Inventor · disambiguated record
Alan B. Minick
Also filed as: MINICK ALAN B
14 granted patents·8 pending applications·148 citations·filing 1995–2016
92Inventor score
Files withUNITED TECHNOLOGIES CORP7MINICK ALAN B6PRATT & WHITNEY ROCKETDYNE INC4AEROJET ROCKETDYNE INC2BUSER MARK F1
Top patents by PatentIndex Score
22 records- 0191US9149870B2Additive manufacturing chamber with reduced loadMINICK ALAN B·Filed 2012·Granted Oct 6, 2015·11 cites·15 claims
- 0291US8695540B2Fuel-cracking diesel engine systemMINICK ALAN B·Filed 2012·Granted Apr 15, 2014·11 cites·21 claims
- 0386US7891298B2Guided projectilePRATT & WHITNEY ROCKETDYNE INC·Filed 2008·Granted Feb 22, 2011·34 cites·23 claims
- 0483US7823510B1Extended range projectilePRATT & WHITNEY ROCKETDYNE INC·Filed 2008·Granted Nov 2, 2010·22 cites·25 claims
- 0571US8883007B2Fluid separation system with reduced foulingBUSER MARK F·Filed 2009·Granted Nov 11, 2014·10 cites·1 claims
- 0670US8091836B2Rotary wing system with ion field flow controlMINICK ALAN B·Filed 2007·Granted Jan 10, 2012·10 cites·15 claims
- 0760US7246483B2Energetic detonation propulsionUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jul 24, 2007·14 cites·33 claims
- 0859US8322981B2Aircraft fluid diversion inlet louverLIGHT STACEY H·Filed 2009·Granted Dec 4, 2012·6 cites·20 claims
- 0958US8839761B2Augmenter for compound compression engineMINICK ALAN B·Filed 2010·Granted Sep 23, 2014·2 cites·1 claims
- 1056US10309344B2Stored pressure driven cycleAEROJET ROCKETDYNE INC·Filed 2014·Granted Jun 4, 2019·1 cites·12 claims
- 1155US2011108019A1Heliostat jointPRATT & WHITNEY ROCKETDYNE INC·Filed 2009·Application pending·0 cites
- 1251US7413149B2Wing enhancement through ion entrainment of mediaUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 19, 2008·9 cites·19 claims
- 1347US2015284072A1Drag reduction through ion field flow controlUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1445US5687562ABypass air valve for turbofan engineUNITED TECHNOLOGIES CORP·Filed 1995·Granted Nov 18, 1997·14 cites·16 claims
- 1545US2014077422A1Reduced build mass additive manufacturing chamberPRATT & WHITNEY ROCKETDYNE INC·Filed 2012·Application pending·0 cites
- 1644US7204078B2Staged emitter-attractor ion driveUNITED TECHNOLOGIES CORP·Filed 2004·Granted Apr 17, 2007·2 cites·14 claims
- 1742US7296965B2Cryogenic bearingsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Nov 20, 2007·2 cites·20 claims
- 1842US2015308348A1Continuous detonation wave turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1941US2011272531A1Drag reduction through ion field flow controlMINICK ALAN B·Filed 2011·Application pending·0 cites
- 2040US2009127401A1Ion field flow control deviceCOUSINS WILLIAM T·Filed 2007·Application pending·0 cites
- 2137US2018142646A1Solid rocket motor with barrierAEROJET ROCKETDYNE INC·Filed 2016·Application pending·0 cites
- 2233US2012204535A1Augmented expander cycleMINICK ALAN B·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →