Patent · US Active

Nose cone for a turbomachine

US7419364B2 · kind B2 · utility

8Cited by
5References
5Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 26, 2005
Grant dateSep 2, 2008
Priority date
Expiry dateDec 3, 2026

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T137/0536
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A nose cone for a turbomachine, such as a turbojet in particular, the cone being mounted on the end of a shaft carrying fan blades and being associated with a controlled axial displacement mechanism, thereby making it possible to modify the axial position of the cone relative to the fan blades.

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