Title of Invention

"COMPRESSOR FOR COMPRESSING A GAS AND A WASTEGATED TURBOCHARGER"

Abstract A wastegated turbocharger comprises a turbine wheel (5) mounted to a shaft (8) for rotation within a turbine housing (4), which is provided with a wastegate valve assembly 18. A compressor wheel (7) rotatably mounted to the shaft (8) for rotation within a compressor housing (6). A pneumatic wastegate actuator (19) is connected by a boost airline (28) to the compressor intake outlet (15). The compressor housing (6) is provided with a command valve mount (23) for directly mounting a wastegate actuator command valve (22) to the compressor housing. The command valve in use operates to selectively vent the boost airline (28) for controlling operation of the wastegate actuator (19). The compressor housing (6) is provided with a first internal passage (25) communicating between the valve mount (23) and the compressor intake outlet volute (15) and a second internal passage (27) communicating between the valve mount (23) and the compressor intake inlet (14). The first internal passage extends into the outlet volute away from the volute walls.
Full Text COMPRESSOR WITH SECONDARY
BOOST AIR OUTLET PASSAGE
This invention relates to a compressor with a secondary boost air outlet. A
compressor may be used to compress gases other than air, and the present invention is
not limited to a compressor which compresses only air. The term "air" as used
throughout this specification should therefore be interpreted as covering any gas. The
invention relates in particular to a turbocharger incorporating a wastegate and
pneumatic wastegate actuator, and more particularly to a command valve arrangement
for controlling the operation of the wastegate actuator.
Turbocllargers are well known devices for supplying air to the intake of an
internal combustion engine at pressures above atmospheric (boost pressures), and are
widely used irl automobiles and the like as well as in industrial applications. A
conventional turbocharger essentially comprises an exhaust gas driven turbine wheel
mounted on a rotatable shaft within a turbine housing. For instance, in a centripetal
turbine the turbine housing defines an annular inlet passageway around the turbine
wheel and a generally cylindrical axial outlet passageway extending from the turbine
wheel. Rotation of the turbine wheel rotates a compressor wheel mounted on the
other end of the shaft within a compressor housing. The rotating compressor wheel
compresses inlet air and delivers the compressed air to the intake manifold of the
engine, thereby increasing engine power.
It is also well known to provide turbochargers with a bypass passageway
between the exhaust inlet and the exhaust outlet portions of the turbine housing to
enable control of the turbocharger boost pressure andlor shaft speed. A wastegate
valve is locateti in the bypass passageway and is controlled to open the passageway
when the pressure level of the boost air increases towards a pre-determined level, thus
allowing some of the exhaust gas to by-pass the turbine wheel preventing the boost
pressure from rising above said level. The wastegate valve is generally actuated by a
pneumatic actuator operated by boost air pressure delivered by the compressor wheel.
The conventional pneumatic actuator comprises a spring-loaded diaphragm (or
a spring loaded sliding seal) housed within a canister, often referred to as the
wastegate actuator can. The actuator can is connected by an airline to the compressor
outlet and is generally mounted on the compressor housing. Communication with the
compressor outlet is via a secondary boost air outlet passage such as a port formed in
the compressor housing. The diaphragm/sliding seal acts on a connecting rod which
extends to the wastegate valve assembly which is mounted in the turbine housing.
The spring bias is such that under low boost pressure conditions the wastegate valve
remains closed. However, when the boost pressure (which is transmitted to the
actuator can from the compressor outlet via the secondary boost air outlet and the
airline) reaches a pre-detennined maximum the diaphragm is moved against the
action of the spring and operates to open the wastegate valve (via the connecting rod)
thereby allowing some exhaust gas to bypass the turbine wheel.
The actuator can is generally connected to the compressor outlet by a flexible
hose. In many cases the connection is direct. However, it is also known to provide a
bleed valve, also referred to as a command valve, in the airline which responds to
appropriate control signals (for instance from the engine management system) to
effectively varj the pressure transmitted to the wastegate actuator can by venting to
atmosphere. This provides for additional control of the wastegate valve over and
above the basic operation dependent upon the pre-determined spring bias. For
instance, the command valve may be operated to effectively modify the pressure at
which the waslegate valve will begin to open which may be desirable in certain
engiile operating conditions.
Wastegate actuator control is not the only situation in which it is necessary to
extract boost a r from the outlet of a compressor via a secondary boost air outlet
passage. For instance, one conventional method of preventing compressor surge is to
install a solenoid valve in an air line ported to the compressor outlet via a secondary
boost air outlet passage to controllably vent boost air fi-om the outlet under conditions
at which the colnpressor is likely to surge. The vented air may typically be vented to
atmosphere via a silencer or returned to the compressor inlet for re-circulation through
the compressor.
Where a valve is used to control the boost air flow through the secondary
boost air outlet passage, it is quite common to mount the valve at a location remote
from the compressor. For instance, some valves are constructed largely from plastic
and therefore must be mounted away from the turbocharger at a cool part of the
engine. Inevitably, remote mounting of the valve (whatever its function) requires
extra air lines and associated fittings. A solution to this problem is provided by
Japanese patent application S62-35565 (laid-open patent application S 63-205419
filed in February 1987). This discloses mounting a solenoid valve directly to the
compressor housing in order to avoid extra air line connections between the valve and
the compressor. The compressor housing is provided with an integral valve mount
located on ar: outside surface of the housing and including a first air port in
communicatio~ with the compressor outlet volute and a second air port in
comm~nicatiow~it~h the compressor air intake. The mount has means for attaching
the solenoid valve and forming a leak-tight seal between the valve and the first and
second air p o ~psr ovided in the valve mount. In this particular instance, the solenoid
valve is provided for surge prevention and thus operates to selectively control flow of
boost air from the compressor outlet to the compressor inlet (via the first and second
air ports respectively) to avoid surge. Exactly the same valve mounting arrangement
has been used for mounting a wastegate actuator command valve, see for instance lJS
6,205,784.
A problem with the known arrangements for extracting air from a compressor
outlet via a secondary boost air outlet passage is that any oil, dirt etc present in the air
is fed to the downstream component (such as a valve or wastegate actuator) which
over time can compromise the operation of the component. For instance, valve ports
can become at least partially clogged by the build-up of oil and particulate material
present in the goost air. This can be particularly problematical where the compressor
is part of a turbocharger fitted to a combustion engine with a closed crank case
ventilation system (CCV). Closed cranked case ventilation is becoming increasingly
prevalent in order to meet modem stringent exhaust emission regulations.
It is a? object of the present invention to obviate or mitigate the above
disadvantages.
According to a first aspect of the present invention there is provided a
compressor for compressing a gas, the compressor comprising a compressor wheel
rotatably mounted within a compressor housing, the compressor housing having a gas
inlet and having a gas outlet volute disposed around the compressor wheel, and
defined by an inner surface or surfaces of the housing, for supplying gas at boost
pressures, a secondary boost gas outlet passage provided in communication with the
outlet volute, wherein the secondary boost gas outlet passage is defined at least in part
by a projectior. which extends into the volute so that the upstream end of the passage
opens at a location spaced from the volute surface.
By locating the inlet of the secondary boost gas passage away from the surface
of the volute the amount of oilldirt etc passing into the passage can be reduced or
eliminated entirely. This is because the oilidirt etc is centrifilged to the volute surface
by the gas flow swirling through the volute and the air flow away from the surface is
clean.
Accordmg to a second aspect of the present invention there is provided a
wastegated turbocharger comprising:
a turbire wheel mounted to a shaft for rotation within a turbine housing, the
turbine housing provided with a wastegate valve assembly;
a compressor wheel rotatably mounted to said shaft for rotation within a
compressor housing, the compressor housing having an intake air inlet and an intake
air outlet volute for supplying air to an internal combustion engine at boost pressures;
a pneumatic wastegate actuator connected by a boost airline to the compressor
intake outlet;
wherein the compressor housing is provided with a command valve mount for
directly mounting a wastegate actuator command valve to the compressor housing, the
command valve in use operating to selectively vent said boost airline for controlling
operation of the wastegate actuator;
the compressor housing defining a first internal passage communicating
between the valve mount and ihe compressor outlet volute, and a second internal
passage communicating between the valve mount and the compressor intake inlet;
wherein the first passage is defined at least in part by a projection which
extends into the volute so that the upstream end of the passage opens at a location
spaced from the volute surface.
According to a third aspect of the present invention there is provided a
wastegated turbocharger comprising:
a turbine wheel mounted to a shaft for rotation within a turbine housing, the
turbine housing provided with a wastegate valve assembly;
a compressor wheel rotatably mounted to said shaft for rotation within a
compressor housing, the compressor housing having an intake air inlet and an intake
air outlet volute for supplying air to an internal combustion engine at boost pressures;
a pneuinatic wastegate actuator connected by a boost airline to the compressor
intake outlet;
whereil a command valve is mounted to a valve mount provided integrally
with the compressor housing, the command valve having a boost air inlet and a vent
outlet for sel.=ctively venting the boost airline for controlling operation of the
wastegate actuator, and wherein the compressor housing is provided with an internal
boost air passage communicating directly between the compressor intake outlet and
the valve boost air inlet, and a vent passage communicating directly between the valve
vent outlet and the compressor intake inlet;
wherein the boost air passage is defined at least in part by a projection which
extends into the volute so that the upstream end of the passage opens at a location
spaced from the volute surface.
Specific embodiments of the present invention will now be described, by way
of example on;y, with reference to the accompanying drawings, in which:
Figure 1 is an axial cross-section through a conventional turbocharger
illustrating the major components of a turbocharger;
Figure 2 illustrates details of a conventional turbocharger wastegate valve and
actuator assembly;
Figure 3 is a schematic perspective external view of a turbocharger
incorporating the present invention; and
Figure 4 is a cross-section through part of the turbocharger compressor
housing and command valve assembly of Figure 3.
Figures 5-8 are cross-sections through further embodiments of the present
invention.
Referring first to figure 1, this illustrates the basic components of a
conventional centripetal type turbocharger. The turbocharger comprises a turbine 1
joined to a cornpressor 2 via a central bearing housing 3. The turbine 1 comprises a
turbine housing 4 which houses a turbine wheel 5. Similarly, the compressor 2
comprises a compressor housing 6 which houses a compressor wheel 7. The turbine
wheel 5 and compressor wheel 7 are mounted on opposite ends of a common shaft 8
which is suppolted on bearing assemblies 9 within the bearing housing 3.
The turbine housing 4 is provided with an exhaust gas inlet 10 and an exhaust
gas outlet 11. The inlet 10 directs incoming exhaust gas to an annular inlet chamber
12 which forms a volute surrounding the turbine wheel 5. The exhaust gas flows
through the turoine 1 and into the outlet 1 1 via a circular outlet opening 13 which is
co-axial with tl-e turbine wheel 5.
The conlpressor comprises an inlet 14 and an outlet volute 15 co-axial with the
compressor wheel 7. As the compressor wheel rotates, air intake is drawn in through
the inlet 14, compressed and delivered to the engine via outlet volute 15. The
illustrated compressor 2 has a map width enhanced (MWE) inlet structure comprising
two co-axial tu5ular inlet sections 14a and 14b. The inner inlet section 14b is shorter
than the outer mlet section 14a and has an inner surface which is an extension of a
surface of the inner wall of the compressor housing which faces the compressor wheel
7. The outer inlet portion 14a is located radially outside the inner inlet portion 14b to
define an annular inlet passage 16 therebetween. Apertures 17 are formed through the
housing at the downstream end of the outer inlet portion 14a and open into the inner
surface of the compressor housing adjacent the compressor wheel 7. As the
compressor wheel 7 rotates at high speed and flow conditions, intake air is drawn into
the compressor housing through the inner inlet portion 14b and also through the
annular passaze 16 and apertures 17. However, as the mass flow through the
conlpressor whsel 7 falls the pressure drop across the apertures 17 falls and eventually
reverses, at which time the airflow direction in the annular passage 16 also reverses
such that some of the air entering the housing through the inner inlet portion 14b is recirculated.
This stabilises the compressor performance in a well known way.
Referring now to figure 2, this illustrates components of a conventional
wastegate valve and wastegate actuator assembly which is not visible from figure 1.
The turbine housing 4 is provided with a bypass passageway (not shown) which
communicates between the exhaust inlet 10 and the exhaust outlet bypassing the
turbine wheel. The bypass passageway communicates with the exhaust inlet 10 via a
circular opening (not shown) which is opened and closed by a wastegate valve
assembly 18 provided for controlling the flow therethrough. In figure 2 the part of the
turbine housing 4 defining the inlet 10 is shown partially cut-away to reveal details of
the wastegate valve assembly 18.
The westegate valve assembly 18 is controlled by a pneumatic wastegate
actuator 19 which is linked to the valve assembly 18 via a connecting rod 20. The
actuator can 19 receives compressed air from the outlet of the compressor 2 via an
airhose (not shown) communicating with a secondary boost av outlet passage (not
shown) providzd through the compressing housing with the outlet volute fitted to
nipple 21 and communicating with a port (not shown) provided in the compressor
housing. The compressor can 19 is conventionally mounted to the outside of the
compressor housing by an appropriate bracket (not shown). Details of the wastegate
valve assembly 18, the actuator can 19, and the mounting arrangements for securing
the actuator can 19 to the compressor are not important to an understanding of the
present invention (and may be entirely conventional) and thus will not be described
further.
Figure 3 is a perspective, external illustration of a wastegated turbocharger
fitted with a \;\,astegate command valve 22 and incorporating the present invention.
Common reference numerals are used to identify components shown in figures 1 and
2.
Referring now to figure 4, this is an enlarged cross-section of part of the
compressor housing of figure 3. The compressor housing, in this case the compressor
cover 6a, is formed with a valve mounting boss 23 which defines an internal opening
24 for receiving one end 22a of the command valve 22 (as illustrated the valve end
22a is screwed into the boss 23 but other fixing arrangements may be provided to suit
the form of valve 22).
The co~npressor cover 6a is provided with three internal bores 25, 26 & 27
which communicate with the boss opening 24 and with respective ports of the
command valvs 22. The first bore 25 is the secondary boost air outlet passage which
communicates with the compressor outlet volute 15 to deliver boost air to the valve
22. The second bore 26 is a boost air supply passage and opens to the outer surface of
the compressor cover 6a and is provided to supply boost air from the valve 22 to the
wastegate actuator via an appropriate hose connection shown by chain dot lines 28.
The third bore 27 is a boost air vent passage and communicates with the compressor
inlet in the region of the annular inlet passage 16.
In accordance with the present invention, the secondary boost air outlet
passage 25 projects into the outlet volute 15 so that the opening 25a at the upstream
end of the passage 25 is spaced from the surface 15a of the volute 15. The inventor
has found that this seemingly simple expedient significantly reduces, and even
entirely eliminates, the passage of oilldirt etc through the secondary boost passage 25.
This is because any oilldirt particles etc are centrifuged onto the volute wall 15a by
the gas flow which swirls through the outlet volute 15. Accordingly, air flowing
through the volute away from the volute surface 15a is cleaner than the air flow close
to the volute surface 15a.
Each of'the bores 26 and 27 may be formed by drilling through the compressor
cover 6a and boss 24. In the illustrated example the boost air vent bore 27 is formed
from two angled portions which may be drilled separately from within the compressor
inlet and boss opening 24 respectively. It will, however, be appreciated that. in other
compressor housing designs it may be possible to provide a straight boost air vent
bore between the command valve and the compressor inlet. Similarly, it will be
understood that the bores 26 and 27 could be cast rather than drilled.
The command valve 22 is a conventional three port proportional solenoid
valve which is operable to selectively connect the boost air inlet bore 25 with either
the boost air outlet bore 26 or boost air vent bore 27 in response to an appropriate
control signal (received from the engine management system or other appropriate
sensor/control arrangement). The valve 22 may thus be operated in essentially the
same manner as a conventional wastegate actuator command valve to control the
boost air supply to the wastegate actuator in accordance with normal operating
parameters. Since the valve itself may be entirely conventional, no details of any
particular valve will be described, but it should be borne in mind that the valve must
be capable of withstanding the relatively high temperature generated at the
compressor anti an appropriate valve should be selected accordingly.
With tke simple embodiment illustrated in Figure 3, the projection into the
volute 15 may be formed as an integral casting formation 6b with the compressor
housing 6a. The bore 25 could either be cast or drilled post-casting. However,
casting such a projection complicates the casting process and thus may add to
manufacturing expense. One alternative is illustrated in Figure 5. The structure
illustrated in Figure 5 is the same as that illustrated in Figure 3 except that the
secondary boost air outlet passage is defined by a member 29 which is fitted into the
boss opening 24 and extends through an aperture 30 which may simply be drilled into
the housing 6a through the bottom of the opening 24. Figure 5 is only a schematic
drawing, and i: will be appreciated that additional features, such as annular seals etc,
may be provided to prevent gas leaking between the aperture 3 0 and member 29.
Two further alternatives are illustrated in Figures 6 and 7. In each case the
valve 22 is modified by provision of an elongate nose or stem 31 (which is directly
equivalent to the projecting portion 6b of Figure 5) which extends through an aperture
30 when the \,alve is installed in the valve mounting boss 23 (vent port 27 is not
visible in Figures 6 and 7). Also shown in Figures 6 and 7 are O-ring seals 23a
provided to provide an air-tight seal between the valve 22 and mounting boss 23.
The embodiments of Figures 6 and 7 differ from one another in that in the
embodiment ol'Figure 7 the aperture 30 is sized to receive only the nose portion 3 1 of
the valve whereas with the embodiment of Figure 7 the aperture 30 is enlarged to
receive a relatively large diameter end portion of the valve 22. The latter arrangement
avoids the need for a separate drilling to form the aperture 30 which instead is formed
by a drilling which defines a part of the boss opening 24.
It will be appreciated that modification may be made to the detail of the
configuration of the valve mounting boss dependent upon the design of the command
valve intended to be used and to the size and positioning of the boost air inlet, outlet
and vent bore:;, as well as the precise location at which these bores open to the
compressor inlet, outlet and outer surface of the compressor housing.
It will also be appreciated that the invention is not limited in application to any
particular form of wastegate actuator or wastegate valve assembly but can be applied
wherever a command valve is desirable to control operation of a pneumatic wastegate
actuator. In addition, it will be understood that the command valve itself can be
controlled in accordance with any conventional methods and engine performance
parameters to provide the same control as a conventional wastegate actuator
command valve.
Valves intended for other purposes may be installed and that the invention is
not limited for use in application with wastegate actuator command valves. For
instance, a valve operated to prevent compressor surge may be installed as suggested
by the Japanese patent application mentioned in the introduction to this specification.
Furtherniore, it should be appreciated that the present invention provides
advantages even where the valve is located remote from the secondary boost air outlet
passage. For -nstance, Figure 8 schematically illustrates an adapter member 32
installed in an aperture 34 provided through a compressor housing 6. One end of the
adapter 32 defines a secondary boost air outlet passage 33 which projects into the
compressor vollste 15, and the other end of the adapter 32 provides a fitting 34 for
attachment of xi air hose (not shown) for feeding the boost air to a remotely located
valve. The adapter 32 is preferably screwed into the aperture 34, and in order to
provide sufficiently long screw thread the compressor housing 6 is preferably formed
with a boss 35 tlhrough which the aperture 34 is drilled.
Furthemlore, the air need not necessarily be supplied to a downstream valve
but could, for instance, be supplied directly to a wastegate actuator or other
component.
Other modifications and applications of the invention will be readily apparent
to the appropriately skilled person.





WE CLAIM:
1. A compressor for compressing a gas, the compressor comprising a compressor wheel (7)
rotatably mounted within a compressor housing (6), the compressor housing having a gas inlet (14)
and having a gas outlet volute (15) disposed around the compressor wheel, and defined by an inner
surface or surfaces of the housing, for supplying gas at boost pressures, a secondary boost gas outlet
passage (25) provided in communication with the outlet volute, characterised in that the secondary
boost gas outlet passage is defined at least in part by a projection which extends into the volute so
that the upstream end of the passage opens at a location spaced from the volute surface (15a) and
said secondary boost gas passage communicates with a port of a downstream valve.
2. A compressor as claimed in claim 1, wherein said projection is defined by a portion of the
housing which projects in to the volute.
3. A compressor as claimed in claim 1, wherein said projection is defined by a member (29)
which extends into the outlet volute through an aperture (30) provided in a wall of the compressor
housing.
4. A compressor as claimed in claim 1, wherein said projection is defined by a projecting
portion of a valve (22) mounted directly to the compressor housing so that said projecting portion
extends into the outlet volute through an aperture (30) provided in the compressor housing.
5. A compressor as claimed in claim 1, wherein the compressor housing is provided with a
valve mount (23) for directly mounting the valve to the compressor housing, said secondary boost
gas outlet passage opening into said valve mount, and an internal passage (27) communicating
between the valve mount and the compressor intake inlet, whereby the valve may operate to pass
boost air from the secondary boost air outlet passage to the compressor inlet.
C 6. A compressor as claimed in claim 4, wherein the compressor housing is provided with a
valve mount (23) for directly mounting the valve to the compressor housing, said aperture opening
into said valve mount, and an internal passage (27) communicating between the valve mount and the
compressor intake inlet, whereby the valve may operate to pass boost air from the secondary boost
air outlet passage to the compressor inlet.
7. A compressor as claimed in claim 4, wherein said valve mount is a boss (23) provided on the
compressor housing and defining an internal recess (24) for receiving a portion of said valve.
8. A compressor as claimed in claim 7, wherein said secondary boost gas outlet passage opens
into said internal recess for direct communication with a boost air inlet and a vent outlet of the valve
respectively.
9. A compressor as claimed in claim 7, wherein the compressor housing is provided with a third
passage (26) communicating with said internal recess and an outer surface of the compressor housing
or boss for supplying boost air from said valve to a downstream component.
10. A compressor as claimed in claim 7, wherein said internal recess in the boss is threaded to
receive a threaded end of said valve.
11. A wastegated turbocharger incorporated with a compressor as claimed in claim 1 to 6,
comprising:
a turbine wheel mounted to a shaft for rotation within a turbine housing, the turbine housing
provided with a wastegate valve assembly;
a pneumatic wastegate actuator (19) connected by a boost airline to the compressor intake
outlet (1 5);
wherein said downstream valve is a control valve which in use operates to selectively vent
said boost airline for controlling operation of the wastegate actuator (1 9).
12. A wastegated turbocharger as claimed in claim 11 :
wherein said control valve is mounted to the valve mount, the control valve having a boost air
inlet and a vent outlet for selectively venting the boost airline for controlling operation of the
wastegate actuator.

Documents:

1058-del-2004-Abstract-(12-09-2013).pdf

1058-del-2004-abstract.pdf

1058-del-2004-Claims-(12-09-2013).pdf

1058-del-2004-claims.pdf

1058-del-2004-Correspondence Others-(12-09-2013).pdf

1058-del-2004-Correspondence Others-(15-05-2012).pdf

1058-del-2004-Correspondence-Others-(05-11-2012).pdf

1058-del-2004-Correspondence-Others-(18-02-2013).pdf

1058-del-2004-Correspondence-Others-(24-07-2013).pdf

1058-del-2004-correspondence.pdf

1058-del-2004-description.pdf

1058-del-2004-drawings.pdf

1058-del-2004-Form-2-(12-09-2013).pdf

1058-del-2004-Form-3-(15-05-2012).pdf

1058-del-2004-Form-3-(24-07-2013).pdf

1058-del-2004-form1.pdf

1058-del-2004-form2.pdf

1058-del-2004-form3.pdf

1058-del-2004-form5.pdf


Patent Number 260410
Indian Patent Application Number 1058/DEL/2004
PG Journal Number 18/2014
Publication Date 02-May-2014
Grant Date 29-Apr-2014
Date of Filing 08-Jun-2004
Name of Patentee HOLSET ENGINEERING CO. LIMITED
Applicant Address St. Andrews Road, Huddersfield, HD1 6RA, UK
Inventors:
# Inventor's Name Inventor's Address
1 JAMES A McEWEN C/o. Holset Engineering Co. Limited, St. Andrews Road, Huddersfield, HD1 6RA
PCT International Classification Number F04C 29/02
PCT International Application Number N/A
PCT International Filing date
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 0313399.8 2003-06-11 U.K.