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Topic:- centrifugal
compressor and
impellor
Submitted To:- Mr.
Aditya mishra
Name:- Shahrukh
UID:- K12105
Stream:- B.Tech (ME)
Semester:- VI
 Introduction
 Classification
 Centrifugal Compressor
 Components
 Application
 Pros & Cons
 An air compressor is a device that converts power
(usually from an electric motor, a diesel engine or a
gasoline engine) into kinetic energy by compressing
and pressurizing air, which, on command, can be
released in quick bursts. There are numerous methods
of air compression, divided into either positive-
displacement or dynamic-displacement types.
Air
Compressor
Positive
Displacement
Reciprocating
Rotary
Dynamic
Displacement
Centrifugal
Axial
 The centrifugal air compressor is
a dynamic compressor which depends on transfer of
energy from a rotating impeller to the air.
 Centrifugal compressors produce high-pressure
discharge by converting angular momentum imparted
by the rotating impeller (dynamic displacement).
 The centrifugal air compressor is an oil free
compressor by design. The oil lubricated running gear
is separated from the air by shaft seals and
atmospheric vents.
 Inlet: The inlet to a centrifugal compressor is typically a simple
pipe. It may include features such as a valve, stationary
vanes/airfoils (used to help swirl the flow) and both pressure
and temperature instrumentation. All of these additional devices
have important uses in the control of the centrifugal compressor.
 Centrifugal Impeller: The key component that makes a
compressor centrifugal is the centrifugal impeller. It is the
impeller's rotating set of vanes (or blades) that gradually raises
the energy of the working gas. This is identical to an axial
compressor with the exception that the gases can reach higher
velocities and energy levels through the impeller's increasing
radius. Euler’s pump and turbine equation plays an important
role in understanding impeller performance.
 Diffuser: The next key component to the simple centrifugal
compressor is the diffuser. Downstream of the impeller in the flow
path, it is the diffuser's responsibility to convert the kinetic energy
(high velocity) of the gas into pressure by gradually slowing (diffusing)
the gas velocity. Diffusers can be vaneless, vaned or an alternating
combination. High efficiency vaned diffusers are also designed over a
wide range of solidities from less than 1 to over 4. Hybrid versions of
vaned diffusers include: wedge, channel, and pipe diffusers. There are
turbocharger applications that benefit by incorporating no diffuser.
 Collector: The collector of a centrifugal compressor can take many
shapes and forms. When the diffuser discharges into a large empty
chamber, the collector may be termed a Plenum. When the diffuser
discharges into a device that looks somewhat like a snail shell, bull's
horn or a French horn, the collector is likely to be termed
a volute or scroll. As the name implies, a collector’s purpose is to gather
the flow from the diffuser discharge annulus and deliver this flow to a
downstream pipe. Either the collector or the pipe may also contain
valves and instrumentation to control the compressor.
 In gas turbines and auxiliary power units.
 In automotive engine and diesel
engine turbochargers and superchargers.
 In pipeline compressors of natural gas to move the gas from
the production site to the consumer.
 In oil refineries, natural gas
processing, petrochemical and chemical plants.
 Air-conditioning and refrigeration and HVAC: Centrifugal
compressors quite often supply the compression in water
chillers cycles.
Pros
 Centrifugal compressors are
used throughout industry
because they have fewer rubbing
parts, are relatively energy
efficient, and give higher airflow
than a similarly
sized reciprocating
compressor or positive-
displacement compressor.
 Centrifugal compressors are
often used in small gas
turbine engines like APUs
(auxiliary power units) and
smaller aircraft gas turbines.
 Their main drawback is that
they cannot achieve the
high compression ratio of
reciprocating compressors
without multiple stages.
 Centrifugal compressors are
impractical, compared to axial
compressors, for use in large gas
turbine engines propelling large
aircraft, due to the resulting
weight and stress, and to the
frontal area presented by the
diffuser.
Cons
Thank You

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K12105 shahrukh

  • 1. Topic:- centrifugal compressor and impellor Submitted To:- Mr. Aditya mishra Name:- Shahrukh UID:- K12105 Stream:- B.Tech (ME) Semester:- VI
  • 2.
  • 3.  Introduction  Classification  Centrifugal Compressor  Components  Application  Pros & Cons
  • 4.  An air compressor is a device that converts power (usually from an electric motor, a diesel engine or a gasoline engine) into kinetic energy by compressing and pressurizing air, which, on command, can be released in quick bursts. There are numerous methods of air compression, divided into either positive- displacement or dynamic-displacement types.
  • 5.
  • 7.  The centrifugal air compressor is a dynamic compressor which depends on transfer of energy from a rotating impeller to the air.  Centrifugal compressors produce high-pressure discharge by converting angular momentum imparted by the rotating impeller (dynamic displacement).  The centrifugal air compressor is an oil free compressor by design. The oil lubricated running gear is separated from the air by shaft seals and atmospheric vents.
  • 8.
  • 9.  Inlet: The inlet to a centrifugal compressor is typically a simple pipe. It may include features such as a valve, stationary vanes/airfoils (used to help swirl the flow) and both pressure and temperature instrumentation. All of these additional devices have important uses in the control of the centrifugal compressor.  Centrifugal Impeller: The key component that makes a compressor centrifugal is the centrifugal impeller. It is the impeller's rotating set of vanes (or blades) that gradually raises the energy of the working gas. This is identical to an axial compressor with the exception that the gases can reach higher velocities and energy levels through the impeller's increasing radius. Euler’s pump and turbine equation plays an important role in understanding impeller performance.
  • 10.
  • 11.  Diffuser: The next key component to the simple centrifugal compressor is the diffuser. Downstream of the impeller in the flow path, it is the diffuser's responsibility to convert the kinetic energy (high velocity) of the gas into pressure by gradually slowing (diffusing) the gas velocity. Diffusers can be vaneless, vaned or an alternating combination. High efficiency vaned diffusers are also designed over a wide range of solidities from less than 1 to over 4. Hybrid versions of vaned diffusers include: wedge, channel, and pipe diffusers. There are turbocharger applications that benefit by incorporating no diffuser.  Collector: The collector of a centrifugal compressor can take many shapes and forms. When the diffuser discharges into a large empty chamber, the collector may be termed a Plenum. When the diffuser discharges into a device that looks somewhat like a snail shell, bull's horn or a French horn, the collector is likely to be termed a volute or scroll. As the name implies, a collector’s purpose is to gather the flow from the diffuser discharge annulus and deliver this flow to a downstream pipe. Either the collector or the pipe may also contain valves and instrumentation to control the compressor.
  • 12.  In gas turbines and auxiliary power units.  In automotive engine and diesel engine turbochargers and superchargers.  In pipeline compressors of natural gas to move the gas from the production site to the consumer.  In oil refineries, natural gas processing, petrochemical and chemical plants.  Air-conditioning and refrigeration and HVAC: Centrifugal compressors quite often supply the compression in water chillers cycles.
  • 13. Pros  Centrifugal compressors are used throughout industry because they have fewer rubbing parts, are relatively energy efficient, and give higher airflow than a similarly sized reciprocating compressor or positive- displacement compressor.  Centrifugal compressors are often used in small gas turbine engines like APUs (auxiliary power units) and smaller aircraft gas turbines.  Their main drawback is that they cannot achieve the high compression ratio of reciprocating compressors without multiple stages.  Centrifugal compressors are impractical, compared to axial compressors, for use in large gas turbine engines propelling large aircraft, due to the resulting weight and stress, and to the frontal area presented by the diffuser. Cons