US1710136A - Composite aluminum to steel cylinder construction - Google Patents
Composite aluminum to steel cylinder construction Download PDFInfo
- Publication number
- US1710136A US1710136A US66175A US6617525A US1710136A US 1710136 A US1710136 A US 1710136A US 66175 A US66175 A US 66175A US 6617525 A US6617525 A US 6617525A US 1710136 A US1710136 A US 1710136A
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- US
- United States
- Prior art keywords
- cylinder
- aluminum
- barrel
- steel
- cylinder barrel
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/02—Cylinders; Cylinder heads having cooling means
- F02F1/04—Cylinders; Cylinder heads having cooling means for air cooling
- F02F1/06—Shape or arrangement of cooling fins; Finned cylinders
- F02F1/08—Shape or arrangement of cooling fins; Finned cylinders running-liner and cooling-part of cylinder being different parts or of different material
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making
Definitions
- This invention relates to a composite aircooled cylinder construction for internal combustion engines, and more particularly to a cylinder construction of this general type employin steel and aluminum.
- the primary object of this invention is to provide a composite cylinder construction of steel and aluminum which will minimize the stress in the steel barrel and eliminate excessive overall expansion.
- the aluminum and steel are placed in such relation as to permit as much freedom of expansion and contraction under heat conditions as is structurally possible.
- Fig. 1 is a plan "iew of the cylinder head of a cylinder constructed according to my invention.
- Fig. 2 is a central vertical section taken on the line 2-2 of Figure 1 and looking in the direction of the arrows.
- Fig. 3 is -a side elevation of the cylinder.
- Fig. 4 is a sectional view on the line 4-4 of Fig. 3 looking in the direction of the arrows.
- I Fig. 5 is a central vertical section of the cylinder barrel.
- Fig. 6 is a sectional view on the line 6-6 of Fig. 5 looking in the direction of the arrows, and
- Fig. 7 is a side elevation of the upper part of the cylinder barrel.
- the numeral 10 designates a steel cylinder barrel having at its upper part two annular flanges or rings near its lower end which is provided with a plurality of receiving suitable bolts or studs for securing the cylinder barrel directly to the crank case. of the engine. 13, the cylinder barrel is provided with screw threads which are adapted to engage corresponding threads on the crank case (not shown) and thereby act as a further means for holdin the crankcase and cylinder barrel together.
- the annular flanges 11 and 12 are provided on their lower and upper faces respectively, with a plurality of spaced notches 16 and 17 and the lower face of flange 12 is formed with similar notches 18 for a purpose which will hereinafter appear.
- the cylinder barrel is preferably tumbled in a receptacle containing powdered zinc and heated, and the sherardizing thus accomplished is subse quently removed by finishing machining op erations from all surfaces of the cylinder except the surface 19 located between the spaced flanges 11 and 12.
- the cylinder barrel has cast upon it an aluminum acket 20 having an upper portion 21 extending above the upper open end of the cylinder barrel and thus enclo ing a combust1on chamber.
- This upper portion 21 of the aluminum alloy jacket is formed with the two branches 22 and 23 of a main inlet conduit 24, and with the two exhaust passages 25 and 26, as the particular cylinder illustrated on .the drawing is provided with two inlet and two exhaust valves.
- Apertured bosses 27 and 28 are also provided on the cylinder head and act as guides for the exhaust and inlet valve stems, respectively.
- the same castin or jacket 20 also encases the working surfaces of the cylinder barrel and has formed thereon the circumferential cooling fins 29.
- the molten aluminum alloy enters the space between the flanges 11 and 12 and contacting with the sherardized surface 19, the molten metal forms a sort of alloy with the zinc coating and as the latter has a mechanical bond with the steel barrel, consisting of particles of zinc located in the pores of the steel, it can be seen that a firm thermal bond is established between the cast alumium and steel along this surface. Since the sherardizing has been removed from the surface 30 of the cylinder barrel, which is located below the flange 12, no bond, other than that due to the natural shrinkage between the aluminum and steel.
- the aluminum en- 'a es in the notches 16, 17 and 18 and the ae et is thus locked from lateral movements with relation to the cylinder barrel.
- a composite cylinder for an air-cooled internal combustion engine comprising in combination, a metallic cylinder barrel in which the piston of the engine is adapted to reciprocate, said cylinder barrel having spaced flanges near one end, a casting of different material encasing said barrel and forming a combustion chamber, and means for forming a thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges.
- a composite cylinder for an air-cooled internal combustion engine comprisin in combination, a metallic cylinder barre in which the piston of the engine is adapted to reciprocate, said cylinder barrel having spaced annular flanges provided with a plurality of notches, a casting of difierent material encasing said barrel and en aging said flanges and the notches thereof or preventing casting in relation to the cylinder barrel, and means for forming a thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges.
- a composite cylinder of an air-cooled internal combustion engine comprising a metallic c linder barrel adapted to be secured to t e crankcase of the engine, a castin of difierent material encasing said barre and forming a combustion chamber,
- a composite cylinder or an air-cooled internal combustion engine comprisin combination, a metallic cylinder barre in which the piston of the engine is ada ted to reciprocate, said cylinder barrel aving spaced annular flanges provided with a plurality of notches, a castingof different material encasing said barrel and en ging said flan es and the notches thereof f ing longitudinal and lateral movement of the casting in relation to the cylinder barrel, and means for forming an intermolecular thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges.
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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
April 23, 1929- G. D. ANGLE ET AL COMPOSITE ALUMINUM TO STEEL CYLINDERbONS'I'RUGTION Filed Oct. 30, 1925 4 Sheets-Sheet l April 3, 1929- G. D. ANGLE ET AL COMPOSITE ALUMINUM T0 STEEL CYLINDER CONSTRUCTION 4 Sheets-Sheet 2 Filed Oct. 30, 1925 gnuentoz April 23, 1929- G. D. ANGLE ET AL 1,710,136
COMPOSITE ALUMINUM TO STEEL CYLINDER CONSTRUCTION Filed Oct. 30, 1925 4 Sheets-Sheet 3 COMPOSITE ALUMINUM TO STEEL CYLINDER CONSTRUCTION Filed Oct. 30, 1925 4 Sheets-Sheet Patented Apr. 23, 1929.-
UNITED STATES PATENT OFFICE.
arm n. ANGLE AND enonen n A. mama, or nn'raorr, mcn'rearr. ooxrosn'n ALUMINUM mo swam. cYLnnmn. consrnuo'rron.
Application filed October 80, 1825. Serial 1T0. 68,175.
This invention relates to a composite aircooled cylinder construction for internal combustion engines, and more particularly to a cylinder construction of this general type employin steel and aluminum.
It has een found with cylinders having cast aluminum looked over the entire outer portion of a steel cylinder barrel, that the overall expansion affects the valve tappet clearance to such a degree that it is very difli-- cult to determine a cold valve timing which gives the proper valve opening and closing points during perati0n. This, of course, applies more especially to valve mechanisms using push rods and rocker arms, particularly those in radial engine construction. Furthermore, due to the greater expansion of aluminum, under working conditions, the stresses produced in the steel barrel from this cause are often very great. v
The primary object of this invention is to provide a composite cylinder construction of steel and aluminum which will minimize the stress in the steel barrel and eliminate excessive overall expansion. To accomplish these purposes the aluminum and steel are placed in such relation as to permit as much freedom of expansion and contraction under heat conditions as is structurally possible.
With these and other objects, consisting of new and useful features of construction and arrangements of parts, in view, the invention will be hereinafter more fully described in connection with the accompanying drawings.
- In the drawings Fig. 1 is a plan "iew of the cylinder head of a cylinder constructed according to my invention.
Fig. 2 is a central vertical section taken on the line 2-2 of Figure 1 and looking in the direction of the arrows.
Fig. 3 is -a side elevation of the cylinder.
Fig. 4; is a sectional view on the line 4-4 of Fig. 3 looking in the direction of the arrows.
I Fig. 5 is a central vertical section of the cylinder barrel.
Fig. 6 is a sectional view on the line 6-6 of Fig. 5 looking in the direction of the arrows, and
Fig. 7 is a side elevation of the upper part of the cylinder barrel.
Like numerals of reference refer to corresponding parts in all the figures of the drawings.
The numeral 10 designates a steel cylinder barrel having at its upper part two annular flanges or rings near its lower end which is provided with a plurality of receiving suitable bolts or studs for securing the cylinder barrel directly to the crank case. of the engine. 13, the cylinder barrel is provided with screw threads which are adapted to engage corresponding threads on the crank case (not shown) and thereby act as a further means for holdin the crankcase and cylinder barrel together. The annular flanges 11 and 12 are provided on their lower and upper faces respectively, with a plurality of spaced notches 16 and 17 and the lower face of flange 12 is formed with similar notches 18 for a purpose which will hereinafter appear. The cylinder barrel is preferably tumbled in a receptacle containing powdered zinc and heated, and the sherardizing thus accomplished is subse quently removed by finishing machining op erations from all surfaces of the cylinder except the surface 19 located between the spaced flanges 11 and 12.
The cylinder barrel has cast upon it an aluminum acket 20 having an upper portion 21 extending above the upper open end of the cylinder barrel and thus enclo ing a combust1on chamber. This upper portion 21 of the aluminum alloy jacket is formed with the two branches 22 and 23 of a main inlet conduit 24, and with the two exhaust passages 25 and 26, as the particular cylinder illustrated on .the drawing is provided with two inlet and two exhaust valves. Apertured bosses 27 and 28 are also provided on the cylinder head and act as guides for the exhaust and inlet valve stems, respectively. The same castin or jacket 20 also encases the working surfaces of the cylinder barrel and has formed thereon the circumferential cooling fins 29.
During the casting operation the molten aluminum alloy enters the space between the flanges 11 and 12 and contacting with the sherardized surface 19, the molten metal forms a sort of alloy with the zinc coating and as the latter has a mechanical bond with the steel barrel, consisting of particles of zinc located in the pores of the steel, it can be seen that a firm thermal bond is established between the cast alumium and steel along this surface. Since the sherardizing has been removed from the surface 30 of the cylinder barrel, which is located below the flange 12, no bond, other than that due to the natural shrinkage between the aluminum and steel.
11 and 12, and a flange 13' Adjacent the bottom flange."
apertures 14for the purpose of exists along this surface. The aluminum en- 'a es in the notches 16, 17 and 18 and the ae et is thus locked from lateral movements with relation to the cylinder barrel.
Under heat conditions, the aluminum is allowed to move freely up and down along the surface 30 of the stee barrel 10. Such an arrangement results in an overall change in distance, due to heat, of only the sum of the expansion of the aluminum above the upper flange or ring 11 and that of the steel below this point, being obviously, practically a minimum for constructions 0 his type.
The heat from the combustion c amber walls is transmitted b the integral aluminum casting distribute throu hout its len h and readily dissipated by t e cooling s formed thereon.
It will be understood that the particular construction described and shown has been chosen for illustrative purposes merely and that the invention as defined by the claims hereunto appended may be otherwise embodied and supplied without departing from the spirit and scope thereof.
We claim:
1. A composite cylinder for an air-cooled internal combustion engine comprising in combination, a metallic cylinder barrel in which the piston of the engine is adapted to reciprocate, said cylinder barrel having spaced flanges near one end, a casting of different material encasing said barrel and forming a combustion chamber, and means for forming a thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges.
2. A composite cylinder for an air-cooled internal combustion engine, comprisin in combination, a metallic cylinder barre in which the piston of the engine is adapted to reciprocate, said cylinder barrel having spaced annular flanges provided with a plurality of notches, a casting of difierent material encasing said barrel and en aging said flanges and the notches thereof or preventing casting in relation to the cylinder barrel, and means for forming a thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges.
3. A composite cylinder of an air-cooled internal combustion engine, comprising a metallic c linder barrel adapted to be secured to t e crankcase of the engine, a castin of difierent material encasing said barre and forming a combustion chamber,
means forming an intermolecular thermal bond between the barrel and casting in the vicinity of the combustion chamber, and means for locking said casting from lateral movement relative to said linder barrel.
.4. A composite cylinder or an air-cooled internal combustion engine, comprisin combination, a metallic cylinder barre in which the piston of the engine is ada ted to reciprocate, said cylinder barrel aving spaced annular flanges provided with a plurality of notches, a castingof different material encasing said barrel and en ging said flan es and the notches thereof f ing longitudinal and lateral movement of the casting in relation to the cylinder barrel, and means for forming an intermolecular thermal bond between said casting and the outer surface of the cylinder barrel included between said flanges. v c
In testimony whereof we afiix our signatures.
GLENN D. ANGLE. GEORGE E. A. HALLETT.
ongitudinal. and lateral movement of the or prevent-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US66175A US1710136A (en) | 1925-10-30 | 1925-10-30 | Composite aluminum to steel cylinder construction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US66175A US1710136A (en) | 1925-10-30 | 1925-10-30 | Composite aluminum to steel cylinder construction |
Publications (1)
Publication Number | Publication Date |
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US1710136A true US1710136A (en) | 1929-04-23 |
Family
ID=22067737
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US66175A Expired - Lifetime US1710136A (en) | 1925-10-30 | 1925-10-30 | Composite aluminum to steel cylinder construction |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442254A (en) * | 1943-03-27 | 1948-05-25 | Joseph E Whitfield | Composite metal article |
US2455457A (en) * | 1941-10-24 | 1948-12-07 | Fairchild Engine & Airplane | Coated metal article |
US2584289A (en) * | 1948-05-13 | 1952-02-05 | Porsche Konstruktionen Gmbh | Cylinder head |
US2969781A (en) * | 1958-12-31 | 1961-01-31 | Gen Motors Corp | Internal combustion engine |
US3096566A (en) * | 1953-02-02 | 1963-07-09 | Sunbeam Corp | Lightweight composite sole plate and method of making the same |
US5179994A (en) * | 1992-01-16 | 1993-01-19 | Cmi International, Inc. | Method of eliminating porosity defects within aluminum cylinder blocks having cast-in-place metallurgically bonded cylinder liners |
US5182854A (en) * | 1992-01-15 | 1993-02-02 | Cmi International, Inc. | Method for metallurgically bonding pressed-in cylinder liners to a cylinder block |
US5280820A (en) * | 1992-01-15 | 1994-01-25 | Cmi International | Method for metallurgically bonding cylinder liners to a cylinder block of an internal combustion engine |
US6443211B1 (en) | 1999-08-31 | 2002-09-03 | Cummins Inc. | Mettallurgical bonding of inserts having multi-layered coatings within metal castings |
US6484790B1 (en) | 1999-08-31 | 2002-11-26 | Cummins Inc. | Metallurgical bonding of coated inserts within metal castings |
-
1925
- 1925-10-30 US US66175A patent/US1710136A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2455457A (en) * | 1941-10-24 | 1948-12-07 | Fairchild Engine & Airplane | Coated metal article |
US2442254A (en) * | 1943-03-27 | 1948-05-25 | Joseph E Whitfield | Composite metal article |
US2584289A (en) * | 1948-05-13 | 1952-02-05 | Porsche Konstruktionen Gmbh | Cylinder head |
US3096566A (en) * | 1953-02-02 | 1963-07-09 | Sunbeam Corp | Lightweight composite sole plate and method of making the same |
US2969781A (en) * | 1958-12-31 | 1961-01-31 | Gen Motors Corp | Internal combustion engine |
US5182854A (en) * | 1992-01-15 | 1993-02-02 | Cmi International, Inc. | Method for metallurgically bonding pressed-in cylinder liners to a cylinder block |
US5280820A (en) * | 1992-01-15 | 1994-01-25 | Cmi International | Method for metallurgically bonding cylinder liners to a cylinder block of an internal combustion engine |
US5179994A (en) * | 1992-01-16 | 1993-01-19 | Cmi International, Inc. | Method of eliminating porosity defects within aluminum cylinder blocks having cast-in-place metallurgically bonded cylinder liners |
US6443211B1 (en) | 1999-08-31 | 2002-09-03 | Cummins Inc. | Mettallurgical bonding of inserts having multi-layered coatings within metal castings |
US6484790B1 (en) | 1999-08-31 | 2002-11-26 | Cummins Inc. | Metallurgical bonding of coated inserts within metal castings |
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