Patent · US Active

Method of releasing a fan blade and assembly for releasing a fan blade from a turbofan engine

US10113442B2 · kind B2 · utility

5Cited by
1References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 15, 2016
Grant dateOct 30, 2018
Priority date
Expiry dateAug 2, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

According to one aspect, a method of releasing a fan blade for testing a turbofan engine includes providing an internal passage with a constant arc through an airfoil arranged about a blisk such that the constant arc of the internal passage aligns with a contour of the blisk. The method further includes packing the internal passage with a charge, modifying the airfoil such that the airfoil is released from the blisk evenly along a chordwise length of the airfoil, and detonating the charge such that the airfoil is released from the blisk at a selected time.

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