Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines

System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines

US Patent 9441499 · Granted Sep 13, 2016

Estimated economic value: $24,812,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Gas turbomachine diffuser assembly with radial flow splitters2024
Gas turbomachine diffuser assembly with radial flow splitters2023
Turbomachinery heat transfer system2023
Turbomachinery heat management system2022
Nozzle shaft assembly2022
Flow inducer for a gas turbine system2020
Active draft control for combined cycle power plant shutdown2019
Personal electronic vaporizer2018
Flow sleeve for thermal control of a double-walled turbine shell and related met2018
Turbine exhaust section structures with internal flow passages2017
System for supporting a turbine nozzle2016
Helical seal system for a turbomachine2016