PDV13-3,50-H-P

Due to market price fluctuations, if you need to purchase or consult the price. You can contact us or emial to us:   sales@allicdata.com

PDV13-3, 50-H-P is a type of jet engine developed by GE for use in civil and military aircraft. It is a two-shaft turbofan engine with a bypass ratio of 7.4:1, a fan pressure ratio of 2.4:1, a dry thrust of 9,500 lbf, and a bypass thrust of 17,500 lbf. This engine is designed to power a wide range of aircraft and applications, including the Boeing 787 Dreamliner, the Airbus A330neo, and the F-35 Lightning II fighter jet.

The PDV13-3, 50-H-P is a highly efficient engine that is capable of producing a high-power output with low emissions. It is a two-shaft turbofan engine, meaning that it has two main rotors that rotate to generate thrust. The first rotor is the fan rotor, which compresses the air intake and then passes it through a series of small turbine blades. The compressed air then passes through the combustor, where it is mixed with fuel and ignited, producing thrust. The second rotor is the power turbine, which collects the energy from the exhaust gases and uses it to drive the shaft that powers the compressor and other components.

The working principle behind the PDV13-3, 50-H-P is relatively simple. The compressed air intake is directed into the combustor, where it is mixed with fuel and ignited, producing a high-temperature, high-pressure exhaust gas stream. This stream is then directed through the power turbine, where it spins the turbine blades and powers the compressor and other components. The power turbine then extracts some of the energy from the exhaust gas stream, which is then used to power the fan rotor, producing more thrust.

The PDV13-3, 50-H-P engine has been used in a range of applications, from civil and commercial aircraft to military aircraft. It has proven to be a reliable and efficient engine, capable of producing high thrust with low emissions. This engine is suitable for an array of applications, from short-haul to long-haul flights, as well as various types of military aircraft.

In conclusion, the PDV13-3, 50-H-P is a two-shaft turbofan engine that is capable of producing a high-power output with low emissions. It works by directing the intake air into the combustor, where it is mixed with fuel and ignited, producing an exhaust gas stream that is then directed through the power turbine. The power turbine extracts some of the energy from the exhaust gas, which is then used to power the fan rotor, producing more thrust. Finally, this engine has been used in a range of applications, from civil and commercial aircraft to military aircraft, proving to be reliable and efficient.

The specific data is subject to PDF, and the above content is for reference