FR-3168207-A1 - HYDRAULIC CONTROL DEVICE FOR A THRUSH REVERSER
Abstract
A hydraulic control device (10) for a thrust reverser (12) of an aircraft propulsion nacelle, comprising: - a hydraulic motor (26) capable of operating as a motor and generator, this motor (26) having an output shaft (38) capable of driving a moving element of a thrust reverser (12), - a hydraulic circuit (36) comprising a solenoid valve (44), and - a control circuit (C1) for the second solenoid valve (44), this control circuit (C1) being configured to control the second solenoid valve (44) based on a signal relating to a position of the output shaft (38) of the motor (26), said circuit (C1) being further configured to control the second solenoid valve (44) based on a signal relating to the temperature of the fluid supplying the device (10) or circulating within the device (10). Figure for the abbreviation: Figure 5
Inventors
- Antoine BIANCHI,
- Hakim MAALIOUNE,
- Cedrik DJELASSI,
- Lucas ALJANCIC,
- Damien PICCOLO,
Assignees
- SAFRAN NACELLES
- SAFRAN AIRCRAFT ENGINES
Dates
- Publication Date
- 20260508
- Application Date
- 20241104