Patent · US Active

Relighting a turbofan engine

US8875519B2 · kind B2 · utility

31Cited by
8References
2Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 22, 2010
Grant dateNov 4, 2014
Priority date
Expiry dateAug 21, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02C7/32
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The method and apparatus for in-flight relighting of a turbofan engine involve in one aspect selectively controlling an accessory drag load on one or more windmilling rotors to permit control of the windmill speed to an optimum value for relight conditions.

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