Patent · US Active

Rotor of an exhaust gas turbocharger

US10253633B2 · kind B2 · utility

5Cited by
6References
9Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 2, 2013
Grant dateApr 9, 2019
Priority date
Expiry dateJun 19, 2034

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2250/712
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A rotor of an exhaust-gas turbocharger includes a rotor hub and rotor blades disposed on the rotor hub. The rotor blades have a blade thickness distribution selected in such a way that the rotor blades have along their extent from a fluid inlet or leading edge to a fluid outlet or trailing edge at least one transition between a stiffness or rigidity-oriented blade thickness distribution and an inertia and stress-oriented blade thickness distribution over the height of the blade.

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