Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Cooled gas turbine component with adjustable cooling

Cooled gas turbine component with adjustable cooling

US Patent 6416279 · Granted Jul 9, 2002

Estimated economic value: $354,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Measuring device and method of determining a depth of field of an optical setup2024
Device for separating foreign particles out of the cooling air that can be fed t2006
Cooled components with conical cooling passages2005
Arrangement for cooling a flow-passage wall surrounding a flow passage, having a2003
Method for providing a curved cooling channel in a gas turbine component as well2003
Apparatus and process for impingement cooling of a component exposed to heat in 2003
Platelike projecting component portion of a gas turbine2003
Blade for gas turbines with choke cross section at the trailing edge2002
Turbine blade with actively cooled shroud-band element2002
Arrangement for cooling a flow-passage wall surrrounding a flow passage, having 2002
Turbine blade wall section cooled by an impact flow2002
Drilled cooling air openings in gas turbine components2002