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
  • F02F3/00—Pistons 
  • F02F3/02—Pistons  having means for accommodating or controlling heat expansion
  • F02F3/04—Pistons  having means for accommodating or controlling heat expansion having expansion-controlling inserts
  • F02F3/08—Pistons  having means for accommodating or controlling heat expansion having expansion-controlling inserts the inserts being ring-shaped
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16J—PISTONS; CYLINDERS; SEALINGS
  • F16J1/00—Pistons; Trunk pistons; Plungers
  • F16J1/04—Resilient guiding parts, e.g. skirts, particularly for trunk pistons
  • F16J1/06—Resilient guiding parts, e.g. skirts, particularly for trunk pistons with separate expansion members; Expansion members
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
  • F05C2201/00—Metals
  • F05C2201/02—Light metals
  • F05C2201/021—Aluminium
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
  • F05C2251/00—Material properties
  • F05C2251/04—Thermal properties
  • F05C2251/042—Expansivity

Definitions

• the invention relates to a piston of light metal .for an internal combustion engine or a compressor.
• light metal as used herein includes aluminium, aluminium alloys, magnesium and magnesium alloys.
• Such pistons have a crown, a gudgeon pin bore and a skirt including portions forming opposed thrust and counter-thrust faces on opposite sides of a plane including the piston axis and the gudgeon pin bore axis.
• an axially and circumf erentially extending gap is commonly provided between an upper end of one or both skirt portions and a lower end- of the crown.
• problems arise if this gap is left unfilled because the crown is not fully supported and because, during expansion and contraction of the crown and skirt, the ends of the gap are stressed and this can lead to piston failure. It has therefore been proposed to fill this gap with an insert of a metal having a coefficient of expansion which is lower than the coefficient of expansion of the piston material.
• the insert is of a ferrous material and includes two diametrically opposed segmental portions which contact and separate respective upper ends of the skirt portions and the lower end of the crown and extend to the exterior surface of the skirt and crown.
• the insert includes cranked strut portions which are connected at an angle to the ends of the segmental portions and are embedded in the piston material to locate the insert.
• a piston of light metal for an internal combustion engine or a compressor comprising a crown, a gudgeon pin bore, a skirt including portions forming opposed thrust faces on opposite sides of a plane including the piston axis and the gudgeon pin bore axis, an upper end of at least one skirt portion being spaced from an adjacent crown portion by an axially and circumferentially extending gap, and an insert of a material of lower coefficient of thermal expansion than the material of the crown and skirt, characterised in that the insert includes a curved section or a
• the curved section or at least one of the plurality of curved sections being within said gap so that the crown is supported on the skirt, and the curved section or at least two of the plurality of curved sections being embedded in the piston material to support the insert.
• Figure 1 is a vertical cross-section through a first embodiment of light metal piston
• Figure 2 is a section on the line A-A of Figure 1;
• Figure 3 is a vertical cross-section through a second embodiment of light metal piston
• Figure 4 is a plan view of an alternative embodiment of an insert for incorporation in the pistons of Figures 1 to 3.
• Figure 5 is a vertical cross-section through a third
• Figure 5A shows an el evation (left-hand side) and a plan (right-hand side) of an insert for incorporation in the embodiment of Figure 5;
• Figure 6 is a section on the line B-B of Figure 5;
• Figure 7 is a vertical cross-section through a fourth embodiment of light metal piston
• Figure 8 is a section on the line C-C of Figure 7;
• Figure 9 is a half plan view (upper part) and an elevation (lower part) of an insert for incorporation in the piston of Figures 7 and 8;
• Figure 10 is a vertical cross-section through a fifth embodiment of a light metal piston
• Figure 11 is a section on the line D-D of Figure 10.
• Figure 12 is a plan view ⁇ upper part) and an elevation (lower part) of an insert for incorporation in the piston of Figures 10 and 11.
• Each piston is formed by casting in a light metal such as aluminium or an aluminium alloy or magnesium or magnesium alloy.
• Each piston comprises a crown 10 which includes an annular portion 11 formed with three axially spaced circumferentially extending ring grooves 12, 13, 14. Each groove has spaced radially extending side walls interconnected by a base.
• the piston also includes two axially aligned gudgeon pin bores 15 formed in respective gudgeon pin bosses 16.
• the piston also includes a skirt 17. Since a connecting rod (not shown), connected to the piston by a gudgeon pin extending through the gudgeon pin bore 15, will not act along the piston axis, diametrically opposed portions 17a, 17b of the- skirt 17 will be urged towards an associated cylinder during reciprocation of the piston. These portions, will thus lie on opposite sides of the plane including the piston axis and the gudgeon pin bore axis.
• the surfaces of these portions 17a, 17b are known as the thrust and counter-thrust faces respectively; the thrust face being the face urged towards the associated cylinder during the expansion stroke and the counter-thrust face being the face urged towards the associated cylinder during the compression stroke.
• each skirt portion 17a, 17b is spaced from the lower end of the crown by an axially and circumferentially extending gap to assist in the control of the thermal expansion of the skirt.
• the gap is formed in the lower side walls and the base of the lowermost piston ring groove 14 and is filled by a curved section 18a, 28, 37a, 41 of an insert 18, 25, 36, 40 whose various alternative constructions will be described below.
• Each curved section 18a, 28, 37a, 41 has a lower radially extending surface which sits in a radially inwardly facing rabbet formed at the upper end of each thrust surface and has an upper radially
• the insert is supported and located by being embedded in the piston material forming the gudgeon pin boss 16.
• the insert 18 of this embodiment is a generally annular shape (as best seen in Figure 2) of constant width along its length and comprises two pairs of curved sections 18a, 18b.
• the insert 18 lies generally in a plane normal to the piston axis.
• Two of the opposed curved sections 18a separate and contact the crown 10 and the skirt portions 17a and 17b and the two remaining curved sections 18b interconnect the ends of the first curved sections 18 ' a and are embedded in and pass through the material of the piston forming the gudgeon pin bosses 16.
• the further curved sections 18b are provided with upwardly arcuate portions 19 which pass around the gudgeon pine bore 15.
• Figure 3 The construction of Figure 3 is generally the same as that of Figure 2 except that a second insert 19 is provided which forms a reinforcement member for the lower ends of the skirt portions.
• the second insert 19 is also made of a material whose coefficient of thermal expansion is less than that of the crown 10 and skirt 17, and has portions 19a received in the interior surfaces of said skirt portions 17a, 17b and portions embedded in the piston material.
• FIG 4 shows an insert 40 which may be substituted for the insert 18 in the piston of Figures 1 to 3.
• the insert 40 comprises two curved sections 41 which separate and contact the crown and the skirt portions 17a, 17b.
• the curved sections 41 have their ends interconnected by curved side sections 44, each of which comprises initial portions 44a having substantially parallel curved edges and leading from respective ends of the curved sections 41 and a central portion 44b whose curved edges converge towards the middle of each side section to form a neck.
• the central portions 44b may be upwardly arcuate, where necessary, to allow them to pass around the gudgeon pin bore 15.
• the third embodiment of piston includes two inserts 25 each having an upper curved portion 28 which contacts and separates the crown and the upper end of a skirt portion and whose ends are embedded in the piston material forming the gudgeon pin boss 16 and having a lower curved section 29 which forms a reinforcing member for the lower ends of the skirt portions and has the ends thereof embedded in the piston material forming the gudgeon pin boss 16.
• Two connecting sections 30 extend within the piston material between the ends of the upper and lower curved sections 28, 29.
• this embodiment of piston is substantially the same as that described above with reference to Figure 3 but in this case two diametrically opposed struts 35 are provided each extending axially along the interior of the associated skirt portion 17a, 17b and interconnecting the curved sections 18a, 19a of the two inserts 18, 19.
• the embodiment of piston shown therein comprises two inserts 36 each formed by an upper portion 37 having a curved section 37a contacting and separating the upper end of the associated skirt portion 17a, 17b and the crown 10 and having curved end sections 37b embedded in the piston material forming a gudgeon pin bore 16 and a lower portion 38 having a curved section 38a forming a reinforcing member for the lower end of the associated skirt portions 17a, 17b and having curved end portions 37b embedded in the piston material forming the gudgeon pin boss 16.
• a strut 38 extends axially along the interior of each skirt portion to interconnect the upper and lower portions.
• the various inserts 18, 25, 37, 40 described above with reference to the drawings have a number of common features. They all include a single curved section or a plurality of consecutive curved sections lying in a plane normal to the piston axis. This form of construction is easy to produce since it can be made by pressing or bending. In addition, an insert of this shape has thermal expansion characteristics which can be determined. Since each insert is wholly or substantially wholly surrounded by or in contact with the material of the piston, the inserts can be readily cast into the piston without the difficulties caused by the need for substantial gaps or voids around the insert.
• the inserts form at least a part of a piston ring groove of the associated piston, allows the overall height, and thus the overall weight, of the piston to be somewhat reduced.
• the sections of the inserts which contact and separate the skirt portions and the crown all terminate radially inwardly of the outer surface of the skirt 17. This prevents the insert contacting and damaging an associated cylinder when in use. This also removes the need to try and machine the insert and the skirt surface together to produce a satisfactory surface.

Landscapes

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

Applications Claiming Priority (2)

Publications (1)

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ID=10525036

Family Applications (1)

Country Status (6)

Cited By (1)

Families Citing this family (4)

Citations (4)

• 1982
  • 1982-08-05 AU AU89909/82A patent/AU8990982A/en not_active Withdrawn
  • 1982-10-01 EP EP82902823A patent/EP0090815A1/en not_active Withdrawn
  • 1982-10-01 WO PCT/GB1982/000280 patent/WO1983001278A1/en not_active Ceased
  • 1982-10-07 ES ES1982277023U patent/ES277023U/es active Pending
  • 1982-10-07 IT IT23658/82A patent/IT1152882B/it active
  • 1982-10-08 IN IN1163/CAL/82A patent/IN156699B/en unknown

Patent Citations (4)

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