Main advantages of the PBS ECS systems include the possibility of cooling, heating and ventilation in one system, minimal power consumption, ecological operation without the need for a coolant and a compact design. Specific applications of the ECS systems include light combat aircraft AERO L-159 ALCA, jet trainers AERO L-39NG and L-39 Albatros, etc.

Key Features - Frequency Range: 8.5 - 10GHz - RX Noise Figure: 3.0dB - RX Small Signal Gain: 21 dB - TX Small Signal Gain: 27dB - TX High Pout: 39dBm - TX High PAE: 37% Chip size: 2.9x2.5x0.1mm  

This EGR-Cooler prototype, developed in collaboration with Hyundai Motor Company, was fabricated using EOS Stainless Steel 316L, renowned for its excellent corrosion resistance and mechanical properties in demanding automotive applications. The part was additively manufactured over a period of 64 hours, demonstrating the advanced capabilities of metal 3D printing for precision and reliability. Unlike conventional designs, this innovative component integrates 14 separate parts into a single, unified structure, greatly simplifying assembly while enhancing operational efficiency. The implementation of a Triply Periodic Minimal Surface (TPMS) structure within the cooler significantly improves heat exchange performance and enables substantial weight reduction, meeting next-generation thermal management requirements. Partners Lab stands as a leader in Korean additive manufacturing technology, offering cutting-edge capabilities in OEM production and collaborative technical development for various industrial sectors. This EGR-Cooler, designed by nTopology, exemplifies our engineering expertise and commitment to delivering high-performance thermal products for automotive and beyond.

ElectroAir’s mobile APA-65 -series combined units consist of frequency converter units (AC rated output power up to 45 kVA) and rectifier units (DC continuous current up to 800A). These units are intended for the ground servicing of all aircraft types with a frequency of 400Hz and voltage 115/200 V and to power on-board electrical equipment and launch aircraft/ helicopters with a voltage of 28.5 VDC. APA-65 series is designed to eliminate CO2 emissions with its unique technical characteristics. Diesel hybrid unit and battery driven unit - unit can perform the complete service of aircraft at remote parking places with diesel engine / through batteries and it is also capable to operate from the 50/60Hz, 400V, 3 phase main power supply grid as any electrical GPU, without fuel consumption and with zero operating emissions. The range of different APA configurations with no emissions allow for safer, cleaner and more practical operational conditions for operators and personnel at the location. These units are very compact in size and weight.

ACE is a comprehensive ecosystem of smart apps designed to streamline the entire aircraft and cabin interior configuration process. From aircraft manufacturers to buyers, leasing companies, and interior suppliers, ACE enables seamless management within a single, fully digital workflow.​ With ACE, you can enhance efficiency, reduce errors, and ensure every step of the configuration process is done accurately and on time.

The maximum transmission distance varies based on the following frequency-related specifications. Camera Frequency Max Cable Length ================ =============== 20 ~ 60 MHz 10 m 60 ~ 80 MHz 7 m 80 ~ 85 MHz 5 m The PoCL Bypass function supports Power over Camera Link (PoCL) operation from the Frame Grabber to the selected camera. However, the power supply to unselected cameras is automatically disabled. To prevent power cutoff, separate power must be provided to the cameras. Configurations are available as follows, including image signal amplification. [Features of CLM-30C4]  Fully supports the Camera Link interface (Area/Line Scan).  Provides manual (switch) or remote (RS232) camera selection.  Allows selection from one of four cameras configured for Base (Layer 1) or Medium/Full (Layer 2) levels.  Supports Base/Medium/Full setups (CC1~4, RS232, LVAL, DVAL, FVAL)  PoCL bypass function: Automatically powers only the selected camera when PoCL-compatible cameras, frame grabbers, and cables are used.  Supports pixel frequency from 20 to 85 MHz.  Supports PoCL signal bypass (patented).  Enables lossless transmission.  Provides additional full-duplex RS232 communication at up to 256 Kbps.  Features a locking DC power jack (Molex).

Engine Start Begins with ATS. The Air Turbine Starter (ATS) is a key component of an aircraft's secondary power system, driven by Bleed Air supplied from the Auxiliary Power Unit (APU) to accelerate the engine up to approximately 8,900 RPM, enabling engine start. Through the in-house development and localization of the ATS, we have incorporated power generation, optimal design of the shear section with consideration of failure, Containment functionality, as well as lubrication and power transmission systems. In addition, we have secured manufacturing and assembly technologies and continue development aimed at successful operation and the establishment of a mass production system.

Each SCU can interface with up to eight (8) fuel probes with temperature detection and/or fuel probes with compensators. It will process capacitive and resistive readings to determine the fuel heights for each probe and transmit the calculated fuel volume to the cockpit.