- What
is a gas turbine?
A gas turbine is an engine that
converts the energy from a flow of gas into mechanical energy.
- How
does a gas turbine work?
Gas turbines work on the Brayton
cycle, which involves compressing air, mixing it with fuel, and igniting the
mixture to create a high-temperature, high-pressure gas. This gas expands
through a turbine, which generates mechanical energy that can be used to power
a variety of machines and equipment.
- What
are the different types of gas turbines?
There are three main types of gas
turbines: aeroderivative, industrial, and heavy-duty.
Aeroderivative gas turbines are used in aviation and small-scale power
generation. Industrial gas turbines are used in power generation and other
industrial applications. Heavy-duty gas turbines are typically used in large
power plants.
- What
are the main components of a gas turbine?
The main components of a gas
turbine include the compressor, combustion chamber, turbine, and exhaust
system. Other auxiliary components may include control systems, lubrication and
cooling systems, fuel and air delivery systems, and instrumentation and
monitoring systems.
In the compressor section, air is
drawn in and compressed up to 40 times ambient pressure and directed to the
combustor section, where fuel is introduced, ignited, and burned.
- What
are the 5 major parts of the gas turbine engine?
Any gas turbine engine consists of:
An air inlet.
Compressor section.
Combustion section.
Turbine section.
Exhaust section.
Accessory section.
- What
is the gas composition in gas turbine?
Today the main gas turbine fuel is
natural gas with methane as the dominating component
and smaller fractions of heavier hydrocarbons. Future gas turbine fuels will
likely include hydrogen gas and biogas with large fractions of carbon dioxide.
- What
is the difference between a gas turbine and a steam turbine?
A gas turbine generates mechanical
energy by burning fuel to create a high-temperature, high-pressure gas that expands
through a turbine. In contrast, a steam turbine uses steam generated from
boiling water to create mechanical energy.
- What
are the advantages of using a gas turbine?
Gas turbines offer several
advantages over other types of power generation, including high efficiency, low
emissions, fast start-up and shutdown, and the ability to operate on a variety
of fuels. They are also relatively compact and require less maintenance than
other types of engines.
- What
is the role of the compressor in a gas turbine?
The compressor is responsible for
compressing air before it enters the combustor. This increases the pressure and
temperature of the air, which allows for more efficient combustion.
- What
is the function of rotor blades in the compressor?
Rotor blades in the compressor are
responsible for compressing air and providing the force needed to move the air
through each stage.
- How is
the air compressed in a gas turbine engine?
The air is compressed by a series
of rotating blades in the compressor section. As the air passes through each
stage of the compressor, it becomes more compressed and its temperature
increases.
- What
is the role of the combustor in a gas turbine?
The combustor mixes fuel with
compressed air and ignites the mixture to create a high-temperature,
high-pressure gas that is used to drive the turbine.
- What
is the function of Crossfire tubes?
Crossfire tubes are used to enable
flames from one combustion chamber to propagate to other chambers in a gas
turbine for better combustion stability and efficiency.
- What
is the role of the turbine in a gas turbine?
The turbine extracts energy from
the high-pressure gas created by the combustor, which is used to power the
generator.
- What
is the role of the generator in a gas turbine?
The generator converts the
mechanical energy from the turbine into electrical energy that can be used to
power equipment.
- How is
the performance of a gas turbine measured?
The performance of a gas turbine is
typically measured by its thermal efficiency, which is the ratio of the energy
output to the energy input. Other performance measures include power output,
exhaust gas temperature, and emissions.
- What
is the difference between an open cycle and a closed cycle gas turbine?
An open cycle gas turbine uses
atmospheric air as the working fluid, which is compressed and heated in the
combustion chamber, and then exhausted to the atmosphere. In contrast, a closed
cycle gas turbine uses a fluid such as helium or carbon dioxide as the working
fluid, which is circulated through the compressor, combustion chamber, and
turbine, and then cooled and compressed again.
- What
is the role of the inlet guide vanes in a gas turbine?
The inlet guide vanes control the
amount of air entering the compressor, which affects the pressure and temperature
of the compressed air.
- What
is the purpose of the diffuser in a compressor?
The diffuser is responsible for
slowing down the high-speed, low-pressure air exiting the compressor and
converting it into high-pressure, low-velocity air that can be used for
combustion.
- What
is the function of the combustion chamber in a gas turbine?
The combustion chamber mixes fuel
with compressed air and ignites the mixture to create a high-temperature,
high-pressure gas that expands through the turbine.
- What
are the most common fuels used in gas turbines?
The most common fuels used in gas
turbines are natural gas, diesel, and aviation fuels.
- What
is the purpose of the exhaust system in a gas turbine?
The exhaust system directs the
high-temperature, high-pressure gases exiting the turbine to a heat recovery
system or to the atmosphere.
- What
is the function of exhaust diffuser in gas turbine?
Gas-turbine exhaust diffusers play
an important role in turbine power output by increasing the pressure ratio
across the last stage of the turbine by making the turbine exit static pressure
subambient.
- What
is the role of the bearing system in a gas turbine?
The bearing system supports and
rotates the turbine and compressor shafts and helps to reduce friction and
wear.
- What
is the importance of blade cooling in gas turbine design?
Blade cooling is important to
prevent high temperatures from damaging the turbine blades, which can lead to
failure and reduced performance.
- What
is the function of the control system in a gas turbine?
The control system is responsible
for monitoring and regulating various parameters of the gas turbine, such as
temperature, pressure, fuel flow, and speed, to ensure safe and efficient
operation. It may also include advanced features such as remote monitoring,
predictive maintenance, and fault diagnosis.
- How is
the speed of a gas turbine controlled?
The speed of a gas turbine is typically
controlled by adjusting the fuel flow to the combustion chamber. As more fuel
is burned, the temperature and pressure of the gas produced by the combustion
process increase, which in turn drives the turbine faster.
- What
is the maximum efficiency that can be achieved by a gas turbine?
The maximum efficiency of a gas
turbine is typically around 60-65%, depending on the design and operating
conditions.
- What
is the purpose of the compressor bleed air system in a gas turbine?
The compressor bleed air system
provides compressed air to other parts of the engine, such as the combustion
chamber or turbine cooling system.
- What
is the function of the intercooler in a gas turbine?
The intercooler reduces the
temperature of the compressed air between stages of the compressor, which
improves efficiency and reduces the risk of compressor stall.
- Where
does compress air will be used?
Compressed air in a gas turbine is
used for various purposes, including turbine cooling, bearing sealing,
pulsation control, and purging.
- What
is a dual-fuel gas turbine?
A dual-fuel gas turbine is a type
of gas turbine that can operate on two different types of fuel, typically
natural gas, and diesel oil. This allows for greater flexibility in fuel choice
and can help to reduce fuel costs.
- What is the function of
the inlet guide vanes in a gas turbine?
The inlet guide vanes regulate the flow of air into the
compressor section of the gas turbine. By adjusting the angle of the vanes, the
amount of air entering the compressor can be controlled, which affects the
power output and efficiency of the turbine.
- What is the difference
between a heavy-duty and an aeroderivative gas turbine?
A heavy-duty gas turbine is
designed for continuous operation in power generation or industrial applications,
while an aeroderivative gas turbine is designed for high-speed, lightweight,
and efficient operation in aviation or marine applications.
- What
is the function of the turbine shroud in a gas turbine?
The turbine shroud helps to prevent
the hot gases from bypassing the turbine blades, which can reduce efficiency
and cause damage to the turbine.
- What
is the purpose of the annular combustor in a gas turbine?
The annular combustor is a type of
combustion chamber that provides efficient mixing of fuel and air and helps to
reduce emissions.
- What
is the difference between a single-shaft and a multi-shaft gas turbine?
A single-shaft gas turbine has a
single shaft connected to both the compressor and the turbine, so the two
components spin at the same speed. A multi-shaft gas turbine has separate
shafts for the compressor and the turbine, allowing them to operate at
different speeds and providing greater flexibility and efficiency in certain
applications.
- What
is the function of the exhaust heat recovery system in a gas turbine?
The exhaust heat recovery system
recovers the waste heat from the exhaust gases and converts it into useful
energy, such as steam for power generation or heating.
- What
is the function of turbine legs?
Turbine legs are used to support
the weight of the gas turbine and maintain proper alignment with the generator
and other components.
- Why is
turbine leg cooling required?
Turbine leg cooling is required to
minimize thermal expansion of the support legs and maintain proper alignment
between the turbine and generator.
- What
are some common maintenance issues with gas turbines?
Common maintenance issues with gas
turbines include compressor fouling, turbine blade erosion, combustion chamber
damage, and bearing wear. Regular maintenance and inspections can help to
prevent these issues and ensure optimal performance.
- What
is the function of the axial flow turbine in a gas turbine?
The axial flow turbine extracts
energy from the high-temperature, high-pressure gas leaving the combustion chamber
and converts it into rotational energy to drive the compressor and generator.
- Explain
the stages of the gas turbine.
The stages of a gas turbine typically consist of a
row of fixed nozzles followed by a row of rotating turbine buckets, with each
stage providing an increase in kinetic energy and pressure drop as the air
moves through the turbine.
- What
is a combined cycle gas turbine (CCGT) plant?
A combined cycle gas turbine (CCGT)
plant is a power generation facility that uses a gas turbine and a steam
turbine together to achieve high efficiency. The waste heat from the gas
turbine is used to generate steam, which drives a steam turbine to produce
additional electricity.
- What
is the purpose of the nozzle guide vanes in a gas turbine?
The nozzle guide vanes direct the
high-velocity gas leaving the turbine to the exhaust system, which helps to
maximize the energy extraction from the gas.
- What
is the function of turning vanes?
Turning vanes are used to turn the
flow of gases from axial to radial direction for better efficiency and
performance.
- What
is a simple cycle gas turbine?
A simple cycle gas turbine is a gas
turbine that operates independently to generate electricity without any
additional energy recovery systems.
- What
is the function of the combustor liner in a gas turbine?
The combustor liner is a component of the combustion
chamber that is designed to withstand high temperatures and protect the
surrounding structure from heat damage. It typically contains fuel injectors,
flame stabilizers, and cooling holes.
- What
is the role of the turbine blade airfoil shape in a gas turbine?
The turbine blade airfoil shape is
designed to maximize energy extraction from the high-temperature, high-pressure
gas leaving the combustion chamber, and to minimize losses due to friction and
turbulence.
- What
is the importance of turbine blade cooling in gas turbine design?
Turbine blade cooling is critical
to prevent blade damage due to high temperatures, and to maintain the
efficiency and performance of the gas turbine.
- What
is the function of the afterburner in a gas turbine?
The afterburner is a combustion
chamber located downstream of the turbine that allows for additional fuel
combustion and energy extraction, which can improve the performance of military
aircraft engines.
- What
is the purpose of the inlet filtration system in a gas turbine?
The inlet filtration system removes
contaminants and particulate matter from the air entering the compressor, which
helps to improve performance and reduce wear on the compressor.
- What
is the function of the turbine blade tip clearance control system in a gas
turbine?
The turbine blade tip clearance
control system adjusts the clearance between the turbine blade tips and the
turbine casing to optimize performance and prevent blade damage due to rubbing.
The stator vanes (also called nozzles) form convergent ducts that convert the gaseous heat and
pressure energy into higher velocity gas flow (Pi). In addition to accelerating
the gas, the vanes "turn" the flow to direct it into the rotor blades
at the optimum angle.
- What
is the difference between a simple cycle gas turbine and a combined cycle
gas turbine?
A simple cycle gas turbine operates
independently to generate electricity without any additional energy recovery
systems, while a combined cycle gas turbine uses waste heat from the gas
turbine to generate steam, which drives a steam turbine to produce additional
electricity.
- What
is the role of the bleed valve system in a gas turbine?
The bleed valve system allows for
the controlled release of compressed air from the compressor to prevent
compressor stall and improve performance.
- Why is
air bleeding required through bleed valves?
Air bleeding through bleed valves
is required for various purposes, including compressor surge protection,
cooling and purging, and control of gas turbine power output.
- What
is the function of the flame holder in a gas turbine combustor?
The flame holder helps to stabilize
the combustion process by creating a region of recirculation and turbulence,
which promotes efficient fuel-air mixing.
- What
is the purpose of the turbine rotor in a gas turbine?
The turbine rotor is the rotating
component that extracts energy from the high-temperature, high-pressure gas
leaving the combustion chamber, and converts it into rotational energy to drive
the compressor and generator.
- What
is the difference between a can-type and an annular-type combustion
chamber in a gas turbine?
A can-type combustion chamber has
individual combustion chambers located around the turbine, while an
annular-type combustion chamber has a single combustion chamber surrounding the
turbine.
- What
is the function of the transition duct in a gas turbine?
The transition duct connects the
combustor to the turbine and helps to direct the hot gases into the turbine
while maintaining high efficiency and minimizing losses.
- What
is the importance of air cooling in gas turbine design?
Air cooling is important to prevent
thermal damage to the turbine components due to high temperatures, and to
improve efficiency and performance.
- What
is the function of the power turbine in a gas turbine?
The power turbine is the component
that converts the rotational energy from the gas turbine into mechanical energy
to drive the generator and produce electricity.
58. What
is the function of the turbine nozzle in a gas turbine?
The turbine nozzle is responsible for
directing the high-velocity gases from the combustion chamber onto the turbine
blades, converting the kinetic energy of the gases into rotational energy to
drive the turbine.
59. How
are gas turbines cooled?
Gas turbines are cooled using a variety of
methods, including air cooling, water cooling, and a combination of the two. Air
is used to cool the turbine blades and vanes, while water is used to cool the
combustion chamber and other high-temperature components.
- How is
the turbine rotor cooled in a gas turbine?
The turbine rotor is cooled by
circulating air or cooling fluid through internal channels in the rotor blades
and disks.
- How is
the fuel-air mixture ignited in a gas turbine?
The fuel-air mixture is ignited by
a spark plug or a pilot flame, which ignites the mixture in the combustion
chamber.
- What
is the function of the generator in a gas turbine power plant?
The generator converts the
mechanical energy from the turbine into electrical energy, which can then be
transmitted to the power grid.
Turbine blades are often coated
with a thermal barrier coating (TBC) made of ceramic
materials such as zirconia. The function of the TBCS is to provide thermal
insulation from the hot gas that flows through the turbine blades. TBCS consist
of two layer coating system which comprise of an oxidation and corrosion
resistant layer called the bond coat and an insulating ceramic top layer called
the top coat.
Compressor blades are sometimes
coated with a layer of anti-corrosive material, such as titanium aluminide
(TiAl), to protect against oxidation and corrosion at high temperatures.
Combustor liners and transition
pieces may be coated with a thermal barrier coating to protect against high
temperatures and improve efficiency.
Some components may also be coated
with special materials to reduce friction and wear, such as diamond-like carbon
(DLC) coatings or ceramic coatings.
- What
materials are used in the gas turbine engine combustor?
The materials of interest are the
nickel- and cobalt-base superalloys for turbine and burner sections of the
engine, and titanium alloys and composites for compressor and fan sections of
the engine.
- Which
material is best for gas turbine?
For most turbine blades are made of
Nickel super-alloys. They have good creep resistance at up to 80% of their
melting point, making them the material of choice for turbine blades.
- What
are the common materials used for gas turbine fabrication?
Common materials used in gas
turbine fabrication include nickel-based alloys, titanium alloys, and ceramic
matrix composites.
- Why
are nickel-based alloys used in gas turbine fabrication?
Nickel-based alloys are known for
their high-temperature strength, corrosion resistance, and thermal fatigue
resistance, making them well-suited for the high-temperature, high-pressure
environments found in gas turbines.
- What
are some common nickel-based alloys used in gas turbine fabrication?
Common nickel-based alloys used in
gas turbine fabrication include Inconel 718, Inconel 625, and Hastelloy X.
- Why
are titanium alloys used in gas turbine fabrication?
Titanium alloys are known for their
high strength-to-weight ratio, good corrosion resistance, and ability to
withstand high temperatures, making them a popular choice for gas turbine
components such as compressor blades.
- What
are some common titanium alloys used in gas turbine fabrication?
Common titanium alloys used in gas
turbine fabrication include Ti-6Al-4V, Ti-6Al-2Sn-4Zr-2Mo, and Ti-6246.
- What
are ceramic matrix composites (CMCs) and why are they used in gas turbine
fabrication?
CMCs are composite materials
consisting of a ceramic matrix reinforced with ceramic fibers. They are known
for their ability to withstand high temperatures and thermal shock, making them
well-suited for use in gas turbine components such as combustors and turbine
blades.
- What
are some common CMCs used in gas turbine fabrication?
Common CMCs used in gas turbine
fabrication include silicon carbide (SiC) and carbon fiber reinforced SiC
(C/SiC).
- What
are some challenges associated with using CMCs in gas turbine fabrication?
CMCs are relatively new materials
and are still being developed and optimized for use in gas turbine
applications. Challenges include cost, manufacturing complexity, and potential
for brittleness under certain conditions.
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