US1562555A - Cylinder - Google Patents

Cylinder Download PDF

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Publication number
US1562555A
US1562555A US302006A US30200619A US1562555A US 1562555 A US1562555 A US 1562555A US 302006 A US302006 A US 302006A US 30200619 A US30200619 A US 30200619A US 1562555 A US1562555 A US 1562555A
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United States
Prior art keywords
cylinder
aluminum
reinforces
reinforce
inserts
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Expired - Lifetime
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US302006A
Inventor
William S Harley
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Harley Davidson Motor Co Inc
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Harley Davidson Motor Co Inc
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Publication date
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Priority to US302006A priority Critical patent/US1562555A/en
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Publication of US1562555A publication Critical patent/US1562555A/en
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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 
    • F02F1/18Other cylinders
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/4927Cylinder, cylinder head or engine valve sleeve making
    • Y10T29/49272Cylinder, cylinder head or engine valve sleeve making with liner, coating, or sleeve

Definitions

  • a further object is to provide a cylinder of high radiating efficiency.
  • a further object is to'niake a cylinder having a large active radiating surface.
  • a further object is to make a light weight cylinder.
  • a further object is to minimize wear.
  • a further object isto reinforce the cylinder at the points where the greatest wear comes.
  • a further object is to produce a coniposife cylinder in such a manner that when the cylinder expands a metal to metal conktact will be maintained whereby the maximum thermal conductivity will be maintained.
  • a further object is to provide a rcin force for a cylinder which will be securely anchored 'in place.
  • a further object is to provide a i'einforce of such configuration that there will be a minimum possibility of a leak along the line of contact between the sides of the reinforce and thc cylinder body.
  • a further object is to so arrange the reinforcing means that strains are properly distributed in the cylinder body.
  • Fig. 1 is a longitudinal sectional view of a gasoline motor cylinder showing in dotted lines the position of the .piston therein.
  • Fig. 2 is a transverse sectional view of the structure shown in Fig. 1, taken along the line 2-2 in Fig. 1.
  • Fig. 3 is a view similar to Fig. 2, showing aI modified arrangement of reinforcing members.
  • Fi 4 is a detail of the reinforcing member sown in Figs. 1, 2 and 3.
  • Figs .5 and 6 show further forms of reinforcing members.
  • Fig. 1 shows a section of a cylinder coinposed of aluminum.
  • Aluminum is used bercause of 'its high thermal conductivity'. This property 1s utilized by employing long radiating ns, thereby securing a large effective radiating surface.
  • the effective use of large radiating surfaces is possible when a metal of high thermal conductivity is used as the heat is readily transmitted to the extreme tips of the radiating fins, thereby making all of the radiating surface effective in securing proper cooling ofthe cylinder.
  • Fig. 1 further shows a section of a cylinder having a main or body portion l, composed of aluminum and reinforced by a plurality of inserts 2 and 3, of harder wearresisting material. These inserts vare distinct and separate from each other, a section. through the cylinder showing about equal alternate widths of reinforces and aluminum, as may be seen from Fig. 2.
  • the lateral thrust from the piston on its 'explosion stroke is toward one side of the cylinder and on its compression stroke toward the other side of the cylinder in a plane through the center line of the cylinder and at right angles to the crankshaft.
  • This lateral thrust is borne successively by the two reinforces or inserts 2-2 on diamctrically opposite sides of the cylinder.
  • Fig. 2 shows four of these reinforces arranged at 90 degree points around the inner portion of the cylinder.
  • the pairof reinforces 3-3 are adapted to take up 'any wear coming upon the sides of the cylinder, and the reinforces'2 are adapted to take up the wear caused by thethrust of the piston previously described.
  • F ig. 3 is a sectional view similar lo Fig. 2, showing 'a construction of cylinder in which there are two reinforces -la corresponding to the reinforces 2-2 Figs. 1 and 2. In some cases it may be found desirable to provide only these two reinforces as they carry the main thrust ofthe piston.
  • Fig. 4f is a detail of the forni of reinforce shown' in' Figs. 1, 2 and 3.
  • This reinforce comprises a main body portion 2, having outwardly projecting lugs or ears 5, provided on each side thereof and arranged in a staggered relation to secure proper anchoring .of the reinforce. Additional means for anchoring the reinforce are provided by means of the ⁇ countersunk holes 6J Fig. shows a reinforce similar to that shown in Fig. 4, except for the shape or configuration of the side ed es thereof. These side edges are formed o a plurality of scallops forming a flnted or wave-like edge 7 for the reinforce.
  • Fig. 6 is a further form of reinforce in which the side edges 8 are straight.
  • the side edges are bevelled so that the surrounding aluminum has a gripping action thereon.
  • the reinforces are properly positioned and cast in the aluminum cylinder, the 'aluminum passing through the countersunk holes and around the bevelled edges and securely anchoring the reinforces in place. Subsequently the aluminum cylinder and reinforces, or inserts, are machined out to the proper cylinder bore. This provides a uniformly smooth inner surface for the composite cylinder.
  • An aluminum cylinder having wear resisting inserts cast integral with the cylinder on opposite sides thereof to take the side thrust of the piston due to the crank connection, there being substantial longitudinally extending portions of the aluminum body exposed Within the cylinder.
  • An aluminum cylinder having a wear resisting insert cast integrally therewith, said insert having conntersunk openings for engagement by the aluminum forming the wall of the casing to securely anchor t'be inserts in position.
  • An aluminum cylinder having n pair of wear resisting inserts cast integrally therewith on opposite sides thereof and extending substantially the length of the cylinder to take the side thrust of the piston due to the crank connection, each of said insertshaving irregular beveled edges for engagement by the aluminum body to securely anchor the same in position.
  • An aluminum cylinder having wear resisting inserts' cast integ1ally therewith and extending longitudinally thereof, each of said inscris having irregular beveled edges and conntcrsnnk openings for cngagen'ient by the aluminum forming the wall of the casing to securely anchor the inserts in position.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Description

Nav. 24,1925. 1,562,555
. W. S.v HARLEY CYLINDER Filed June 5, 1919 2 Sheets-Sheet 1 Nov. 24,1925. 1,562,555
W. S. HARLEY CYLINDER Filed June 5. 1919 2 Sheets-Sheet 2 vvlO Patented Nov. 24, '1.925.'
UNITED STATES. PAT-ENT o1=i=ic|i:.l
WIIILLIJALMI S. HARLEY, OF MILWAUKEE, WISCONSIN, ASSIGNOR TO HARLEY-DAVIDSON' MOTOR CO., OF MILWAUKEE, WISCONSIN, A CORPORATION OF WISCONSIN. I
CYLINDER.
Appiication inea J'un'e 5,'i919. serial No. 302,006.-
To all whom t 'mag/(concern:
Be it known that I, YVILLIAM S. HARLEY,
a citizen of the United States, residing at B'Iilwaukee, in the county of Milwaukee and State of lVisconsin, have invented new to make a cylinder of a metal of high.
thermal conductivity.
A further object is to provide a cylinder of high radiating efficiency.
A further object is to'niake a cylinder having a large active radiating surface.
' A further object is to make a light weight cylinder.
A further object is to minimize wear.
A further object isto reinforce the cylinder at the points where the greatest wear comes.
A further object is to produce a coniposife cylinder in such a manner that when the cylinder expands a metal to metal conktact will be maintained whereby the maximum thermal conductivity will be maintained.
A further object is to provide a rcin force for a cylinder which will be securely anchored 'in place.
A further object is to provide a i'einforce of such configuration that there will be a minimum possibility of a leak along the line of contact between the sides of the reinforce and thc cylinder body.
A further object is to so arrange the reinforcing means that strains are properly distributed in the cylinder body.
Embodinients of the invention are shown in the accompanying drawings.
Fig. 1 is a longitudinal sectional view of a gasoline motor cylinder showing in dotted lines the position of the .piston therein.
Fig. 2 is a transverse sectional view of the structure shown in Fig. 1, taken along the line 2-2 in Fig. 1.
Fig. 3 is a view similar to Fig. 2, showing aI modified arrangement of reinforcing members.
Fi 4 is a detail of the reinforcing member sown in Figs. 1, 2 and 3.
Figs .5 and 6 show further forms of reinforcing members.
Fig. 1 shows a section of a cylinder coinposed of aluminum. Aluminum is used bercause of 'its high thermal conductivity'. This property 1s utilized by employing long radiating ns, thereby securing a large effective radiating surface. The effective use of large radiating surfaces is possible when a metal of high thermal conductivity is used as the heat is readily transmitted to the extreme tips of the radiating fins, thereby making all of the radiating surface effective in securing proper cooling ofthe cylinder.
Fig. 1 further shows a section of a cylinder having a main or body portion l, composed of aluminum and reinforced by a plurality of inserts 2 and 3, of harder wearresisting material. These inserts vare distinct and separate from each other, a section. through the cylinder showing about equal alternate widths of reinforces and aluminum, as may be seen from Fig. 2.
The lateral thrust from the piston on its 'explosion stroke is toward one side of the cylinder and on its compression stroke toward the other side of the cylinder in a plane through the center line of the cylinder and at right angles to the crankshaft. This lateral thrust is borne successively by the two reinforces or inserts 2-2 on diamctrically opposite sides of the cylinder.
Fig. 2 shows four of these reinforces arranged at 90 degree points around the inner portion of the cylinder. The pairof reinforces 3-3 are adapted to take up 'any wear coming upon the sides of the cylinder, and the reinforces'2 are adapted to take up the wear caused by thethrust of the piston previously described.
F ig. 3 is a sectional view similar lo Fig. 2, showing 'a construction of cylinder in which there are two reinforces -la corresponding to the reinforces 2-2 Figs. 1 and 2. In some cases it may be found desirable to provide only these two reinforces as they carry the main thrust ofthe piston.
Fig. 4f is a detail of the forni of reinforce shown' in' Figs. 1, 2 and 3. This reinforce comprises a main body portion 2, having outwardly projecting lugs or ears 5, provided on each side thereof and arranged in a staggered relation to secure proper anchoring .of the reinforce. Additional means for anchoring the reinforce are provided by means of the `countersunk holes 6J Fig. shows a reinforce similar to that shown in Fig. 4, except for the shape or configuration of the side ed es thereof. These side edges are formed o a plurality of scallops forming a flnted or wave-like edge 7 for the reinforce.
Fig. 6 is a further form of reinforce in which the side edges 8 are straight.
In all of the forms of reinforcing or wear resisting members, the side edges are bevelled so that the surrounding aluminum has a gripping action thereon.
In making the cylinder the reinforces are properly positioned and cast in the aluminum cylinder, the 'aluminum passing through the countersunk holes and around the bevelled edges and securely anchoring the reinforces in place. Subsequently the aluminum cylinder and reinforces, or inserts, are machined out to the proper cylinder bore. This provides a uniformly smooth inner surface for the composite cylinder.
In the form of reinforce shown in Figs. 4 and 5, any slight opening that might occur between the edges of the reinforce and the cylinder body proper, due to unequal expansion. would offer a tortuous path to any leaking gases which might pass by the piston.
By having the reinforces of relatively small lateral dimensions as compared with the inner periphery of the cylinder, such reinforces will not tend to pull away from the cylinder body, but will move outwardly with the cylinder body as the cylinder expands, although the reinforces and cylinder may have different roellicients of expansion. This insures a cylinder of high thermal. conductivity and unitary construction in which the strains are 'properly distributed in the cylinder body.
By forming the cylinder of a metal of high thermal conductivity and by providing Wide radiating fins, a cylinder of high radiating efficiency is produced.
It is to be understood that where aluminum is referred to herein, that it is intended to include also aluminum alloys.
vposition and for dissipating heat.
2. An aluminum cylinder having wear resisting inserts cast integral with the cylinder on opposite sides thereof to take the side thrust of the piston due to the crank connection, there being substantial longitudinally extending portions of the aluminum body exposed Within the cylinder.
l 3. An aluminum cylinder having a small number of relatively large wear resrsting longitudinally extending inserts cast integral with the cylinder on opposite sides thereof to take the side thrust of the piston due to the angularity of the crank connection, each of said inserts having indented edges for engagement with the aluminum body for holding the insert in position and for dissipating the heat.
4. An aluminum cylinder having a wear resisting insert cast integrally therewith, said insert having conntersunk openings for engagement by the aluminum forming the wall of the casing to securely anchor t'be inserts in position.
5. An aluminum cylinder having n pair of wear resisting inserts cast integrally therewith on opposite sides thereof and extending substantially the length of the cylinder to take the side thrust of the piston due to the crank connection, each of said insertshaving irregular beveled edges for engagement by the aluminum body to securely anchor the same in position.
An aluminum cylinder having wear resisting inserts' cast integ1ally therewith and extending longitudinally thereof, each of said inscris having irregular beveled edges and conntcrsnnk openings for cngagen'ient by the aluminum forming the wall of the casing to securely anchor the inserts in position.
In witness whereof, I have hereunto subscribed my name.
WILLIAM S. HARLEY.
US302006A 1919-06-05 1919-06-05 Cylinder Expired - Lifetime US1562555A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2534406A (en) * 1944-09-22 1950-12-19 Jr Harry M Bramberry Coated metal article and method of making the same
US2600529A (en) * 1946-06-19 1952-06-17 Fairchild Engine & Airplane Engine cylinder construction for cooling valve seat inserts
US4260658A (en) * 1979-06-21 1981-04-07 Kobe, Inc. Erosion resistant surface
US20060112924A1 (en) * 2002-08-24 2006-06-01 Helmut Schaefer Cylinder liner for a cylinder crankcase
US20100095838A1 (en) * 2008-10-17 2010-04-22 Caterpillar Inc. Engine cylinder liner

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2534406A (en) * 1944-09-22 1950-12-19 Jr Harry M Bramberry Coated metal article and method of making the same
US2600529A (en) * 1946-06-19 1952-06-17 Fairchild Engine & Airplane Engine cylinder construction for cooling valve seat inserts
US4260658A (en) * 1979-06-21 1981-04-07 Kobe, Inc. Erosion resistant surface
US20060112924A1 (en) * 2002-08-24 2006-06-01 Helmut Schaefer Cylinder liner for a cylinder crankcase
US7240608B2 (en) * 2002-08-24 2007-07-10 Daimlerchrysler Ag Cylinder liner for a cylinder crankcase
US20100095838A1 (en) * 2008-10-17 2010-04-22 Caterpillar Inc. Engine cylinder liner
US7975601B2 (en) 2008-10-17 2011-07-12 Caterpillar Inc. Engine cylinder liner

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