Assignee
BEECK ALEXANDER R
US·13 granted patents·4 pending applications·177 citations·filing 2004–2012
Top patents by PatentIndex Score
17 records- 0194US8092175B2Turbine bladeBEECK ALEXANDER R·Filed 2007·Granted Jan 10, 2012·42 cites·17 claims
- 0290US8961135B2Mateface gap configuration for gas turbine engineBEECK ALEXANDER R·Filed 2011·Granted Feb 24, 2015·18 cites·18 claims
- 0389US8176720B2Air cooled turbine component having an internal filtration systemBEECK ALEXANDER R·Filed 2009·Granted May 15, 2012·31 cites·14 claims
- 0487US9017030B2Turbine component including airfoil with contourBEECK ALEXANDER R·Filed 2011·Granted Apr 28, 2015·10 cites·19 claims
- 0586US8961134B2Turbine blade or vane with separate endwallBEECK ALEXANDER R·Filed 2011·Granted Feb 24, 2015·8 cites·11 claims
- 0685US8690158B2Axially angled annular sealsBEECK ALEXANDER R·Filed 2010·Granted Apr 8, 2014·9 cites·16 claims
- 0784US8192166B2Tip shrouded turbine blade with sealing rail having non-uniform thicknessBEECK ALEXANDER R·Filed 2009·Granted Jun 5, 2012·25 cites·20 claims
- 0878US8322977B2Seal structure for preventing leakage of gases across a gap between two components in a turbine engineBEECK ALEXANDER R·Filed 2009·Granted Dec 4, 2012·15 cites·17 claims
- 0968US8690536B2Turbine blade tip with vortex generatorsBEECK ALEXANDER R·Filed 2010·Granted Apr 8, 2014·3 cites·17 claims
- 1061US8769816B2Method of assembling a gas turbine engineBEECK ALEXANDER R·Filed 2012·Granted Jul 8, 2014·2 cites·12 claims
- 1161US8313286B2Diffuser apparatus in a turbomachineBEECK ALEXANDER R·Filed 2009·Granted Nov 20, 2012·6 cites·20 claims
- 1254US8257032B2Gas turbine with a guide vaneBEECK ALEXANDER R·Filed 2008·Granted Sep 4, 2012·5 cites·7 claims
- 1352US8616848B2Turbine blade damping device with controlled loadingBEECK ALEXANDER R·Filed 2009·Granted Dec 31, 2013·3 cites·16 claims
- 1449US2010196139A1Leakage flow minimization system for a turbine engineBEECK ALEXANDER R·Filed 2009·Application pending·0 cites
- 1546US2014060001A1Gas turbine engine with shortened mid sectionBEECK ALEXANDER R·Filed 2012·Application pending·0 cites
- 1641US2013121806A1Exhaust diffuser for a gas turbine, and method thereofBEECK ALEXANDER R·Filed 2011·Application pending·0 cites
- 1727US2006198916A1Method for producing ceramic objectsBEECK ALEXANDER R·Filed 2004·Application pending·0 cites
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