Control Surface Actuator Drive for Maneuverable Airplane ПР–172 Prototype for 5-th Generation Airplanes

Purpose

The drive ПP–172 is designed for control surface displacement according to the signals. It is a servo system with continuous control, which provides transformation of input electric signals to mechanical displacement of output components.

Description

The Unit comprises the following blocks:
— DC contactless electric motor;
— power reducer;
— ball-screw transmission;
— drive reducer of ball position;
— potentiometer;
— rocker;
— braid with electrical connector.
Control Unit ПP-172 is designed for the following functions:
— interaction with control system;
— control of arresting of output components;
— realization of servo positioning;
— protection and control of the drive.

Technical data:

1. Maximum rotation shaft load torque 103 N.m, 10,5kgf.m
2. Deflection angle versus neutral position 34°±1,0°, max
3. Range of variation of control input signal 10±0,1V
4. Idle run angular speed 350°/c, minimum
5. Angular speed torque 60 N.m 170°/c, minimum
6. Angular speed maximum torque 35°/c, minimum
7. Zero position shift 0,3° max
8. Mass of Electric Actuator 1,7 kg
9. Mass of Control Unit 4,5 kg per 4 pcs

Hz Mn Nm Amplitude, dB Shift, grades
1 60 1.0-1.5 10
6 60 1.0-1.5 20
20 60 1.0-1.5 55
40 60 1.0-1.5  

 

1.0-1.5