Weight Reduction: Eliminates complex hydraulic lines, pumps, and fluids, thereby reducing overall aircraft weight. Maintenance Efficiency: Simplifies maintenance requirements by removing hydraulic components that are prone to leakage and degradation. Improved Reliability: Provides precise braking control with fewer mechanical parts, resulting in higher system reliability and reduced downtime. Integration with Advanced Systems: Enables seamless connection with modern avionics and aircraft health monitoring systems, supporting predictive maintenance and optimized performance.

Flight safety equipment that supports safe take-off and landing control of aircraft in the airport control area. Design and Manufacture - Antenna Housing - Driving Unit - Environmental Control Unit

Type : Radial (3P) Size(Ø, mm) : 82 × 58 Weight(kg) : 0.55 N. Speed(rpm) : 6,200 N. Torque(Nm) : 2 N. Power(kW) : 1.3

To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

Liquid Measurement Systems (LMS) provides fuel gauging and interface controls for service, maintenance, and flight crew personnel, at the primary refuel point on the aircraft.

External Refuel Preselect Panels can display the quantity of fuel in each tank, calculate the total quantity of fuel onboard, allow service teams to pre-select desired fuel quantity, and display fault codes. LMS’ external refuel preselect panels are compact, lightweight, and rugged systems that can be adapted to a variety of platforms.

Military and Commercial

In high-reliability industries such as aerospace, defense, and nuclear, embedded software is emerging as a core competitive advantage, driving increasing demand for systems based on safety certification. Ansys SCADE is a model-based solution that supports the entire lifecycle of safety-critical software—from design to certification—for applications such as flight control systems, engine controllers, and cockpit display systems (CDS). It ensures high reliability, real-time performance, and safety compliance required for the development of complex avionics systems. Key Features - Model-based embedded software development and automatic code generation - Compliance with aerospace safety certification standards such as DO-178C, ARINC 661, and FACE™

Development of an integrated support system for total life cycle management of weapon systems