UNMANNED PLATFORMS
FSA100-0000-00
FSA100-0000-00
Rotary Servo Actuator
Rotary Servo Actuator
FSA100-0000-00 rotary servo actuators are flight-proven with 50,000+ flight hours. These actuators are currently used as air intake actuators on unmanned platforms.
FSA100 series actuators produce 1.1Nm nominal torque at 180°/s nominal speed.
Auxiliary control servo actuator
Flight-proven, 50,000+ flight hours
In-flight health monitoring
High power-to-weight ratio
FSA101-0000-00
FSA101-0000-00
Rotary Servo Actuator
Rotary Servo Actuator
FSA101-0000-00 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are flight proven with 120,000+ flight hours.
Primary & secondary flight control surface servo actuator
Flight-proven, 120,000+ flight hours
In-flight health monitoring
High power-to-weight ratio
Compatible with MIL- STD-461E ve MIL-STD-810G
FSA101-0000-01
FSA101-0000-01
Rotary Servo Actuator
Rotary Servo Actuator
FSA101-0000-01 rotary servo actuator is used to position the primary and secondary flight control surfaces on unmanned platforms. Being a variant of FSA101 series, FSA101-0000-01 actuators differ with the integrated electromagnetic brake. These actuators are flight proven with 25,000+ flight hours.
Primary & secondary flight control surface servo actuator
Flight-proven, 25,000+ flight hours
In-flight health monitoring
Lightweight structure (Actuator + Controller)
Compatible with MIL- STD-461E ve MIL-STD-810G
FSA102-0000-00
FSA102-0000-00
Rotary Servo Actuator
Rotary Servo Actuator
FSA102 rotary servo actuators are used to position the primary and secondary flight control surfaces on unmanned platforms. These actuators are currently in use in various unmanned platforms, with accumulated flight hours over 60,000.
Primary & secondary flight control surface servo actuator
Flight-proven, 60,000+ flight hours
In-flight health monitoring
Lightweight structure (Actuator + Controller)
Compatible with MIL- STD-461E ve MIL-STD-810G
FSA201-0000-00
FSA201-0000-00
Linear Servo Actuator
Linear Servo Actuator
FSA201-0000-00 series are linear servo actuators designed for unmanned platforms, delivering 200N rated force. These actuators are electronically and mechanically redundant. FSA201 series actuators are used for primary flight control surfaces, with accumulated flight hours of 250,000+.
Redundant primary flight control
Flight-proven, 250,000+ flight hours
In-flight health monitoring
Lightweight structure (Actuator + Controller)
MANNED FIXED-WING PLATFORMS
GSE101-0000-06
GSE101-0000-06
Linear Actuator
Linear Actuator
Developed for a civil aviation platform and integrated into wing structure to control spoiler flight control surface. Special feedback mechanism and sensor unit provides absolute positioning. Civil aviation certification process completed.
ASD101-0000-02
ASD101-0000-02
Controller
Controller
ASD101-0000-02 is a controller unit which controls for 2 GSE101-0000-06 units simultaneously.
Filter, contoller and driver card is designed to meet DO160 (Enviromental Conditions) and DO254 (Hardware Specifications). The product is compliant to civil aviation standards. It can be customized for various types of servo actuators.
HRP101-0000-00
HRP101-0000-00
Rudder Pedal
Rudder Pedal
Developed for use in the jet trainer’s fly-by-wire flight control system, the Rudder Pedal equipment converts pilot commands into input signals to the rudder function, brake function and nose gear steering function. This equipment also has mechanisms that provide artificial feeling to the pilot while performing the rudder, braking and steering functions.
An electromechanical actuator that adjusts thepedal distance to ensure comfortable use by pilots of varying heights is also part of the Rudder Pedal equipment.
Redundant arhitecture tailored with aircraft systems
Customized artificial feeling
Lightweight structure
Customized for HMI Considerations
ATK100-0000-00
ATK100-0000-00
Gun Turret Control System
Gun Turret Control System
The T-129 ATAK helicopter is a development project consisting of subsystems that provide nose gun guidance and fire control.
The subsystems designed, manufactured and qualified by ANDAR as part of this program are:
– Turret Electronic Control Unit: The unit that provides the interface between the Gun and the Pilot over the MIL-STD-1553B protocol and controls the electronic/electromechanical units.
· Servo Motor: Rotary motors that move the gun turret in elevation and azimuth.
· Gun Drive: The rotary motors that feeds ammunition to the revolving gun.
· Elbow: Ammunition feeding support motor.
· Round Counter Sensor: Magnetic sensor that counts how many shots are fired.
· Firing Contact: Ignition contact that interfaces with the projectile for electronic ignition.
· Feeder Solonoid: Solenoid that opens the ammunition feeding path.
· Elevation and Training Sensors
· Harnesses
First Rotary Turret Gun subsystem developed in Turkey. The system can also be used on ground, naval and other aerial platforms.
Provides remote control of a Gun Turret
Operation is possible at helicopter speeds up to 140 knots and the firing position is maintained under all critical flight and maneuver conditions.
Provides flexible and fixed modes of fire.
In case of aircraft or turret power failure the weapon returns to the fixed forward firing position and is automatically locked.
In-flight health monitoring
Operating Temperature -40°C / +55°C
MANNED ROTORCRAFT PLATFORMS
TS1000
TS1000
Trim Actuator
Trim Actuator
TS1000 is a rotary type electromechanical trim actuator designed for use on a civil utility rotorcraft.
It is integrated into the helicopter rotor flight control system and transfers the commands from the autopilot computer to the mechanical flight control system as physical movement. Then mechanical flight control system provides control input to the servo hydraulic actuators that actuate the primary controls of the helicopter. When the autopilot mode is disabled, trim actuators provide the pilot an artificial feeling under normal flight scenarios, thus providing a more controlled and comfortable flight. Additionally, the trim actuator is used for the neutral point of the controls for a trimmed flight.
Unique design for manned platforms
High precision control at the output shaft
Lightweight structure
Redundant Architecture
Equipped with Shear Pin for Jamming
Customized Artificial Feeling
Anti Backlash system at the output shaft
EMB101-0000-00
EMB101-0000-00
Electromagnetic Brake
Electromagnetic Brake
Developed by ANDAR for a CS27 certified helicopter program to integrate into primary flight control surfaces, EMB101 electromagnetic brake has a highly specialized and customized structure, designed to meet customer requirements. It provides high holding torque with its specially designed structure and special material.
The electromagnetic brake is integrated into the trimming system, allowing the pilot to manually adjust the neutral point of the controller by releasing the brake and holding the newly trimmed neutral point. It provides comfortable control to the pilot depending on the changes in flight conditions.
RBS101-0000-00
RBS101-0000-00
Rotor Brake System
Rotor Brake System
Rotor Brake System consists of an electromechanical brake with floating caliper and its control box.
The rotor brake functions at a point connecting the main rotor and tail rotor in the helicopter and has the capacity to stop both of them. The main purpose of the system is to stop the rotor after the helicopter landing and enable comfortable evacuation.
Unique integrated design of brake and controller
Robust system for harsh environment
Lightweight structure with carbon disc and pad
Safety critical equipment
ATK100-0000-00
ATK100-0000-00
Gun Turret Control System
Gun Turret Control System
The T-129 ATAK helicopter is a development project consisting of subsystems that provide nose gun guidance and fire control.
The subsystems designed, manufactured and qualified by ANDAR as part of this program are:
– Turret Electronic Control Unit: The unit that provides the interface between the Gun and the Pilot over the MIL-STD-1553B protocol and controls the electronic/electromechanical units.
· Servo Motor: Rotary motors that move the gun turret in elevation and azimuth.
· Gun Drive: The rotary motors that feeds ammunition to the revolving gun.
· Elbow: Ammunition feeding support motor.
· Round Counter Sensor: Magnetic sensor that counts how many shots are fired.
· Firing Contact: Ignition contact that interfaces with the projectile for electronic ignition.
· Feeder Solonoid: Solenoid that opens the ammunition feeding path.
· Elevation and Training Sensors
· Harnesses
First Rotary Turret Gun subsystem developed in Turkey. The system can also be used on ground, naval and other aerial platforms.
Provides remote control of a Gun Turret
Operation is possible at helicopter speeds up to 140 knots and the firing position is maintained under all critical flight and maneuver conditions.
Provides flexible and fixed modes of fire.
In case of aircraft or turret power failure the weapon returns to the fixed forward firing position and is automatically locked.
In-flight health monitoring
Operating Temperature -40°C / +55°C
URBAN AIR MOBILITY VEHICLES
HOW WE WORK
Designing and producing market leading electromechanical actuators requires a multidisciplinary team and full knowledge of the system -including subcomponents.
At ANDAR, we design and develop 100% of all our products and complement our design with our in-house production capabilities for delivering end-to-end solutions to meet our customers’ needs.
We design and produce flightworthy products based on aerospace & certification standards (MIL-STD-810, MIL-STD-461, DO254, DO160). Our tools and procedures are compliant to ARP4761 to support integrators safety assessment process. We are in process of acquiring AS9100 certification covering all these aspects.