Inventor · disambiguated record
Jeff Miller
Also filed as: MILLER JEFF · MILLER JEFF H · MILLER JEFF HARLEY
10 granted patents·1 pending application·82 citations·filing 2000–2022
87Inventor score
Top patents by PatentIndex Score
11 records- 0186US9399920B2Turbine blade rail damperUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 26, 2016·5 cites·20 claims
- 0282US8951013B2Turbine blade rail damperMILLER JEFF H·Filed 2011·Granted Feb 10, 2015·9 cites·12 claims
- 0374US7273352B2Inlet partial blades for structural integrity and performanceUNITED TECHNOLOGIES CORP·Filed 2004·Granted Sep 25, 2007·24 cites·30 claims
- 0466US6752594B2Split blade frictional damperBOEING CO·Filed 2002·Granted Jun 22, 2004·21 cites·21 claims
- 0561US6944158B1Flow integrity for path transitioning data switchCIT ALCATEL·Filed 2000·Granted Sep 13, 2005·11 cites·24 claims
- 0656US11560899B2Pump with axially-elongated annular seal element between inducer and impellerAEROJET ROCKETDYNE INC·Filed 2018·Granted Jan 24, 2023·0 cites·9 claims
- 0746US9022742B2Blade shroud for fluid elementMILLER JEFF H·Filed 2012·Granted May 5, 2015·1 cites·1 claims
- 0843US12461511B2Development of a product using a process control plan digital twinBOEING CO·Filed 2022·Granted Nov 4, 2025·0 cites·22 claims
- 0943US11268515B2Turbopump with axially curved vaneAEROJET ROCKETDYNE INC·Filed 2015·Granted Mar 8, 2022·0 cites·13 claims
- 1043US7066714B2High speed rotor assembly shroudUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jun 27, 2006·11 cites·22 claims
- 1141US2007036642A1Bridged inducerBOEING CO·Filed 2005·Application pending·0 cites
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