Inventor · disambiguated record
Friedrich Soechting
Also filed as: SOECHTING FRIEDRICH · SOECHTING FRIEDRICH O
27 granted patents·2 pending applications·2,239 citations·filing 1988–2005
98Inventor score
Top patents by PatentIndex Score
29 records- 0198US5931638ATurbomachinery airfoil with optimized heat transferUNITED TECHNOLOGIES CORP·Filed 1997·Granted Aug 3, 1999·241 cites·17 claims
- 0298US5419039AMethod of making an air cooled vane with film cooling pocket constructionUNITED TECHNOLOGIES CORP·Filed 1994·Granted May 30, 1995·144 cites·6 claims
- 0398US5392515AMethod of manufacturing an air cooled vane with film cooling pocket constructionUNITED TECHNOLOGIES CORP·Filed 1992·Granted Feb 28, 1995·148 cites·4 claims
- 0497US6402470B1Method and apparatus for cooling a wall within a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jun 11, 2002·217 cites·15 claims
- 0596US5720431ACooled blades for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1988·Granted Feb 24, 1998·172 cites·7 claims
- 0696US5405242ACooled vaneUNITED TECHNOLOGIES CORP·Filed 1990·Granted Apr 11, 1995·103 cites·8 claims
- 0795US7033138B2Ring segment of gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Apr 25, 2006·116 cites·4 claims
- 0895US6514042B2Method and apparatus for cooling a wall within a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2001·Granted Feb 4, 2003·93 cites·7 claims
- 0991US6247896B1Method and apparatus for cooling an airfoilUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jun 19, 2001·102 cites·24 claims
- 1090US6994514B2Turbine blade and gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Feb 7, 2006·58 cites·13 claims
- 1190US6419446B1Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jul 16, 2002·110 cites·28 claims
- 1290US6164912AHollow airfoil for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1998·Granted Dec 26, 2000·100 cites·10 claims
- 1390US5599166ACore for fabrication of gas turbine engine airfoilsUNITED TECHNOLOGIES CORP·Filed 1994·Granted Feb 4, 1997·110 cites·3 claims
- 1489US5645397ATurbine vane assembly with multiple passage cooled vanesUNITED TECHNOLOGIES CORP·Filed 1995·Granted Jul 8, 1997·95 cites·12 claims
- 1585US6860108B2Gas turbine tail tube seal and gas turbine using the sameMITSUBISHI HEAVY IND LTD·Filed 2003·Granted Mar 1, 2005·44 cites·5 claims
- 1685US6761529B2Cooling structure of stationary blade, and gas turbineMITSHUBISHI HEAVY IND LTD·Filed 2002·Granted Jul 13, 2004·48 cites·6 claims
- 1785US6210112B1Apparatus for cooling an airfoil for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2000·Granted Apr 3, 2001·41 cites·3 claims
- 1883US7552647B2Turbine blade fatigue life evaluating methodMITSUBISHI HEAVY IND LTD·Filed 2005·Granted Jun 30, 2009·12 cites·4 claims
- 1980US6722138B2Vane platform trailing edge coolingUNITED TECHNOLOGIES CORP·Filed 2000·Granted Apr 20, 2004·42 cites·2 claims
- 2078US6280140B1Method and apparatus for cooling an airfoilUNITED TECHNOLOGIES CORP·Filed 1999·Granted Aug 28, 2001·60 cites·21 claims
- 2178US6050777AApparatus and method for cooling an airfoil for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1997·Granted Apr 18, 2000·55 cites·8 claims
- 2271US6983659B2Turbine blade creep life evaluating method, turbine blade creep elongation strain measuring apparatus, and turbine bladeMITSUBISHI HEAVY IND LTD·Filed 2003·Granted Jan 10, 2006·27 cites·19 claims
- 2371US6742991B2Turbine blade and gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Jun 1, 2004·28 cites·12 claims
- 2465US6988872B2Turbine moving blade and gas turbineMITSUBISHI HEAVY IND LTD·Filed 2003·Granted Jan 24, 2006·23 cites·8 claims
- 2554US6758651B2Gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Jul 6, 2004·14 cites·3 claims
- 2651US6004100ATrailing edge cooling apparatus for a gas turbine airfoilUNITED TECHNOLOGIES CORP·Filed 1997·Granted Dec 21, 1999·26 cites·11 claims
- 2749US6887039B2Stationary blade in gas turbine and gas turbine comprising the sameMITSUBISHI HEAVY IND LTD·Filed 2002·Granted May 3, 2005·10 cites·5 claims
- 2838US2006269409A1Gas turbine moving blade having a platform, a method of forming the moving blade, a sealing plate, and a gas turbine having these elementsMITSUBISHI HEAVY IND LTD·Filed 2005·Application pending·0 cites
- 2933US2004073400A1Method for managing lifespans of high temperature gas turbine components and its implementation through computer programMITSUBISHI HEAVY IND LTD·Filed 2002·Application pending·0 cites
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