The actuator is used to control the emergency ram air intake. It contains one permanent magnet DC motor and a thermo switch, operating via a two-step reduction gear train and an acme jack screw.
The actuator is used to control the emergency ram air intake with one permanent magnet DC motor. It operates via a two-step reduction gear train and an acme jack screw with high static load capacity.
The actuator activates the air intake flap of the APU of the world’s most modern commercial aircraft. It is engineered to meet the highest reliability standards and ensure long-life performance.
The actuator activates the air intake duct of the APU. An acme jack screw is driven via a two-step gear train, forming a linear, self-locking output. The stroke is limited electrically.
The actuator activates the air intake flap actuator of Europe’s most modern military transport aircraft. It is engineered to withstand harsh environmental conditions during operation.
The highly reliable actuator activates the air intake duct of the APU. The acme jack screw is operated by a DC permanent magnet motor. The stroke is limited electrically by micro switches.
The engine throttle actuator is installed in an Unmanned Aerial Vehicle (UAV). It includes control electronics for position loop closure and performs the movement of the lever. A second motor is installed for redundancy.
All trim actuators artificially simulate the trim forces in all dimensions. They consist of a damper or friction brake to provide shock- and oscillation-less quick adjustment of trim position.
The seat actuator is installed in business class seats to ensure a secure and reliable adaptation of the seating position. The unit is lightweight, designed to meet the latest standards.
The sill actuator is a component of the cargo loading system of the airplane. The ram rod end operates the sill door latches, allowing the movement to open the “Y” latches of the sill doors.
The lock actuator is installed in cargo freighter systems to prevent unintended movement of cargo containers. It is used to control the X and Y-Z locking units of the cargo system.
The actuator is a lock and release unit used on a high-performance military jet. It releases a drogue parachute coming off the aft section of the aircraft just after landing.
The tail rotor actuator is installed on the rear end of a heavy-lift transport helicopter. It operates the angle-of-attack rear rotor blades and prevents the turning of the tail rotor in the air system. It is equipped with a thermal overload protection system.
The servo N2 actuator is installed on Airbus Helicopters BO105 rotary aircraft and supports the aircraft’s rotor head steering capability to the maximum standards.
