US2456272A - Engine cylinder construction - Google Patents

Engine cylinder construction Download PDF

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Publication number
US2456272A
US2456272A US687884A US68788446A US2456272A US 2456272 A US2456272 A US 2456272A US 687884 A US687884 A US 687884A US 68788446 A US68788446 A US 68788446A US 2456272 A US2456272 A US 2456272A
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Prior art keywords
liner
cylinder
casing
aluminum
barrel
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US687884A
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Alfred T Gregory
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Fairchild Engine and Airplane Corp
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Fairchild Engine and Airplane Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F1/26Cylinder heads having cooling means
    • F02F1/28Cylinder heads having cooling means for air cooling
    • F02F1/30Finned cylinder heads
    • F02F1/34Finned cylinder heads with means for directing or distributing cooling medium 

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

Dec@ 14 1948 A. r. GREGQRY 2,456,272
' ENGINE CYLINDER CONSTRUCTION Filed Aug.' 2, 1946 2 sums-sheet 1 n A TORNE YS.
.De.14,194s. K A, T., GREGORY 2,456,272
ENGINE CYLINDER CONSTRUCTION Filed Aug. 2, 1946 2 Sheets-Sheet 2 1N VEN TOR.
ALFRED 7'. GREGORY Patented Dec. 14, im
ENGINE CYLINDER CONSTRUCTION Alfred T. Gregory, Manhasset, N. Y., assigner to Fairchild Engine and Airplane Corporation, Farmingdale, N. Y., a corporation of Maryland Application August 2, 1946, Serial No. 687,884
(Cl. 12S-193) claims. i
This invention relates to cylinders having heatradiating surfaces, and has particular reference to cylinders for air-cooled internal combustion engines, although the invention is not limited to that use.
Cylinders for air-cooled internal combustion engines are commonly constructed of two basic elements, a steel sleeve known as the cylinder barrel, and an aluminum head of forged or cast construction which is screwed and shrunk onto the cylinder barrel and sometimes is bolted to the cylinder barrel. Both the cylinder head and barrel are provided with external fins for dissipating heat, and in some cases the cylinder barrel is encased in a mud of metal of 'high heatconductivity, such as aluminum, in which the heat-dissipating fins are machinedor otherwise provided. y
There are many limitations to cylinders of the above type construction, such as the manner of attaching the head to the barrel, which is a limiting factor in the strength of the cylinder, because heavy wall thicknesses must be maintained in the aluminum head to provide adequate strength to grip the cylinder barrel. The sealing of the joint between the head and the barrel is an extremely important problem, in view of the high loads carried across the joint and the thermal distortions which take place under operat ing conditions. The joint, furthermore, provides a' heat dam, obstructing the flow of heat from the inner cylinderwall surface to the cooling fins on the lower portions of the cylinder head. The above problems, while serious in a radial type aircooled engine, become even more so for inline type engines where cylinder spacing is dependent to a considerable extent upon the space required for passing cooling air over the tins in the region between cylinders. The one-piece cylinder liner, including barrel vand head, encased in a muil of aluminum, offers a partial solution to thecooling problem because thickened walls for joints are not needed and more intercylinder air space results, but in the case of overhead valve 'mechanisms, the considerable 'operating load thereof presents a problem because of the low physical strength of aluminum. Various expedients have been proposed in the effort to solve this problem, but they involve complicated and expensive loadtransierring structures.
In accordance with the present invention, a unitary or one-piece cylinder liner encased in aluminum is provided which not only affords the adequate cooling air circulation between closelyspaced cylinders, but also provides adequate sui!- port for overhead load, so that the invention is applicable to overhead valve mechanism engines without requiring special 'load-transferring arrangements.
The preferred xembodiment of the invention consists of a one-piece or unitary steel cylinder liner encased in aluminum muff extending over the head of the liner so as to form an aluminum pad of substantial area, to which a steel deck plate is unitarily bonded and on which the overhead valve meohanism, including the cam housing, valve springs. and the like, is wholly supported and secured. Spark plug bushings and intake and exhaust duct liners may be secured directly to the cylinder liner and also encased in the aluminum, but in most instances duct liners will be found ,unnecessary with the construction of the present invention. t
It will be seen` that the aluminum mud not only affords high cooling efficiency, lightness, and enables closer cylinder spacing without limiting cooling air circulation, but it also minimizes distortion of the thinnest linervduring temperature fluctuaton because of its low strength. Further more, notwithstanding the low strength of the aluminum, the novel construction of the muil.' nevertheless enablesitfto act as a medium to distribute and transfer the valve mechanism loads directly from the decir plate to the liner and thence to the crank-case or engine bed without the ald of special or separate load-transferring members.
For a more complete understanding of the invention, reference may be had to the accompanying drawings, in which:
Figure 1 is an axial section through an internal combustion engine cylinder embodying the present invention, as seen along line I-I of Fig. 2;
Fig. 2 is a plan view of the cylinder with the valve-operating mechanism removed, as seen along the line 2 24 of Fig. 1; and
Fig. 3 is a transverse section through the cylinder at the spark plug bushings, as seen along the line 3-3 of Fig. 1. y
Referring to the drawing, numeral 'i0 designates a one-piece Ior unitary engine cylinder liner, preferably of steel. having the proper strength requirements, andmade either by joining a tubular cylinder barrel portion il to a dome-shaped head or cap i2 by welding at I3, or by forging, shaping, or machining the entire liner Ill from one poice of metal. Spark plug bosses or bushings il are attached to the cylinder liner Ill by welding, brazing, or the like. Similarly, valve seat pockets I5 are pressed or other- 3 wise formed in the dome or cap li, and valve seat-inserts It and i1 are pressed, braced, or otherwise securely fastened in position within the valve seat pockets Il. The lower end of the liner Ill may be provided with a mounting flange il whereby the entire cylinder may be secured to the crank-case of the engine.
Formed independently of the cylinder liner Il are deck plates il and 2li having recesses 2|, whose bases are arranged normally to the axes of the respective intake and exhaust valve seats il and i'l. These deck plates il and 2l are made of high strength material, such as cast steel, and are tapped at 22 for cap bolts or other fastening means, this tapping being performed either before or after the deck plates are placed on the cylinder unit in the manner to be described.
The deck plates il and 2li, and the cylinder liner I are spaced, and, at the same time, united permanently and rigidly together by a unitary casing 23 for the cylinder liner I0, which also includes the lateral extensions for intake and exhaust ports 2l and 23, these extensions also providing large area pads 24 and 25 lying between deck plates I3 and 2l and the dome or cap I2 of the liner i0 and constituting the support for the deck plates Il and 20. The material of which mui! or casing 23 and its integral pads 24 and 2B are formed is preferably commercially pure aluminum, but it may be an aluminum-base alloy of such composition as to substantially retain the high heat-conductivity and low weight of aluminum. Preferably the method of forming the aluminum casing 23 and bonding it to the steel cylinder liner l0 and deck plates I8 and 2li is that disclosed in Patent No. 2,396,730, issued March 19, 1948, to Whitfield and Sheshunoif. Preferably commercially pure aluminum is employed., notwithstanding its low physical strength, which is compensated by the present invention so that it constitutes the major loadcarrying element of the structure, as will be described. Also, the low strength commercially pure aluminum has the advantage that it minimizes distortion of the cylinder liner i0 during `thermal expansion and contraction, thus enabling a thin, high strength liner l0 to be used. The casing 23 thereby affords substantially all of the support for the mechanism carried by the deck plates I3 and 20, as will be described. This aluminum casing 23 is bonded to the cylinder liner I0 so that no heat dam exists between the aluminum and the steel to retard heat conduction from the interior of the liner I0 to the cylinder fins. Also, the deck plates i3 and 2li are bonded to the aluminum casing 23 in the same way.
Thin heat conducting hns are either formed in the aluminum during casting of the casing 23, or are machined therein after casting. Preferably such fins are perpendicular to the cylinder axis, as indicated at 23, except for those that lie between the deck plates i3 and 20, which are axial, as indicated at 21.
In casting the casing 23 and pads 24 and 2l of aluminum around the cylinder liner vi3 and between it and the deck plates i3 and 20, the aforementioned intake and exhaust ports 28 and 23, respectively, are formed by a` coring operation or by liners of thin preferably heat-resisting sheet metal, not shown, but conforming to known constructions. Holes 30 and 3i may be cored or bored and reamed through the corresponding pads 24y and 28 in axial alignment with the corresponding valve seats ii and I1, respectively,
aecomo for receiving the corresponding valve stem guides or bushings 32 and 33, respectively, which may be pressed, shrunk. or otherwise securely. fitted in place.
Slldable axially in these valve guide bushings 32 and 33 are the intake and exhaust valves 3l and 35, respectively, whose corresponding valve springs 36 and 3l directly engage the recessed surfaces 2| of deck plates i9 and 20, and whose rocker arms and corresponding cam mechanisms are bolted or otherwise secured directly on the deck plates I8 and 2li by cap screws threaded into the tapped holes 22. The construction of the valve-operating mechanism, generally designated 38 in Fig. l, is conventional and forms no part of the present invention, it being sucient to illustrate one common form of such mechanism to show how it is mounted directly on the deck plates i9 and 20. It will be understood that in case of inline engines, a row or bank of such cylinders is mounted on a crank-case and that the valve-operating mechanism 38 is actuated by a common cam shaft 39 which extends along the heads of the row of cylinders. Also that a cam box preferably encloses the valveoperating mechanism and, being of conventional construction, need not be shown.
The cylinder oi' this invention, particularly when applied to internal combustion engines in the manner described, enables close spacing of the cylinders and deeper ns, without restricting circulation of cooling air between the cylinders, because the head is not enlarged transversely to compensate for thickened walls normally required to carry the loads or occasioned by screw threads joining the cylinder barrel and head. Also, ample cooling space is provided between the pads 24 and 25 and their corresponding deck plates i9 and 20, this space being filled with the axial ns 21, as shown.
The large area surface of the deck plates i9 and 20 resting on commensurately large mass of the alumnium casing 23, including the pads 24 and 25, reduces the unit load from the valveoperating mechanism on the casing 23,'so that the latter, although of low strength material, is nevertheless capable of sustaining the load which is re-distributed over .the surface area of the liner I0 through the strong chemical bond between the alumnium and steel, so that the unit load on the liner i0 is relatively small. Hence, the liner ill need not be made thick and heavy,
i but is required merely to be formed oi sufilciently high strength material to withstand internal combustion gas pressures and piston side loads to which it is subjected in use. For example, the cylinder liner i0 may be made of very high strength material to resist such gas pressures within the cylinder, and may be made comparatively thin and light, being backed by the aluminum mass afforded by the casing 23.
In this way, lightness of construction and compactness are obtained by reason of the division of the cam-shaft loads and internal cylinder pressures between the casing 23, as a whole, and the liner i0. It is understood that the deck plates I9 and 20 are likewise of high strength material, so as to resist bending and distortion, with the aid ff the aluminum pads 24 and 25 which serve as a backing for the deck plates i3 and 20, as well as distribution of the load from the deck plates over a large area. Particularly in inline types of engines, wherein a row of cylinders is attached to a common valve gear housing, the deck plates I9 and 20 prevent or reduce wear between the valve gear housing and the cylinder heads engaging the same.
Although the cylinder liner I is preferably made of high strength steel, the barrel portion Il, where the barrel and head or cap are welded together, may be made of different material having greater wearing properties for cooperation with the piston. Likewise, the spark plug bosses or bushings I4 may be ofl material suitable for that purpose, preferably material of high corrosion resistance, such as steels containing chromium and the like. Such bosses or bushings i4 need not be heavy because of the backing alforded by the aluminum casing 23, which is also bonded to the exterior surfaces of the bosses or bushings I4, according to the aforementioned process. Likewise, where liners are used for intake and exhaust ports 28 and 29, they may be of thin heat-resisting material, such as sheet metal, as they are supported by the aluminum casing 23, which is bonded to them.
Although a preferred embodiment of the invention has been illustrated and described herein, it is to be understood that it is not limited to internal combustion engine cylinders but is equally applicable to pump cylinders and the like, and is otherwise susceptible to changes in fo'rm and detail within the scope of the appended claims.
I claim:
1. A cylinder for the overhead valve type of internal combustion engine and the like, comprising a barrel and head liner of ferrous metal having high structural strength, a casing for said barrel and head liner of light weight `metal integrally secured thereto and having a structural strength less than the ferrousmetal of said liner, lateral extensions on that portion of said casing overlying the head of said liner and forming a platform substantially normal to the axis of said cylinder and having an area substantially greater than the cross-sectional area of said casing around the barrel of said liner, and a platform integrally united with the casing metal of said extensions for mounting the operating mechanism for said overhead valves on said' casing, whereby the operating load of said valve mechanism is transmitted from said platform solely through said casing to said liner.
2. A cylinder for the overhead valve type of internal combustion engine and the like, comprising a barrel and head liner of ferrous metal having high .structural strength, a boss for a spark plug projecting from said liner, a casing for said barrel and head liner of light weight metal integrally secured thereto and having a structural strength less than the ferrous metal of said liner, lateral extensions on that portion of said casing overlying the head of said liner and forming an area substantially greater than the cross-sectional area of said casing around the barrel of said liner, a platform on said extended portion of said casing, and means for mounting the operating mechanism for said overhead valves on said platform, whereby the operating load of said valve mechanism is transmitted from said platform solely through said casing to said liner.
3. A cylinder for the overhead valve .type of internal combustion engine and the like, the combination of a unitary thin-wall barrel and head liner of ferrous metal and having insumcient structural strength to withstand full operating loads Without external support, a massive casing for said barrel and head liner of light weight metal integrally secured thereto and serving as a coextensive support therefor, and supporting means integrally united with said casing metal for mounting the overhead valveoperating mechanism on that portion of said casing overlying the head of said liner, said easing being the sole load transferring means between said liner and supporting means whereby the operating load of said valve mechanism is distributed solely through said casing over a substantial area of said liner covered by said casing.
4. A cylinder for the overhead valve type of internal combustion engine and the like, the combination of a unitary thin-walled barrel and head liner of ferrous metal and having .insufflcient structural strength to withstand full operating loads without external support, a massive casing for said barrel and head liner of aluminum base metal integrally secured thereto and serving vas a coextensive support therefor, and a platform integrally secured to that portion of said casing overlying the head of said liner for y mounting valve operating means, whereby the operating load of said valve mechanism is distributed from said platform solely through said.
casing to and over a substantial area of said liner covered by said casing.
5. A cylinder for the overhead valve type of internal combustion engine and the like, the combination of a unitary thin-walled barrel and head liner of ferrous metal and having insuill- 'a platform secured to said extension and lying substantially normal to the axisy of said cylinder, and means on said platform for mounting the overhead valve-operating mechanism, where' by the operating load of said valve mechanism is distributed by said platform solely through said casing to and over a substantial area of said liner covered by said casing.
ALFRED T. GREGORY.
REFERENCES CITEDV The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,741,678 Brewer Dec. 31, 1929 2,227,933 Hersey Jan. 7, 1941
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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736300A (en) * 1951-06-05 1956-02-28 Gen Motors Corp Engine cylinder construction
DE1001860B (en) * 1952-05-15 1957-01-31 Kloeckner Humboldt Deutz Ag Cylinder head for internal combustion engines
US3000370A (en) * 1959-11-09 1961-09-19 Gen Motors Corp Cylinder liner and valve seat assembly
US3316888A (en) * 1965-01-15 1967-05-02 Continental Aviat & Eng Corp Cylinder head construction
US3521607A (en) * 1969-07-24 1970-07-28 Continental Motors Corp Engine cylinder and head construction
US4030470A (en) * 1974-12-12 1977-06-21 Outboard Marine Corporation Lined engine block member including a threaded opening and method for providing same
FR2356008A1 (en) * 1976-06-22 1978-01-20 Nat Res Dev ELEMENT OF CONSTRUCTION OF AN INTERNAL COMBUSTION ENGINE PROMOTING ITS COOLING
US4162662A (en) * 1976-01-15 1979-07-31 Jean Melchior Two-stroke internal combustion engines
US4723518A (en) * 1985-12-25 1988-02-09 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder head with valve seat formed integrally by copper alloy cladding layer and underlying alloy layer
US4883030A (en) * 1987-11-26 1989-11-28 Toyota Jidosha Kabushiki Kaisha Combustion chamber of a two-stroke engine
US4938183A (en) * 1987-12-24 1990-07-03 Ford Motor Company Method of making and apparatus for monoblock engine construction
US4957081A (en) * 1988-08-30 1990-09-18 Toyota Jidosha Kabushiki Kaisha Combustion chamber of an engine
US5404846A (en) * 1994-04-29 1995-04-11 Outboard Marine Corporation Four stroke one-piece engine block construction
US8440585B2 (en) 2003-04-23 2013-05-14 Energy & Environmental Research Center Foundation Process for regenerating a spent sorbent
US10124293B2 (en) 2010-10-25 2018-11-13 ADA-ES, Inc. Hot-side method and system
US10159931B2 (en) 2012-04-11 2018-12-25 ADA-ES, Inc. Control of wet scrubber oxidation inhibitor and byproduct recovery
US10343114B2 (en) 2004-08-30 2019-07-09 Midwest Energy Emissions Corp Sorbents for the oxidation and removal of mercury
US10427096B2 (en) 2010-02-04 2019-10-01 ADA-ES, Inc. Method and system for controlling mercury emissions from coal-fired thermal processes
US10465137B2 (en) 2011-05-13 2019-11-05 Ada Es, Inc. Process to reduce emissions of nitrogen oxides and mercury from coal-fired boilers
US10471412B2 (en) 2013-03-06 2019-11-12 Midwest Energy Emissions Corp. Activated carbon sorbent including nitrogen and methods of using the same
US10589225B2 (en) 2004-08-30 2020-03-17 Midwest Energy Emissions Corp. Sorbents for the oxidation and removal of mercury
US10767130B2 (en) 2012-08-10 2020-09-08 ADA-ES, Inc. Method and additive for controlling nitrogen oxide emissions
US10828596B2 (en) 2003-04-23 2020-11-10 Midwest Energy Emissions Corp. Promoted ammonium salt-protected activated carbon sorbent particles for removal of mercury from gas streams
US11179673B2 (en) 2003-04-23 2021-11-23 Midwwest Energy Emission Corp. Sorbents for the oxidation and removal of mercury

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1741678A (en) * 1927-07-15 1929-12-31 Harold F Pitcairn Valve-operating mechanism
US2227933A (en) * 1939-04-25 1941-01-07 United Aircraft Corp Finned engine cylinder

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1741678A (en) * 1927-07-15 1929-12-31 Harold F Pitcairn Valve-operating mechanism
US2227933A (en) * 1939-04-25 1941-01-07 United Aircraft Corp Finned engine cylinder

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736300A (en) * 1951-06-05 1956-02-28 Gen Motors Corp Engine cylinder construction
DE1001860B (en) * 1952-05-15 1957-01-31 Kloeckner Humboldt Deutz Ag Cylinder head for internal combustion engines
US3000370A (en) * 1959-11-09 1961-09-19 Gen Motors Corp Cylinder liner and valve seat assembly
US3316888A (en) * 1965-01-15 1967-05-02 Continental Aviat & Eng Corp Cylinder head construction
US3521607A (en) * 1969-07-24 1970-07-28 Continental Motors Corp Engine cylinder and head construction
US4030470A (en) * 1974-12-12 1977-06-21 Outboard Marine Corporation Lined engine block member including a threaded opening and method for providing same
US4162662A (en) * 1976-01-15 1979-07-31 Jean Melchior Two-stroke internal combustion engines
FR2356008A1 (en) * 1976-06-22 1978-01-20 Nat Res Dev ELEMENT OF CONSTRUCTION OF AN INTERNAL COMBUSTION ENGINE PROMOTING ITS COOLING
US4723518A (en) * 1985-12-25 1988-02-09 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder head with valve seat formed integrally by copper alloy cladding layer and underlying alloy layer
US4883030A (en) * 1987-11-26 1989-11-28 Toyota Jidosha Kabushiki Kaisha Combustion chamber of a two-stroke engine
US4938183A (en) * 1987-12-24 1990-07-03 Ford Motor Company Method of making and apparatus for monoblock engine construction
US4957081A (en) * 1988-08-30 1990-09-18 Toyota Jidosha Kabushiki Kaisha Combustion chamber of an engine
US5404846A (en) * 1994-04-29 1995-04-11 Outboard Marine Corporation Four stroke one-piece engine block construction
US8440585B2 (en) 2003-04-23 2013-05-14 Energy & Environmental Research Center Foundation Process for regenerating a spent sorbent
US11806665B2 (en) 2003-04-23 2023-11-07 Midwwest Energy Emissions Corp. Sorbents for the oxidation and removal of mercury
US11179673B2 (en) 2003-04-23 2021-11-23 Midwwest Energy Emission Corp. Sorbents for the oxidation and removal of mercury
US10828596B2 (en) 2003-04-23 2020-11-10 Midwest Energy Emissions Corp. Promoted ammonium salt-protected activated carbon sorbent particles for removal of mercury from gas streams
US10343114B2 (en) 2004-08-30 2019-07-09 Midwest Energy Emissions Corp Sorbents for the oxidation and removal of mercury
US10926218B2 (en) 2004-08-30 2021-02-23 Midwest Energy Emissions Corp Sorbents for the oxidation and removal of mercury
US10933370B2 (en) 2004-08-30 2021-03-02 Midwest Energy Emissions Corp Sorbents for the oxidation and removal of mercury
US10589225B2 (en) 2004-08-30 2020-03-17 Midwest Energy Emissions Corp. Sorbents for the oxidation and removal of mercury
US10596517B2 (en) 2004-08-30 2020-03-24 Midwest Energy Emissions Corp. Sorbents for the oxidation and removal of mercury
US10668430B2 (en) 2004-08-30 2020-06-02 Midwest Energy Emissions Corp. Sorbents for the oxidation and removal of mercury
US10427096B2 (en) 2010-02-04 2019-10-01 ADA-ES, Inc. Method and system for controlling mercury emissions from coal-fired thermal processes
US10730015B2 (en) 2010-10-25 2020-08-04 ADA-ES, Inc. Hot-side method and system
US10124293B2 (en) 2010-10-25 2018-11-13 ADA-ES, Inc. Hot-side method and system
US10465137B2 (en) 2011-05-13 2019-11-05 Ada Es, Inc. Process to reduce emissions of nitrogen oxides and mercury from coal-fired boilers
US10758863B2 (en) 2012-04-11 2020-09-01 ADA-ES, Inc. Control of wet scrubber oxidation inhibitor and byproduct recovery
US10159931B2 (en) 2012-04-11 2018-12-25 ADA-ES, Inc. Control of wet scrubber oxidation inhibitor and byproduct recovery
US10767130B2 (en) 2012-08-10 2020-09-08 ADA-ES, Inc. Method and additive for controlling nitrogen oxide emissions
US10471412B2 (en) 2013-03-06 2019-11-12 Midwest Energy Emissions Corp. Activated carbon sorbent including nitrogen and methods of using the same
US11059028B2 (en) 2013-03-06 2021-07-13 Midwwest Energy Emissions Corp. Activated carbon sorbent including nitrogen and methods of using the same

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