The Fuel Heater is engine-mounted with fluid connections to both the engine fuel supply system and the engine lube oil system. The heater provides fuel heating for fuel de-icing, using engine lube oil flow during aircraft cold start and cold operation periods. REPAIR PROGRAM • Triumph has the expertise only the OEM can offer • OEM repairs are more dependable, increase MTBF and cost less long-term • Repair price is all inclusive • TAT 45 days approx

Localization development for general parts of Naval Logistics Command in progress

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.

The AGTR-NG4 is designed for applications demanding high-speed data acquisition and reliable operation in extreme conditions. Its compact size, low weight, and robust design make it ideal for integration into aerospace platforms. Key Features: - 4 Optical Channels: Enables simultaneous data acquisition from multiple FBG sensors. - 22 kHz Sampling Rate - Onboard Data Processing and Storage: Features an integrated miniature single-board computer for efficient data management. - Rugged Design: Validated for MIL-STD-810 and MIL-STD-461, ensuring reliable operation in harsh environments. - Wide Temperature Range: Operates effectively from -45°C to +85°C. - Versatile Communication: Supports Ethernet, UDP, and TCP/IP protocols. - ARINC 801 Optical Interface: Ensures compatibility with aerospace communication standards.

The World's Most Complete Selection with Lightning Fast (Same-day!) Availability for: AS85049 (M85049), D38999, MIL-DTL-26500, MIL-DTL-28840, MIL-DTL-83513, MIL-DTL-83538, MIL-DTL-83723, MIL-S-81824, MS17349, MS27291 and Other Military Standard and Commercial Backshell Derivatives.

A reliable, quality full or semi-auto version of the rifle that has written entire volumes in history. A basic, non-nonsense version that stays true to the original.

Model-Based Systems Engineering (MBSE) is a methodology that integrates design, analysis, and verification activities throughout the system lifecycle using architecture models. By modeling requirements, functions, structure, and behavior, MBSE supports consistent and informed decision-making. Ansys SAM (System Architecture Modeler) supports the latest system modeling language, SysML v2, and enables both graphical and textual modeling, real-time collaboration, and model management. Ansys ModelCenter integrates various engineering tools and builds automated workflows, enabling what-if simulations and trade studies. By connecting architecture models with simulation models, it supports consistent design analysis and requirements validation using a single source of truth (ASoT).

The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.