Patent · US Active

Position sensor for aircraft nacelle thrust reverser door

US12085042B2 · kind B2 · utility

0Cited by
8References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 7, 2022
Grant dateSep 10, 2024
Priority date
Expiry dateMar 9, 2042

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/821
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A position sensor for an aircraft nacelle thrust reverser door for an aircraft turbojet engine includes a target to be detected, a detector having a detection range and including a detection head configured to detect the target when it enters its detection range, and a target guide configured to guide the target in order to position it in the detection range of the detector. The detector is stationary relative to the target guide. In one form, the target is intended to be positioned on the door, and the detector and the target guide are intended to be positioned on a stationary structure of the thrust reverser. In another form, the target is intended to be positioned on a stationary structure of the thrust reverser, and the detector and the target guide are intended to be positioned on the door.

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