Due to industrialization and huge household usage of electricity there is energy crises world wide. There is reduction of natural sources oil, water reservoirs, to make cheaper energy aerodynamic based Gas Turbines in combine & open cycle power plant are commonly used for electricity. Hydro power generation is also very cheep and dual benefit source of power generation. The aim of this forum is to share experience and awareness about modern techniques and up coming events in energy sector.
Friday, November 14, 2008
BASIC PRINCIPLE OF GAS TURBINE
The balloon drawings above illustrate the basic principles upon which gas turbine engines
operate. Compressed inside a balloon, as in (A) above, exerts force upon the confines of the
balloon. Air, which has weight and occupies space, by definition, has mass. The mass of the air
is roportionalt to its density, and ensityi is roportionalt to temperature and pressure. The ir
mass confined inside the balloon, accelerates from the balloon, creating a force as it is released
(B). This force increases as mass and acceleration increase, as stated in Newton's second law;
force equals mass times acceleration (F = MA). The force created by the acceleration of the air
mass nside the balloon results n an equal and opposite force that causes the balloon to be
propelled in the opposite direction, as stated in Newton's third law.
For every action, there is an equal and opposite reaction.)
Replacing the air inside the balloon, as in (C), sustains the force and, although impractical,
allows a load to be driven by the force of the air mass accelerating across and driving a turbine,
as in (D).
In (E), a more practical means of sustaining the force of an accelerating air mass used to drive a
load is illustrated. A housing contains a fixed volume of air, which is compressed by a motor-
driven compressor. Acceleration of the compressed air from the housing drives a turbine that is
connected to the load.
In (F), fuel is injected between the compressor and the turbine to further accelerate the air mass,
thus multiplying the force used to drive the load.
In (G), the motor is removed and the compressor is powered by a portion of the combustion gas,
thus making the engine self-sufficient as long as fuel is provided.
In (H), a typical gas turbine-engine operation is represented. Intake air is compressed, mixed
with fuel and ignited. The hot gas is expanded across a turbine to provide mechanical power and
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