The family of PBS TJ40 turbojet engines features a compact design and excellent thrust-to-weight ratio. The engines are available in several versions incl. the PBS TJ40-G2 with high electric power output. Its distinctive features include simple and compact design, low weight and plug & play solution (all components including ECU integrated in the engine body). The engine weighs only 3.6 kg and provides a maximum thrust of 425 N.

Our commercial aerospace AGSE products are relied upon by aviation companies around the world to keep their aircraft serviced and flying. The test and servicing equipment we engineer and distribute are key to the success of commercial aviation.

In an uncertain world, L3Harris is anticipating and rapidly responding to challenges with agile technology - creating a safer and more secure future.

Temperature / Flame Resistant Seals Reinforced & Non-Reinforced Seals Vulcanized Bonding Custom Technical Elastomeric Solutions

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.

GE's T901 Engine for ITEPA test cell is not a combat mission. In combat, there is no time for an unproven design. With more than 100 million flight hours of ...

A gearbox refers to a mechanical device made up of various gears to transmit the power needed to rotate a shaft. Depending on the type of speed transmission, it is divided into a reduction gearbox and an increaser gearbox. If the speed of the driven shaft is lower than that of the drive shaft, it is called a reduction gearbox, and if it is higher, it is called an increaser gearbox. A reduction gearbox is mainly used to obtain high torque by reducing the rotation speed of the drive source (motor) to the required rotation speed, and an increase gearbox is used to obtain high-speed rotation by increasing the limited rotation speed of the drive source (motor). It is used for this purpose. Depending on the type of gear (helical gear, bevel gear, planetary gear, worm gear, etc.), it can be manufactured in various shapes.

The engine offers a take-off power of up to 180 kW (235 hp). Excellent power-to-weight ratio. Small installation dimensions. Two outpu shaft speed configurations. Stable operation at high and low temperatures.