US2387971A

US2387971A - Cylinder liner and cylinder

Info

Publication number: US2387971A
Application number: US471982A
Authority: US
Inventors: Aspin Frank Metcalf; Ellinghouse Frederick
Original assignee: Individual
Current assignee: Individual
Priority date: 1942-01-14
Filing date: 1943-01-11
Publication date: 1945-10-30
Anticipated expiration: 1962-10-30

Description

Patented Oct. 3 0, 1.945

2,387,971 minnen LINER AND CYLINDER Frank Metcalf Aspin, Bur

house, Solih y, and Frederick Ellingull, England .Application January 11, 1943, Serial No. 471,982 In Great Britain January 14, 1942 (ci. sos- 3) Claims.

Thisinvention relates to cylinder liners and cylinders for internal combustion engines, compressors and like machines embodying a piston and cylinder which normally operate at considerably elevated temperatures.

There are many known advantages in the use of light alloys, such as magnesium and aluminium alloys, in the manufacture of such machines, but there are also known disadvantages of which perhaps the most important are the general unsuitability of such metals to provide the wearing surface of the cylinder. There is the consequent necessity of fitting a liner and the very real diiculty of securing such liner owing to the fact that the light alloys in general have a higher coefiicient of expansion and lower tensile strength than the usual cylinder metals such as iron including special cast irons. There is also the factor of heat interchange which where the cooling medium does not itself contact the liner requires elective contact between the liner and body of the cylinder in spite of the different rates of expanson in order that the heat of the liner may be dissipated. Cylinder liners have under such conditions been fitted so as to have a uniform inter'- ference fit throughout the length of their engagement, but this of itself has been found to be only partially successful.

The object of the invention is an improved method oflxing and complementary construction of liner and cylinder body.

The invention comprises the method of securing a preformed liner of one metal in a preformed housing of another metal such as a steel liner in an aluminium cylinder bodyy of an internal combustion engine, wherein the liner metal has a relatively lower co-eflicient of expansion than the housing metal, which includes the step of forming the housing and liner with complementary engaging surfaces relatively slightly tapered in both directions axially and of such diameters as to provide a relative interference fit having pressures which are in a gradient in both directions axially.

I'he invention also includes the further step wherein the liner is assembled in the housing by creating a temporary substantial vtemperature difference such that the said interference 'fit is temporarily removed.

According to the invention the combination of a liner and housing such as a steel liner in an aluminium cylinder of an internal combustion engine, wherein the liner is of a metal having a relatively lower co-eficient of expansion than the metal of the housing, characterised in that the liner and housing are preformed so that their complementary engaging surfaces are relative'y slightly tapered in both directions axially and of such diameters as to provide a relative interference t having pressures which are in a gradient in both directions axially.

The liner may also be characterised in that the exterior surface is rough ground to provide slight surface undulation and may be further characterised in that the slight taper of the liner provides a barrel or waisted shape.

According to a further feature of the invention the housing having a liner as aforesaid is characterised in that the bore is machine nished to give slight surface undulation.

Such an assembly may be further characterised in that the undulations in the bore cross with those on the surface of the liner or in that the bore is slightly tapered complementary to the taper of the liner. Such taper may be in the same or the opposite sense relative to that of the liner so long as it is complementary, i. e. such as to provide the required relative taper for an interference fit which will give pressure gradients within practical proportions relative to the materials used.

In the accompanying drawing:

Fig. 1 is a diagrammatic section of a cylinder of an internal combustion engine having a bore tted with a liner according to one example of the invention.

Fig. 2 is an exaggerated section of the construction of Fig. 1.

Figs. 3, 4 and 5 shw modified forms of the invention.

As illustrated in Fig. 1 the cylinder body a which is made of cast magnesium alloy having a coeicient of expansion of .00026 per degree C., is

machined with a cylindrical bore. The liner b of cast iron having a coeicient of expansion of .000011 per degree C., is machined externally with a slight taper or waist and is flanged at c at one end. The external diameter and taper are such that at the centre the interference t, before assembly, is .001" per inch diameter, whilst at the ends the interference t is .002 per inch diameter, at normal room temperature. The tapered interference fit, giving a pressure gradient, is represented diagrammatically in section by the wedge-shaped line. The mean interference t is therefore .0015" per inch diameter.

As shown in Fig. 3, the liner b has a waist taper with an enlarged cylindrical waist portion d.

As shown in Figs. 4 and 5, the liner b has a intimate, almost bonded, contact.

4barrel-shaped taper, whilst in Fig. 5 there is a central cylindrical portion d.

In all the forms shown herein, the internal bore of the cylinder is cylindrical, i. e. without taper.

The internal bore of the liner will be finished after assembly to eliminate any cylinder distortion.

In machining the parts, the cylinder-bore is preferably honed, so as to provide relatively microscopic undulations in cross lines. whilst lthe outer surface of.the liner is relatively rough ground.

The method of assembly is to freeze the liner and heat the cylinder until the contraction of the one and the expansion of the other exceeds the interference. including the effect of the taper, when the liner is slipped into the bore of the cylinder body. As the parts assume an equal temperature the interference is established, the

liner expanding and the body contracting until the complementary surfaces come together, expelling air between the surfaces. Any air trapped between'the surfaces appears ultimately to be dispersed through the pores of the metal. The pressure of the interference fit is such that the slight undulations or roughness formed by the machine finish of the liner and cylinder body, and the grain thereof are forced one into the other, according to whichever yields first providing partial compacting of the surfaces and This result produces an increased contact area and provides foreilicient heat interchange. The slight relative taper produces a pressure gradient because the interference throughout the length of contact is a progressive graduation.

v Obviously the metals must be carefully selected for their essential properties of expansion coefilcient and strength as well as for their suitability for the other required known characteristics and the degree of interference llt must be mich that at the low temperature limit of normal working, the pressures due to difference of Iexpansion coefficient will not cause fracture or 'exceed the elastic limit so as to crush either metal with the effect of loosening the liner before the Jternperature .limit is reached at which must fstill remain som-e ldegree of interference fflt.

The invention is obviously not limited to all vtlie :details of the examples above described, for instance "other metals than those specified could be used 'for the lcylinder body and liner. `the .receiving bore in the cylinder body could be made ita-pered las vwell as lor instead of the taper fof vthe .liner ibefore .insertion of the liner whilst :still providingfa zslightlrelative taper so that there 'will be a progressive range of interference pres- .sure as naturally occur in the case of Fig. 1. Moreover., if y:desired an intermediate metal may be appliedz-sayiinfathin layer, to either the liner or cylinder bore where such will provide better bonding to the contacting surfaces of the metals which are selected for the cylinder body and' liner respectively.

What we claim is:

1. The method of securing a preformed liner of one metal in a preformed housing of another metal such as a steel liner in an aluminum cylinder body of an internal combustion engine wherein the liner metal has a relatively lower.

coeflicient of expansion than the metal of the housingwhich includes the step of slightly tapering the housing and liner axially in two directions and of such diameters to provide complementary engaging surfaces having a relative in- Also -coeiiicient of expansion than the housing metal which includes the step of slightly tapering the housing and liner axially in two directions and of such diameters as to provide complementary engaging surfaces having a relative interference fit having pressures which are in a gradient in both directions axially and including the'further step of creating a temporary substantial difference of temperature sufficient to temporarily remove said interference fit whereby the liner is secured in the housing by shrinkage.

-3. 'I'he method of securing a preformed liner of one metal in a preformed housing of another metal such as a steel liner in an aluminum cylinder body of an internal combustion 'engine wherein the liner metal has a relatively lower coefficient of expansion than the housing metal which includes the step of slightly tapering the housing and liner axially in two directions and of such diameters as to provide complementary engaging surfaces having a relative interference fit having pressures which are in a gradient in both directions axially including forming in the complementary engaging surfaces of the housing and liner slight and relatively crossing undulations.

4. The combination of an aluminum cylinder of an internal combustion engine, and a steel liner having a relatively lower coefficient of expansion than the cylinder, the liner and the cylinder being preformed and slightly tapered axially in two directions forming complementary engaging surfaces having a relative interference fit having pressures which are in a gradient in two directions axially.

5. The combination of an aluminum cylinder of an internal combustion engine, and a steel liner having a relatively lower coefficient of expansion than the cylinder, the liner and the cylinder'being preformed and slightly tapered axially in two directions forming complementary engaging surfaces having a relative interference fit having pressures which are in 1a gradient in two directions axially.. one of said complementary engaging surfaces being smooth and provided with undulations.

6. The combination of an' aluminum cylinder of an .internal combustion engine, and a steel liner having a relatively lower coefficient of expansion than the cylinder, the liner and the cylinder being preformed and slightly tapered axially in two directions forming complementary engaging surfaces having a relative interference fit having pressures which are in a gradient in two directions axially, one of said complemens,ss7,e7 1 v nt having pressures which are in a gradient in two directions axially.

8. The combination ot a cylinder of an internal combustion engine, and a liner having a relatively lower co-eilicient of expansion than the cylinder, the liner and cylinder being preformed and slightly tapered in two directions, forming complementary engaging surfaces having a relative interference ilt having pressures which are in a gradient in two directions axially.

9. For use with an aluminum pre-formed internal combustion engine cylinder slightly tapered axially in two directions, a pre-formed steel liner having a relatively lower co-efiicient of expansion than the cylinder and slightly tapered axially in two directicnsand sized and shaped to have an interference ilt in the cylinder and having pressures which are in a gradient in two directions axially when the cylinder is shrunk on the liner.

10. For use with a pre-formed steel liner slightly tapered axially in two directions. a preformed aluminum internal combustion engine cylinder having a relatively higher co-eilicient of expansion than the liner and slightly tapered axially in two directions and sized and shaped to have an interference tit with the liner and having pressures which are in a gradient in two directions axially when the cylinder is shrunk on the liner.

FRANK M. ASPIN. FREDERICK ELLINGHOUBE.