Patent · US Active

Fan rotor with flow induced resonance control

US10458436B2 · kind B2 · utility

2Cited by
30References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 22, 2017
Grant dateOct 29, 2019
Priority date
Expiry dateDec 22, 2037

Classification

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

Abstract

A rotor for a gas turbine is disclosed which includes alternating first and second set of rotor blades, the first set of rotor blades having a baseline profile and the second set of rotor blades having a profile with a cutback relative to the baseline profile, the cutback removing a portion of the baseline profile surrounding a maximum deflection point of a selected natural vibration mode. The cutback may be a leading edge cutback at a span position located a distance away from the hub between 50% and 90% of the total span length. The selected natural vibration mode may be a natural vibration mode higher than the 1st natural vibration mode, more specifically may be the 4th natural vibration mode.

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