Patent · US Active

Blade preloading system

US8186961B2 · kind B2 · utility

17Cited by
15References
12Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJan 23, 2009
Grant dateMay 29, 2012
Priority date
Expiry dateOct 31, 2030

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49321
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A removable fan blade of a turbofan engine includes a blade root at one end thereof. A rotor disk has a retention slot having dimensions corresponding for receiving the root of the fan blade in the slot. An elongated resilient member extends within the retention slot in a lengthwise direction between the root of the fan blade and the bottom of the retention slot and an elongated member extends lengthwise between the root of the fan blade and the elastomeric member to compress the resilient member and provide a radial preload to the fan blade.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.