US2110064A - Liner for the cylinders of reciprocating piston machines - Google Patents

Liner for the cylinders of reciprocating piston machines Download PDF

Info

Publication number
US2110064A
US2110064A US100740A US10074036A US2110064A US 2110064 A US2110064 A US 2110064A US 100740 A US100740 A US 100740A US 10074036 A US10074036 A US 10074036A US 2110064 A US2110064 A US 2110064A
Authority
US
United States
Prior art keywords
liner
liners
cylinders
piston
bores
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
Application number
US100740A
Inventor
Grinham Edward George
Dawtrey Lewis Henry
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Standard Motor Co Ltd
Original Assignee
Standard Motor Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Standard Motor Co Ltd filed Critical Standard Motor Co Ltd
Application granted granted Critical
Publication of US2110064A publication Critical patent/US2110064A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J10/00Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
    • F16J10/02Cylinders designed to receive moving pistons or plungers
    • F16J10/04Running faces; Liners

Definitions

  • This invention relates to multi-cylinder internal-combustion engines, whether spark-ignited or operating by compression-ignition, of the kind having cylinder liners of hard-wearing material fitted in bores in a cylinder block having a liquidcooling passage in it.
  • the invention does not relate to so-called wet liners such as are built up of two or more parts and the outer surfaces of which are in direct contact with the cooling liquid.
  • the bores in the cylinder block are machined to receive the pistons and their outer ends are counter-bored and fitted with the liners each of which has an axial length which does not exceed half the piston stroke.
  • Figure 1 is a fragmentary sectional elevation of a cylinder block, of an internal-combustion engine, adapted according to the invention
  • Figure 2 is a graph showing cylinder wear along the length of the bore
  • Figures 3 and 4 are sectional elevations of another form of liner for use according to the invention, Figure 4 being a section taken on the line IVIV of Figure 3;
  • Figure 5 is a section showing another form of liner.
  • FIG. l of the drawing parts of only two bores 9, 9 in the cylinder block ID are shown, the latter having at H a liquid-cooling passage of known form.
  • the outer ends of the cylinder bores are shown as having been machined to receive the liners i2, i2.
  • the liner may be of cast iron provided that it is suitably hardened and tempered, or it may be formed of other materials.
  • a liner is inserted in position in the counter-bored end after having had its temperature materially reduced, as by means of liquid air.
  • the inner end of the liner may with advantage be suitably chamfered externally, as shown at I3, to facilitate its being driven into position when in the frozen state.
  • the axial length of a liner is approximately only A, of the piston stroke, as it will be seen from Figure 2 that the wear occurring in the cylinder bore is a maximum at a plane of the bore corresponding to the position of-the outer piston-ring I l when the piston I5 is at top dead centre, and that the wear is localized so that the length of any material wear is approximately only one-third of the piston stroke from top dead angles to its main axis, it is possible to reduce the likelihood of a ledge eventually forming as wear takes place.
  • a short liner of the kind described By fitting a short liner of the kind described the cost of a full-sized liner is avoided. Moreover, a short liner can in most cases be fitted to existing engines without risk of weakening the cylinder block, owing to the fact that the latter is relatively stiff at its outer end where the liner is fitted. Furthermore when designing a new multicylinder engine, it full length liners are to be fitted it may be necessary, if the water space between the cylinders is not to be unnecessarily restricted, to provide for a larger cylinder-block than would be the case it short liners according to the invention were to be fitted as these do not tend to restrict the water space.
  • an arrangement according to the invention is the following: the heat from the piston head is dissipated mainly through the piston rings to the contacting surface.
  • the piston rings are in contact with the cylinder blocks casting for longer periods during the piston stroke than with the relatively short liner.
  • a multi-cylinder internal-combustion 'engine having' 'a cylinder block; the latter having a plurality of bores therein and a liquid-cooling space between the bores, said block having the outer ends of the bores counterbored, hard-wearing liners immovably fitted in said counterbores, the external inner edges of said liners being chamlfered to facilitate said liners being driven into said counterbores, and pistons adapted to be reclprocated in the bores of said block and in the bores of said liners and at top dead centre to reach substantially to the outer ends of said liners; each of said pistons having a piston ring near the head which at top dead centre engages the associated liner near its outer end, said liners being of a length approximately equal to onethird of the distance traversed by said rings.

Landscapes

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

Description

March 1, 1938. E. G. GRINHAM ET AL 2,110,054
LINER FOR THE CYLINDERS 0F BECIPROCATING PISTON MACHINES Filed Sept. 14, 1936 cm; of EA. Inn- O O'Q25 005 0 2275 0'! IO [w man g zaww flaw/Z3 63 6 4.
flll'orne s Patented Mar. 1, 1938 UNITED, STATES PATENT OFFICE LINER FOR THE CYLINDERS 0F BECIPRO- CATING PISTON MACHINES Application September 14, 1936, Serial No. 100,740 In Great Britain May 22, 1936 2 Claims.
This invention relates to multi-cylinder internal-combustion engines, whether spark-ignited or operating by compression-ignition, of the kind having cylinder liners of hard-wearing material fitted in bores in a cylinder block having a liquidcooling passage in it.
The invention does not relate to so-called wet liners such as are built up of two or more parts and the outer surfaces of which are in direct contact with the cooling liquid.
According to the invention, the bores in the cylinder block are machined to receive the pistons and their outer ends are counter-bored and fitted with the liners each of which has an axial length which does not exceed half the piston stroke.
In the accompanying drawing:--
Figure 1 is a fragmentary sectional elevation of a cylinder block, of an internal-combustion engine, adapted according to the invention;
Figure 2 is a graph showing cylinder wear along the length of the bore;
Figures 3 and 4 are sectional elevations of another form of liner for use according to the invention, Figure 4 being a section taken on the line IVIV of Figure 3; and
Figure 5 is a section showing another form of liner.
Like numerals indicate like parts throughout the drawing.
In Figure l of the drawing parts of only two bores 9, 9 in the cylinder block ID are shown, the latter having at H a liquid-cooling passage of known form. The outer ends of the cylinder bores are shown as having been machined to receive the liners i2, i2. The liner may be of cast iron provided that it is suitably hardened and tempered, or it may be formed of other materials. In the preferred method of fitting, a liner is inserted in position in the counter-bored end after having had its temperature materially reduced, as by means of liquid air. The inner end of the liner may with advantage be suitably chamfered externally, as shown at I3, to facilitate its being driven into position when in the frozen state.
The axial length of a liner is approximately only A, of the piston stroke, as it will be seen from Figure 2 that the wear occurring in the cylinder bore is a maximum at a plane of the bore corresponding to the position of-the outer piston-ring I l when the piston I5 is at top dead centre, and that the wear is localized so that the length of any material wear is approximately only one-third of the piston stroke from top dead angles to its main axis, it is possible to reduce the likelihood of a ledge eventually forming as wear takes place.
When the liners are in position the bores of the cylinder block and liners can be machined together.
By fitting a short liner of the kind described the cost of a full-sized liner is avoided. Moreover, a short liner can in most cases be fitted to existing engines without risk of weakening the cylinder block, owing to the fact that the latter is relatively stiff at its outer end where the liner is fitted. Furthermore when designing a new multicylinder engine, it full length liners are to be fitted it may be necessary, if the water space between the cylinders is not to be unnecessarily restricted, to provide for a larger cylinder-block than would be the case it short liners according to the invention were to be fitted as these do not tend to restrict the water space.
Another important advantage oi. an arrangement according to the invention, is the following: the heat from the piston head is dissipated mainly through the piston rings to the contacting surface. With the present construction the piston rings are in contact with the cylinder blocks casting for longer periods during the piston stroke than with the relatively short liner. Thus the conduction of heat from the piston head is increased above a construction with a long liner due to the fact that the conductivity of the heat passage from the rings through the liner to the cylinder block casting is not so great as that from the piston rings direct to the cylinand at top dead centre to reach substantially to 55 the outer ends of said liners, each of said pistons having a piston ring near the head which at top dead centre engages the associated liner near its 7 outer end, said liners being of a length approximateiy equal to one-third of the distance traversed by said rings;
2. A multi-cylinder internal-combustion 'engine having' 'a cylinder block; the latter having a plurality of bores therein and a liquid-cooling space between the bores, said block having the outer ends of the bores counterbored, hard-wearing liners immovably fitted in said counterbores, the external inner edges of said liners being chamlfered to facilitate said liners being driven into said counterbores, and pistons adapted to be reclprocated in the bores of said block and in the bores of said liners and at top dead centre to reach substantially to the outer ends of said liners; each of said pistons having a piston ring near the head which at top dead centre engages the associated liner near its outer end, said liners being of a length approximately equal to onethird of the distance traversed by said rings.
EDWARD G. GRINHAM. LEWIS H. DAW'I'REY.
US100740A 1936-05-22 1936-09-14 Liner for the cylinders of reciprocating piston machines Expired - Lifetime US2110064A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2110064X 1936-05-22

Publications (1)

Publication Number Publication Date
US2110064A true US2110064A (en) 1938-03-01

Family

ID=10898708

Family Applications (1)

Application Number Title Priority Date Filing Date
US100740A Expired - Lifetime US2110064A (en) 1936-05-22 1936-09-14 Liner for the cylinders of reciprocating piston machines

Country Status (1)

Country Link
US (1) US2110064A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3476020A (en) * 1968-09-03 1969-11-04 Caterpillar Tractor Co Engine block with case hardening of cylinder walls

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3476020A (en) * 1968-09-03 1969-11-04 Caterpillar Tractor Co Engine block with case hardening of cylinder walls

Similar Documents

Publication Publication Date Title
FI66675B (en) KYLD KOLV FOER FOERBRAENNINGSMOTORER
US20160097340A1 (en) Cylinder liner assembly having air gap insulation
US20150377177A1 (en) Cylinder liner having roll-burnished recess
US2110064A (en) Liner for the cylinders of reciprocating piston machines
US2108392A (en) Cylinder liner for internal-combustion engines
US1710136A (en) Composite aluminum to steel cylinder construction
US3351044A (en) Internal combustion engines
US2130923A (en) Piston land construction
US2184820A (en) Internal combustion engine
CN203515829U (en) Air cylinder sleeve of diesel engine
US2126089A (en) Internal combustion engine
US2253739A (en) Piston and ring
GB234232A (en) Improvements in cylinder liners for internal combustion engines
US2572392A (en) Engine cooling, cylinder jacket, and head construction
US3021183A (en) Cylinder and piston structures
US1944708A (en) Piston
US1898145A (en) Composite cylinder for internal combustion engines
US1347480A (en) Internal-combustion motor
JP6574990B2 (en) Piston with reduced topland height and closely topland piston shape
US1329822A (en) Composite piston for internal-combustion motors
US3213766A (en) Light weight piston
US2284152A (en) Piston
US1891638A (en) Cylinder block construction
US2154717A (en) Cylinder head
US1413372A (en) Cylinder construction