Inventor · disambiguated record
Alexander Beeck
Also filed as: BEECK ALEXANDER · BEECK ALEXANDER DR · BEECK ALEXANDER R · BEECK ALEXANDER RALPH
64 granted patents·12 pending applications·1,839 citations·filing 1994–2018
99Inventor score
Files withBEECK ALEXANDER R17ALSTOM SWITZERLAND LTD15ASEA BROWN BOVERI10SIEMENS AG7ALSTOM TECHNOLOGY LTD5
Top patents by PatentIndex Score
76 records- 0198US6241469B1Turbine bladeASEA BROWN BOVERI·Filed 1999·Granted Jun 5, 2001·107 cites·13 claims
- 0296US6265022B1Process of plugging cooling holes of a gas turbine componentABB ALSTOM POWER CH AG·Filed 2000·Granted Jul 24, 2001·93 cites·19 claims
- 0395US8047001B2Media mixing insert for turbine blade in turbine engineSIEMENS AG·Filed 2007·Granted Nov 1, 2011·38 cites·18 claims
- 0495US6705383B2Process for the rapid production of hollow components of flow machines for manufacturing developmentALSTOM TECHNOLOGY LTD·Filed 2001·Granted Mar 16, 2004·43 cites·5 claims
- 0595US6514041B1Carrier for guide vane and heat shield segmentALSTOM SWITZERLAND LTD·Filed 2001·Granted Feb 4, 2003·84 cites·24 claims
- 0694US8092175B2Turbine bladeBEECK ALEXANDER R·Filed 2007·Granted Jan 10, 2012·42 cites·17 claims
- 0792US6412541B2Process for producing a thermally loaded castingALSTOM POWER NV·Filed 2001·Granted Jul 2, 2002·80 cites·16 claims
- 0891US6416282B1Rotor for a gas turbineALSTOM·Filed 2000·Granted Jul 9, 2002·66 cites·12 claims
- 0991US6183199B1Cooling-air boreABB RESEARCH LTD·Filed 1999·Granted Feb 6, 2001·137 cites·21 claims
- 1090US8961135B2Mateface gap configuration for gas turbine engineBEECK ALEXANDER R·Filed 2011·Granted Feb 24, 2015·18 cites·18 claims
- 1189US8176720B2Air cooled turbine component having an internal filtration systemBEECK ALEXANDER R·Filed 2009·Granted May 15, 2012·31 cites·14 claims
- 1289US7467922B2Cooled turbine blade or vane for a gas turbine, and use of a turbine blade or vane of this typeSIEMENS AG·Filed 2005·Granted Dec 23, 2008·33 cites·9 claims
- 1388US6644920B2Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine componentALSTOM SWITZERLAND LTD·Filed 2001·Granted Nov 11, 2003·50 cites·11 claims
- 1488US5513982ACombustion chamberABB MANAGEMENT AG·Filed 1994·Granted May 7, 1996·55 cites·24 claims
- 1587US9017030B2Turbine component including airfoil with contourBEECK ALEXANDER R·Filed 2011·Granted Apr 28, 2015·10 cites·19 claims
- 1687US8376697B2Gas turbine sealing apparatusSIEMENS ENERGY INC·Filed 2009·Granted Feb 19, 2013·27 cites·20 claims
- 1786US8961134B2Turbine blade or vane with separate endwallBEECK ALEXANDER R·Filed 2011·Granted Feb 24, 2015·8 cites·11 claims
- 1885US8690158B2Axially angled annular sealsBEECK ALEXANDER R·Filed 2010·Granted Apr 8, 2014·9 cites·16 claims
- 1985US7300253B2Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ringSIEMENS AG·Filed 2005·Granted Nov 27, 2007·27 cites·15 claims
- 2084US8192166B2Tip shrouded turbine blade with sealing rail having non-uniform thicknessBEECK ALEXANDER R·Filed 2009·Granted Jun 5, 2012·25 cites·20 claims
- 2184US6884029B2Heat-tolerated vortex-disrupting fluid guide componentSIEMENS WESTINGHOUSE POWER·Filed 2002·Granted Apr 26, 2005·32 cites·19 claims
- 2283US6131800AMethod for coating and welding stator vanes of a gas turbineABB ALSTOM POWER CH AG·Filed 2000·Granted Oct 17, 2000·31 cites·16 claims
- 2381US6534975B2Nondestructive method for determining the thickness of a metallic protective layer on a metallic base material via a different type of layer between the metallic protective layer and the metallic base materialALSTOM SWITZERLAND LTD·Filed 2001·Granted Mar 18, 2003·26 cites·13 claims
- 2480US7927073B2Advanced cooling method for combustion turbine airfoil filletsSIEMENS ENERGY INC·Filed 2007·Granted Apr 19, 2011·21 cites·18 claims
- 2579US5518311AMixing chamber with vortex generators for flowing gasesABB MANAGEMENT AG·Filed 1994·Granted May 21, 1996·52 cites·18 claims
- 2678US8322977B2Seal 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
- 2778US6340284B1Turbine blade with actively cooled shroud-band elementALSTOM SWITZERLAND LTD·Filed 1999·Granted Jan 22, 2002·62 cites·13 claims
- 2876US6481966B2Blade for gas turbines with choke cross section at the trailing edgeALSTOM SWITZERLAND LTD·Filed 2000·Granted Nov 19, 2002·35 cites·11 claims
- 2976US6446710B2Arrangement for cooling a flow-passage wall surrrounding a flow passage, having at least one rib elementALSTOM SWITZERLAND LTD·Filed 2000·Granted Sep 10, 2002·35 cites·14 claims
- 3076US6012723ABrush gasketASEA BROWN BOVERI·Filed 1997·Granted Jan 11, 2000·51 cites·8 claims
- 3174US7722326B2Intensively cooled trailing edge of thin airfoils for turbine enginesSIEMENS ENERGY INC·Filed 2007·Granted May 25, 2010·14 cites·20 claims
- 3274US6641360B2Device and method for cooling a platform of a turbine bladeALSTOM SWITZERLAND LTD·Filed 2001·Granted Nov 4, 2003·33 cites·11 claims
- 3374US5827045AThermally loaded blade for a turbomachineASEA BROWN BOVERI·Filed 1997·Granted Oct 27, 1998·53 cites·13 claims
- 3473US9528706B2Swirling midframe flow for gas turbine engine having advanced transitionsMONTGOMERY MATTHEW D·Filed 2013·Granted Dec 27, 2016·3 cites·6 claims
- 3573US8770924B2Gas turbine engine with angled and radial supportsBEECK ALEXANDER·Filed 2011·Granted Jul 8, 2014·6 cites·20 claims
- 3669US6565317B2Platelike projecting component portion of a gas turbineALSTOM SWITZERLAND LTD·Filed 2001·Granted May 20, 2003·7 cites·8 claims
- 3768US8690536B2Turbine blade tip with vortex generatorsBEECK ALEXANDER R·Filed 2010·Granted Apr 8, 2014·3 cites·17 claims
- 3866US6308511B1Method and device for cooling guide vanes in a gas turbine plantASEA BROWN BOVERI·Filed 1999·Granted Oct 30, 2001·44 cites·7 claims
- 3965US6516865B1Hollow-cast componentALSTOM·Filed 2000·Granted Feb 11, 2003·19 cites·10 claims
- 4064US5564896AMethod and apparatus for shaft sealing and for cooling on the exhaust-gas side of an axial-flow gas turbineABB MANAGEMENT AG·Filed 1995·Granted Oct 15, 1996·45 cites·6 claims
- 4163US6857639B2Gap seal for sealing a gap between two adjacent componentsALSTOM TECHNOLOGY LTD·Filed 2003·Granted Feb 22, 2005·23 cites·5 claims
- 4261US8769816B2Method of assembling a gas turbine engineBEECK ALEXANDER R·Filed 2012·Granted Jul 8, 2014·2 cites·12 claims
- 4361US8313286B2Diffuser apparatus in a turbomachineBEECK ALEXANDER R·Filed 2009·Granted Nov 20, 2012·6 cites·20 claims
- 4461US6499943B1Friction-susceptible component of a thermal turbo machineALSTOM SWITZERLAND LTD·Filed 2000·Granted Dec 31, 2002·19 cites·20 claims
- 4559US6916021B2Sealing arrangementALSTOM TECHNOLOGY LTD·Filed 2003·Granted Jul 12, 2005·20 cites·21 claims
- 4658US6276692B1Non-contact sealing of gaps in gas turbinesASEA BROWN BOVERI·Filed 1999·Granted Aug 21, 2001·32 cites·32 claims
- 4758US6068445ACooling system for the leading-edge region of a hollow gas-turbine bladeABB RESEARCH LTD·Filed 1998·Granted May 30, 2000·34 cites·9 claims
- 4857US6695036B2Method for producing a cast part, model mold, and ceramic insert for use in this methodALSTOM SWITZERLAND LTD·Filed 2001·Granted Feb 24, 2004·4 cites·11 claims
- 4957US6422811B1Cooling arrangement for blades of a gas turbineALSTOM SWITZERLAND LTD·Filed 2000·Granted Jul 23, 2002·14 cites·15 claims
- 5056US6739594B2Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing jointALSTOM TECHNOLOGY LTD·Filed 2001·Granted May 25, 2004·6 cites·17 claims
Showing the top 50 of 76 patent records by PatentIndex Score.
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