Inventor · disambiguated record
David R. Malley
Also filed as: MALLEY DAVID R
9 granted patents·3 pending applications·193 citations·filing 1977–2011
89Inventor score
Top patents by PatentIndex Score
12 records- 0193US4219592ATwo-way surfacing process by fusion weldingUNITED TECHNOLOGIES CORP·Filed 1977·Granted Aug 26, 1980·62 cites·12 claims
- 0286US7244320B2Methods for repairing gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jul 17, 2007·28 cites·25 claims
- 0384US4579602AForging process for superalloysUNITED TECHNOLOGIES CORP·Filed 1983·Granted Apr 1, 1986·38 cites·6 claims
- 0483US7708846B2Superalloy stabilizationUNITED TECHNOLOGIES CORP·Filed 2005·Granted May 4, 2010·6 cites·23 claims
- 0573US7854064B2Enhanced weldability for high strength cast and wrought nickel superalloysUNITED TECHNOLOGIES CORP·Filed 2006·Granted Dec 21, 2010·15 cites·21 claims
- 0671US5938863ALow cycle fatigue strength nickel base superalloysUNITED TECHNOLOGIES CORP·Filed 1996·Granted Aug 17, 1999·26 cites·40 claims
- 0760US7303112B2Repair of braze joint and article repairedUNITED TECHNOLOGIES CORP·Filed 2004·Granted Dec 4, 2007·10 cites·34 claims
- 0855US4654091AElimination of quench cracking in superalloy disksUNITED TECHNOLOGIES CORP·Filed 1982·Granted Mar 31, 1987·8 cites·1 claims
- 0948US2008029500A1Brazing repairsUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 1045US2009094829A1Method for ultrasonic peening of gas turbine engine components without engine disassemblyUNITED TECHNOLOGIES CORP·Filed 2007·Application pending·0 cites
- 1140US8127442B2Compressor blade flow form technique for repairMULLOOLY JOHN F·Filed 2005·Granted Mar 6, 2012·0 cites·8 claims
- 1237US2011308290A1Method for ultrasonic peening of gas turbine engine components without engine disassemblyBUNTING BILLIE W·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →