Patent · US Active

Translating cascade hidden blocker door thrust reverser

US10208708B2 · kind B2 · utility

6Cited by
25References
18Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJan 29, 2015
Grant dateFeb 19, 2019
Priority date
Expiry dateDec 3, 2035

Classification

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

Abstract

Aspects of the disclosure are directed to a thrust reverser system of an aircraft comprising: a translating cascade sleeve, a blocker door, and a kinematic mechanism configured to actuate the blocker door, the kinematic mechanism comprising: a first link coupled to the translating cascade sleeve, a second link coupled to the first link and a fixed structure, and a third link coupled to the first link and the blocker door.

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