US2240967A - Piston - Google Patents

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US2240967A
US2240967A US323326A US32332640A US2240967A US 2240967 A US2240967 A US 2240967A US 323326 A US323326 A US 323326A US 32332640 A US32332640 A US 32332640A US 2240967 A US2240967 A US 2240967A
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piston
skirt
portions
head
bearing
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US323326A
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William M Venner
Jr Percy L Bowser
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STERLING Corp
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STERLING 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
    • F02F3/00Pistons 
    • F02F3/02Pistons  having means for accommodating or controlling heat expansion
    • F02F3/04Pistons  having means for accommodating or controlling heat expansion having expansion-controlling inserts
    • F02F3/042Pistons  having means for accommodating or controlling heat expansion having expansion-controlling inserts the inserts consisting of reinforcements in the skirt interconnecting separate wall parts, e.g. rods or strips
    • 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
    • F02F3/00Pistons 
    • F02F3/02Pistons  having means for accommodating or controlling heat expansion
    • F02F3/027Pistons  having means for accommodating or controlling heat expansion the skirt wall having cavities
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/02Light metals
    • F05C2201/021Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/04Heavy metals
    • F05C2201/0433Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0448Steel

Definitions

  • Another method has been to insert in the plston structure at appropriate places elements of a material having a lower rate of thermal expansion than aluminum such as steel, the location of such steel inserts being such that their expansion takes the place of aluminum expansion and at a rate more nearly that of the cylinder.
  • One of the objectsA o f this invention is to provide a piston structure in which an increased accuracy of the control of expansion of the bearing portions of the skirt may be obtained.
  • Another object is to provide a structure in which the controlling eiect of elements having a lower rate of expansion than aluminum may be so coordinated as to control with improved accuracy the expansion of the entire bearing area of the skirt.
  • Another object is to provide a structure coordibearing 5.
  • Figure 1 is ⁇ a side view taken along the wrist pin axis of a piston embodying this invention.
  • Figure 2 is a vertical section of the same taken at right angles to the wrist pin axis and about on line 2-2 of Figure 3.
  • Figure 3 is a horizontal section taken on line I 3-3 of Figure 1, and
  • Figure 4 is a plan view showing one way in which the control elements may be formed.
  • the piston illustrated comprises a head I having the usual piston ring grooves 2 and a skirt indicated generally at 3.
  • the skirt is provided with cylinder bearing portions 4 which are machined to iit the cylinder wall.
  • wrist pin bearings 5 In the regions between the cylinder bearing portions 4 are provided wrist pin bearings 5 for the usual piston pin.
  • These bearings are supported from the head I by connectors 6 extending upwardly to the head, and these connectors may be reinforced by ribs 1.
  • One or both of the bearing portions 4 are separated from the head by horizontal slots 8.
  • the slots 8 communicate at their ends with downwardly extending slots 9.
  • the slots 9 extend vertically at thel upper part of the skirt and then turn laterally toward the bearing portion 4, having an intermediate angular portion and a lower horizontal portion.
  • These slots may also be curved instead of angular. as shown, and their curvature may be greater or less according to the design of piston required. They may even extend downwardly at any suitable angle to a point 'below the 'I'his arrangement provides at the sides of the bearing portion 4 outwardly extending wing portions Ill which are free of both the head and the connectors 6. This renders these wing portions free for exure in a horizontal plane, the degree of exibility being controllable by varying the shape and depth of the slots 9.
  • One or both of the bearing portions 4 may be provided, as shown in the drawing, with a control element II constructed of a material having a lower rate of thermal expansion than that of the piston metal.
  • These elements I I are cast into the piston skirt, as shown in Figures 2 and 3, in a position extending circumferentially along and v within the upper part thereoiand so as to extend nating the action of controlling elements of less expansibility, acting both as thermostatic control elements and as elements directly limiting the expansion of the skirt.
  • the invention of this application 1 s an imalong the wing portions I0.
  • These elements may 'be provided with recesses I2 of any suitable form so that the piston metal may upon casting interlock securely with these elements, as may be seen in Figure 3'. It will be seen that the upper part 'of each bearing portion 4 with its extending.
  • wings I0 together with the elements II, form a cally to vary the curvature of this portion of the 4bearing face in a horizontal plane, flexing the bearing portion inwardly thereof rises.
  • a second control element I3 Extending across the linterior of the piston skirt is a second control element I3 also constructed of a materialhaving a lower rate of thermal expansion than the piston metal. 'I'his element is anchored at its ends to the upper parts of the thrust bearing portions 4.
  • This element I3 may be formed as a separate member secured 'at its ends to the piston skirt either by casting the ends into the piston metal or attaching them in any other suitable manner to thepiston skirt or to the elements II.
  • a convenient and economical way of making these elements is to form a punching, such as shown in Figure 4, having the elements il and I3 included in aunitary integral structure which may be formed by a single punching operation. This both secures the element I3 to the elements II and provides for accurately spacing the latter.
  • the cross bar 2,240,967 bimetallic member which may act thermostatiportion of the skirt to which it is connected.
  • the difference between the tendency of the skirtvto expand and its actual expansion probably causes flexure of the portion 4 adjacent the lower ends of the slots 9.
  • the extreme lower end of the skirt is believed to operate at a lower temperature than 'the upper end on laccount of the longer path of flow for the heat to reach the lower end. Accordingly, restraint of the tendency to expand is not requiredat the lower end to as great an extent as at the upper end and may be taken care of by providing the recesses I5 or the elliptical form, as pointed out above, to permita slight change of shape under pressure against the cylinder wall.
  • a slight recess I5 may be formed also at the rim portion.
  • TheA interior of the piston may be provided with Y lugs I6 of any desired shape to provide some excess metal which may be removed in order to bal-
  • the normal tendency of the bearing portions 4 to expand in accordance with the rate of expanslon ,of aluminum is restrained at the upper part of the skirt by the element I3 which has a lower rate of expansion and probably operates at a somewhat lower temperature.
  • the element I3 which has a lower rate of expansion and probably operates at a somewhat lower temperature.
  • This path of flow is lengthened by the slots 9 which compel the heat to travel around those slots to a point in the piston illustrated near the middle of the bearing portion 4 and from that point upwardly toward the to'p of the skirt and to the wing portions I0.
  • This tends to keep this upper portion of the skirt and the wing portions at a considerably lower temperature than/they would attain in the absence of the slots 9. This, therefore, reduces the amount which the upper part of the piston would expand if unrestrained, while in addition thereto the cross bar I3 forcibly restrains expansion for the reason.
  • this invention provides a piston -in which the fit of the thrust bearing portion is controlled by controlling both its lateral curvature by means of the elements Il and the outward movement of the two portions 4 by means of the element I3. Accordingly, both the diameter and the curvature of the bearing portions of the piston are controlled, particu larly at the upper part thereof where the control is most important because the expansion is usually greater at that point.
  • a light-metal pistonof the character described having a head, wrist pin bearings connected with said head', a skirt connected with said bearings but having a cylinder-bearing portion separated from said head in the region between said bearings, a control element of a material having a lower rate of thermal expansion than the piston metal cast into said cylinder-bearingA portion so as to extend circumferentially along and within the upper part thereof but terminating near the-lateral limits of said bearing portion in order to form therewith a bimetallic member, and a second control element having a lower rate of thermal expansion than the piston metal connected to said separated portion of the skirt near the middle thereof and extending across the interior of said skirt and anchored to the opposite wall thereof.
  • a light-metal piston of the character de'- scribed having a head, wrist pin bearings con- ⁇ nected with said head, a skirt connected with said bearings but having cylinder-bearing portions separated from said head in the regions be-4 tween said bearings, control elements of a material having a lower rate of thermal expansion than the piston metal cast into said cylinderbearing portions so as to extend circumferential'- ly along and within the upper parts .thereof but terminating near the lateral limits of said bearing portions in order to form therewith bimetallic members, and a control element having a lower rate of thermal expansion than the piston metal extending across the interior of said skirt and anchored to the upper parts of saidl cylinderbearing portions.
  • a light metal piston of the character described having a head, wrist pin bearings con'- nected with said head, a skirt connected with said bearings but ⁇ having a cylinder-bearing portion head and said bearings in the region between said bearings so as to provide lateralLv extending wing portions free for radial strict, a control element of a material having a expansion than the piston constructed to ilex inwardly in the regions of middle thereof. and extending radially inwardlyl from said connection and anchored at its other end.
  • a light-metal piston of Vthe character described having a head, wrist pin bearings conl nected with said head, a skirt connected with said bearings but having -cylinder-bearing portions separated from said head and-said bearings in the regions between said bearings so as to provide laterally extending wing portions free for radial iiexure,' control elements of a material having a lower rate 'of thermal expansion than i the piston metal cast into saidcylinder-bearing portions so as to extend circumferentially along and within the wing portions thereof but terminating near the lateral limits of said bearing portions in order t0 form therewith bimetallic members, and a control element having a lower rate of thermal expansion than the piston metal extending across the interior of said skirt and anchored to the upper parts of said cylinderbearing portions.
  • a control element comprising, relativelyseparated arcuately extending end members of a material having a lower rate of thermal expansion than the piston metal connected medially thereof by an expansion-restrainingtie member of similar material.
  • a light metal piston of the character described comprising, a head, a skirt, wrist pin bearings connected with said head and said skirt, said skirt having cylinder-engaging portions separated from said head -and constructed to ex inwardly in the regions of said bearings, andan element extending circumferentially inside of and attached to each of said cylinder-engaging portions, said element having a rate of expansion lower than that of said portion and adapted' to ex said portion inwardly in said regions thermostatically, said elements having connecting means extending across the piston.
  • a light metal piston of the character described comprising, a head, a skirt, wrist pin tions separated from said head circumferentially and separated from said connectors terminally,
  • said bearings and elements having a rate of expansion lower than that of said cylinder-engaging portions, one of said elements extending circumferentially inside of and cast to each of said portions and terminating therewith, adapted to ilex each said portion inwardly in said regions thermostatically', said elements having connecting means extending across the piston.
  • a control element comprising, an expansion-restraining cross member, and an arcuate skirtbending member connected to and extending in opposite lateral directions from the end of said cross member, said members being constructed of materialhaving a lower rate of thermal expansion than the piston metal.

Description

Patented May 6, 1941 UNITED STATE s PATENT OFFICE Pls'roN William M. Venner, Richmond Heights, and Percy L. Bowser,
Jr., University City, Mo., assignors to The Sterling Corporation, St. Louis, Mo., a corporation oi' Delaware Application Miu-ch 11, 1940, serial No, 323,326
Claims.
of compensating for the greater rate of thermal expansion of aluminum than that of cast iron, `of which the cylinder is universally constructed. Two .general methods of attack have been iollowed heretofore. In one of these the piston skirt, and particularly those portions which bear vupon the cylinder wall, is rendered resilient so that it may yield under the pressure exerted against the cylinder wall when thermal expansion takes place. Such yieldability is provided by cutting certain portions of the piston free of the expanding parts for.; a portion of their extent so that they may yield by Ilexure of other parts. Instead of completely'lsevering the yieldable parts, loops of metal have been interposed be tween the bearing portions and their supporting parts, which loops are intended to yield by iiexure when the pressure comes on.
Another method has been to insert in the plston structure at appropriate places elements of a material having a lower rate of thermal expansion than aluminum such as steel, the location of such steel inserts being such that their expansion takes the place of aluminum expansion and at a rate more nearly that of the cylinder.
None of these schemes'have been able to compensate ior the expansion of aluminum to a sunlcient degree of accuracy to provide a piston which will be entirely free from danger of injury due to over expansion. A denite problem, therefore, still exists in this iield of controlling the expansion of the bearing portions of the skirt to such a degree of exactness' that a substantially uniform clearance between the skirt and the cylinder wall is maintained while both piston and cylinder rise 'in temperature under the normal operation of the engine.
One of the objectsA o f this invention, therefore, is to provide a piston structure in which an increased accuracy of the control of expansion of the bearing portions of the skirt may be obtained.
Another object is to provide a structure in which the controlling eiect of elements having a lower rate of expansion than aluminum may be so coordinated as to control with improved accuracy the expansion of the entire bearing area of the skirt.
Another object is to provide a structure coordibearing 5.
provement on that of' our application, Serial No.
299,050, ledOctober 12, 1939.
- Further objects will appear from the following description taken in connection with the accompanying drawing, in which:
' Figure 1 is` a side view taken along the wrist pin axis of a piston embodying this invention.
Figure 2 is a vertical section of the same taken at right angles to the wrist pin axis and about on line 2-2 of Figure 3.
Figure 3 is a horizontal section taken on line I 3-3 of Figure 1, and
Figure 4 is a plan view showing one way in which the control elements may be formed.
l Referring to the drawing, the piston illustrated comprises a head I having the usual piston ring grooves 2 and a skirt indicated generally at 3. In the piston illustrated the skirt is provided with cylinder bearing portions 4 which are machined to iit the cylinder wall. In the regions between the cylinder bearing portions 4 are provided wrist pin bearings 5 for the usual piston pin. These bearings are supported from the head I by connectors 6 extending upwardly to the head, and these connectors may be reinforced by ribs 1.
, One or both of the bearing portions 4 are separated from the head by horizontal slots 8. The slots 8 communicate at their ends with downwardly extending slots 9. In the arrangement illustrated, the slots 9 extend vertically at thel upper part of the skirt and then turn laterally toward the bearing portion 4, having an intermediate angular portion and a lower horizontal portion. These slots may also be curved instead of angular. as shown, and their curvature may be greater or less according to the design of piston required. They may even extend downwardly at any suitable angle to a point 'below the 'I'his arrangement provides at the sides of the bearing portion 4 outwardly extending wing portions Ill which are free of both the head and the connectors 6. This renders these wing portions free for exure in a horizontal plane, the degree of exibility being controllable by varying the shape and depth of the slots 9.
One or both of the bearing portions 4may be provided, as shown in the drawing, with a control element II constructed of a material having a lower rate of thermal expansion than that of the piston metal. These elements I I are cast into the piston skirt, as shown in Figures 2 and 3, in a position extending circumferentially along and v within the upper part thereoiand so as to extend nating the action of controlling elements of less expansibility, acting both as thermostatic control elements and as elements directly limiting the expansion of the skirt. n, The invention of this application 1s an imalong the wing portions I0. These elements may 'be provided with recesses I2 of any suitable form so that the piston metal may upon casting interlock securely with these elements, as may be seen in Figure 3'. It will be seen that the upper part 'of each bearing portion 4 with its extending.
wings I0, together with the elements II, form a cally to vary the curvature of this portion of the 4bearing face in a horizontal plane, flexing the bearing portion inwardly thereof rises.
Extending across the linterior of the piston skirt is a second control element I3 also constructed of a materialhaving a lower rate of thermal expansion than the piston metal. 'I'his element is anchored at its ends to the upper parts of the thrust bearing portions 4. This element I3 may be formed as a separate member secured 'at its ends to the piston skirt either by casting the ends into the piston metal or attaching them in any other suitable manner to thepiston skirt or to the elements II. A convenient and economical way of making these elements is to form a punching, such as shown in Figure 4, having the elements il and I3 included in aunitary integral structure which may be formed by a single punching operation. This both secures the element I3 to the elements II and provides for accurately spacing the latter. Before assembling as the temperature this composite member in the piston the cross bar 2,240,967 bimetallic member which may act thermostatiportion of the skirt to which it is connected. The difference between the tendency of the skirtvto expand and its actual expansion probably causes flexure of the portion 4 adjacent the lower ends of the slots 9. The extreme lower end of the skirt is believed to operate at a lower temperature than 'the upper end on laccount of the longer path of flow for the heat to reach the lower end. Accordingly, restraint of the tendency to expand is not requiredat the lower end to as great an extent as at the upper end and may be taken care of by providing the recesses I5 or the elliptical form, as pointed out above, to permita slight change of shape under pressure against the cylinder wall.
When the piston skirt heats up the upper portion adjacent the slot 8 on account of the thermostatic action-of the two metals which are intimately interlocked along this part of fthe skirt -tends to change its curvature slightly by bending inwardly at the wing portions I0. Experience has shown that one of the most diicult points of the piston skirt to control is the upper side corners of the bearing face, namely at the wing portions I0. This arrangement of thermostatic action, therefore, may be adjusted so as to bend A these wing portions inward as the piston heats recessed slightly, as indicated at I4, so as to permit the-pin bearings to expand without danger of coming against the cylinder walls. The lower rim of the skirt may be circumferentially con-` tinuous with the bearing portions 4 so as to maintain a bearing on the cylinder wall, or these portions of the skirt may be ground elliptical, or
a slight recess I5 may be formed also at the rim portion.
TheA interior of the piston may be provided with Y lugs I6 of any desired shape to provide some excess metal which may be removed in order to bal- The normal tendency of the bearing portions 4 to expand in accordance with the rate of expanslon ,of aluminum is restrained at the upper part of the skirt by the element I3 which has a lower rate of expansion and probably operates at a somewhat lower temperature. As the heat which causesexpanslon of the bearing portions 4 must iiow to 4those portions from the head I through the piston metal, the only path of flow available is along the connectors 6. This path of flow is lengthened by the slots 9 which compel the heat to travel around those slots to a point in the piston illustrated near the middle of the bearing portion 4 and from that point upwardly toward the to'p of the skirt and to the wing portions I0. This tends to keep this upper portion of the skirt and the wing portions at a considerably lower temperature than/they would attain in the absence of the slots 9. This, therefore, reduces the amount which the upper part of the piston would expand if unrestrained, while in addition thereto the cross bar I3 forcibly restrains expansion for the reason. that its own expansion is less for the same 4temperature while its actual temperature is probably less than thatof the ance a set of pistons according to the usual pracup and the proportions of the two metals may be adjusted to control the amount of bending with great accuracy. Accordingly, the curvature of the upper portion of the piston skirt may be made to conform very accurately to that of the cylinder wall at all temperatures. In addition to this, since the slot Y9 renders the wing portions I0 free for flexure radially, in case the control of the curvature is not quite exact or in case the cylinder should become warped, as is often the case, any excess pressure of the cylinder wall on the wing portions l0 may flex those portions inwardly without generating suiiicient pressure to score or injure the bearing surface. At the same time these wing portions extend laterally to a considerable spread on each side of the center line of the bearing' portion 4, and, accordingly, the lateralposition of the piston in the cylinder is firmly controlled and any tendency to rock is thereby greatly reduced.
While it hasbeen found advisable in most cases to provide slots 8 and 9 on both sides of the piston, the advantages of this invention may be obtained to a. proportionate extent if one of the bearing portions 4 is made integral with the piston head or the slots 9 omitted on one side.
Itwill be seen, therefore, that this invention provides a piston -in which the fit of the thrust bearing portion is controlled by controlling both its lateral curvature by means of the elements Il and the outward movement of the two portions 4 by means of the element I3. Accordingly, both the diameter and the curvature of the bearing portions of the piston are controlled, particu larly at the upper part thereof where the control is most important because the expansion is usually greater at that point.
It is obvious that various changes may be made in the details of construction within the scope of the appended claims without departing from the spirit of this invention, and it is understood therefore that the invention is not limited to the speciilc details shown and described.
The invention having thus been described,
what is claimed is:
l. A light-metal piston of the character denected with said head, a skirt connected with said Separated from said lower rate of thermal metal cast into said cylinder-bearing portion so .bearings but having a cylinder-bearing portion separated from said head in the region between said bearings, a control element of a material having a lower rate of thermal expansion than the piston metal cast into said cylinder-bearing portion so as to extend circumferentially along and within the upper part. thereof but terminating near the lateral limits of said bearing portion in order to form therewith abimetallic member, and a second control element having a. lower rate of thermal expansion than the piston metal connected to said separated portion of the skirt near the middle thereof and extendingradially inwardly from said connection and anchored at its other end. f
2. A light-metal pistonof the character described, having a head, wrist pin bearings connected with said head', a skirt connected with said bearings but having a cylinder-bearing portion separated from said head in the region between said bearings, a control element of a material having a lower rate of thermal expansion than the piston metal cast into said cylinder-bearingA portion so as to extend circumferentially along and within the upper part thereof but terminating near the-lateral limits of said bearing portion in order to form therewith a bimetallic member, and a second control element having a lower rate of thermal expansion than the piston metal connected to said separated portion of the skirt near the middle thereof and extending across the interior of said skirt and anchored to the opposite wall thereof. I
3. A light-metal piston of the character de'- scribed, having a head, wrist pin bearings con-` nected with said head, a skirt connected with said bearings but having cylinder-bearing portions separated from said head in the regions be-4 tween said bearings, control elements of a material having a lower rate of thermal expansion than the piston metal cast into said cylinderbearing portions so as to extend circumferential'- ly along and within the upper parts .thereof but terminating near the lateral limits of said bearing portions in order to form therewith bimetallic members, and a control element having a lower rate of thermal expansion than the piston metal extending across the interior of said skirt and anchored to the upper parts of saidl cylinderbearing portions.
4. A light-metal piston'of the character de- `scribed,..having ahead, wrist pin bearings convnected with ,said head, a skirt connect-.ed with said bearings but having cylinder-bearing p0rtions separated from said head in the regions between said bearing control elements of a material havinga lower rate of thermal expansion than the piston metal c ast intosaid cylinderbearing portions so as to extend circumferentially along and within the upper parts thereof but terminating near the lateral limits of said bearing portions in order to form therewith bimetallic members, and a control element having a low- '.er-'rate of thermal expansion than the piston metal extending across the interior of said skirt and anchored to said iirst control elements.
5. A light metal piston of the character described, having a head, wrist pin bearings con'- nected with said head, a skirt connected with said bearings but `having a cylinder-bearing portion head and said bearings in the region between said bearings so as to provide lateralLv extending wing portions free for radial haute, a control element of a material having a expansion than the piston constructed to ilex inwardly in the regions of middle thereof. and extending radially inwardlyl from said connection and anchored at its other end.
6. A light-metal piston of Vthe character described, having a head, wrist pin bearings conl nected with said head, a skirt connected with said bearings but having -cylinder-bearing portions separated from said head and-said bearings in the regions between said bearings so as to provide laterally extending wing portions free for radial iiexure,' control elements of a material having a lower rate 'of thermal expansion than i the piston metal cast into saidcylinder-bearing portions so as to extend circumferentially along and within the wing portions thereof but terminating near the lateral limits of said bearing portions in order t0 form therewith bimetallic members, anda control element having a lower rate of thermal expansion than the piston metal extending across the interior of said skirt and anchored to the upper parts of said cylinderbearing portions.
'7. In a piston of the character described, a control element comprising, relativelyseparated arcuately extending end members of a material having a lower rate of thermal expansion than the piston metal connected medially thereof by an expansion-restrainingtie member of similar material.
8. A light metal piston of the character described, comprising, a head, a skirt, wrist pin bearings connected with said head and said skirt, said skirt having cylinder-engaging portions separated from said head -and constructed to ex inwardly in the regions of said bearings, andan element extending circumferentially inside of and attached to each of said cylinder-engaging portions, said element having a rate of expansion lower than that of said portion and adapted' to ex said portion inwardly in said regions thermostatically, said elements having connecting means extending across the piston.
9. A light metal piston of the character described, comprising, a head, a skirt, wrist pin tions separated from said head circumferentially and separated from said connectors terminally,
said bearings, and elements having a rate of expansion lower than that of said cylinder-engaging portions, one of said elements extending circumferentially inside of and cast to each of said portions and terminating therewith, adapted to ilex each said portion inwardly in said regions thermostatically', said elements having connecting means extending across the piston. i
10. In a piston of the 'character described, a control element comprising, an expansion-restraining cross member, and an arcuate skirtbending member connected to and extending in opposite lateral directions from the end of said cross member, said members being constructed of materialhaving a lower rate of thermal expansion than the piston metal.
US323326A 1940-03-11 1940-03-11 Piston Expired - Lifetime US2240967A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2464554A (en) * 1944-08-11 1949-03-15 Vacuum Air Pressure Company Lt Piston and expansion means therefor
US2497380A (en) * 1945-10-05 1950-02-14 William M Venner Piston
US2513437A (en) * 1945-10-05 1950-07-04 William M Venner Piston
US2563887A (en) * 1948-03-02 1951-08-14 Thompson Prod Inc Strut type piston
US2576655A (en) * 1947-01-02 1951-11-27 William M Venner Piston
US2607643A (en) * 1949-01-14 1952-08-19 Thompson Prod Inc Strut type piston
US2643921A (en) * 1947-12-12 1953-06-30 William M Venner Trunk piston
US2661256A (en) * 1950-05-02 1953-12-01 Schmidt Gmbh Karl Light metal piston for combustion engines
DE944590C (en) * 1953-03-17 1956-06-21 Daimler Benz Ag Pistons, especially for internal combustion engines
DE1062486B (en) * 1954-01-13 1959-07-30 Augsburg Nuernberg A G Zweigni Forced circulation lubrication and cooling for the working piston of internal combustion engines
US3805677A (en) * 1972-03-01 1974-04-23 Trw Inc Two-piece oil-cooled piston with thermal expansion control

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2464554A (en) * 1944-08-11 1949-03-15 Vacuum Air Pressure Company Lt Piston and expansion means therefor
US2497380A (en) * 1945-10-05 1950-02-14 William M Venner Piston
US2513437A (en) * 1945-10-05 1950-07-04 William M Venner Piston
US2576655A (en) * 1947-01-02 1951-11-27 William M Venner Piston
US2643921A (en) * 1947-12-12 1953-06-30 William M Venner Trunk piston
US2563887A (en) * 1948-03-02 1951-08-14 Thompson Prod Inc Strut type piston
US2607643A (en) * 1949-01-14 1952-08-19 Thompson Prod Inc Strut type piston
US2661256A (en) * 1950-05-02 1953-12-01 Schmidt Gmbh Karl Light metal piston for combustion engines
DE944590C (en) * 1953-03-17 1956-06-21 Daimler Benz Ag Pistons, especially for internal combustion engines
DE1062486B (en) * 1954-01-13 1959-07-30 Augsburg Nuernberg A G Zweigni Forced circulation lubrication and cooling for the working piston of internal combustion engines
US3805677A (en) * 1972-03-01 1974-04-23 Trw Inc Two-piece oil-cooled piston with thermal expansion control

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