The temperature switch is a high-class and accurate sensing device particularly developed for combat helicopter platforms. It is used and proven on Airbus Helicopters Tiger, meeting all performance data.
The pressure switch provides an electrical signal at a specific hydraulic pressure. It transforms hydraulic pressure into a mechanical movement via a multi-thickness pressure sensing membrane. Civil and military platforms have benefited from the high-end design for many decades.
The pressure switch is meant for aviation potable water and waste systems. Our prime customer Airbus successfully operates the product on multiple systems in its legacy and next-generation aircraft.
The pressure switch provides an electrical signal at a specific hydraulic pressure. It transforms hydraulic pressure into a mechanical movement via a multi-thickness pressure sensing membrane. A snap mechanism amplifies it into a usable stroke for the micro-switch.
The pedal sensor unit was specifically designed to accurately determine the pedal position of the Eurofighter. Hence, the pilot is able to complete each mission with the best flight characteristics.
The ramp system of the NH90 is managed and controlled by the control unit. There are connections to the ramp and hatch actuators, the cabin control panel, the cockpit control panel, and more.
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.
The Stick Position Augmentation System (SPAS) features an electric actuator that, as a function of airspeed and collective pitch, introduces an aft cyclic control input as airspeed increases.
