Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS3173451 A
Publication typeGrant
Publication dateMar 16, 1965
Filing dateJun 23, 1960
Priority dateJun 23, 1960
Publication numberUS 3173451 A, US 3173451A, US-A-3173451, US3173451 A, US3173451A
InventorsSlayter Games
Original AssigneeOwens Corning Fiberglass Corp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Cast manifold with liner
US 3173451 A
Images(2)
Previous page
Next page
Description  (OCR text may contain errors)

March 16, 1965 e. SLAYTER CAST MANIFOLD WITH LINER 2 Sheets-Sheet 1 Filed June 23, 1960 INVENTOR 64,1455 5L A Wm BY g jilflw ATTORNEYS March 16, 1965 s. SLAYTER 3,173,451

CAST MANIFOLD WITH LINER Filed June 25, 1960 2 Sheets-Sheet 2 1111111111111!!!IIIIIIIIIII/ INVENTOR 614M155 Sun me Arrow/5Y5 United States Patent 3,173,451 CAST MANIFOLD WITH LINER Games Slayter, Newark, Ohio, assignor to Owens-Corning Fiberglas Corporation, a corporation of Delaware Filed June 23, 1960, Ser. No. 38,188 3 Claims. (Cl. 138-445) This invention relates to a technique for making lined cast bodies and more particularly to a technique for making lined cast bodies in which a fibrous liner functions as a core and also forms a part of the finished casting.

The principles of the invention have been found to be particularly effective in the manufacture of mufflng systems for internal combustion engines. It has been discovered that the use of an insulating, refractory liner in one or more components of an exhaust system has a beneficial effect in reducing deleterious contaminants in exhaust gases in several ways. The insulating effect of the liner enables heat of the exhaust gases to be retained for a longer period of time. As a consequence, the gases will remain longer at a temperature sufficiently high for secondary combustion to occur, and the combustion of a greater portion of the hydrocarbons is enabled. The liner also prevents contact between the exhaust gases and cast iron or steel components of the muifling system, and thus prevents the possibility of a reaction which would otherwise cause certain hydrocarbons in the exhaust gases to be increased. Finally, when the liner includes titania fiber-s, a reduction of hydrocarbons in the exhaust gases is achieved by virtue of catalysts, more complete combustion apparently being accomplished.

Because of these beneficial effects, it has been proposed to use such a liner on the interior surfaces of manifolds, exhaust pipes, and muiflers. While the liners can be used in most mufflers and exhaust pipes in the form of separate cylindrical bodies, many manifolds are of cast iron and are of rather complicated shapes which prevent the use of similar separate liner bodies therein.

In accordance with the instant invention, it has been discovered that lined manifolds and similar cast bodies can be produced by employing the liner material as at least a part of a mold core and casting metal therearound. The liner consists of highly refractory fibers, such as crystalline titania fibers, and a suitable binder. The cast metal flows partially into interstices between portions of the fibers of such a liner and thereby forms an interlocking bond therewith.

The technique according to the invention can also be used for casting lined cylinder heads. Such heads retain more heat and may be maintained above the ignition point of the incoming air-fuel mixture in a suitable engine to provide a continuous ignition point therefor without the continuous use of spark plugs.

It is, therefore, an object of the invention to provide an improved technique for producinglined castings.

Another object of the invention is to provide a simpler technique for producing cast bodies having at least one surface covered with a fibrous liner.

A further object of the invention is to provide a technique for producing cast bodies with fibrous liners effectively bonded thereto.

Still another object of the invention is to provide a cast component for a muffiing system in which a liner is cast into the component.

Still a further object of the invention is to provide a component for a muffling system, which component contains a fibrous liner effectively bonded thereto.

Other objects and advantages of the invention will be apparent from the following detailed description of a preferred embodiment thereof, reference being made to the accompanying drawings, in which:

FIG. 1 is a somewhat schematic view in perspective of an engine employing a lined, cast manifold, with parts broken away and with parts in cross section, made according to the principles of the invention;

FIG. 2 is a view in cross section, taken along line 2-2 of FIG. 1, of a mold including a core for use according to the principles of the invention;

FIG. 3 is a view in cross section taken along the line 3-3 of FIG. 2; and

FIG. 4 is a view in vertical cross section of a completed casting which includes a liner in accordance with the invention.

Referring to FIG. 1, a manifold 10 made in accordance with the invention is shown connected to one bank of four cylinders of an engine 12. The manifold 10 includes a liner 14 which was a core in the original mold from which the manifold 10 was cast. The manifold 10 was made by pouring molten metal into the mold, around and directly in contact with the core to form an integral bond therewith. It will be readily understood that most manifolds are of such relatively complex shape that it is physically impossible for separate liner segments to be inserted therein after casting thereof.

Referring to FIGS. 2 and 3, the manifold 10 is made in a suitable mold 16 which is disposed within a flask l8 composed of a drag 20 and a cope 22. The drag 20 includes a lower mold cavity 24 formed in foundry sand according to usual foundry practices and the cope 22 includes an upper mold cavity 26 which is also formed in foundry sand according to usual foundry techniques. The cavities 24 and 26 each can be formed in several parts when dictated by sound foundry practices. The lower and upper cavities 24 and 26 form the outer surfaces of the manifold 10 when molten cast iron is poured into a sprue 28 having the usual pouring basin 30.

Within the mold cavity is a core 32 comprising highly refractory fibers, preferably of crystalline titania, and a binder. The fiber core 32. is produced by forming a moldable mixture of the fibers and binder material and mold ing the mixture into the shape of the interior of the manifold 10 by means of a core mold, in a manner which is well known in the art. The core 32 is preferably hollow to provide for passage through the manifold 10 of exhaust gases, although the material of which the core 32 is made can be sufiiciently porous that the entire manifold 10 can be filled therewith, the exhaust gases then passing directly through the resulting porous body. However, in most instances it is desirable to form an unobstructed passage through the core 32. This can be accomplished by providing the core 32 with its own inner core 34 of sand and a binder. An inorganic binder of montmorillonite has been found to be particularly effective for the core although the usual organic binder used in ordinary foundry practices can be employed. The sand core 34 is made by usual core-molding techniques and is subsequently placed in the mold for the fibrous core 32, with the core 32 then being formed therearound. The fibrous core 32 and the inner, sand core 34 can be held in the mold cavities 24 and 26 by any conventional means, the particular method of support for the cores 32 and 34 forming no part of the invention. For example, the sand core 34 can extend beyond the fibrous core 32 and be supported in recesses 36 of the mold cavities 24 and 26, or chaplets can be employed. If the fibrous core 32 is used without the sand core 34, then the core 32 can be supported by chaplets or can extend into the recesses 36 and be subsequently trimmed off when the casting is completed.

According to one specific technique employed in male ing cast bodies with fibrous liners, a mixture was prepared from, by weight, 70 parts of crystalline titania fibers at least A" long and preferably in the order of /2 long, 20 parts of montmorillonite, 10 parts of soda-lime glass, and 20 parts of wood sawdust. Enough water was added to this mixture to provide a mortar-like consistency and it was then shaped around the sand core 34, the sand core previously having been made of the same shape as the exhaust gas passage within the manifold 10. The resulting combination core was fired at 2500 F. to form a hardened body, the fibrous core being, by volume, 70% air, 20% titania crystals, and binder. The fibrous core was then supported in the position in the mold recess indicated in FIGS. 2 and 3 and molten iron was poured therearound and allowed to solidify. After the cast iron had cooled, the mold was disassembled and the inner, sand core was then removed to leave the completed casting with the fibrous liner eifectively bonded to the iron by virtue of interlocking.

Another lined, cast body was made by the same technique set forth above except that the fibrous core and sand core were placed in the mold in their green, unfired state. The heat from the cast iron which was then poured thereover at approximately 2600 F. caused the binder of the fibrous case to harden and leave an integral liner in the resulting cast body.

Other binders, such as bentonite, koalinite, or similar clays, can be used in place of the montmorillonite and soda-lime glass, and other organic particles can be used in place of the sawdust. In many instances, sufficient porosity can be obtained by reducing the amount of binder without using any organic material at all.

If the degree of penetration of the molten cast iron into the fibrous core is excessive, additional binder can be used or the exterior of the fibrous core can be sprayed with any of a number of mold coating materials known in the art to reduce the porosity thereof. Similarly, if penetration is not sufficient, less binder can be used or a greater amount of organic material can be employed in the fibrous core mixture to increase porosity thereof. It the thickness of the inner relative to the thickness of the core is sufficiently high so that the heat of the cast iron does not fully harden the fibrous core, the completed lined casting can be fired at a temperature below the melting point of the cast iron to complete the curing of the fibrous core.

While titania fibers are preferred in the fibrous core 32, other highly refractory fibers which will withstand the heat of the molten iron can be employed. For example, Zircon and zirconia fibers are suitable for this purpose, the titania fibers being preferred only because of a catalytic effect they have on the combustion of exhaust gases.

It has been found that blue titania fibers, made by heattreating the fibers in an oxygen deficient atmosphere or by subjecting them to an oxygen deficient atmosphere after formation, are more effective as a catalyst and are preferred where a catalytic etfect is desired. The blue fibers can also be made by adding 20 parts of zinc or magnesium powder to the previously described fibrous core composition, the metal powder apparently removing oxygen from the fibers, either directly or indirectly, by removing oxygen from the atmosphere which in turn removes oxygen from the titania fibers,

Various modifications of the above described embodiments of the invention will be apparent to those skilled in the art and it is to be understood that such modifications are within the spirit and scope of the invention, as defined in the appended claims.

I claim:

1. A lined, cast metal manifold including a main chamber and a plurality of connecting passages for connecting the main chamber with exhaust ports of an internal combustion engine, said manifold comprising a layer including separate, particulate, highly refractory fibers and a refractory, inorganic binder, and a body of a cast metal effectively bonded to said layer with part of the cast metal extending partially into said layer, said binder having a melting point in excess of the melting point of the metal constituting said cast metal body.

2. A lined, cast manifold including a main chamber and a plurality of connecting passages for connecting the main chamber with exhaust ports of an internal combustion engine, said manifold comprising a porous layer inciuding separate, particulate, highly refractory fibers and a refractory, inorganic binder, and a body of a metal cast therearound and effectively bonded to said layer with part of the cast metal extending into interstices of said layer.

3. A body according to claim 2 wherein the pores in said porous layer are present in an amount of at least approximately by volume.

References Cited in the file of this patent UNITED STATES PATENTS 713,123 Lougee Nov. 11, 1902 889,071 Van Voorhis May 26, 1908 1,512,862 Sayre Oct, 21, 1924 1,664,296 Hamerstadt Mar. 27, 1928 1,703,417 Donaldson Feb. 26, 1929 1,909,975 Mackey et al May 23, 1933 1,961,721 Van Lautschoot June 5, 1934 2,048,247 Davis July 21, 1936 2,431,143 Schulte Nov. 18, 1947 2,459,907 Winslow et al. Jan. 25, 1949 2,728,124 Sofield Dec, 27, 1955 2,745,437 Comstock May 15, 1956 2,897,556 Chini Aug. 4, 1959 2,907,084 Wood Oct. 6, 1959 2,962,806 Stumbods Dec. 6, 1960 2,968,652 Mertes Jan. 17, 1961 2,971,251 Willemse Feb. 14, 1961 2,977,326 Nixon Mar. 28, 1961 3,002,920 Porter Oct. 3, 1961 3,043,094 Nichols July 10, 1962 3,066,365 Moore Dec, 4, 1962 FOREIGN PATENTS 496,537 Great Britain Dec. 1, 1938 OTHER REFERENCES Elam: Product Engineering, July 1954, pages 166-169.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US713123 *Dec 2, 1901Nov 11, 1902Clifton Mfg CompanyElectric conduit.
US889071 *Nov 13, 1906May 26, 1908George S Van VoorhisMethod of making bushings.
US1512862 *Mar 17, 1920Oct 21, 1924American Abrasive Metals CompaBrake shoe
US1664296 *Jul 31, 1926Mar 27, 1928Rockwood Mfg CompanyMachine for die-casting pulleys and the like
US1703417 *Jun 7, 1921Feb 26, 1929 oxi hamilton
US1909975 *Nov 3, 1930May 23, 1933Globe Oil Tools CoMounting for hard cutting material
US1961721 *Jun 29, 1932Jun 5, 1934Iowa Malleable Iron CompanyCasting method
US2048247 *Feb 19, 1934Jul 21, 1936Gen Motors CorpBearing and method of making same
US2431143 *Aug 26, 1943Nov 18, 1947Lummus CoFibrous catalyst system
US2459907 *Sep 4, 1942Jan 25, 1949Nat Carbon Co IncMethod of conducting chemical reactions
US2728124 *Mar 26, 1952Dec 27, 1955Gifford Wood CoMethod of forming cylindrical shell with abrasive internal linings
US2745437 *Sep 12, 1951May 15, 1956Norton CoReinforced ceramic body of revolution
US2897556 *Sep 4, 1957Aug 4, 1959Sperry Rand CorpMethod of coring holes in castings
US2907084 *Mar 27, 1956Oct 6, 1959Aluminum Co Of AmericaHollow cores for making castings
US2962806 *Jul 18, 1955Dec 6, 1960Engelhard Ind IncLaminated thermostatic metal
US2968652 *Nov 27, 1957Jan 17, 1961Sun Oil CoPolymerization process with a catalyst prepared by subjecting ticl3 to ultrasonic vibrations and adding an aluminum alkyl
US2971251 *Jun 20, 1955Feb 14, 1961Philips CorpSemi-conductive device
US2977326 *Dec 15, 1958Mar 28, 1961Universal Oil Prod CoActivated refractory inorganic oxide
US3002920 *Dec 10, 1958Oct 3, 1961Exxon Research Engineering CoHydroforming catalyst and process
US3043094 *Feb 29, 1960Jul 10, 1962Alco Products IncExhaust manifolds
US3066365 *Jul 2, 1958Dec 4, 1962Pittsburgh Plate Glass CoDestructible reinforced sand core for metal casting
GB496537A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3292662 *Jul 8, 1963Dec 20, 1966Sunao NishiLance pipe for the injected oxygen in steel making
US3371794 *Nov 28, 1966Mar 5, 1968Dorr Oliver IncManifolded hydrocyclone unit
US3456914 *Oct 23, 1965Jul 22, 1969Johns ManvilleInorganic fiber riser sleeves
US3718172 *Jul 16, 1971Feb 27, 1973Gen Motors CorpMethod of forming a thermally insulated composite article
US3863701 *May 17, 1972Feb 4, 1975Toyota Motor Co LtdProcess for manufacturing heat-insulated castings
US3919755 *Oct 31, 1973Nov 18, 1975Toyota Motor Co LtdMethod of making a high-strength heat-insulating casting
US3939897 *Jul 10, 1973Feb 24, 1976Toyota Jidosha Kogyo Kabushiki KaishaMethod for producing heat-insulating casting
US4003422 *Apr 21, 1975Jan 18, 1977Schramm Buford JProcess for making a composite cylinder head assembly
US4078584 *Sep 19, 1975Mar 14, 1978CoflexipPipe system for collecting petroleum from off-shore wells located at great depths
US4168610 *Mar 29, 1978Sep 25, 1979Caterpillar Tractor Co.Exhaust manifold with reflective insulation
US5014903 *Apr 12, 1990May 14, 1991Cyb Frederick FHeat-retaining exhaust components and method of preparing same
US5018661 *Mar 19, 1990May 28, 1991Cyb Frederick FHeat-resistant exhaust manifold and method of preparing same
US5055435 *Apr 12, 1990Oct 8, 1991Ngk Insulators, Ltd.Ceramic materials to be insert-cast
US5251683 *Mar 11, 1991Oct 12, 1993General Motors CorporationMethod of making a cylinder head or other article with cast in-situ ceramic tubes
US5260116 *Mar 8, 1991Nov 9, 1993Ngk Insulators, Ltd.Heat and shock resistance; noncracking, compressive strength; gasoline and diesel engines
US5493859 *Jan 21, 1994Feb 27, 1996Nippondenso Co., Ltd.For adsorbing exhaust material
US5819806 *Jul 1, 1997Oct 13, 1998Daikyo Co., Ltd.Channel housing with curving channels, and a manufacturing method therefor
US5941284 *Jul 22, 1998Aug 24, 1999Daikyo Co., Ltd.Channel housing with curving channels, and a manufacturing method therefor
DE2759571C2 *Mar 15, 1977Oct 7, 1982Bayerische Motoren Werke Ag, 8000 Muenchen, DeTitle not available
WO1997006909A1 *Jul 16, 1996Feb 27, 1997Northrop Grumman CorpCeramic liner infiltrated with pre-ceramic polymer resin
WO1997007079A1 *Jul 16, 1996Feb 27, 1997Northrop Grumman CorpMetal coated, ceramic, fiber reinforced ceramic manifold
Classifications
U.S. Classification138/145, 164/98, 138/111, 106/38.22, 138/143, 106/38.27, 164/95
International ClassificationF01N3/26, B22D19/00, F01N13/18, F01N13/10
Cooperative ClassificationB22D19/00, F01N2510/06, F01N13/102, F01N13/1866, F01N2310/02, F01N3/26, F01N2450/28, F01N2510/02
European ClassificationB22D19/00, F01N3/26, F01N13/10B, F01N13/18E1