Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas 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 ring

Gas 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 ring

US Patent 7300253 · Granted Nov 27, 2007

Estimated economic value: $1,118,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Guide vane for a turbomachine2021
Swirling midframe flow for gas turbine engine having advanced transitions2016
Rotating machine2016
Sealing arrangement for a thermal machine2016
Turbomachine clearance control configuration using a shape memory alloy or a bim2015
Thermally loaded, cooled component2015
Turbine component including airfoil with contour2015
Turbine blade or vane with separate endwall2015
Mateface gap configuration for gas turbine engine2015
Method of assembling a gas turbine engine2014
Gas turbine engine with angled and radial supports2014
Axially angled annular seals2014