US3765479A - Liquid cooled engine - Google Patents

Liquid cooled engine Download PDF

Info

Publication number
US3765479A
US3765479A US00110727A US3765479DA US3765479A US 3765479 A US3765479 A US 3765479A US 00110727 A US00110727 A US 00110727A US 3765479D A US3765479D A US 3765479DA US 3765479 A US3765479 A US 3765479A
Authority
US
United States
Prior art keywords
conduit
inlet
engine
coolant
passageway
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 - Lifetime
Application number
US00110727A
Inventor
R Fish
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of US3765479A publication Critical patent/US3765479A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/10Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
    • F28D7/106Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically consisting of two coaxial conduits or modules of two coaxial conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • F01N3/04Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust using liquids
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • ABSTRACT A novel engine cooling system which incorporates a special heat exchanger.
  • the heat exchanger replaces the conventional exhaust inlet or inlet manifold of an internal combustion engine.
  • the heat exchanger includes an exhaust conduit having an inlet portion, an intermediate portion and an outlet portion.
  • Encompassing walls define two separate flowpaths for cool- WITH COOLING PASSAGES I O8 ENGINE BLOCK ant such that the coolant is in thermal communication with the exhaust conduit.
  • a first one of these passages extends only over the inlet portion of the exhaust conduit; the other of the coolant passageways extends over the intermediate and outlet portions of the conduit although it can, and, in the embodiment shown, does extend over the inlet portion as well.
  • the heat exchanger is connected to receive exhaust gases from the engine. lts coolant passageways are connected in a circuit which includes an inlet by which make-up water is introduced into a pump which forces fluid through the first passageway of the heat exchanger into the cooling passages of the engine from whence it is circulated back to the inlet side of the pump when the coolant has a temperature below a selected value.
  • the coolant temperature rises above that value, it is permitted to flow past a thermostatic valve to the second coolant passageway of the heat exchanger, after which it is exhausted to the exhaust gas stream.
  • the heat exchanger is oriented so that one portion of the second coolant passageway is disposed above other portions and the conduit is arranged so that flow is confined at one point along the length of the exhaust conduit to flow in the region of that uppermost point whereby the second fluid passageway is maintained substantially full of coolant from that point upstream.
  • One of the objects of the invention is to provide an improved liquid cooling system for engines which combines the engine and its coolant passageways with conduits, pumps, valves and a heat exchange structure ar ranged for preheating liquid coolant before introduction into the engine passages and for cooling the conduit by which exhaust gases are lead from the engine. Provision of that novel structure, and provision of the novel cooling system made possible by its combination with an engine, are both objects of the invention.
  • the invention is not limited to use in connection with inboard marine engines. However, the invention is especially well-adapted for that application. Accordingly, it is one of the objects to provide an improved cooling system circuit and structure for that application.
  • it is advantageous to mount the propulsion engine back adjacent to the transom for direct connection to a steerable propeller drive and propeller. Locating the engine in that fashion introduces a number of problems. Special design is ordinarily required to ensure that the engine structure imposes no serious limitation on the steering system. In addition, space limitations ordinarily require that the engine enclosure be as small as possible and that boat occupants be seated and that gear be placed immediately adjacent to the engine.
  • That spatial limitation gives rise to the requirement that engine heat be minimized by use of an effective and efficient cooling arrangement.
  • the exhaust gases in the case of most engines, are exhausted from a series of space ports. Consequently, the manifold in which they are collected for explusion outside the boat extends substantially over the whole length of the engine and is exposed at the interior of the engine. In the case of V8 engines two such manifolds are employed.
  • One of the objects of the invention is to make it more feasible to employ an engine of conventional design which requires large, exposed exhaust gas collection manifolds.
  • a related object is to provide an engine and engine cooling system for limiting the maximum engine temperature and for greatly reducing exhaust conduit temperature.
  • FIG. 1 is a pictorial view of a marine engine which is fitted with the cooling circuit of the invention including the novel heat exchanger structure that it provides;
  • FIG. 2 is a diagram of the cooling system circuit employed in the engine of FIG. 1;
  • FIG. 3 is a pictorial view of the novel heat exchanger employed in the invention.
  • FIG. 4 is a cross-sectional view taken on line 4--4 of FIG. 3;
  • FIG. 5 is a cross-sectional view taken on line 55 of FIG. 3;
  • FIG. 6 is a cross-sectional view taken on the vertical, longitudinal midplane of the U-shaped portion of the heat exchanger of FIG. 3, except that portions have been cut away to expose the nature of the double walled construction;
  • FIG. 7 is a cross-sectional view taken on line 7-7 of FIG. 6.
  • the engine selected for illustration in FIG. 1 is an internal combustion unit which uses gasoline as fuel and is generally of the same type and style as the engines used in passenger automobiles.
  • the engine is generally designated 10. Its block 12 is provided with internal passageways by which a coolant may flow.
  • a pulley 14 at the lower, forward end of the engine is driven by the engines crankshaft.
  • a belt 16 transmits power from that pulley to a cam driven pump 18 by which coolant is pumped through the system.
  • the numeral 20 designates an air filter; the element 22 is the oil pan.
  • the exhaust manifolds do differ, however. They are heat exchangers. In this case it has been assumed that the engine is of the V8 variety with four exhaust ports at the right and four at the left.
  • the right exhaust manifold heat exchanger structure is designated by the numeral 24 and the left one is designated 26.
  • the exhaust gas is expelled from the heat exchanger through a flexible conduit 28 through an opening in the boats transom.
  • the boats transom was omitted from FIG. 1 so that the propeller 30 and the propeller drive housing 32 would be visible.
  • a part 34 of the transmission s system is mounted forward to the transom and the remainder is mounted behind it.
  • the transom is placed just rearward of the U-shaped portions 36 and 38 of the two heat exchangers.
  • the boat may be steered by pivoting the propeller drive housing 32 about a pivot axis rearward of the transom.
  • the force by which it is made to pivot is applied to a tiller arm 40 which is arranged to extend through or over the transom.
  • Steering cables 42 extend in opposite directions from a connection to the end of the tiller bar 40 through the spaces defined by the U- shaped rear sections 36 and 38 of the two heat exchangers. Guides for those cables are attached to the housing within those spaces. This arrangement is particularly advantageous.
  • the U-shape of the heat exchanger structure is doubly functional in that it ensures a generally uniform high degree of exhaust gas cooling, as well as providing protection for, and against, the tiller bar while providing a high order of stability for the steering cable system in the region of tiller bar movement.
  • the heat exchangers both include a passageway or conduit for exhaust gases and two liquid coolant passageways.
  • the inner exhaust conduit is jacketed to form a double walled arrangement. Exhaust gases flow in the conduit defined by the inner wall and the cooling liquid flows in the space between the double walls. That space is divided by blocking walls into two flowpaths.
  • the exhaust conduit is connected to the exhaust ports of the engine by laterally and downwardly extending connecting conduits that are not visible in FIG. 1. They can be seen in FIG. 3 and one of them is shown in crosssection in FIG. 5.
  • the exhaust conduit extends over the length of the engine and through the U-shaped section of the heat exchanger housing to an exit point at its junction with the flexible conduit 28.
  • One of the liquid passageways extends only part way over the length of the exhaust conduit. It extends over that part, called the inlet region, where the exhaust gases are collected.
  • Flow lines connected to the exchanger structure at both ends of that passage are connected at thier opposite ends to fittings at the forward end of the engine block.
  • the two conduits associated with heat exchanger 26 are identified in FIG. 1 by the reference numerals 44 and 46.
  • Another conduit 48 interconnects the inner passages of the engine block with the other liquid flow passage in exchanger 26. That passageway has an outlet near the outlet of the exchanger at the point of its connection with flexible conduit 28.
  • FIG. 2 The interconnection of the engine pump, control valve, and the several conduits with the passageways of the manifold structure is illustrated in FIG. 2.
  • the engine block and its cooling passages are illustrated by a block 50.
  • the engine block is provided with four exhaust gas outlet ports on each side. For identification, one of those outlet ports has been designated 52 in FIG. 2.
  • the lateral, connecting conduit 54 leads from that exhaust port opening to a port 56 which opens to the interior of the heat exchange structure 24.
  • the preferred arrangement is illustrated in detail in FIG. 5.
  • Pump 18 of FIG. 2 is the same one designated 18 in FIG. 1.
  • the exhaust gases are collected in the exhaust conduit which is formed by an inner wall generally designated 58 in FIG. 2. Those gases pass through the conduit moving rearwardly through the U-shaped section 36 of the structure and then emerge at the junction with the flexible conduit 60.
  • the latter is like the flexible conduit 28 with the exception that it is connected to the other of the two heat exchangers.
  • the exhaust conduit portion of the exchanger is conveniently considered to comprise three portions.
  • the first is called an inlet portion and is that portion of the conduit in which the exhaust gases are collected.
  • the numeral 62 in the case of U shaped member 38, and the numeral 64 in the case of U-shaped member 36, identify a dam in one of the two liquid flow passageways.
  • The'portion of the exhaust conduit which lies upstream from the vicinity of that dam, and downstream from the inlet portion is called the intermediate portion. That portion of the exhaust conduit which lies downstream from the vicinity of the dam is called the exhaust or outlet portion.
  • the liquid passageways are formed by the double walls of the exchanger structure.
  • the inner walls are generally designated 58.
  • the inner wall 58 defines a passageway in which cooling liquid is preheated.
  • This passageway, numbered 68, is called the preheating passageway.
  • Another portion of the outer wall cooperates with wall 58 to define a second passageway for liquid coolant which is called the exhaust conduit cooling passageway" or cooling passageway 72.
  • the preheating passageway extends approximately the length of the inlet portion of the exhaust conduit.
  • the cooling passageway extends over the intermediate portion of the exhaust conduit and over at least part of the exhaust portion of that conduit.
  • the cooling passageway 72 extends substantially entirely around the exhaust conduit and the passageway has been extended in the diagram to the inner region of the U- shaped section 76 to illustrate that this is so.
  • walls that define the exhaust conduit are generally designated 74.
  • the wall that cooperates with that inner conduit to form the exhaust conduit cooling passage 76 is desig- I nated 78.
  • the wall that cooperates with inner wall 74 to form the precooling passageway 80 is designated by reference numeral 82.
  • the inlet to that passage is designated 83 and the outlet is numbered 84.
  • the inlet 85 of the exhaust conduit cooling passageway is at the forward end of the structure and the outlet 86 is at the rearward end adjacent the connection with the flexible conduit 28.
  • the precooling passageway has an inlet 86 and an outlet 87.
  • the exhaust conduit cooling passageway has an inlet 88 and an outlet 89.
  • the engine block cooling passage system includes inlets 91 and 92. It includes a recirculation outlet 90, a primary outlet 94 and a safety bypass passageway 95. That outlet bypasses the thermostatic valve 96. That valve is connected in series between outlets 94 and the inlets 85 and 88 of the two exhaust conduit passageways. Valve 96 and inlet 85 are interconnected by the conduit 48 which was visible in FIG. 1. The valve 96 and inlet 88 are connected by a conduit 98. Outlet 84 and engine block unit 92 are interconnected by the conduit 46. On the other side of the engine, engine block inlet 91 and precooling passage outlet 87 are interconnected by a conduit 100.
  • the outlet side of pump 18 is connected to precooling passageway 80 by the conduit 44 and is connected to the inlet opening 86 of the other precooling passageway by a conduit 102.
  • Cooling water either sea water or fresh water, enters the system at an inlet 104 and is conducted by a passageway 106 to the inlet side of pump 108.
  • the recirculation outlet is connected by a conduit 108 back to the inlet side of the pump.
  • that cooling water has reached a temperature sufficiently high to open the thermostatic valve 96 it exits the engine at outlet and travels by conduit 108 to the junction with conduit 106. Thereafter, it again flows to the inlet section of pump 18 to be recirculated through the preheating passageways 80 and 68.
  • the cooling circuit arrangement offers a number of advantages. It is desirable to have the heat rise in the engine block occur as uniformly as possible following engine start-up.
  • the invention helps to achieve that result by precirculating the water contained in the engine block past the hottest portion, the inlet portion, of the exhaust conduit. In the preferred form, that passageway is limited substantially to the inlet portion of the exhaust conduit as illustrated in FIG. 2. It will be shown subsequently, in examination of FIG. 5, that the preheating passageway encompasses a larger portion of the inlet portion of the exhaust conduit than does the cooling passageway. The result is rapid preheating of the cooling water. During initial operation that feature helps raise engine block temperature uniformly and rapidly.
  • a further advantage is that the coolant that flows through the preheated passageway derives its heat from the hottest part of the exhaust conduit so that excessive heat rise is avoided.
  • the engine occupies a premium space.
  • the engines themselves are available in compact form.
  • the space that must be devoted to the engine is function not only of engine size but is also a function of engine temperature. If the temperature can be minimized, the size of the engine compartment 0r enclosure can be reduced. In large mea.
  • the size of that compartment is determined by maximum engine temperature rather than by average temperature. Accordingly, it is desirable to provide an engine cooling system which minimizes peak temperature as well as average temperature. Efficiency demands that the cooling system contribute to engine warm-up. Within the engine itself, these antithetical requirements are dealt with by the thermostatic valve. In this case, it is desired not only to control block temperature but also to control exhaust conduit temperature. Here, too, the requirements are different during the start-up and the run condition. In this case, the invention solves the problem by the special arrangement of its exhaust manifold and heat exchange structure and by the combination with that structure of the thermostatic valve and the flow circuit arrangement. During the start-up period, the short but large area preheating passageway provides the heat input necessary to ensure the requisite degree of block temperature uniformity.
  • the preheating passageway is assisted in its function by the thermostatic valve which ensures recirculation of the coolant with minimum introduction of cold water. After the engine is heated, the coolant is expelled from the system and new coolant is introduced. That new coolant has a much lower temperature and serves to carry away large quantities of heat from the hottest, inlet section of the exhaustconduit.
  • the cooling passage of the exchanger is supplied with coolant only after the engine is heated. It completely surrounds the intermediate portion of the exhaust conduit to ensure that a maximum volume of water is exposed, through a maximum heat exchange surface, to the heat of the exhaust gases.
  • the cooling passage is extended forwardly adjacent the inlet portion of the exhaust passage to the extent that the surface area of the exhaust conduit does not need to be encompassed by the preheating conduit.
  • approximately onefourth of the conduit wall in the inlet portion forms a part of the cooling passageway while three-fourths of that wall forms a part of the preheating passageway.
  • the heat exchange structure is oriented so that dams 62 and 64 are at an uppermost point thereby to ensure that the passageway is completely filled with coolant upstream from that point. Below the dam, the coolant is finally expelled into the stream of exhaust gases, cooling those gases sufficiently so that flexible conduit of conventional material can withstand their temperatures.
  • FIGS. 3 through 7. A preferred heat exchange structure is shown in FIGS. 3 through 7.
  • the whole structure 24 is shown in FIG. 3. It comprises a straight section 110, having an end closure 112 at its forward end, and the U-shaped section 36 at its rearmost end.
  • the three sections are cast separately and are bolted together.
  • Bolts 114 connect the forward closure to the straight section 112 and the bolts 116 connect the U-shaped section to the straight section.
  • the conduit 54 is the one that was identified in connection with the description of FIG. 2 and is the one shown in cross-section in FIG. 5.
  • the exit opening for the exhaust conduit is designated 118 and it is on this element that the flexible conduit 60 is fitted.
  • the flexible conduit has been omitted from the figure so that the outlet opening 86 of the coolant passage is made visible.
  • the threaded boss 120 which can be seen on the upper inner surface of the U-shaped section 36, accommodates a fitting through which the steering cable is run.
  • the numeral 122 identifies a drain port for the cooling passageway.
  • elbow 124 is connected to the inlet opening and forms part of conduit 48.
  • the nipple 126 forms part of the coolant passage outlet opening 84.
  • the cooling passage extends over the length of the straight section 112' and it continues into the lower forward portion of the U-shaped section 36. Except in the region of the four passageways by which exhaust gases are admitted into the exchanger, the preheating passageway extends between the double walls of the structure at its sides and at its bottom.
  • the exhaust conduit is defined by the inner walls 58.
  • the cooling passageway is defined by the lower one and the side ones of those inner walls and by the outer walls 66 at the sides and the bottom of the structure.
  • the coolant passage is the upper one in FIG. and is defined by the upper wall 58 at its inside and the wall 70 at its outside.
  • the passageway is necked down at 130 because the outer wall is indented to accommodate the bolts 114.
  • the rearmost region of the precooling passage is shown at the lower left in FIG. 6.
  • the cross-sectional view in that figure is taken on the vertical, longitudinal midplane of the U-shaped section 36.
  • the far wall of this structure is double; part of it has been broken away to make it clear that the upper section of wall 58 extends throughout the length of the precooling passageway with respect to the coolant passageway even though the exhaust conduit turns upwardly and continues through portion 58a of that wall.
  • the inner wall has been broken away above the Webb 58a to show that from that point on downstream all of the space between the inner and outer walls is part of the cooling passageway.
  • a dam is formed transversely across that flow passage on the plane 7--7 of FIG. 6.
  • the dam is formed by a webb that interconnects the inner and outer walls except at the upper portion of the space between them.
  • the edge of the dam visible in FIG. 6 is designated 140.
  • FIG. 7 is a cross-sectional view taken on line 7--7 which illustrates this construction. Below the dam the cooling passageway encompasses the exhaust conduit over most of its area so that additional cooling is accomplished.
  • the dam is located at the highest point in the coolant flowpath so that the flowpath must be completely filled upstream from that point. Removal of the dam from that high point does not destroy the value of the invention although efficiency would be lowered somewhat.
  • the dam may haveany convenient form. Thus, it could comprise any kind of structural division of the coolant passageway into upstream and downstream sections interconnected at an elevated point.
  • a heat exchanger comprising an exhaust conduit formed by an encompassing wall and defining an inlet portion for receiving exhaust gas from the engine exit port, an intermediate portion, and an outlet end portion for discharging exhaust gas that has traversed said intermediate portion after entering at the inlet portion;
  • a jacket comprising said encompassing wall and an overlying outer wall, said jacket being formed to define two passageways capable of conducting liquid coolant, one of said passageways extending over the inlet portion of said exhaust conduit, the other one of said passageways extending over the intermediate portion of said exhaust conduit;
  • said jacket further comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an initial portion of its length before fluid can be discharged from said outlet opening.
  • said jacket comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an upstream portion of its length, said means comprising mounting means for mounting said conduit with one portion of said other one of said passageways uppermost and of dam means in the form of a darn interconnecting said inner and outer walls except in the region of said one portion of said other of said passageways for confining flow to that one portion.
  • an elongate exhaust conduit comprising an inlet section, an intermediate section and an outlet section, said conduit being formed with openings in its inlet section by which exhaust gases may be admitted thereto so that they will traverse the conduit from its inletsection through its intermediate section to be expelled at said outlet section;
  • means comprising a first enclosing wall overlying portions of said exhaust conduit at its inlet section and defining'a first passageway for coolant having inlet and outlet openings;
  • conduit comprises a horizontal section and an inverted U- shaped section, said first enclosing wall overlying the horizontal section and said second enclosing wall overlying the inverted U-shaped section.
  • said U- shaped section comprises a double-walled jacket and said means for confining the flow to said one portion of said'second passageway comprises a dam disposed between the walls of the conduit and the second overlying wall except at an upper region of said U-shaped sec tion.
  • the invention defined in claim 9 which further comprises an inlet conduit for make-up water connected to the inlet side of said pump, means interconnecting the passageways of the engine with the inlet side of said pump, said means for permitting flow of coolant from the engine passageways to said second conduit comprising a thermostatic valve.

Abstract

A novel engine cooling system which incorporates a special heat exchanger. The heat exchanger replaces the conventional exhaust inlet or inlet manifold of an internal combustion engine. The heat exchanger includes an exhaust conduit having an inlet portion, an intermediate portion and an outlet portion. Encompassing walls define two separate flowpaths for coolant such that the coolant is in thermal communication with the exhaust conduit. A first one of these passages extends only over the inlet portion of the exhaust conduit; the other of the coolant passageways extends over the intermediate and outlet portions of the conduit although it can, and, in the embodiment shown, does extend over the inlet portion as well. The heat exchanger is connected to receive exhaust gases from the engine. Its coolant passageways are connected in a circuit which includes an inlet by which make-up water is introduced into a pump which forces fluid through the first passageway of the heat exchanger into the cooling passages of the engine from whence it is circulated back to the inlet side of the pump when the coolant has a temperature below a selected value. When the coolant temperature rises above that value, it is permitted to flow past a thermostatic valve to the second coolant passageway of the heat exchanger, after which it is exhausted to the exhaust gas stream. The heat exchanger is oriented so that one portion of the second coolant passageway is disposed above other portions and the conduit is arranged so that flow is confined at one point along the length of the exhaust conduit to flow in the region of that uppermost point whereby the second fluid passageway is maintained substantially full of coolant from that point upstream.

Description

Unite @fiates E teiit- [191 Fish [ Oct. 16, 1973 LIQUID COOLED ENGINE [76] Inventor: Robert F. Fish, 877 W. 17th St.,
Costa Mesa, Calif.
[22] Filed: Jan. 28, 1971 [21] Appl. No.: 110,727
Primary ExaminerCharles Sukalo Attorney-Nienow & Frater [57] ABSTRACT A novel engine cooling system which incorporates a special heat exchanger. The heat exchanger replaces the conventional exhaust inlet or inlet manifold of an internal combustion engine. The heat exchanger includes an exhaust conduit having an inlet portion, an intermediate portion and an outlet portion. Encompassing walls define two separate flowpaths for cool- WITH COOLING PASSAGES I O8 ENGINE BLOCK ant such that the coolant is in thermal communication with the exhaust conduit. A first one of these passages extends only over the inlet portion of the exhaust conduit; the other of the coolant passageways extends over the intermediate and outlet portions of the conduit although it can, and, in the embodiment shown, does extend over the inlet portion as well. The heat exchanger is connected to receive exhaust gases from the engine. lts coolant passageways are connected in a circuit which includes an inlet by which make-up water is introduced into a pump which forces fluid through the first passageway of the heat exchanger into the cooling passages of the engine from whence it is circulated back to the inlet side of the pump when the coolant has a temperature below a selected value. When the coolant temperature rises above that value, it is permitted to flow past a thermostatic valve to the second coolant passageway of the heat exchanger, after which it is exhausted to the exhaust gas stream. The heat exchanger is oriented so that one portion of the second coolant passageway is disposed above other portions and the conduit is arranged so that flow is confined at one point along the length of the exhaust conduit to flow in the region of that uppermost point whereby the second fluid passageway is maintained substantially full of coolant from that point upstream.
11 Claims, 7 Drawing Figures PAIENTEDncI 16 I975 sum 1 OF 3 INVENTOR ROBERT F. FISIH ENGINE. BLOCK 54 5 WITH COOLING 94 PASSAGES BY w HM ATTORNEYS PATENTEDUCI 16 ms 3, 765479 SHEET 2 BF 5 INVENTOR ROBERT F FISH ATTORNEYS PATENTED OCT 16 I975 3.765.419 SHEET 3 SF 3 ATTORNEYS LIQUID COOLED ENGINE This invention relates to improvements in liquid cooled engines and it relates particularly to an improved engine for marine application.
One of the objects of the invention is to provide an improved liquid cooling system for engines which combines the engine and its coolant passageways with conduits, pumps, valves and a heat exchange structure ar ranged for preheating liquid coolant before introduction into the engine passages and for cooling the conduit by which exhaust gases are lead from the engine. Provision of that novel structure, and provision of the novel cooling system made possible by its combination with an engine, are both objects of the invention.
It will be apparent that the invention is not limited to use in connection with inboard marine engines. However, the invention is especially well-adapted for that application. Accordingly, it is one of the objects to provide an improved cooling system circuit and structure for that application. In certain classes of boats, it is advantageous to mount the propulsion engine back adjacent to the transom for direct connection to a steerable propeller drive and propeller. Locating the engine in that fashion introduces a number of problems. Special design is ordinarily required to ensure that the engine structure imposes no serious limitation on the steering system. In addition, space limitations ordinarily require that the engine enclosure be as small as possible and that boat occupants be seated and that gear be placed immediately adjacent to the engine. That spatial limitation gives rise to the requirement that engine heat be minimized by use of an effective and efficient cooling arrangement. The exhaust gases, in the case of most engines, are exhausted from a series of space ports. Consequently, the manifold in which they are collected for explusion outside the boat extends substantially over the whole length of the engine and is exposed at the interior of the engine. In the case of V8 engines two such manifolds are employed. One of the objects of the invention is to make it more feasible to employ an engine of conventional design which requires large, exposed exhaust gas collection manifolds. A related object is to provide an engine and engine cooling system for limiting the maximum engine temperature and for greatly reducing exhaust conduit temperature.
These and other objects and advantages of the invention are realized by the combination with an engine of the kind that has exhaust ports and internal passageways for fluid coolant of a heat exchanger means comprising an exhaust gas conduit formed by an inner wall and extending from the region of the engine exhaust ports to an intermediate gas flow conducting portion and then to an outlet section for discharging that exhaust gas and, which further comprises a jacket formed by said inner wall and an overlying outer wall, the outer wall being arranged to define two separate passageways FIG. 1 is a pictorial view of a marine engine which is fitted with the cooling circuit of the invention including the novel heat exchanger structure that it provides;
FIG. 2 is a diagram of the cooling system circuit employed in the engine of FIG. 1;
FIG. 3 is a pictorial view of the novel heat exchanger employed in the invention;
FIG. 4 is a cross-sectional view taken on line 4--4 of FIG. 3;
FIG. 5 is a cross-sectional view taken on line 55 of FIG. 3;
FIG. 6 is a cross-sectional view taken on the vertical, longitudinal midplane of the U-shaped portion of the heat exchanger of FIG. 3, except that portions have been cut away to expose the nature of the double walled construction; and
FIG. 7 is a cross-sectional view taken on line 7-7 of FIG. 6.
The engine selected for illustration in FIG. 1 is an internal combustion unit which uses gasoline as fuel and is generally of the same type and style as the engines used in passenger automobiles. The engine is generally designated 10. Its block 12 is provided with internal passageways by which a coolant may flow. A pulley 14 at the lower, forward end of the engine is driven by the engines crankshaft. A belt 16 transmits power from that pulley to a cam driven pump 18 by which coolant is pumped through the system. The numeral 20 designates an air filter; the element 22 is the oil pan.
Thus far described the unit does not differ materially from an ordinary automobile engine. The exhaust manifolds do differ, however. They are heat exchangers. In this case it has been assumed that the engine is of the V8 variety with four exhaust ports at the right and four at the left. The right exhaust manifold heat exchanger structure is designated by the numeral 24 and the left one is designated 26. In this embodiment the exhaust gas is expelled from the heat exchanger through a flexible conduit 28 through an opening in the boats transom.
The boats transom was omitted from FIG. 1 so that the propeller 30 and the propeller drive housing 32 would be visible. A part 34 of the transmission s system is mounted forward to the transom and the remainder is mounted behind it. Thus, the transom is placed just rearward of the U-shaped portions 36 and 38 of the two heat exchangers.
The boat may be steered by pivoting the propeller drive housing 32 about a pivot axis rearward of the transom. The force by which it is made to pivot is applied to a tiller arm 40 which is arranged to extend through or over the transom. Steering cables 42 extend in opposite directions from a connection to the end of the tiller bar 40 through the spaces defined by the U- shaped rear sections 36 and 38 of the two heat exchangers. Guides for those cables are attached to the housing within those spaces. This arrangement is particularly advantageous. The U-shape of the heat exchanger structure is doubly functional in that it ensures a generally uniform high degree of exhaust gas cooling, as well as providing protection for, and against, the tiller bar while providing a high order of stability for the steering cable system in the region of tiller bar movement.
The heat exchangers both include a passageway or conduit for exhaust gases and two liquid coolant passageways. The inner exhaust conduit is jacketed to form a double walled arrangement. Exhaust gases flow in the conduit defined by the inner wall and the cooling liquid flows in the space between the double walls. That space is divided by blocking walls into two flowpaths. The exhaust conduit is connected to the exhaust ports of the engine by laterally and downwardly extending connecting conduits that are not visible in FIG. 1. They can be seen in FIG. 3 and one of them is shown in crosssection in FIG. 5. The exhaust conduit extends over the length of the engine and through the U-shaped section of the heat exchanger housing to an exit point at its junction with the flexible conduit 28. One of the liquid passageways, in this embodiment, extends only part way over the length of the exhaust conduit. It extends over that part, called the inlet region, where the exhaust gases are collected. Flow lines connected to the exchanger structure at both ends of that passage are connected at thier opposite ends to fittings at the forward end of the engine block. The two conduits associated with heat exchanger 26 are identified in FIG. 1 by the reference numerals 44 and 46. Another conduit 48 interconnects the inner passages of the engine block with the other liquid flow passage in exchanger 26. That passageway has an outlet near the outlet of the exchanger at the point of its connection with flexible conduit 28.
The interconnection of the engine pump, control valve, and the several conduits with the passageways of the manifold structure is illustrated in FIG. 2. In that figure, the engine block and its cooling passages are illustrated by a block 50. The engine block is provided with four exhaust gas outlet ports on each side. For identification, one of those outlet ports has been designated 52 in FIG. 2. The lateral, connecting conduit 54 leads from that exhaust port opening to a port 56 which opens to the interior of the heat exchange structure 24. The preferred arrangement is illustrated in detail in FIG. 5.
Pump 18 of FIG. 2 is the same one designated 18 in FIG. 1. The exhaust gases are collected in the exhaust conduit which is formed by an inner wall generally designated 58 in FIG. 2. Those gases pass through the conduit moving rearwardly through the U-shaped section 36 of the structure and then emerge at the junction with the flexible conduit 60. The latter is like the flexible conduit 28 with the exception that it is connected to the other of the two heat exchangers.
The exhaust conduit portion of the exchanger is conveniently considered to comprise three portions. The first is called an inlet portion and is that portion of the conduit in which the exhaust gases are collected. In
general, that part extends from the forward end of the exhaust conduit to a point just downstream of the rearmost of the exhaust inlet openings. The numeral 62 in the case of U shaped member 38, and the numeral 64 in the case of U-shaped member 36, identify a dam in one of the two liquid flow passageways. The'portion of the exhaust conduit which lies upstream from the vicinity of that dam, and downstream from the inlet portion is called the intermediate portion. That portion of the exhaust conduit which lies downstream from the vicinity of the dam is called the exhaust or outlet portion.
The liquid passageways are formed by the double walls of the exchanger structure. In the case of manifold 24 the inner walls are generally designated 58. Together with a portion of the outer wall that is identified by the reference numeral 66, the inner wall 58 defines a passageway in which cooling liquid is preheated. This passageway, numbered 68, is called the preheating passageway. Another portion of the outer wall cooperates with wall 58 to define a second passageway for liquid coolant which is called the exhaust conduit cooling passageway" or cooling passageway 72. In this embodiment the preheating passageway extends approximately the length of the inlet portion of the exhaust conduit. The cooling passageway extends over the intermediate portion of the exhaust conduit and over at least part of the exhaust portion of that conduit. It may, and in this embodiment it does, extend over the inlet portion of the exhaust conduit as well. In the intermediate portion of the exhaust conduit, the cooling passageway 72 extends substantially entirely around the exhaust conduit and the passageway has been extended in the diagram to the inner region of the U- shaped section 76 to illustrate that this is so.
The arrangement of the other exhaust manifold structure 26 is similar. For identification, walls that define the exhaust conduit are generally designated 74. The wall that cooperates with that inner conduit to form the exhaust conduit cooling passage 76 is desig- I nated 78. The wall that cooperates with inner wall 74 to form the precooling passageway 80 is designated by reference numeral 82. The inlet to that passage is designated 83 and the outlet is numbered 84. The inlet 85 of the exhaust conduit cooling passageway is at the forward end of the structure and the outlet 86 is at the rearward end adjacent the connection with the flexible conduit 28. In the lower part of FIG. 2 the precooling passageway has an inlet 86 and an outlet 87. The exhaust conduit cooling passageway has an inlet 88 and an outlet 89. The engine block cooling passage system includes inlets 91 and 92. It includes a recirculation outlet 90, a primary outlet 94 and a safety bypass passageway 95. That outlet bypasses the thermostatic valve 96. That valve is connected in series between outlets 94 and the inlets 85 and 88 of the two exhaust conduit passageways. Valve 96 and inlet 85 are interconnected by the conduit 48 which was visible in FIG. 1. The valve 96 and inlet 88 are connected by a conduit 98. Outlet 84 and engine block unit 92 are interconnected by the conduit 46. On the other side of the engine, engine block inlet 91 and precooling passage outlet 87 are interconnected by a conduit 100. The outlet side of pump 18 is connected to precooling passageway 80 by the conduit 44 and is connected to the inlet opening 86 of the other precooling passageway by a conduit 102. Cooling water, either sea water or fresh water, enters the system at an inlet 104 and is conducted by a passageway 106 to the inlet side of pump 108. The recirculation outlet is connected by a conduit 108 back to the inlet side of the pump.
Make-up water enters in at inlet 104 and proceeds by conduit 106 to the inlet side of pump 18 where it is forced through conduits 44 and 102 to enter into the precooling passageways 80 and 68. The water flows through those passageways and emerges at outlets 84 and 87. It then proceeds by conduits 46 and 100 to engine - block inlets 92 and 91, respectively. Until that cooling water has reached a temperature sufficiently high to open the thermostatic valve 96, it exits the engine at outlet and travels by conduit 108 to the junction with conduit 106. Thereafter, it again flows to the inlet section of pump 18 to be recirculated through the preheating passageways 80 and 68. When this circulating water has reached a temperature sufficiently high to open the thermostatic valve 96, then the water is free to flow from the engine to conduits 48 and 98 to inlets 85 and 88 of the two exhaust conduit cooling passageways 76 and 72. Those passageways must become entirely filled with water downstream of their respective dams 62 and 64, before any of the water they contain can be expelled to that portion of the passageway that surrounds the outlet section of the exhaust conduit. This result is achieved by providing the heat exchange structure with a downstream section that is placed generally above and higher than any other section of the exhaust system. That section could be U-shaped, V- shaped, or otherwise shaped to accomplish that result. In the preferred embodiment, the U-shape is employed because it provides a number of advantages. It removes the cooling function to the very rear of the boat, or at least to the rear of the engine; it provides a very effective and efficient means for protecting the tiller linkage and for guiding the steering cables; and it has certain manufacturing advantages.
The cooling circuit arrangement offers a number of advantages. It is desirable to have the heat rise in the engine block occur as uniformly as possible following engine start-up. The invention helps to achieve that result by precirculating the water contained in the engine block past the hottest portion, the inlet portion, of the exhaust conduit. In the preferred form, that passageway is limited substantially to the inlet portion of the exhaust conduit as illustrated in FIG. 2. It will be shown subsequently, in examination of FIG. 5, that the preheating passageway encompasses a larger portion of the inlet portion of the exhaust conduit than does the cooling passageway. The result is rapid preheating of the cooling water. During initial operation that feature helps raise engine block temperature uniformly and rapidly. Subsequently, it minimizes extreme thermal differences by preventing direct introduction into the heated block of very much colder sea water. A further advantage is that the coolant that flows through the preheated passageway derives its heat from the hottest part of the exhaust conduit so that excessive heat rise is avoided.
In most small boat designs, the engineoccupies a premium space. The engines themselves are available in compact form. However, the space that must be devoted to the engine is function not only of engine size but is also a function of engine temperature. If the temperature can be minimized, the size of the engine compartment 0r enclosure can be reduced. In large mea.
sure, the size of that compartment is determined by maximum engine temperature rather than by average temperature. Accordingly, it is desirable to provide an engine cooling system which minimizes peak temperature as well as average temperature. Efficiency demands that the cooling system contribute to engine warm-up. Within the engine itself, these antithetical requirements are dealt with by the thermostatic valve. In this case, it is desired not only to control block temperature but also to control exhaust conduit temperature. Here, too, the requirements are different during the start-up and the run condition. In this case, the invention solves the problem by the special arrangement of its exhaust manifold and heat exchange structure and by the combination with that structure of the thermostatic valve and the flow circuit arrangement. During the start-up period, the short but large area preheating passageway provides the heat input necessary to ensure the requisite degree of block temperature uniformity. The preheating passageway is assisted in its function by the thermostatic valve which ensures recirculation of the coolant with minimum introduction of cold water. After the engine is heated, the coolant is expelled from the system and new coolant is introduced. That new coolant has a much lower temperature and serves to carry away large quantities of heat from the hottest, inlet section of the exhaustconduit. The cooling passage of the exchanger is supplied with coolant only after the engine is heated. It completely surrounds the intermediate portion of the exhaust conduit to ensure that a maximum volume of water is exposed, through a maximum heat exchange surface, to the heat of the exhaust gases. The cooling passage is extended forwardly adjacent the inlet portion of the exhaust passage to the extent that the surface area of the exhaust conduit does not need to be encompassed by the preheating conduit. In this embodiment, approximately onefourth of the conduit wall in the inlet portion forms a part of the cooling passageway while three-fourths of that wall forms a part of the preheating passageway. The heat exchange structure is oriented so that dams 62 and 64 are at an uppermost point thereby to ensure that the passageway is completely filled with coolant upstream from that point. Below the dam, the coolant is finally expelled into the stream of exhaust gases, cooling those gases sufficiently so that flexible conduit of conventional material can withstand their temperatures.
A preferred heat exchange structure is shown in FIGS. 3 through 7. The whole structure 24 is shown in FIG. 3. It comprises a straight section 110, having an end closure 112 at its forward end, and the U-shaped section 36 at its rearmost end. The three sections are cast separately and are bolted together. Bolts 114 connect the forward closure to the straight section 112 and the bolts 116 connect the U-shaped section to the straight section. There are four inlet conduits that afford communication for exhaust gases from the exit ports of the engine to the inlet section of the exhaust conduit. The conduit 54 is the one that was identified in connection with the description of FIG. 2 and is the one shown in cross-section in FIG. 5. The exit opening for the exhaust conduit is designated 118 and it is on this element that the flexible conduit 60 is fitted. The flexible conduit has been omitted from the figure so that the outlet opening 86 of the coolant passage is made visible. The threaded boss 120, which can be seen on the upper inner surface of the U-shaped section 36, accommodates a fitting through which the steering cable is run. Just below that, the numeral 122 identifies a drain port for the cooling passageway. At the front closure 112, elbow 124 is connected to the inlet opening and forms part of conduit 48. Just below, the nipple 126 forms part of the coolant passage outlet opening 84.
In this embodiment, the cooling passage extends over the length of the straight section 112' and it continues into the lower forward portion of the U-shaped section 36. Except in the region of the four passageways by which exhaust gases are admitted into the exchanger, the preheating passageway extends between the double walls of the structure at its sides and at its bottom. Thus, in FIG. 5 the exhaust conduit is defined by the inner walls 58. The cooling passageway is defined by the lower one and the side ones of those inner walls and by the outer walls 66 at the sides and the bottom of the structure. The coolant passage is the upper one in FIG. and is defined by the upper wall 58 at its inside and the wall 70 at its outside. The passageway is necked down at 130 because the outer wall is indented to accommodate the bolts 114.
That the two passageways are separated is illustrated by the cross-sectional, pictorial view of end member 1 12 in FIG. 4. The slot 132 communicates only with the upper coolant passage of the straight section 110 and with the elbow 124. On the other hand, nipple 126 communicates with the bottom and the side openings that comprise the precooling passageways 68.
The rearmost region of the precooling passage is shown at the lower left in FIG. 6. The cross-sectional view in that figure is taken on the vertical, longitudinal midplane of the U-shaped section 36. The far wall of this structure is double; part of it has been broken away to make it clear that the upper section of wall 58 extends throughout the length of the precooling passageway with respect to the coolant passageway even though the exhaust conduit turns upwardly and continues through portion 58a of that wall. The inner wall has been broken away above the Webb 58a to show that from that point on downstream all of the space between the inner and outer walls is part of the cooling passageway. A dam is formed transversely across that flow passage on the plane 7--7 of FIG. 6. The dam is formed by a webb that interconnects the inner and outer walls except at the upper portion of the space between them. The edge of the dam visible in FIG. 6 is designated 140. FIG. 7 is a cross-sectional view taken on line 7--7 which illustrates this construction. Below the dam the cooling passageway encompasses the exhaust conduit over most of its area so that additional cooling is accomplished.
The extent to which that passage is filled with water, and therefore the extent to which cooling is accomplished in that portion, depends upon the size of opening 86 and the rate at which 18 forces coolant to flow. The pump 18 is driven at a speed that varies with engine speed. In a marine engine, engine load is rather directly related to engine speed and heating is rather directly related to engine load. As a consequence, if the outlet opening 86 is not unduly large, the amount of water in the final section of the cooling passage will vary with load and the quantity of heat that must be removed from the exhaust gases.
Advantageously, the dam is located at the highest point in the coolant flowpath so that the flowpath must be completely filled upstream from that point. Removal of the dam from that high point does not destroy the value of the invention although efficiency would be lowered somewhat. The dam may haveany convenient form. Thus, it could comprise any kind of structural division of the coolant passageway into upstream and downstream sections interconnected at an elevated point. Y
Although I have shown and described certain specific embodiments of my invention, I am fully aware that many modifications thereof are possible. My invention, therefore, is not to be restricted except insofar as is necessitated by the prior art.
I claim:
1. For use in cooling an engine which has an exhaust gas exit port and has an inlet opening and an outlet opening for receiving and discharging fluid, respectively:
a heat exchanger comprising an exhaust conduit formed by an encompassing wall and defining an inlet portion for receiving exhaust gas from the engine exit port, an intermediate portion, and an outlet end portion for discharging exhaust gas that has traversed said intermediate portion after entering at the inlet portion;
a jacket comprising said encompassing wall and an overlying outer wall, said jacket being formed to define two passageways capable of conducting liquid coolant, one of said passageways extending over the inlet portion of said exhaust conduit, the other one of said passageways extending over the intermediate portion of said exhaust conduit; and
means interconnecting said heat exchanger and said engine such that exhaust gas is permitted to flow to said exhaust conduit, coolant is permitted to flow from said one passageway to said engine inlet, and fluid from said engine outlet is permitted to flow to said other one of said passageways.
2. The invention defined in claim 1 in which said other one of said passageways is formed with an outlet openingwhich opens at the interior of said exhaust conduit.
3. The invention defined in claim 2 in which said jacket further comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an initial portion of its length before fluid can be discharged from said outlet opening.
4. The invention defined in claim 1 in which said jacket comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an upstream portion of its length, said means comprising mounting means for mounting said conduit with one portion of said other one of said passageways uppermost and of dam means in the form of a darn interconnecting said inner and outer walls except in the region of said one portion of said other of said passageways for confining flow to that one portion.
5. In combination:
an elongate exhaust conduit comprising an inlet section, an intermediate section and an outlet section, said conduit being formed with openings in its inlet section by which exhaust gases may be admitted thereto so that they will traverse the conduit from its inletsection through its intermediate section to be expelled at said outlet section;
means comprising a first enclosing wall overlying portions of said exhaust conduit at its inlet section and defining'a first passageway for coolant having inlet and outlet openings;
means comprising a second enclosing wall overlying portions of said conduit at its intermediate section and at its outlet section and defining inlet and outlet openings; and
means for orienting said conduit and enclosing walls such that one portion of the flowpath formed by said conduit and said second enclosing wall is uppermost in the vicinity of the juncture of said intermediate section and said outlet section of said conduit and for confining flow of fluid along said second passageway to flow substantially at said uppermost region.
6. The invention defined in claim together with an engine comprising a plurality of spaced exhaust gas outlet ports, an inlet opening for coolant, an outlet opening for coolant, and internal passageways interconnecting said inlet and said outlet;
means interconnecting the outlet ports of the engine with the openings in the inlet section of said exhaust conduit;
' means for connecting said first passageway and the passageways through said engine and said second passageway in series, in that order, comprising a first conduit extending from said first passageway defined by said first overlying wall to the inlet of said engine, and comprising a second interconnecting conduit extending from the outlet of said engine to said second passageway defined by said second overlying wall.
7. The invention defined in claim 6 together with means for forcing a flow of coolant into said first passageway and for permitting flow of coolant from said passageways of the engine to said second passageway when said coolant has a temperature exceeding a selected value.
8. The invention defined in claim 7 in which said first passageway is confined to the inlet area of said exhaust conduit and in which said second passageway extends throughout the length of said exhaust conduit.
9. The invention defined in claim 6 in which said conduit comprises a horizontal section and an inverted U- shaped section, said first enclosing wall overlying the horizontal section and said second enclosing wall overlying the inverted U-shaped section.
10. The invention defined in claim 9 in which said U- shaped section comprises a double-walled jacket and said means for confining the flow to said one portion of said'second passageway comprises a dam disposed between the walls of the conduit and the second overlying wall except at an upper region of said U-shaped sec tion.
11. The invention defined in claim 9 which further comprises an inlet conduit for make-up water connected to the inlet side of said pump, means interconnecting the passageways of the engine with the inlet side of said pump, said means for permitting flow of coolant from the engine passageways to said second conduit comprising a thermostatic valve.

Claims (11)

1. For use in cooling an engine which has an exhaust gas exit port and has an inlet opening and an outlet opening for receiving and discharging fluid, respectively: a heat exchanger comprising an exhaust conduit formed by an encompassing wall and defining an inlet portion for receiving exhaust gas from the engine exit port, an intermediate portion, and an outlet end portion for discharging exhaust gas that has traversed said intermediate portion after entering at the inlet portion; a jacket comprising said encompassing wall and an overlying outer wall, said jacket being formed to define two passageways capable of conducting liquid coolant, one of said passageways extending over the inlet portion of said exhaust conduit, the other one of said passageways extending over the intermediate portion of said exhaust conduit; and means interconnecting said heat exchanger and said engine such that exhaust gas is permitted to flow to said exhaust conduit, coolant is permitted to flow from said one passageway to said engine inlet, and fluid from said engine outlet is permitted to flow to said other one of said passageways.
2. The invention defined in claim 1 in which said other one of said passageways is formed with an outlet opening which opens at the interior of said exhaust conduit.
3. The invention defined in claim 2 in which said jacket further comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an initial portion of its length before fluid can be discharged from said outlet opening.
4. The invention defined in claim 1 in which said jacket comprises means for insuring that said other one of said passageways is substantially completely filled with coolant along an upstream portion of its length, said means comprising mounting means for mounting said conduit with one portion of said other one of said passageways uppermost and of dam means in the form of a dam interconnecting said inner and outer walls except in the region of said one portion of said other of said passageways for confining flow to that one portion.
5. In combination: an elongate exhaust conduit comprising an inlet section, an intermediate section and an outlet section, said conduit being formed with openings in its inlet section by which exhaust gases may be admitted thereto so that they will traverse the conduit from its inlet section through its intermediate section to be expelled at said outlet section; means comprising a first enclosing wall overlying portions of said exhaust conduit at its inlet section and defining a first passageway for coolant having inlet and outlet openings; means comprising a second enclosing wall overlying portions of said conduit at its intermediate section and at its outlet section and defining inlet and outlet openings; and means for orienting said conduit and enclosing walls such that one portion of the flowpath formed by said conduit and said second enclosing wall is uppermost in the vicinity of the juncture of said intermediate section and said outlet section of said conduit and for confining flow of fluid along said second passageway to flow substantially at said uppermost region.
6. The invention defined in claim 5 together with an engine comprising a plurality of spaced exhaust gas outlet ports, an inlet opening for coolant, an outlet opening for coolant, and internal passageways interconnecting said inlet and said outlet; means interconnecting the outlet ports of the engine with the openings in the inlet section of said exhaust conduit; means for connecting said first passageway and the passageways through said engine and said second passageway in series, in that order, comprising a first conduit extending from said first passageway defined by said first overlying wall to the inlet of said engine, and comprising a second interconnecting conduit extending from the outlet of said engine to said second passageway defined by said second overlying wall.
7. The invention defined in claim 6 together with means for forcing a flow of coolant into said first passageway and for permitting flow of coolant from said passageways of the engine to said second passageway when said coolant has a temperature exceeding a selected value.
8. The invention defined in claim 7 in which said first passageway is confined to the inlet area of said exhaust conduit and in which said second passageway extends throughout the length of said exhaust conduit.
9. The invention defined in claim 6 in which said conduit comprises a horizontal section and an inverted U-shaped section, said first enclosing wall overlying the horizontal section and said second enclosing wall overlying the inverted U-shaped section.
10. The invention defined in claim 9 in which said U-shaped section comprises a double-walled jacket and said means for confining the flow to said one portion of said second passageway comprises a dam disposed between the walls of the conduit and the second overlying wall except at an upper region of said U-shaped section.
11. The invention defined in claim 9 which further comprises an inlet conduit for make-up water connected to the inlet side of said pump, means interconnecting the passageways of the engine with the inlet side of said pump, said means for permitting flow of coolant from the engine pAssageways to said second conduit comprising a thermostatic valve.
US00110727A 1971-01-28 1971-01-28 Liquid cooled engine Expired - Lifetime US3765479A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11072771A 1971-01-28 1971-01-28

Publications (1)

Publication Number Publication Date
US3765479A true US3765479A (en) 1973-10-16

Family

ID=22334593

Family Applications (1)

Application Number Title Priority Date Filing Date
US00110727A Expired - Lifetime US3765479A (en) 1971-01-28 1971-01-28 Liquid cooled engine

Country Status (1)

Country Link
US (1) US3765479A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3921398A (en) * 1973-08-10 1975-11-25 Outboard Marine Corp Exhaust manifold with high rise water tube
US3968767A (en) * 1974-06-24 1976-07-13 Outboard Marine Corporation Marine propulsion device adapted for a sailboat
US4573318A (en) * 1985-01-25 1986-03-04 Brunswick Corporation Exhaust elbow for marine propulsion system
US4811560A (en) * 1986-09-16 1989-03-14 Sanshin Kogyo Kabushiki Kaisha Exhaust system for marine propulsion
US4977741A (en) * 1988-04-05 1990-12-18 Brunswick Corporation Combination exhaust manifold and exhaust elbow for marine propulsion system
US5067448A (en) * 1988-09-27 1991-11-26 Sanshin Industries Co., Ltd. Exhaust cooling device for small sized boat engine
US5251439A (en) * 1988-09-22 1993-10-12 Sanshin Kogyo Kabushiki Kaisha Exhaust device for small sized boat engine
US5463990A (en) * 1994-10-05 1995-11-07 Outboard Marine Corporation Outboard motor with four-stroke engine and exhaust gas discharge system therefor
US5544631A (en) * 1994-10-05 1996-08-13 Outboard Marine Corporation Cylinder head construction for outboard motor with four-stroke engine
US6378299B1 (en) * 2001-03-16 2002-04-30 Fred J. Schlehuber Engine exhaust cooling system
CN101975100A (en) * 2010-11-11 2011-02-16 奇瑞汽车股份有限公司 Engine exhaust cooler

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1914604A (en) * 1930-01-24 1933-06-20 Foster Wheeler Corp Air preheater
US1931781A (en) * 1929-05-14 1933-10-24 Detroit Lubricator Co Flow control device
US2475552A (en) * 1946-10-07 1949-07-05 John Roehrich Controlled temperature manifold

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1931781A (en) * 1929-05-14 1933-10-24 Detroit Lubricator Co Flow control device
US1914604A (en) * 1930-01-24 1933-06-20 Foster Wheeler Corp Air preheater
US2475552A (en) * 1946-10-07 1949-07-05 John Roehrich Controlled temperature manifold

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3921398A (en) * 1973-08-10 1975-11-25 Outboard Marine Corp Exhaust manifold with high rise water tube
US3968767A (en) * 1974-06-24 1976-07-13 Outboard Marine Corporation Marine propulsion device adapted for a sailboat
US4573318A (en) * 1985-01-25 1986-03-04 Brunswick Corporation Exhaust elbow for marine propulsion system
US4811560A (en) * 1986-09-16 1989-03-14 Sanshin Kogyo Kabushiki Kaisha Exhaust system for marine propulsion
US4977741A (en) * 1988-04-05 1990-12-18 Brunswick Corporation Combination exhaust manifold and exhaust elbow for marine propulsion system
US5251439A (en) * 1988-09-22 1993-10-12 Sanshin Kogyo Kabushiki Kaisha Exhaust device for small sized boat engine
US5067448A (en) * 1988-09-27 1991-11-26 Sanshin Industries Co., Ltd. Exhaust cooling device for small sized boat engine
US5463990A (en) * 1994-10-05 1995-11-07 Outboard Marine Corporation Outboard motor with four-stroke engine and exhaust gas discharge system therefor
US5544631A (en) * 1994-10-05 1996-08-13 Outboard Marine Corporation Cylinder head construction for outboard motor with four-stroke engine
US6378299B1 (en) * 2001-03-16 2002-04-30 Fred J. Schlehuber Engine exhaust cooling system
CN101975100A (en) * 2010-11-11 2011-02-16 奇瑞汽车股份有限公司 Engine exhaust cooler

Similar Documents

Publication Publication Date Title
US4991546A (en) Cooling device for boat engine
US3765479A (en) Liquid cooled engine
US5746270A (en) Heat exchanger for marine engine cooling system
US4082068A (en) V-engine cooling system particularly for outboard motors and the like
US4621594A (en) Single-circuit cooling system for intercooled marine engines
EP1817184B1 (en) Amphibious vehicle comprising an exhaust cooling system
US4504238A (en) Fluid cooler for marine drives
US7264520B1 (en) Cooling system for an outboard motor having both open and closed loop portions
US9359058B1 (en) Outboard marine propulsion devices and methods of making outboard marine propulsion devices having exhaust runner cooling passages
US5921829A (en) Outboard motor cooling system
EP0126620A2 (en) Engine cooling system
US7581582B2 (en) Exhaust cooling system of an amphibious vehicle
US7503819B1 (en) Closed cooling system for a marine engine
US4977741A (en) Combination exhaust manifold and exhaust elbow for marine propulsion system
US5103774A (en) Water cooling means for engine
US6135064A (en) Engine drain system
US4768580A (en) Marine propulsion device oil cooling arrangement
CA2175023C (en) Engine for outboard engine system
US3283498A (en) Exhaust elbow
US7094118B1 (en) Heat exchanger for a marine propulsion system
US11072408B1 (en) Marine engines and cooling systems for cooling lubricant in a crankcase of a marine engine
GB2348485A (en) Engine cooling system
DE19803228A1 (en) Motor vehicle engine coolant conveyance system
US7390232B1 (en) Exhaust system for a marine engine
US3125081A (en) Cooling systems for marine engines