Patent · US Active

Control method for actuating a thrust reverser

US8151550B2 · kind B2 · utility

5Cited by
4References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2005
Grant dateApr 10, 2012
Priority date
Expiry dateApr 24, 2028

Classification

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

Abstract

The invention relates to a control method for opening or closing a turbojet engine thrust reverser (1) by using at least one mobile cowl (2) displaceable by means of at least one electric motor (7) consisting in analyzing at least one parameter representative for a pressure in the turbojet engine jet and in carrying out an operating sequence in which the operating parameters of the electric motor (7) are adjusted to a situation.

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