Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine spindle bolt structure with reduced fretting motion

Gas turbine spindle bolt structure with reduced fretting motion

US Patent 8465259 · Granted Jun 18, 2013

Estimated economic value: $838,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Compressor bleed cooling system for mid-frame torque discs downstream from a com2020
Rotor disc with fluid removal channels to enhance life of spindle bolt2018
Rotor disc with fluid removal channels to enhance life of spindle bolt2018
Belly band seal with anti-rotation structure2017
Turbine rotor nut and bolt arrangement with improved fatigue resistance under ce2017
Gas turbine sealing band arrangement having a locking pin2017
Gas turbine spindle bolt structure with reduced fretting fatigue2017
Gas turbine spindle bolt structure with reduced fretting fatigue2017
Method and apparatus for turbine engine thru bolt stud and nut retention2016
Gas turbine including belly band seal anti-rotation device2016
Gas turbine including belly band seal anti-rotation device2016
Gas turbine engine2015