Inventor
BEECK ALEXANDER
US42 patents
⚠️ This page may combine multiple inventors who share the name “BEECK ALEXANDER”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
ALSTOM SWITZERLAND LTD
15 patentsUS6514041B1Feb 4, 2003
Carrier for guide vane and heat shield segment
ALSTOM SWITZERLAND LTD84 citations97
US6340284B1Jan 22, 2002
Turbine blade with actively cooled shroud-band element
ALSTOM SWITZERLAND LTD62 citations95
US6644920B2Nov 11, 2003
Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine component
ALSTOM SWITZERLAND LTD50 citations93
US6534975B2Mar 18, 2003
Nondestructive 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 material
ALSTOM SWITZERLAND LTD26 citations92
US6481966B2Nov 19, 2002
Blade for gas turbines with choke cross section at the trailing edge
ALSTOM SWITZERLAND LTD35 citations92
US6446710B2Sep 10, 2002
Arrangement for cooling a flow-passage wall surrrounding a flow passage, having at least one rib element
ALSTOM SWITZERLAND LTD35 citations91
US6499943B1Dec 31, 2002
Friction-susceptible component of a thermal turbo machine
ALSTOM SWITZERLAND LTD19 citations90
US6641360B2Nov 4, 2003
Device and method for cooling a platform of a turbine blade
ALSTOM SWITZERLAND LTD33 citations89
US6422811B1Jul 23, 2002
Cooling arrangement for blades of a gas turbine
ALSTOM SWITZERLAND LTD14 citations84
US6640597B2Nov 4, 2003
Method for reducing variance in the coolant consumption of components of a turbo-machine
ALSTOM SWITZERLAND LTD9 citations74
US6333069B1Dec 25, 2001
Method for preventing harm from constrictions formed during coating with a protective coat in the cooling holes of gas-cooled parts
ALSTOM SWITZERLAND LTD10 citations74
US6565317B2May 20, 2003
Platelike projecting component portion of a gas turbine
ALSTOM SWITZERLAND LTD7 citations73
US6589011B2Jul 8, 2003
Device for cooling a shroud of a gas turbine blade
ALSTOM SWITZERLAND LTD3 citations62
US6575698B2Jun 10, 2003
Sealing of a thermal turbomachine
ALSTOM SWITZERLAND LTD4 citations60
US6695036B2Feb 24, 2004
Method for producing a cast part, model mold, and ceramic insert for use in this method
ALSTOM SWITZERLAND LTD4 citations57
ASEA BROWN BOVERI
10 patentsUS6241469B1Jun 5, 2001
Turbine blade
ASEA BROWN BOVERI107 citations98
US5827045AOct 27, 1998
Thermally loaded blade for a turbomachine
ASEA BROWN BOVERI53 citations96
US6012723AJan 11, 2000
Brush gasket
ASEA BROWN BOVERI51 citations93
US6312218B1Nov 6, 2001
Sealing arrangement
ASEA BROWN BOVERI26 citations92
US6308511B1Oct 30, 2001
Method and device for cooling guide vanes in a gas turbine plant
ASEA BROWN BOVERI44 citations92
US6276692B1Aug 21, 2001
Non-contact sealing of gaps in gas turbines
ASEA BROWN BOVERI32 citations91
US6193468B1Feb 27, 2001
Hollow-cast component
ASEA BROWN BOVERI12 citations73
US5765366AJun 16, 1998
Fuel feed for gas turbines having an annular combustion chamber
ASEA BROWN BOVERI12 citations70
US6343474B1Feb 5, 2002
Cooling passage of a component subjected to high thermal loading
ASEA BROWN BOVERI10 citations69
US6162018ADec 19, 2000
Rotor for thermal turbomachines
ASEA BROWN BOVERI8 citations66
ALSTOM TECHNOLOGY LTD
5 patentsUS6705383B2Mar 16, 2004
Process for the rapid production of hollow components of flow machines for manufacturing development
ALSTOM TECHNOLOGY LTD43 citations92
US6857639B2Feb 22, 2005
Gap seal for sealing a gap between two adjacent components
ALSTOM TECHNOLOGY LTD23 citations91
US6916021B2Jul 12, 2005
Sealing arrangement
ALSTOM TECHNOLOGY LTD20 citations89
US6739594B2May 25, 2004
Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint
ALSTOM TECHNOLOGY LTD6 citations63
US6682304B2Jan 27, 2004
Cooled gas turbine blade
ALSTOM TECHNOLOGY LTD3 citations62