Turbine Engine Sections

The cold section and the hot section 1 the cold section includes the engine inlet compressor and turbine sections 2 the hot section includes the combustor diffuser and exhaust sections regarding the above statements.

Turbine engine sections. The turbine section of a gas turbine engine is located aft or downstream of the combustion chamber. Turbine the turbine is a series of bladed discs that act like a windmill extracting energy from the hot gases leaving the combustor. Actual simple open cycle performance.

Turboprop turboshaft and turbofan engines have additional turbine stages to drive a propeller bypass fan or helicopter rotor. Jump to navigation jump to search. The inlet compressor fan combustor turbine and nozzle.

A turboshaft engine that has a turbine wheel or stage of turbine wheels that is not used to drive the compressor of the gas generator section of the engine. From wikipedia the free encyclopedia. The combustion section houses the combustion process which raises the temperature of the air passing through the engine.

Jet engines come in a variety of shapes and sizes but all jet engines have certain parts in common. 1 turbojet 2 turboprop 3 turboshaft electric generator 4 high bypass turbofan 5 low bypass afterburning turbofan. Gas turbine engines have come a long way in the past 100 years.

Examples of gas turbine configurations. A gas turbine also called a combustion turbine is a type of continuous and internal combustion engine. And while turbojets turboprops turbofans and turboshafts all have their differences they way they produce power is essentially the same.

Type of internal combustion engine. The major part of this energy is required at the turbine or turbine stages to drive the compressor. The turbine assembly consists of two basic elements.