Patent · US Active

Method for manufacturing a shaft of a gas-turbine engine, in particular a radial shaft or a shaft arranged at an angle to the machine axis

US9211684B2 · kind B2 · utility

0Cited by
8References
5Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 11, 2013
Grant dateDec 15, 2015
Priority date
Expiry dateMay 28, 2034

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16C2360/23
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A method for manufacturing a radial shaft of a gas-turbine engine which is made up of +/−45° layers, zero layers and +/−30° layers of carbon fiber composite and connected to load-input end pieces via sinusoidal connecting areas.

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