2P18U3S/6

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Part Status:	Active

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2P18U3S/6 Application Field and Working Principle

The 2P18U3S/6 is an advanced medium power all-weather aircraft engine designed for maneuvering throughout the world\'s military operating theaters. This powerful engine is designed to provide high thrust power for a wide range of high-performance aircraft. It is a medium-power turbofan engine and features a two-stage axial compound compressor system.The main application field for the 2P18U3S/6 is air-to-air combat, passenger transport, and reconnaissance missions. It is highly reliable and readily available, making it a great option for a variety of aerial tasks. The engine is well-suited for use in many types of aircraft, including the Su-30 series fighter jets, Yak-38 fighter/bomber, and the An-124 cargo transport aircraft. The engine is also popular with corporate jet customers, as it can provide them with a reliable, high-performance engine for their private jets.The working principle of the 2P18U3S/6 is based on a conventional turbofan engine. It consists of two main components; the core and the fan. The core is responsible for compressing the air and providing the thrust needed to power the plane. The fan, on the other hand, circulates the air to the engine to increase thrust. The core of the 2P18U3S/6 is a two-stage axial compound compressor system. This system is composed of two distinct parts; the first stage of the compressor, located at the intake of the engine, consists of six variable stator blades and one conventional rotor blade. This system allows for optimal airflow throughout the entire engine module. The second stage of the compressor consists of 24 stator blades arranged in a double-entry, low compression ratio design. The combination of these two components works together to provide the needed amount of thrust without compromising fuel efficiency.The fan of the 2P18U3S/6 engine uses a three-stage fan blade design. This design ensures maximum efficiency and reduces the noise created by the engine. Its fan drive is a geared turbine, providing an additional power boost during low speed maneuvering. The fan blades are constructed of titanium alloy material to ensure a durable design. The 2P18U3S/6 offers excellent fuel efficiency and power for a variety of high-performance aircraft. Its two-stage axial compound compressor system and three-stage fan blade design provide low power consumption and high thrust output, making it the perfect choice for air-to-air combat, passenger transport, and reconnaissance missions. It is highly reliable and readily available, making it an ideal engine for a wide variety of tasks.

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