Inventor · disambiguated record
Robert L. Memmen
Also filed as: MEMMEN ROBERT L · SHELKOVOY LEGAL REPRESENTATIVE · SHELKOVOY LEGAL REPRESENTATIVE EVGENIY A
29 granted patents·5 pending applications·475 citations·filing 1983–2020
97Inventor score
Files withUNITED TECHNOLOGIES CORP13MEMMEN ROBERT L7BROSTMEYER JOSEPH D5FLORIDA TURBINE TECH INC5BELOUSOV IGOR V3
Top patents by PatentIndex Score
34 records- 0199US7306026B2Cooled turbine airfoils and methods of manufactureUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 11, 2007·70 cites·14 claims
- 0298US9643281B1Process of forming a metal part from a metal powder using a laser to melt the metal powder over a support surface that can be easily removed after the metal part has been formedMEMMEN ROBERT L·Filed 2016·Granted May 9, 2017·40 cites·1 claims
- 0398US7172012B1Investment castingUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 6, 2007·71 cites·19 claims
- 0497US9991763B1Gas turbine engine with multiple electric generatorsFLORIDA TURBINE TECH INC·Filed 2017·Granted Jun 5, 2018·13 cites·5 claims
- 0596US10801338B1Apparatus and process of forming an integrally bladed rotor with cooled single crystal blades and an equiax nickel diskFLORIDA TURBINE TECH INC·Filed 2018·Granted Oct 13, 2020·4 cites·9 claims
- 0696US8556578B1Spring loaded compliant seal for high temperature useMEMMEN ROBERT L·Filed 2012·Granted Oct 15, 2013·36 cites·17 claims
- 0795US9506350B1Turbine rotor blade of the spar and shell constructionMEMMEN ROBERT L·Filed 2016·Granted Nov 29, 2016·12 cites·12 claims
- 0894US8500405B1Industrial stator vane with sequential impingement cooling insertsFLORIDA TURBINE TECH INC·Filed 2012·Granted Aug 6, 2013·34 cites·15 claims
- 0991US10731485B1Apparatus and process of forming an integrally bladed rotor with cooled single crystal blades and an equiax nickel diskFLORIDA TURBINE TECH INC·Filed 2020·Granted Aug 4, 2020·2 cites·8 claims
- 1090US10024170B1Integrally bladed rotor with bore entry cooling holesMEMMEN ROBERT L·Filed 2016·Granted Jul 17, 2018·6 cites·13 claims
- 1190US9604756B1Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted Mar 28, 2017·3 cites·2 claims
- 1289US7325587B2Method for casting cooling holesUNITED TECHNOLOGIES CORP·Filed 2005·Granted Feb 5, 2008·15 cites·17 claims
- 1386US10024190B1Apparatus and process for forming an air cooled turbine airfoil with a cooling air channel and discharge slot in a thin wallMEMMEN ROBERT L·Filed 2016·Granted Jul 17, 2018·4 cites·8 claims
- 1485US9611755B2Turbine stator vane with insert and flexible sealMEMMEN ROBERT L·Filed 2014·Granted Apr 4, 2017·8 cites·11 claims
- 1583US7520312B2Investment castingUNITED TECHNOLOGIES CORP·Filed 2006·Granted Apr 21, 2009·6 cites·21 claims
- 1683US7216428B2Method for turbine element repairingUNITED TECHNOLOGIES CORP·Filed 2003·Granted May 15, 2007·40 cites·22 claims
- 1780US4512159AClip attachmentUNITED TECHNOLOGIES CORP·Filed 1984·Granted Apr 23, 1985·41 cites·2 claims
- 1879US7509734B2Repairing turbine elementUNITED TECHNOLOGIES CORP·Filed 2003·Granted Mar 31, 2009·13 cites·18 claims
- 1977US10794190B1Cast integrally bladed rotor with bore entry coolingFLORIDA TURBINE TECH INC·Filed 2018·Granted Oct 6, 2020·2 cites·8 claims
- 2076US9410869B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2015·Granted Aug 9, 2016·1 cites·3 claims
- 2175US9654161B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted May 16, 2017·1 cites·2 claims
- 2270US4542867AInternally cooled hollow airfoilUNITED TECHNOLOGIES CORP·Filed 1983·Granted Sep 24, 1985·36 cites·6 claims
- 2360US8864956B2Multi-component depositionBELOUSOV IGOR V·Filed 2009·Granted Oct 21, 2014·1 cites·21 claims
- 2458US9500564B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted Nov 22, 2016·0 cites·4 claims
- 2558US2016305436A1Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Application pending·0 cites
- 2655US7329436B2Vapor deposition of dissimilar materialsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 12, 2008·5 cites·20 claims
- 2754US8563890B2Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2012·Granted Oct 22, 2013·0 cites·22 claims
- 2853US8122600B2Fan and compressor blade dovetail restoration processKINSTLER MONIKA D·Filed 2003·Granted Feb 28, 2012·6 cites·11 claims
- 2952US8367963B2Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 5, 2013·4 cites·24 claims
- 3051US8286582B2Vapor deposition of dissimilar materialsBELOUSOV IGOR V·Filed 2007·Granted Oct 16, 2012·1 cites·19 claims
- 3150US2010196684A1Turbine Element RepairUNITED TECHNOLOGIES CORP·Filed 2010·Application pending·0 cites
- 3241US2008057254A1Turbine element repairUNITED TECHNOLOGIES CORP·Filed 2007·Application pending·0 cites
- 3337US2005205415A1Multi-component depositionBELOUSOV IGOR V·Filed 2004·Application pending·0 cites
- 3434US2006275108A1Hammerhead fluid sealMEMMEN ROBERT L·Filed 2005·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Robert L. Memmen files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →