3609/10

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

3609/10 is a type of gas turbine engine developed by GE Aviation, its application field and working principles are widely used in aircraft propulsion systems. The 3609/10 was the first production engine to reach a thrust level of 33,500 pounds-force in the late 1970s and remained in production for over 20 years.

The engine was initially designed as a military fighter engine, but its application field has widened to include commercial aviation, aerospace, and industrial applications. The 3609/10 engine is designed for high thrust and a wide operating range, enabling it to power a variety of aircraft, including trainers, fighters, transport aircraft, helicopters, business jets, and missiles.

The 3609/10 turbine is constructed with an axial-flow turbine and a single-stage power turbine. The axial-flow turbine is made up of metal blades arranged in a chordal fashion along the circumference of a cylindrical chamber, with the intake air passing over the blades to provide thrust. The power turbine is a two-stage turbine, with the first stage extracting energy from the exhaust gases to power the compressor, and the second stage providing additional thrust.

The compressor is a centrifugal type, composed of two sections. In the first section, the air is compressed to twice atmospheric pressure. In the second section, the air is compressed to a pressure of 3.5 times that of the atmosphere. The compressor is driven by the power turbine and helps in maintaining the aerodynamic performance of the engine by allowing a smoother transition of the air as it passes from the low-pressure inlet to the high pressure compressor.

The 3609/10 engine uses a single fuel system with a pressurized fuel system and distribution control. The fuel system is designed to maintain a high fuel pressure, while the distribution control allows for precise control of fuel flow. The fuel is injected into the combustion chamber and mixed with the air, creating a combustible mixture for efficient combustion.

The engine is designed to be both cost effective and reliable. The engine utilizes an efficient design with advanced materials to reduce weight while maintaining a reliable, cost-effective product. The engine is designed to have a long life with minimal maintenance and repairs. The engine is designed to burn fuel efficiently while reducing emissions.

The 3609/10 engine has become widely used in various aircraft propulsion systems due to its high thrust, wide range of operating speeds, and efficiency. The engine has been designed to meet the demands of modern aircraft propulsion systems, and its application field and working principles have proven to be reliable and cost-effective.

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