With more than 33,000 delivered to date, CFM56® engines mainly power single-aisle commercial jets from Airbus and Boeing. The CFM56®, developing 18,500 to 33,000 lb of thrust, set a standard in this market. It owes its impressive success to exceptional performance and reliability, the result of the two partners' technical excellence.

C-UAS 30kW SBC HEL Source

1. 용도 : 전자제어기로부터 공급되는 전력으로 빠르게 가열하는 장치 2. 기능 : 8,200 Kcal/hr(차체 특성에 따른 난방효율 최적화 설계, 운용간 안정성 확보) 3. 관련 장비/체계 분야 : 단거리지대공무기(천마) 4. 관심 협업 분야 / 목표시장(국가) - 전차ㆍ장갑차 그 밖의 전투기동장비 / 국내 방위산업시장 및 해외 (미국, 멕시코, 프랑스, 이스라엘, 인도네시아, 말레이시아, 아랍에미리트, 유엔국 등) 5. 기타사 - 영구자석 기반 발전기 기술 및 고효율 에너지변환 기술(특허보유) - 국방규격화 완료, 해외수출 경쟁력 제품

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.

Connectors

Monitors abnormal engine operation based on digital and analog signals from the aircraft engine. It calculates engine life indices and detects engine malfunctions for generate a Pilot Fault List (PFL), which will stored in memory. When an engine failure is detected, it provides warning for display on the Central Maintenance Panel (CMP). Developed as a replacement for obsolete, achieving 60% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x16 Discrete Inout - x14 Discrete Output - x3 Analog Input - x1 RS-232 - Size: 283 x 265 x 89 (mm) - Weight : 4.1Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 25W)

Depending on the applications of our customers we offer a very wide range of technical solutions of assemblies and / or mechanical subassemblies with various characteristics. ABC offers a wide range of solutions ranging from micro-mechanics to large systems, based on standard solutions already developed and / or customized solutions as needed by the customer.

Intel® 14th/13th/12th-Gen Core™ 24C/ 32T 35W/ 65W CPU Affordable IP66-rated design for waterproof and dustproof Up to 96GB DDR5 4800 SODIMM -25°C to 70°C wide-temperature fanless operation 3x 2.5Gb and 1x Gb Ethernet ports via M12 X-coded connectors, with 802.3at PoE+ option 1x waterproof USB3.2 Type-C port supporting alternative mode for DisplayPort and USB3.2 dual output 8V to 48V DC input with built-in ignition power control