Why combustion chamber is used in gas turbine?

The objective of the combustor in a gas turbine is to add energy to the system to power the turbines, and produce a high-velocity gas to exhaust through the nozzle in aircraft applications.

What is the purpose of combustion chamber?

A Combustion Chamber is the area within the Cylinder where the fuel/air mix is ignited. As the Piston compresses the fuel/air mix and makes contact with the Spark Plug, the mixture is combusted and pushed out of the Combustion Chamber in the form of energy.

What is the advantage of a multi can combustion chamber?

The advantage of can-type combustion chambers is that they are simple in design, they have very good structural strength and they can be removed and replaced individually.

What is multiple chamber?

An arrangement in which a number of individual chambers are disposed around the engine. The chambers are interconnected and fed by the individual ducts from the compressor. See cannular.

What is multiple combustion chamber?

Multiple combustion chambers. (Source: Rolls Royce.) The separate flame tubes are all interconnected. This allows each tube to operate at the same pressure and also allows combustion to propagate around the flame tubes during engine starting.

What is the purpose of the turbine section in a gas turbine engine?

The turbine section of the gas turbine engine has the task of producing usable output shaft power to drive the propeller. In addition, it must also provide power to drive the compressor and all engine accessories.

What is the purpose of turbine section?

The turbine (and exhaust) section. The turbine section of the gas turbine engine has the task of producing usable output shaft power to drive the propeller. In addition, it must also provide power to drive the compressor and all engine accessories.

How do gas turbine engines work?

As hot combustion gas expands through the turbine, it spins the rotating blades. The rotating blades perform a dual function: they drive the compressor to draw more pressurized air into the combustion section, and they spin a generator to produce electricity.

What is the purpose of the turbine in a jet engine?

As the jets of gas shoot backward, the engine and the aircraft are thrust forward. As the hot air is going to the nozzle, it passes through another group of blades called the turbine. The turbine is attached to the same shaft as the compressor. Spinning the turbine causes the compressor to spin.

How does a gas turbine engine work?

THE GAS TURBINE CYCLE. The basic principle of the airplane turbine engine is identical to any and all engines that extract energy from chemical fuel. The basic 4 steps for any internal combustion engine are: 1. Intake of air (and possibly fuel). 2. Compression of the air (and possibly fuel).

What is the basic principle of an airplane turbine engine?

The basic principle of the airplane turbine engine is identical to any and all engines that extract energy from chemical fuel. The basic 4 steps for any internal combustion engine are: 1. Intake of air (and possibly fuel). 2. Compression of the air (and possibly fuel).

How are combustion chambers arranged in a gas turbine?

The combustion chambers are always arranged coaxially with the compressor and turbine regardless of type, since the chambers must be in a through-flow position to function efficiently. All combustion chambers contain the same basic elements: There are currently three basic types of combustion chambers, variations within type being in detail only.

What is the function of the combustion section of a jet engine?

These other engine types have some jet velocity out the rear of the engine but most of the thrust or power is generated by the additional turbine stages driving a large fan, propeller, or helicopter rotor blades. The primary function of the combustion section is, of course, to burn the fuel/air mixture, thereby adding heat energy to the air.