Inventor · disambiguated record
Robert Russell Mayer
Also filed as: MAYER JR ROBERT R · MAYER ROBERT R · MAYER ROBERT RUSSELL
24 granted patents·2 pending applications·1,143 citations·filing 1993–2022
97Inventor score
Files withUNITED TECHNOLOGIES CORP12GEN ELECTRIC9KVM TECHNOLOGIES INC2MAYER ROBERT RUSSELL2RAYTHEON TECH CORP1
Top patents by PatentIndex Score
26 records- 0196US5480062AVacuum operated medicine dispenserKVM TECHNOLOGIES INC·Filed 1995·Granted Jan 2, 1996·303 cites·5 claims
- 0295US10167727B2Gas turbine engine blade containment systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 1, 2019·11 cites·4 claims
- 0395US6448685B1Stator core assemblyGEN ELECTRIC·Filed 2000·Granted Sep 10, 2002·57 cites·13 claims
- 0494US9255487B2Gas turbine engine seal carrierMAYER ROBERT RUSSELL·Filed 2012·Granted Feb 9, 2016·30 cites·16 claims
- 0594US9140137B2Gas turbine engine mid turbine frame bearing supportMAYER ROBERT RUSSELL·Filed 2012·Granted Sep 22, 2015·23 cites·15 claims
- 0694US6464230B1Flexible magnetic rubber brush seal for generatorsGEN ELECTRIC·Filed 2000·Granted Oct 15, 2002·45 cites·20 claims
- 0794US6378873B1Low flow fluid film seal for hydrogen cooled generatorsGEN ELECTRIC·Filed 2000·Granted Apr 30, 2002·56 cites·8 claims
- 0893US6406027B1Brush seal and machine having a brush sealGEN ELECTRIC·Filed 2000·Granted Jun 18, 2002·48 cites·7 claims
- 0991US5405048AVacuum operated medicine dispenserKVM TECHNOLOGIES INC·Filed 1993·Granted Apr 11, 1995·355 cites·73 claims
- 1088US10927687B2Gas turbine engine blade containment systemUNITED TECHNOLOGIES CORP·Filed 2018·Granted Feb 23, 2021·3 cites·10 claims
- 1183US6257588B1Brush seal and rotary machine including such brush sealGEN ELECTRIC·Filed 1998·Granted Jul 10, 2001·43 cites·17 claims
- 1282US6669202B1Multi-core brush seal assembly for rotary machinesGEN ELECTRIC·Filed 2002·Granted Dec 30, 2003·22 cites·28 claims
- 1381US6685190B1Ventilated trickle sealGEN ELECTRIC·Filed 2000·Granted Feb 3, 2004·21 cites·23 claims
- 1480US7789125B2Extended impingement cooling device and methodUNITED TECHNOLOGIES CORP·Filed 2007·Granted Sep 7, 2010·17 cites·6 claims
- 1578US7270175B2Extended impingement cooling device and methodUNITED TECHNOLOGIES CORP·Filed 2004·Granted Sep 18, 2007·44 cites·7 claims
- 1676US7017334B2Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewithUNITED TECHNOLOGIES CORP·Filed 2003·Granted Mar 28, 2006·39 cites·34 claims
- 1770US11939924B2Synchronized air modulating systemRAYTHEON TECH CORP·Filed 2022·Granted Mar 26, 2024·0 cites·7 claims
- 1870US6681476B2Method of forming a stator core assemblyGEN ELECTRIC·Filed 2001·Granted Jan 27, 2004·13 cites·9 claims
- 1969US6502824B2Brush seal for a bearing cavityGEN ELECTRIC·Filed 2000·Granted Jan 7, 2003·13 cites·9 claims
- 2061US11492977B2Synchronized air modulating systemUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 8, 2022·0 cites·9 claims
- 2154US10352248B2Synchronized air modulating systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 16, 2019·0 cites·10 claims
- 2252US10753279B2Gas turbine engine mid turbine frame bearing supportUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 25, 2020·0 cites·7 claims
- 2350US11428243B2Variable vane arrangement with vane receptacle insert(s)UNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 30, 2022·0 cites·11 claims
- 2448US9995171B2Cooling passages for a mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·0 cites·10 claims
- 2539US2016341070A1Gas turbine engine having energy dissipating gap and containment layerUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2639US2016341075A1Energy dissipating core case containment section for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
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