PRODUCTS

PRODUCTS

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)

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.

Rotary absolute positioning sensor

Anti-rotation system

Retractable under 300N

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.

High accuracy control

Integrated to mechanical flight controls

High performance output

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

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.

High holding torque

Lightweight structure

Minimal backlash

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

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)

GSE101-0000-00

GSE101-0000-00

Linear Actuator

Linear Actuator

GSE101-0000-00 is designed and developed for use in guidance systems. Indigenous design includes a high power slotless BLDC motor along with gearbox and encoder.

Incremental rotary encoder

Field-proven

Configurations for different stroke, load & speed

Optional absolute position feedback

Optional Holding Brake

GSE101-0000-03

GSE101-0000-03

Linear Actuator

Linear Actuator

This actuator is a variant of GSE101-0000-00 where mechanical joint geometry and operating range are customized for the application.

Incremental rotary encoder

Field proven

GSE101-0000-05

GSE101-0000-05

Linear Actuator

Linear Actuator

A variant of GSE101-000-00 where mechanical joint geometry and operating range are customized for the application. Includes a linear absolute positioning sensor and anti-rotation system.

Linear absolute positioning sensor

Anti-rotation system

GSE101-0000-09

GSE101-0000-09

Linear Actuator

Linear Actuator

Includes the highest dynamic and static load limits among GSE101 product family along with linear absolute positioning sensor and antirotation system.

Linear Absolute Positioning Sensor

High Static Load Limit

Anti-rotation system

GSE102-0000-00

GSE102-0000-00

Linear Actuator

Linear Actuator

This solution is designed specifically for circumstances with volume and interface limitations. Parallel configuration of the motor and output drive with an intention to reduce products total length.

Linear Absolute Positioning Sensor

Anti-rotation System

GSE103-0000-00

GSE103-0000-00

Linear Actuator

Linear Actuator

This product includes a 900W output power slotless BLDC motor, planetary gear box, electromechanical power-off brake, and incremental rotary encoder.

Incremental rotary encoder

Power-off brake

High power density planetary gearbox

High stroke capacity

RPU101-0000-00

RPU101-0000-00

Antenna Rotary Positioning Unit

Antenna Rotary Positioning Unit

RPU is a pan-tilt system, which stands out with its 80kg load capacity, 0.1 degree positioning accuracy and compact structure. This rotary positioning unit offers 2 degrees of freedom. It can scan ± 180 degrees in pan movement and ± 90 degrees in tilt movement. Version with 3 degrees of freedom and different options is still under development.

RPU is used as an antenna routing unit on land and sea platforms and can be controlled by auxiliary control units: HCU (hand control unit) and RCU (surface mountable control unit).

Lightweight integrated design

High accuracy position control

Robust structure

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