Note: Descriptions are shown in the official language in which they were submitted.
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A TUR_.BOCHARGER ASSEMBLY
This invention relates to a turbocharger assembly for an
internal combustion engine.
The practice of supercharging internal combustion
engines by means of turbochargers to improve their power
output is well known.
For single-stage turbocharging it may be sufficient to
use a single supercharger large enough to supply air to all
cylinders. For larger engines,~in particular those having
two rows of cylinders, each row of cylinders may be provided
with its own supercharger. An example of such an arrangement
is disclosed in United Kingdom Patent GB437078.
The pressure ratio obtainable by a single stage
turbocharger is somewhat limited, and for higher performance,
multiple stage turbocharging has been employed, the required
degree of compression being provided by disposing a high
pressure turbocharger in series with a low pressure
turbocharger. Exhaust gas from the engine first passes
through the turbine of the high pressure turbocharger and
then passes through the turbine of the low pressure
turbocharger. Similarly, air at atmospheric pressure is
first compressed in the low pressure compressor and is then
further compressed in the high pressure compressor.
Where two-stage turbocharging is applied to large
engines, the low pressure turbocharger may prove to be
physically large. To overcome the problems associated with
the use of a large low pressure turbocharger it is known to
provide an arrangement comprising two sets of two-stage
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turbochargers in which each two-stage turbocharger comprises
two low pressure turbochargers connected in parallel with
each other, the parallel combination being coupled in series
with a single high pressure turbocharger. An engine
utilising this arrangement is described in the publication
LSM, August 1993, pages 53 -54 "High Speed Variety - Paxman's
new high performing 12 VP185 boasts a genuinely versatile
design". This design allows all the turbochargers to be of
the same size, thereby eliminating the height and bulk
previously associated with low pressure turbochargers. In
this prior art arrangement, two sets of 2-stage
turbochargers are mounted in a single integrated unit
tailored to the requirements of the engine for which they
were designed. While this arrangement has proved to be
satisfactory, it is not suitable for larger engines
requiring a greater number of turbochargers or smaller
engines requiring only one set of turbochargers.
The present invention arose while seeking to
provide an improved turbocharger assembly which can be used
singly or in multiples on a variety of different sized
engines.
In accordance with the invention, a turbocharger
assembly for a supercharged internal combustion engine
comprises:
a group of three turbochargers consisting of a
first high pressure turbocharger and second and third low
pressure turbochargers, each turbocharger including a
turbine and a compressor arranged on a common rotational
axis, each turbine and each compressor having an input and
an output, the turbine inputs of the second and third
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turbochargers being connected in parallel with each other
but in series with the turbine output of the first
turbocharger and the compressor outputs of the second and
third turbochargers being connected in parallel with each
other but in series with the compressor input of the first
turbocharger: and
a multi-sided enclosure supporting the
turbochargers such that the compressors are outside the
enclosure and the turbines are inside the enclosure;
wherein the enclosure includes a first, centrally
positioned, substantially planar side supporting the first
turbocharger and second and third substantially planar sides
arranged on opposing flanks of the first side to support the
second and third turbochargers respectively, the second and
third sides of the enclosure being angled with respect to
the first side, whereby the rotational axes of the second
and third turbochargers, as extended beyond the
turbochargers, form a "V" shape with respect to each other
and with respect to the extended rotational axis of the
first turbocharger, and the turbine outputs of the second
and third turbochargers converge towards each other and
connect to exhaust duct means extending within the enclosure
transversely of the rotational axes of the turbochargers.
This arrangement allows a particularly compact and
substantially symmetrical layout to be employed which
minimises the length of ducting required to couple the high
pressure turbine outlet to the low pressure turbine inlets.
It is possible to employ a number of identical
turbocharger modules, each constructed in accordance with
the invention, on a single engine, the number of modules
depending on the size of the engine; and a small engine
requiring only a single module. The resulting uniformity of
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design between different engines can help economy of
production and ease of servicing and provision of spares.
The turbochargers of the or each assembly or
module may be substantially identical. This also leads to
an economical arrangement both in terms of cost and in the
number of different types of components required; both for
initial construction and subsequent maintenance.
The fact that in the invention the compressors are
outside the enclosure and the turbines are inside the
enclosure simplifies the problems associated with heat loss
from the components through which hot exhaust gases pass.
It also protects personnel from accidental contact with the
hot components.
Where the design is such as to allow exhaust gas
leakage from the turbines and/or the ducting associated
therewith, the enclosure may advantageously serve to collect
such leakage and channel it to an exhaust duct.
Alternatively, the enclosure.may be made gas tight so as to
allow a back pressure build up inside it thereby preventing
further leakage.
The fact that in the invention compressors of the
low-pressure turbochargers are coupled in parallel to supply
air to the compressor of the high-pressure turbocharger
provides an arrangement which requires less height than an
equivalent two-stage turbocharger in which a high pressure
compressor is supplied with air by a single low-pressure
compressor.
The invention also provides a turbocharger module
for a turbocharged internal combustion engine, comprising a
plurality of turbocharger cartridges, each cartridge having
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a turbine rotor and a compressor impeller mounted~on a
common shaft running in bearings, each cartridge being
mounted in a respective bore in a wall of a supporting
enclosure such that its turbine rotor projects into the
enclosure and its compressor impeller is outside the
enclosure, wherein for each bore.a face of a turbine housing
is tightly secured to wn internal surface region of the wall
surrounding said bore, said internal wall surface region and
said face being a good mechanical fit to each other thereby
to provide a low thermal resistance path to heat flow by
conduction from the turbine housing into the wall, each
turbine housing receiving a turbine rotor of the respective
cartridge therein, the cartridge being held concentric with
the turbine housing by a contact region between the turbine
housing and the cartridge, which contact region is smaller
in area than the area of contact between the face of the
turbine housing and the internal wall surface region, the
contact region providing the only significant region of
direct mechanical contact between the turbine housing and
the cartridge, whereby during operation of the cartridges,
heat from the turbine casing is shunted away from the
cartridges into the wall of the enclosure.
Embodiments of the invention will now be described
by way of example, with reference to the drawings, in which
Figure 1 shows a plan view of a turbocharger
module in accordance with the invention;
Figure 2 shows a plan view of three turbocharger
modules in accordance with the invention;
Figure 3 shows a partly sectioned side view of
Figure 2;
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Figure 4 shows a plan view of a first diesel
engine in accordance with the invention;
Figure 5 shows a plan view of a second diesel
engine in accordance with the invention;
Figures 6 to 8 illustrate a turbocharger suitable
for use with the invention.
Referring to Figure l, a turbocharger module 100
comprises three turbochargers. Each turbocharger comprises
a turbine housing, a compressor housing, and a cartridge
assembly comprising a turbine wheel and a compressor
impeller mounted on a common shaft, and bearings for the
shaft.
A first turbocharger comprises turbine housing 1
and a compressor housing 2. A second turbocharger comprises
a second turbine housing 3 and a second compressor
housing 4.
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A third turbocharger comprises a third turbine housing 5 and
a third compressor housing 6. The turbochargers are mounted
on the walls of a supporting enclosure 9. The construction
of the turbochargers and their mode of support will be
S described later with reference to Figures 6 to 8.
The gas outlet of the first turbine housing is connected
to the gas inlets of the second and third turbine housings in
common via a branch conduit 10. The joints between the
branch conduit 10 and the low pressure turbine housings 3, 5
comprise respective laterally-sliding flanges 50, 51 mounted
with a close-clearance on their respective turbine housing
flanges 52, 53. The respective ends of the branches of the
branch conduit are axially slidably mounted inside the
sliding flanges with a close clearance. The gas outlets of
the second and third turbine housings 3, 5 are coupled to
respective trumpets 7,8 which direct the exhaust gas into an
exhaust pipe, not shown. The first turbine housing 1 has a
gas inlet arranged to receive exhaust gas at high pressure.
The second and third turbochargers are symmetrically disposed
on opposite sides of the first turbocharger. This
arrangement provides a compact layout and allows the exhaust
gas inlet pipe and the exhaust pipe to be disposed on a
central axis.
The arrangement of one high pressure turbine in series
with two low pressure turbines allows satisfactory
performance to be obtained when a common design of cartridge
is utilised for all three turbochargers. While acceptable
performance may be attained by using a common design of
turbine housing, it may be preferable for the first turbine
housing l to be different from the second and third turbine
housings 3, 5 in order to optimise efficiency.
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The enclosure 9 has hollow walls to allow coolant to be
passed therethrough. The enclosure has a lid, not shown in
Figure 1, which is likewise of hollow construction.
Apertures 11 allow for passage of coolant between the
S enclosure and the lid. The input and output connections for
passage of coolant have been omitted from the figures f.or
clarity. The compressor housings 2, 4, 6 have respective air
outlet ports 13, 14, 15 and respective air inlet ports 16,
17, 18. The compressor housings can be oriented at any
desired angle with respect to the enclosure and are secured
in position by tightening their respective V-band clamps 12.
In Figures 2 and 3 three turbocharger modules 21, 22,
23, each as shown in Figure 1, are shown arranged in a line
on an engine, for use as two-stage turbochargers.
In Figure 2, module 23 is shown with its lid 19 in
position. Module 21 is shown partly cut away to illustrate
the recess provided to allow clearance for the intermediate
pressure duct 27b, 27c associated with an adjacent
turbocharger module. Figure 3 is a sectional view of Figure
2 along III-III with all lids in position.
Each lid 19 has a respective seating 30 to accommodate
a respective exhaust pipe 40 and sealing gasket 31. The
seating is disposed about an aperture aligned with the ends
of trumpets 7, 8 such that a clearance exists between the
trumpets and the wall 32 of the aperture..
The base of each box has a respective aperture 41 to
accommodate a respective exhaust conduit 42 which brings
exhaust gas from the exhaust manifold, not shown, of the
engine to a respective input port 111 of each high pressure
turbine housing 1. In the present embodiment, the exhaust
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manifold is jacketed to prevent escape of any exhaust gas
which might leak from joints in the exhaust system to the
immediate vicinity of the engine. The aperture 41 provides
communication between the space enclosed by the jacket of the
exhaust, not shown, and the interior of the enclosure 9. The
interior of enclosure 9 communicates with the interior of the
exhaust pipe 40 via the clearance between the trumpets 7, 8
and the wall 32 referred to earlier. This arrangement allows
any gas which may escape from joints in the exhaust ductwork
to escape via the exhaust pipe.
Figure 4 shows an arrangement in accordance with the
invention as applied to an 18 cylinder engine 400. Only the
turbocharger modules and their associated ductwork and
coolers have been shown for clarity. The engine has three
turbocharger modules 21, 22, 23 arranged in a line along the
engine. The turbocharger modules are connected to function
as two-stage turbochargers. The respective outlets 14a, 14b,
14c of each of the second compressors 4a, 4b, 4c are
connected in parallel to a first intermediate pressure (I. P.)
air inlet duct 24a. The respective outlets of each of the
third compressors 6a, 6b, 6c are likewise connected in
parallel to a second I.P. air inlet duct 24b. Air at
atmospheric pressure is brought to the inputs of the
respective second and third compressors via air filters and
ductwork which has been omitted for clarity. The first and
second I.P. inlet ducts 24a, 24b terminate at respective
inlet ports 25a, 25b of intercoolers 26a, 26b. After being
cooled, the cooled air at intermediate pressure passes along
one or more I.P. outlet ducts, not shown. In the present
embodiment the engine is of Vee block construction with two
rows of cylinders, and this duct may be conveniently routed
in the space between the rows of cylinders.
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Branch pipes 27a, 27b, 27c convey air from the I.P.
outlet duct to respective input ports of the respective
first, high pressure, compressors 2a, 2b, 2c of turbocharger
modules 21, 22, 23. The high pressure outlet of compressor
2c is connected to an input port of an aftercooler 28 via a
first high pressure(HP) duct 200, the outlet of high pressure
compressor 2b to a second input port of aftercooler 28 via a
second HP duct 201, the outlet of high pressure compressor 2a
is connected to the input ports of the aftercooler via a
balancing pipe 203 which communicates with both HP ducts 200,
201. After being cooled, the air leaving the aftercooler 28
is supplied to the inlet manifolds of the engine, not shown,
via respective high pressure air conduits 204a, 204b.
It can be seen that the configuration of the
turbocharger module allows a particularly compact ductwork
layout to be provided, whilst still allowing access to the
individual turbocharger for overhaul and/or replacement.
In a modification, not shown, a single relatively large
intercooler is used in place of the two separate relatively
small intercoolers 26a, 26b.
Figure 5 shows a 12 cylinder engine 600 in accordance
with the invention. This embodiment uses two turbocharger
modules 601, 602. The outputs of the second compressors are
coupled in parallel to a first I.P. duct 24a, the outputs of
the third compressors are coupled in parallel to a second
I.P. duct 24b. The first and second IP inlet ducts 24a, 24b
terminate at respective inputs 25a, 25b of the intercoolers
26a, 26b. The outputs of the high pressure compressors of
module 602 and 601 are coupled via respective HP ducts 200,
201 to aftercoolers 28a, 28b.
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Tn a modification, not shown, the aftercoolers 28a and
28b are combined into a single unit. Tn a further
modification, not shown, the intercoolers 26a, 26b are
similarly combined into a single unit.
The construction of a turbocharger suitable for use with
the invention will now be described with reference to Figures
6 to 8.
The turbocharger comprises four principal components.
These are
(a) a turbine housing 800
(b) a compressor housing 810
(c) a cartridge 850 comprising the moving parts of the
turbocharger; and
(d) an intermediate portion 950 of the wall 90 of the
housing 9.
The cartridge 850 comprises a compressor impeller 812
and a turbine rotor 814 mounted on a common shaft 816 running
in bearings 809. The cartridge 850 has oilways 861 adapted
to supply lubricating oil to the bearings 809' and an oil
drain duct 862 for oil emerging from the bearings 809. The
oilways 861 and duct 862 terminate in an axial face 807 of
the cartridge 850. A heat shield 830 shields the bearings
from hot exhaust gases in the turbine in known manner. The
housing wall 90 has an oil feed conduit 802 terminating at a
first face 803 of the wall 90 and arranged to communicate
with the oilway 861 in the cartridge 850 when the cartridge
is assembled to the first face 803. The wall 90 also has an
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oil drain duct 804 terminating at the first face 803 and
arranged to communicate with the oil drain duct 862. The
housing has "0" ring oil seals 805, 806 adapted to seal the
oilways and oil drain ducts.
5
To assemble the turbocharger, the turbine housing 800.is
aligned with a bore 851 in a support region 950 of the wall
90 using an arbor (not shown) or by making registers in the
wall and the turbine housing. The turbine housing 800 is
10 secured in position with fasteners 910 engaging tapped holes
916 in the turbine casing 800, and washers 912. On
tightening the fasteners 910, axial face 820 of turbine
casing 800, is drawn tightly against a first face 807 of
region 950. The faces 820 and 807 are machined to provide a
gas-tight join therebetween when the faces are drawn
together. Next the cartridge 850 is inserted into the bore
851. The region 950 has a second face 803 adapted to engage
with the axial face 817 of the cartridge 850. The thickness
of the region 950 is such that, when face 807 engages face
803, the turbine rotor 814 is correctly disposed with respect
to the turbine housing 800. The cartridge is held concentric
with the turbine casing by a spigot 870 having a close fit in
a narrow circular register 871 in the turbine housing 800.
The cartridge 850 is secured to the second face 803 by
fasteners 920 and washers 922 which engage tapped holes 924
in the region 950. On tightening the fasteners 920, the "0"
ring seals 805,806 are compressed to seal the oil feed and
the oil drain connections.
Finally the compressor housing 810 is assembled to the
cartridge 850 and secured in place by means of a Vee-section
clamping ring 12. This allows the radial orientation of the
housing 810 to be adjusted so as to bring the compressor
outlet port 813 to any desired position. It will be seen
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that, on completion of the assembly, the region 950 becomes
an integrated part of the turbocharger assembly, its
thickness determining the alignment of the turbine rotor
relative to the turbine housing.
S
It can be seen that, should a turbocharger become faulty
in service, to replace the cartridge 850 carrying the moving
parts it is only necessary to disconnect the air inlet duct
(not shown) from the air inlet , the air outlet duct from the
air outlet 803, remove clamp 12, pull off the compressor
casing 810, release the fasteners 920 and withdraw the
cartridge 850. A replacement cartridge can then be refitted
in the manner described previously. It is not necessary to
disturb the turbine housing 800 or the exhaust conduits
coupled to the turbine inlet or outlet ports. Thus when, as
in the embodiments described above, the turbine is mounted in
a sealed enclosure, the integrity of the sealing of the
enclosure is not broken. This affords simple and rapid
turbine removal and replacement.
Attaching the turbine housing directly to the wall of
the casing provides significant advantages in heat transfer,
as much of the heat transferred from the exhaust gases to the
turbine casing is diverted away from the bearings and flows
directly to the wall whence it can be removed via the coolant
therein. This avoids problems experienced by certain prior
art turbochargers, wherein heat from the hot turbine housing
flows via that portion of the turbocharger housing
intermediate the turbine and the compressor to cooler regions
and, should an engine have to be suddenly shut down and as a
consequence, the oil pump providing forced lubrication (and
cooling) of the turbocharger bearings ceases to operate, the
high thermal gradient between the turbine casing (which can
be at red heat) and the~cooler regions can be such as to
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cause carbonization of the lubricating oil in the bearings.
In the turbocharger described above, the relatively
narrow annular region where the spigot 870 mates with the
register 871 is the only significant region where direct
mechanical contact offering a low thermal resistance exists
between the hot turbine casing 800 and the cartridge 850
containing the bearings. The air gap associated with the
relatively loose fit between the other regions provides an
increased thermal resistance to heat flow by conduction.
Further, the direct connection between the turbine casing 800
and the wall 90, which, as noted may be hollow to accommodate
coolant, is via mating surfaces 871 and 807 which have been
machined to provide a good mechanical fit, and which
therefore provide a low thermal resistance path to heat flow
by conduction, which path shunts heat away from the bearings
within cartridge 850.
The arrangements described above are given by way of
example only, and a number of modifications are possible
within the scope of the invention.
While the type of turbocharger described above is
preferred, it is not essential, and any other suitable
turbocharger may be employed.
A balancing pipe may be provided where there are an
uneven number of turbocharger modules. Alternatively, the
inlet casing to a single (rather than twin) aftercooler may
be used as a mixing plenum. The compressor outlets may be
connected to the air inlets of their associated change air
coolers via individual conduits rather than by means of
branches to a common conduit. Where a jacketed exhaust is
employed, this need not communicate with the interior of the
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housing which supports the turbochargers. While it is
advantageous in the interests of manufacturing economy for
all turbochargers to be identical, it is not essential. It
may be found that to obtain the highest efficiency, the high
pressure turbocharger needs to be different from the low
pressure turbochargers. However, the arrangement will still
provide significant space advantageous compared with
arrangements utilising a single low-pressure compressor to
supply a single high pressure compressor. The enclosure need
not. be water-cooled.
The enclosure may be sealed, with no communication
between the interior of the enclosure and the exhaust pipe.
The back-pressure developed within the enclosure will tend to
inhibit further leakage of exhaust gas.
The enclosure need not be sealed. The support need not
be an enclosure if the turbocharger is used on an engine
which is installed in a situation where ventilation is such
that the removal of the heat radiated by the turbines and the
dissipation of any leaking of exhaust gas is not a problem.
In such situations the turbochargers may be supported by
their exhaust gas inlet and/or outlet ports or the ductwork
connected thereto or by support brackets in known manner.
The intermediate pressure air conduit may comprise two
or more discrete conduits rather than a single conduit. A
number of groups of intercoolers and/or aftercoolers may be
provided, distributed about the engine so as to minimise the
length of air ducts.
The second and third compressors of the or each module
may be connected in parallel with each other. Such an
arrangement is particularly suitable for smaller engines
requiring only one turbocharger assembly, but may also be
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utilised where a plurality of turbocharger assemblies are
employed.
