Generic
Definitions
A/R
·
A/R describes a geometric property of all compressor and turbine
housings. Increasing compressor A/R optimizes the performance
for low boost applications. Changing turbine A/R has many effects.
By going to a larger turbine A/R, the turbo comes up on boost
at a higher engine speed, the flow capacity of the turbine is
increased and less flow is wastegated, there is less engine backpressure,
and engine volumetric efficiency is increased resulting in more
overall power
Choke Line
· The choke line is on the right hand side of a compressor map
and represents the flow limit. When a turbocharger is run deep
into choke, turbo speeds will increase dramatically while compressor
efficiency will plunge (very high compressor outlet temps), and
turbo durability will be compromised.
CHRA
· Center housing rotating assembly - The CHRA includes a complete
turbocharger minus the compressor, turbine housing, and actuator.
Clipper Turbine Wheels
· When an angle is machined on the turbine wheel exducer (outlet
side), the wheel is said to be 'clipped'. Clipping causes a minor
increase in the wheel's flow capability, however, it dramatically
lowers the turbo efficiency. This reduction causes the turbo to
come up on boost at a later engine speed (increased turbo lag).
High performance applications should never use a clipped turbine
wheel. All Garrett GT turbos use modern unclipped wheels.
Corrected Airflow
· Represents the corrected mass flow rate of air, taking into
account air density (ambient temperature and pressure)
Example:
Air Temperature (Air Temp) - 60°F
Barometric Pressure (Baro) - 14.7 psi
Engine air consumption (Actual Flow) = 50 lb/min
Corrected Flow= Actual Flow Ö([Air
Temp+460]/545)
Baro/13.95
Corrected Flow= 50*Ö([60+460]/545) = 46.3 lb/min
14.7/13.95
Efficiency Contours
· The efficiency contours depict the regional efficiency of the
compressor set. This efficiency is simply the percentage of turbo
shaft power that converts to actual air compression. When sizing
a turbo, it is important to maintain the proposed lugline with
a high efficiency range on the map.
Free-Float
· A free floating turbocharger has no wastegate device. This turbocharger
can't control its own boost levels. For performance applications,
the user must install an external wastegate.
GT
· The GT designation refers to Garrett's state-of-the-art turbocharger
line. All GT turbos use modern compressor and turbine aerodynamics
which represent huge efficiency improvements over the old T2,
T3, T3/T4, T04 products. The net result is increased durability,
higher boost, and more engine power over the old product line.
On-Center Turbine Housings
· On-center turbine housings refer to an outdated style of turbine
housing with a centered turbine inlet pad. The inlet pad is centered
on the turbo's axis of rotation instead of being tangentially
located. Using an on-center housing will significantly lower the
turbine's efficiency. This results in increased turbo lag, more
backpressure, lower engine volumetric efficiency, and less overall
engine power. No Garrett OEM's use on-center housings.
Pressure Ratio
· Ratio of absolute outlet pressure divided by absolute inlet
pressure
Example:
Intake manifold pressure (Boost) = 12 psi
Pressure drop, intercooler (DPIntercooler)
= 2 psi
Pressure drop, air filter (DPAir
Filter) = 0.5 psi
Atmosphere (Atmos) = 14.7 psi at sea level
PR= Boost +DPIntercooler+ Atmos
Atmos-DPAir
Filter
PR= 12+2+14.7 = 2.02
14.7-.5
Surge Line
· The surge region, located on the left hand side of the compressor
map, is an area of flow instability typically caused by compressor
inducer stall. The turbo should be sized so that the engine does
not operate in the surge range. When turbochargers operate in
surge for long periods of time, bearing failures may occur.
Trim
· Trim is an area ratio used to describe both turbine and compressor
wheels. Trim is calculated using the inducer and exducer diameters.
As trim is increased, the wheel can support more air/gas flow.
Wastegate
· A wastegated turbocharger includes an integral device to limit
turbo boost. This consists of a pneumatic actuator connected to
a valve assembly mounted inside the turbine housing. By connecting
the pneumatic actuator to boost pressure, the turbo is able to
limit its maximum boost output. The net result is increased durability,
quicker time to boost, and adjustability of boost.
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