AU451237B2 - Exhaust gas manifold - Google Patents
Exhaust gas manifoldInfo
- Publication number
- AU451237B2 AU451237B2 AU44614/72A AU4461472A AU451237B2 AU 451237 B2 AU451237 B2 AU 451237B2 AU 44614/72 A AU44614/72 A AU 44614/72A AU 4461472 A AU4461472 A AU 4461472A AU 451237 B2 AU451237 B2 AU 451237B2
- Authority
- AU
- Australia
- Prior art keywords
- shell
- sleeves
- outlet conduit
- inlet
- intermediate shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/08—Other arrangements or adaptations of exhaust conduits
- F01N13/10—Other arrangements or adaptations of exhaust conduits of exhaust manifolds
- F01N13/102—Other arrangements or adaptations of exhaust conduits of exhaust manifolds having thermal insulation
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
- Exhaust Gas After Treatment (AREA)
Description
44 614
This invention relates to internal combustion engines, particularly the internal combustion engines in motor vehicles, contribute a substantial amount of exhaust
products to the atmosphere including substantial amounts of the oxides of nitrogen, hydrocarbons and carbon monoxide which are discharged from such engines in the exhaust gases. These pollutants when introduced into the atmosphere in sufficient quantities produce an atmospheric condition referr to as air pollution or smog.
Exhaust manifold gas temperatures will vary from 6000 F. to over 18000 F. depending upon where the temperatures
are measured and the engine operating conditions. If the exhaust gases are permitted to be retained in the manifold at the higher temperatures for a relatively short period of time, and mixed homogeneously with air, the unburned hydrocarbons
and carbon monoxide in the exhaust gases will be oxidized
to thus reduce the amount of such pollutants that are dischar from the manifold. However, with the manifold designs heretofore employed, the mass of the manifold prevents it from being brought up to a high temperature quickly to achieve such oxidation. Further, becaus of its mass, the manifold cannot retain a large volume of the exhaust gases therein so that the gases are not retained therein for a period sufficient to achieve any significant degree of oxidation. 2 451 237
44,614 2
The present invention provides a means.of obtaining
a higher sensible exhaust gas temperature quickly and for increasing the dwell time of the gases in the manifold, thereby providing homogenous mixing of the exhaust gases and air while at the same time providing a lightweight manifold construction which will be able to withstand its inherent expansion and contraction due to the elevated
temperatures caused by the oxidation of the smog-producing
pollutants within the manifold.
In accordance with one form of the invention, there
is provided an outer shell having a plurality of inlet conduits adapted to be connected to the exhaust ports of an internal combustion engine and an outlet conduit adapted to be connected to an exhaust pipe. Carried within said outer shell on a plurality of brackets 4raan intermediate shell comprising a plurality of slidably interfit sleeves with the outer ends of the outermost pair of said sleeves being closed by a pair of end caps. One of the sleeves has an outlet
conduit projecting outwardly therefrom and slidably received
in the outer shell outlet conduit. An inner shell is carried within the intermediate shell and comprises a
plurality of open-ended slidably interfit sleeves. An inlet conduit is fixedly mounted on each pair of inner and
intermediate shell-forming sleeves andis slidably received
in one of the .inlet conduits on said outer shell.
8 451,237
44,61472
Thus, the exhaust gases pass successively through the
inlet conduits, the inner shell, and the intermediate
shell for discharge through the outlet conduits. And with the slidable constructions of the intermediate and inner
shells and inlet and outlet conduits, said intermediate
and inner shells are free to expand and contract with
respect to the outer shell without warping.
The accompanying drawings illustrate the invention.
In such drawings:
Fig. 1 is a longitudinal medial section through an
exhaust gas manifold embodying the invention;
Fig. 2 is an enlarged transverse section taken on
the line 2-2 of Fig. 1;
Fig. 3 is a longitudinal medial section similar to Fig.
1, but showing a modified form of the invention; and
Fig. 4 is an enlarged transverse section taken on
the line 4-4 of Fig. 3.
In the embodiment of the invention as illustrated
in Figs. 1 and 2, the manifold is provided with an outer shell 10 conveniently formed as a pair of metal castings
12 and 13 rigidly interconnected by bolts 14. A plurality of longitudinally spaced inlet conduits 16 project outwardly
from the casting 12 and are provided at their outer ends
with mounting flanges 17 adapted to be connected to the
exhaust ports of an internal combustion engine. An outlet
4 451,237
44,614 2
conduit 20 projects outwardly from the casting 13 and
is provided at its outer end with a mounting flange 21
adapted to be connected to an exhaust pipe. For reasons that will become more apparent hereinafter, a collar 22 is mounted in the outlet 20 and projects radially inwardly
therefrom.
Carried within the outer shell 10 is an intermediate
shell 25 formed from a plurality of longitudinally extending
interfitting sheet-metal sleeves 26, 27, 28 and 29. As shown in Fig. 1, each of the sleeves 26-28 is offset radially
inwardly, as at 30, and a colar 32 is mounted around each such shell in alignment with its offset 30 to define
therewith an annular channel 33. Thus, as shown, sleeve 27 is slidably received in channel 33 on sleeve 26, sleeve
28 is slidably received in channel 33 on sleeve 27, and sleeve 29 is slidably received in channel 33 on sleeve 28. The ends of the shell 25 are closed by a pair of end caps
on the opposed ends of sleeves 26 and 29. Each of the sleeves 26-29 is slidably supported on a plurality of arcuate brackets 37 mounted on the inner face of the
outer shell 10 and projecting radially inwardly therefrom.
Preferably, the brackets 37 are disposed opposite the inlets
56 for the sleeves 26, 27 and 29 for holding said inlets in the outer shell inlets 16. Thus, each of the sleeves is free to expand and contract with respect to each of the S 451, 237
44,614 /72
other sleeves and the outer shell
As shown in Figs. 1 and 2, an outlet opening 39
is formed in sleeve 28. An outlet conduit 40 is mounted in the opening 39 as by having its inner end deformed to
define an annular channel 42 bindingly received over the
circumferential edge of said opening. The conduit projects outwardly from sleeve 28 and is slidably received
in the outlet collar 22 mounted in the outer shell outlet
The conduit 40 and collar 22 also help retain the
inlet 56 on shell 28 in its outer shell inlet 16.
An inner shell 45 is carried within the intermediate
shell 25 and comprises a plurality of longitudinally extending
sheet-metal sleeves 46, 47, 48 and 49 disposed in axial
alignment with the intermediate shell-forming sleeves 26-29,
respectively. As shown in Fig. 1, each of the shells 46-48
is offset radially inwardly at one of its ends,as at 50, and
with each of said offsets being slidably received in the
adjacent end of the next adjacent sleeve to thus permit
each of said sleeves to expand and contract with respect
to each of the other sleeves. The ends of the outermost sleeves 46 and 49 are spaced inwardly from the ends caps
to thus dispose the inner shell 45 in open communication
with the intermediate shell
Each of the sleeves 46-49 is provided with an inlet
451,237
4, 614 2
opening 53 disposed in radial alignment with an inlet
opening 54 formed in each of the sleeves 26-29. An inlet
conduit 56 is connected to each of the sleeves 46-49, and
to this end, the inner end of each of said inlet conduits 56
is deformed to define a channel 58 bindingly received over
the circumferential edges of the openings 53 and 54. The
outer end of each of the inlet conduits 56 is slidably
received in one of the aligned inlet conduits 16 on the
outer shell casting 12.
As shown in Fig. 2, the intermediate and inner shells o'e and 45 a-]/in the form of closed curves and have
elliptical cross-sections. And each of the inner shell-
forming sleeves 46-49 is eccentrically carried within its
associated intermediate shell-forming sleeves 26-29 so that the
sleeves forming the intermediateaid inner shells are
disposed in abutting engagement immediately adjacent their
inlet openings 53 and 54 but are spaced from each other
throughout the remainder of their circumferential extents.
Conveniently, a compressible insulation 60 is interposed
between the outer and intermediate shells 10 and 25 and in
the space between their respective outletconduits 20 and
for thus thermally insulating the outer shell from the
intermediate shell. With the major portion of the inner
shell 45 being spaced from the intermediate shell 25, there
will thus be little thermal conductivity between said inner 7 451,237
44, 614 i2
and outer shells.
In the operation of the manifold shown in Figs. 1 and 2, the exhaust gases enter the manifold through the inlet
cnduits 16 and 56 where they are discharged into the inner
shell 45. The gases exit the inner shell through the
opposed ends of the inner shell sleeves 46 and 49 into the intermediate shell 25 for discharge through the outlet
conduits 20 and 40. With the inner and intermediate shells
being formed of sheet-metal, the exhaust gases will rapidly .bring said shells up to a temperature substantially corres-
ponding to the temperature of the gases entering the mani-
fold. And by reason of the circuitous flow path through the
manifold, said exhaust gases will be retained within the
manifold for a period of time substantially greater than
with a conventional manifold. This increased dwell time at a quickly elevated temperature will cause oxidation
of the pollutants in the exhaust gases. With the spaced relationship between the several shells, the elevated
temperature rithin the inner shell will be maintained
without causing an excessive heating of the outer shell
Further, the sliding sleeved construction of the inner and
intermediate shells permits the inner and outer shells to
freely expand and contract without warping due to
temperature changes within the manifold. S 451,237
44,614 M
The embodiment of the invention illustrated in Figs.
3 and 4 differs from the embodiment shown in Figs. 1 and 2 in the construction of the inner shell. The construction of the outer shell 10' and intermediate shell 25' is identical to that previously described and illustrated in Figs. 1 and
2 of the drawings.
Thus, the outer shell 10' can be formed as a pair of
metal castings 2' and 3' rigidly interconnected by bolts
14'. A plurality of inlet conduits 16' project outwardly
from casting 12', and an outlet conduit 20' projects outwardly
from castings 13'.
The intermediate shell 25', which is carried within and
in spaced relation to the outer shell 10', is insulated from said outer shell by a layer of compressible insulation
The shell 25' is formed from a plurality of longi-
tudinally extending, alidably interfitting, sheet-metal
sleeves 26', 27', 28', and 29'. Each of the sleeves 26'-28' is offset radially inwardly, as at 30', and a collar 32'
extends around each such sleeve in alignment with the offset
therein to define with said offset an annular channel
33'. The adjacent end of the next adjacent sleeve is slidably
received in each of the channels 33' to thus permit said
sleeves to expand and contract with respect to each other. End caps 35' are mounted on the opposite ends of sleeves 26'
and 29' to close the ends of the shell 25'. The sleeves 26' 9 451,237
44614/72
are slidably supported on a plurality of brackets 37'
interposed between the outer and intermeidate shells.
An outlet opening 39' is formed in sleeve 28', and
an outlet conduit 40' is mounted in said openings, as by
having its inner end deformed to form annular channel
bindingly received over the circumferential edge of said
opening. The conduit 40' projects outwardly and is
slidably received in an outlet collar 22' mounted in the
outer shell outlet
An inlet opening 54' is also formed in each of the
sleeves 26'-29', and an inlet conduit 56' is connected to
each of said sleeves as by having its inner end deformed
to define a channel 58' bindingly received over the
circumferential edge of its associated sleeve opening 54'.
The outer end of each of the inlet conduits 56' is slidably
received in one of the aligned inlet conduits 16' .on the
outer shell castings 12' and-the inner end of each of
said conduits is in open communication with an inner shell
The inner shell 45' is carried within the intermediate
shell 25', and comprises a plurality of longitudinally
extending sheet-metal plates 46', 47', 48', and 49'
connected to the inner walls of the intermediate shell-
forming sleeves 26'-29' respectively. As shown, each of
the plates 46'-49' extends diagonally across its associated 451,237
44,614/72
intermediate shell-forming sleeve and is connected
along its longitudinal edges to said sleeve. Each of the plates 47'-49' is offset inwardly at one of its
ends, as at 61. The offset 61 on each of the plates
47'-49', which is not connected to its associated inter-
mediate shell-forming sleeve, is slidably received in the
adjacent end of the next adjacent plate Thus, as shown in
Fig. 3, offset 61 on plate 47' is slidably received in the
adjacent end of plate 47', and offset 61 on plate 49' is
slidably received in the adjacent end of plate 49'. In this manner, each of the plates is free to expand and
contract with its associated intermediate shell-forming
sleeve with respect to the other plates and shell-forming
sleeves as well as the outer shell
The operation of the embodiment illustrated in Figs.
3 and 4 is like that of the embodiment shown in Figs. 1
and 2. That is, the ases enter the manifold through the
inlet conduits *15and56' where they are discharged
into the inner shell 45'. The gases exit said inner shell
at the opposite ends of the inner shell plates 46' and 49'
into the intermediate shell 25' and are discharged through
the outlet conduits 25' and
While the inner shell-forming plates 46'-49' have been
illustrated as being nonperforated, they may, if desired,
have perforations formed therein to thus provide a less 11 451,237
44,61472
restricted gas flow between the inner and intermediate
shells for increasing gas flow rate through the manifold
and reducing back pressure therein.
The embodiments have been illustrated as employing an
outer shell formed as a metal casting. It is to be under-
stood, of course, that said outer shell may be formed
from sheet-metal components if desired. It is also
contemplated that air may be introduced into the manifold
but this may be done in any convenient manner, such as
for example, introducing it with the exhaust gases at the
various manifold inlets connected to the engine exhaust
ports.
12 451,237
Claims (1)
- 44 6 14 2 The claims defining the invention are as follows:1. An exhaust gas manifold for an internal combustionengine, comprising an enclosed outer shell, a plurality offirst inlet conduits and a first outlet conduit on said outershell, an enclosed intermediate shell carried within said outershell, a second outlet conduit on said intermediate shellprojecting outwardly into said first outlet conduit, an innershell carried within said intermediate shell in open communica-tion therewith, means for permitting said intermediate shellto longitudinally expand and contract with respect to saidouter shell, a plurality of second inlet conduits in opencommunication with said inner shell and projecting outwardlyfrom openings formed in said intermediate shell into saidfirst inlet conduits and means for permitting said inner shellto longitudinally expand and contract with respect to saidintermediate shell and said second inlet and outlet conduits.An exhaust gas manifold as set forth in claim 1 withthe -addition that means are provided for supporting saidintermediate shell in spaced relation to said outer shell.3. An exhaust gas manifold as set forth in claim 1 withthe addition that a collar is mounted in said first outletconduit and said second outlet conduit is slidably received insaid collar whereby said first and second outlet conduits aredisposed in spaced relation to each other and said secondoutlet conduit is movable with respect to said first outletconduit.4. An exhaust gas manifold for an internal combustion engine, comprising an enclosed outer shell, a plurality of first inlet conduits and a first outlet conduit on said outer 13 45123744,614 72 shell, an enclosed intermediate shell carried within said outer shell, a second outlet conduit on said intermediate shell projecting outwardly into said first outlet conduit, an inner shell carried within said intermediate shell in open communication therewith, and a plurality of second inlet con- duits in open communication with said inner shell and project- ing outwardly from openings formed in said intermediate shell into said first inlet conduits, each of said intermediate and inner shells comprising a plurality of longitudinally extend- ing slidably interfit sleeves with a pair of caps mounted on the sleeves of.the intermediate shell at the opposite ends thereof.An exhaust gas manifold as set forth in claim 4 in which means are interposed between said outer shell and each of the lsleeves forming the intermediate shell for holding said intermediate and outer shells in spaced relation to each other6. An exhaust gas manifold as set forth in claim 4 in which the outermost ends of the outermost pair of sleeves forming said inner shell are spaced from said pair of end caps7. An exhaust gas manifold for an internal combustion engine, comprising an enclosed outer shell, a plurality of first inlet conduits and a first outlet conduit on said outer shell, an enclosed intermediate shell carried within said outer shell, a second outlet conduit on said intermediate shel projecting outwardly into said first outlet conduit, an innershell carried within said intermediate shell in open communi- cation therewith, said inner shell comprising a plurality of lor itudinally extending sleeves with each of said sleeves being slidably interfit in the next adjacent sleeve, and a 14 451,23744,61472 plurality of second inlet conduits in open communication withsaid inner shell and projecting outwardly from the openingsformed in said intermediate shell into said first inletconduits.8. An exhaust gas manifold for an internal combustionengine, comprising an enclosing outer shell, a plurality offirst inlet conduits and a first outlet conduit on said outer shell, an enclosed intermediate shell carried within said outer shell, a second outlet conduit on said intermediate shell projecting outwardly into said first outlet conduit, an inner shell carried within said intermediate shell in open communi- cation therewith, a plurality of second inlet conduits in open communication with said inner shell and projecting outwardly from openings formed in said intermediate shell into said first inlet conduits, said inner shell comprising a plurality of longitudinally extending sleeves, each of said sleeves being slidably interfit with the next adjacent sleeve, one of said second inlet conduits being in open communication with each of said sleeves, and means on said second inlet conduits for mounting them on said sleeves and interconnecting said sleeves and intermediate shell.9. An exhaust gas manifold for an internal combustion engine, comprising an enclosed outer shell, a plurality of first inlet conduits and a first outlet conduit on said outer shell, an enclosed intermediate shell carried within said outer shell, a second outlet conduit on said intermediate shell projecting outwardly into said first outlet conduit, an inner shell carried within said intermediate shell in open communication therewith, a plurality of second inlet conduits 4 5 1 2, 3 744,614M~ in open communication with said inner shell and projecting outwardly from openings formed in said intermediate shell into said first inlet conduits, each of said intermediate and inner shells comprising a plurality of longitudinally extending slidably interfit sleeves in the form of closed curves, said second inlet conduit being mounted in an inlet opening in one of the Intermediate shell-forming sleeves, each of said second inlet conduits being mounted in aligned inlet openings in the inner and intermediate shell-forming sleeves, each of said inner shell-forming sleeves abutting one of the inter- mediate shell-forming sleeves adjacent their aligned inlet openings, and means on each of said inlet conduits for inter- connecting each pair of inner and intermediate shell-forming sleeves at their aligned inlet openings.An exhaust gas manifold for an internal combustion engine, comprisingwi enclosed outer shell, a plurality of first inlet conduits and a first outlet conduit on said outer shell,. an enclosed intermediate shell carried within said outer shell,.a second outlet condlait on said intermediate shel). projecting outwardly Into said first outlet conduit, an inner shell carried within said intermediate shell in open communication therewith, and a plurality of second inlet con- duits in open comunication with said inner shell and pro- jecting outwardly from openings formed in said intermediate shell into said first Inlet conduit, said intermediate shell comprising a plurality of slidably Interfit sleeves, means closing the ends of said intermediate shell, and said inner shell comprising a plurality of plates mounted in and extend- Ing across said sleeves with each of said plates being slid- 16 451,23744,614 72 ably interfit with the next adjacent plate.11. An exhaust gas manifold as set forth in claim 10 in which the outermost ends of the outermost pair of plates form-ing said inner shell are spaced from said means closing theends of said intermediate shell.12. An exhaust gas manifold as set forth in claim in which at least one of said plates has a plurality ofopenings formed therein.13. An exhaust gas manifold for an internal combustion engine, comprising an enclosed outer shell, a plurality of first inlet conduits and a first outlet conduit on said outershell, an enclosed intermediate shell carried within saidouter shell, a secord outlet conduit on said intermediate shellprojecting outwardly into said first outlet conduit and innershell carried within said intermediate shell in open communi-cation therewith, a plurality of second inlet conduits inopen communication with said inner shell and projecting out-wardly from openings formed in said intermediate shell intosaid first inlet conduits, said intermediate shell comprising a plurality of slidably interfit sbeves, means closing the ends of said intermediate shell, said inner shell comprisinga plurality of plates mounted in and extending across saidsleeves, each of said plates being slidably interfit with the next adjacent plate, said second inlet conduit being mountedon one of said sleeves, and one of said second inlet conduits being mounted on each of said sleeves. I451,23744.614/7 14. An exhaust gas manifold as set forth in claim 1 wit] the addition that said first inlet and outlet conduits aremovable with respect to said second inlet and outlet conduit:respectively.DATED this 25th day of June, 1974.ARVIN INDUSTRIES, INC.EDWD. WATERS SONS, Patent Attorneys, Russell Street, Melbourne, Victoria, AUSTRALIA.6 18 4 51, 23744.61417ZFi .219 451,23744.6 14 m7Fig.-4451.237
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US20449471A | 1971-12-03 | 1971-12-03 | |
| USUS204,494 | 1971-12-03 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU4461472A AU4461472A (en) | 1974-02-21 |
| AU451237B2 true AU451237B2 (en) | 1974-08-01 |
Family
ID=22758137
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU44614/72A Expired AU451237B2 (en) | 1971-12-03 | 1972-07-17 | Exhaust gas manifold |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3775979A (en) |
| JP (1) | JPS5146207B2 (en) |
| AU (1) | AU451237B2 (en) |
| CA (1) | CA961723A (en) |
| DE (1) | DE2238256C3 (en) |
| FR (1) | FR2164263A5 (en) |
| GB (1) | GB1374830A (en) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2201710A5 (en) * | 1972-10-03 | 1974-04-26 | Peugeot & Renault | |
| DE2351979C2 (en) * | 1973-10-17 | 1985-03-21 | Fa. J. Eberspächer, 7300 Esslingen | Reactor for the afterburning of combustible components in exhaust gases from internal combustion engines |
| DE2441655C2 (en) * | 1974-08-30 | 1982-12-09 | Audi Nsu Auto Union Ag, 7107 Neckarsulm | Reactor for an internal combustion engine for the afterburning of unburned components in the exhaust gas |
| CA1048358A (en) * | 1975-04-30 | 1979-02-13 | Shuichi Yamazaki | Exhaust manifold for internal combustion engines |
| US4055043A (en) * | 1975-11-11 | 1977-10-25 | Toyota Jidosha Kogyo Kabushiki Kaisha | Manifold reactor |
| DE2632514C2 (en) * | 1976-07-20 | 1978-06-22 | Bayerische Motoren Werke Ag, 8000 Muenchen | Exhaust gas reactor for internal combustion engines |
| DE2653263C3 (en) * | 1976-11-24 | 1983-05-11 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Exhaust pipe |
| US4182122A (en) * | 1978-02-15 | 1980-01-08 | Caterpillar Tractor Co. | Insulated exhaust manifold |
| US4168610A (en) * | 1978-03-29 | 1979-09-25 | Caterpillar Tractor Co. | Exhaust manifold with reflective insulation |
| DE3445916C1 (en) * | 1984-12-17 | 1986-07-24 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Exhaust pipe for a supercharged, multi-cylinder piston internal combustion engine |
| US4644747A (en) * | 1986-02-10 | 1987-02-24 | General Motors Corporation | Low-stress shielded exhaust passage assemblies |
| DE4207048C1 (en) * | 1992-03-06 | 1993-06-03 | Mtu Friedrichshafen Gmbh | Double wall exhaust pipe for IC engine - has two types of tube sections, with different profiles, with c-profile sections supported on stop edges of inner wall |
| DE19511514C1 (en) * | 1995-03-29 | 1996-08-01 | Daimler Benz Ag | Exhaust manifold for IC engine |
| GB2302366A (en) * | 1995-06-21 | 1997-01-15 | Ford Motor Co | I.c.engine exhaust manifold |
| JPH09125948A (en) * | 1995-10-31 | 1997-05-13 | Toshiomi Hayashi | Method and structure for assembling engine exhaust system piping |
| US6324838B1 (en) * | 1999-10-07 | 2001-12-04 | Metaldyne Tubular Products, Inc. | Flow deflector member for exhaust manifold |
| US20080066465A1 (en) * | 2006-09-20 | 2008-03-20 | Francis Andrew Maidens | Turbocharger header for an internal combustion engine |
| FI125443B (en) * | 2011-08-29 | 2015-10-15 | Wärtsilä Finland Oy | Apparatus for treating exhaust gases of a piston-type combustion engine and a piston-type combustion engine |
| DE102015113137B4 (en) * | 2015-08-10 | 2021-01-14 | Tenneco Gmbh | Exhaust housing |
| DE102022118914A1 (en) * | 2022-07-28 | 2024-02-08 | Purem GmbH | Exhaust gas routing component for an exhaust system of an internal combustion engine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3413803A (en) * | 1967-02-24 | 1968-12-03 | Du Pont | Exhaust manifold reaction system and apparatus |
| US3581494A (en) * | 1970-01-02 | 1971-06-01 | Arvin Ind Inc | Exhaust gas manifold |
| US3633368A (en) * | 1970-08-12 | 1972-01-11 | Du Pont | Exhaust gas reactor |
| US3635031A (en) * | 1970-09-09 | 1972-01-18 | Gen Motors Corp | Exhaust manifold reactor |
-
1971
- 1971-12-03 US US00204494A patent/US3775979A/en not_active Expired - Lifetime
-
1972
- 1972-07-10 CA CA146,714A patent/CA961723A/en not_active Expired
- 1972-07-17 AU AU44614/72A patent/AU451237B2/en not_active Expired
- 1972-07-18 GB GB3348272A patent/GB1374830A/en not_active Expired
- 1972-08-03 DE DE2238256A patent/DE2238256C3/en not_active Expired
- 1972-09-14 JP JP47092734A patent/JPS5146207B2/ja not_active Expired
- 1972-12-01 FR FR7242909A patent/FR2164263A5/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS4864316A (en) | 1973-09-06 |
| AU4461472A (en) | 1974-02-21 |
| FR2164263A5 (en) | 1973-07-27 |
| DE2238256B2 (en) | 1979-01-04 |
| DE2238256A1 (en) | 1973-06-07 |
| GB1374830A (en) | 1974-11-20 |
| US3775979A (en) | 1973-12-04 |
| JPS5146207B2 (en) | 1976-12-08 |
| DE2238256C3 (en) | 1979-08-23 |
| CA961723A (en) | 1975-01-28 |
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