 Turbine blade creep life evaluating method, turbine blade creep elongation strain measuring apparatus, and turbine blade Charles Ellis, Yasuoki Tomita, Yugo Tokunaga 2006-01-10
6887039 Stationary blade in gas turbine and gas turbine comprising the same Satoshi Hada, Masamitsu Kuwabara, Junichiro Masada, Yasuoki Tomita 2005-05-03
6860108 Gas turbine tail tube seal and gas turbine using the same Yasuoki Tomita, Shunsuke Torii 2005-03-01
6761529 Cooling structure of stationary blade, and gas turbine Satoshi Hada, Masamitsu Kuwabara, Junichiro Masada, Yasuoki Tomita 2004-07-13
6758651 Gas turbine Yasuoki Tomita, Shigehiro Shiozaki 2004-07-06
6742991 Turbine blade and gas turbine Satoshi Hada, Masamitsu Kuwabara, Junichiro Masada, Yasuoki Tomita 2004-06-01
6722138 Vane platform trailing edge cooling Alan D. Bessette 2004-04-20
6514042 Method and apparatus for cooling a wall within a gas turbine engine William S. Kvasnak, Ronald S. LaFleur, Christopher R. Joe, Joe Moroso, Douglas A. Hayes 2003-02-04
6419446 Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine William A. Kvasnak, Karen A. Thole, Gary A. Zess 2002-07-16
6402470 Method and apparatus for cooling a wall within a gas turbine engine William S. Kvasnak, Ronald S. LaFleur, Christopher R. Joe, Joe Moroso, Douglas A. Hayes 2002-06-11
6280140 Method and apparatus for cooling an airfoil William A. Kvasnak, Thomas A. Auxier, James P. Downs, William H. Calhoun, Douglas A. Hayes 2001-08-28
6247896 Method and apparatus for cooling an airfoil Thomas A. Auxier, James P. Downs, William S. Kvasnak, William H. Calhoun, Douglas A. Hayes 2001-06-19
6210112 Apparatus for cooling an airfoil for a gas turbine engine Martin G. Tabbita, James P. Downs, Thomas A. Auxier 2001-04-03
6164912 Hollow airfoil for a gas turbine engine Martin G. Tabbita, James P. Downs, Thomas A. Auxier, Frederick Steinbauer, Jr. 2000-12-26
6050777 Apparatus and method for cooling an airfoil for a gas turbine engine Martin G. Tabbita, James P. Downs, Thomas A. Auxier 2000-04-18
6004100 Trailing edge cooling apparatus for a gas turbine airfoil Hans R. Przirembel 1999-12-21
5931638 Turbomachinery airfoil with optimized heat transfer David A. Krause, Dominic J. Mongillo, Mark F. Zelesky 1999-08-03
5720431 Cooled blades for a gas turbine engine Robert R. Sellers, Frank W Huber, Thomas A. Auxier 1998-02-24
5645397 Turbine vane assembly with multiple passage cooled vanes William L Plank, Kenneth B. Hall 1997-07-08
5599166 Core for fabrication of gas turbine engine airfoils Donald L. Deptowicz 1997-02-04
5419039 Method of making an air cooled vane with film cooling pocket construction Thomas A. Auxier, Hans R. Przirembel 1995-05-30