GB2161242A - Seal/bearing member for piston - Google Patents
Seal/bearing member for piston Download PDFInfo
- Publication number
- GB2161242A GB2161242A GB08517272A GB8517272A GB2161242A GB 2161242 A GB2161242 A GB 2161242A GB 08517272 A GB08517272 A GB 08517272A GB 8517272 A GB8517272 A GB 8517272A GB 2161242 A GB2161242 A GB 2161242A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- sleeve
- bearing
- cylinder
- piston core
- 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.)
- Granted
Links
Classifications
-
- 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
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3204—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings with at least one lip
-
- 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
- F16J1/02—Bearing surfaces
-
- 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
- F05C2225/00—Synthetic polymers, e.g. plastics; Rubber
- F05C2225/04—PTFE [PolyTetraFluorEthylene]
Abstract
A piston and cylinder oil-free compressor has a cylinder and a piston which reciprocates therein the piston having a non-deformable core (7) and a bearing or wear sleeve (8) formed of a material offering sliding wear resistance compatible with the cylinder and being provided with an integral resiliently deflectable seal (10) which maintains sealing engagement with the bore of the cylinder. Other embodiments are also shown. <IMAGE>
Description
SPECIFICATION
Piston and cylinder apparatus
This invention relates to piston and cylinder apparatus and relates especially but not exclusively to such apparatus wherein a piston is intended to operate in a cylinder without added lubrication.
The most commonly used air compressors for charging reservoirs in compressed air systems such as installed on vehicles for braking and other functions employ conventional metallic piston reciprocably slideable in cast iron cylinder bores and they require a suitable lubricating oil supply. Such compressors are usually driven by the vehicle engine and also receive their lubricating oil supply from the engine. There is, therefore, an inherent practical constraint placed upon the positioning of the compressor on the vehicle.
Additionally, such compressors tend to permit carry-over of oil vapour or droplets with the compressed air into the compressed air system and precautions such as filters and drain valves are essential to prevent such oil reaching sensitive working parts of the system. Such filters tend to become blocked and therefore require frequent replacement.
Various proposals have been made to construct substantially "oil-free" piston and cylinder compressors the bearings of which have sealed-in lubrication and one object of the invention is to provide an improvement to such compressors.
According to the present invention there is provided a piston and cylinder apparatus having a substantially non-deformable piston core characterised by a bearing or wear sleeve located thereon before insertion into the cylinder bore, sald sleeve being formed of a material offering sliding wear resistance compatible with the cylinder bore and being provided with an integral inwardly resiliently deflectable compression seal slidingly and sealingly engageable with the cylinder bore.
In one embodiment said bearing or wear sleeve extends over the full length of the skirt of the piston and is provided with an inner bead locatable with the piston core.
The moulded sleeve may be closed at one end so as to enclose the head of the piston core.
In an alternative embodiment, said bearing or wear sleeve may be located in a circumferential groove of the piston.
In an embodiment when the groove of the piston is located near the top of the piston a further bearing or wear ring may be located in a groove near the lower end of a skirt of the piston.
In order that the invention may be more clearly understood and readily carried into effect the same will be further described by way of example with reference to the accompanying drawings of which:
Figure 1(a) illustrates one example in part-sectional diagrammatic view,
Figure 1(b) illustrates in its free state a moulded piston sleeve used in the apparatus of Fig. 1.
Figure 1(c) is a further view of the moulded sleeve taken on the direction of the arrow 'A'.
Figures 2 and 3 illustrate an alternative embodiments and
Figure 4 illustrates an example of a double acting piston assembly.
Referring to the part-sectional view of a portion of a single cylinder air compressor, as shown in
Fig. 1 of the drawing, the cylinder is denoted by reference 1 and a cylinder head and valve-plate assembly which is normally bolted on is represented by the block 2. The gudgeon pin end of a connecting rod 3 is provided with a sealed-in needle bearing 4 and a gudgeon pin 5 with end pads, one of which is shown at 6. The gudgeon pin 5 is retained in an aluminium piston core 7 by means of lockedin set screws 16. The piston core 7 is provided with a moulded polytetrafluorethylene cup-shaped bearing shroud 8 before insertion into aluminium bore of cylinder 1. The natural moulded form of the skirt of shroud 8 is as shown at 9 in Fig. 1(b) of the drawings.The lower edge of the skirt carries an inwardly projecting bead 12 of thickness which varies as shown in Fig. 1(c) and which when deflected inwards engages a rebate at the lower edge 13 of the skirt of the inner core 7. To permit such inward deflection the skirt of the cup-shaped liner has axial slots such as 15 extending upwards to a point somewhat below the root of the sealing part 10.
Surrounding a head-portion 14 which is of smaller diameter than the remainder of the piston skirt, there is resiliently deformable annular sealing part 10, the undeformed shape of which is shown in
Fig. 1(b). In order to insert the thus assembled piston in the cylinder the skirt 9 of the shroud and the annular seal part 10 are compressed inwardly to reduce this diameter to fit the cylinder bore and upon entry into the bore. The inwardly projected bead 12 is thus brought into engagement with the lower edge rebate 13 of the piston core thereby retaining the liner and the piston core together in operation.
As an alternative to the bead 12 engaging with the lower edge of the piston core, lugs may be provided within the shroud 8 to locate in the transverse gudgeon pin recesses of the piston core 7 to retain the sleeve in position on the core.
Referring to Fig. 2, an alternative piston construction is shown wherein the gudgeon pin end of a connecting rod 23 is provided with a sealed bearing or bush 24 and the gudgeon pin is again located in the core of the piston by a small locked locating set-screw 25. The piston core is formed of a lower part 21 between which and an upper part 22 is clamped, by screws 20, an an inwardly projecting annular retaining bead 26 of a carbon-filled polytetrafluorethylene bearing sleeve. The bearing sleeve has a resiliently deformable seal bead 28 similar to the seal bead 11 of Fig. 1 and a similarly slotted skirt portion 29 with a lower inwardly projecting bead 30 locating in an annular rebate 31 formed in the lower edge of the piston core part 21.
In a variant of Fig. 2 the lower bead 30 may be dispensed together with and the mentioned slots.
The skirt is then required simply to be press-fitted over the lower part 21 of the piston core before at tachment of the upper part 22.
In yet another variant of the arrangement shown in Fig. 2, the gudgeon pin 25 may be located by screws such as 20 which are positioned and having projections made long enough to extend into one or more suitable locating holes provided in the gudgeon pin.
In yet another variant of the arrangement of Fig.
2 the mentioned holes in the gudgeon pin may be tapped with screw threads to receive the screws 20 which are then preferably a clearing fit in the lower part of the piston core.
In yet another bariant, the lower part of the piston core may be cut away in way of the gudgeon pin permitting assembly of the gudgeon pin thereto from beneath to be retained in position by screws tapped into the gudgeon pin.
In a further variant on the arrangement shown in Fig.1 the bearing shroud (8) may be replaced, as shown in Fig. 3 by upper and lower bearing rings 40 and 41 located in respective grooves 42 and 43 formed in the main body 44 of an aluminium air compressor piston. As in the cases of Figs. 2 and 3, the gudgeon pin 45 is located in the transverse bore 46 of the piston by at least one retaining screw 47. The connecting rod 48 is pivotable on a sealed bush or bearing 49 as before.
The upper bearing-ring 40 is fomred with a section generally as shown on an enlarged scale in
Fig. 4b from which it will be seen that this ring comprises an upper thickened bearing-portion 50 and a lower portion 51 which extends radially upwards and is deflectable through a position such as shown dotted when the piston is inserted in an aluminium bore of a cylinder indicated by the broke lines 52 of Fig. 3(a).
The upper bearing-ring 40 and the lower bearing-ring 41 are manufactured by compression moulding or by machining from a suitably carbonfilled polytetrafluorethylene material but other suitable plastics materials such as polyetheretherketone may be used. The dimensions of these bearing-rings and the depth of the upper and lower grooves 42 and 43 formed in the piston body 44 are such as to permit the bearing-rings 40 and 41 to be stretched over the external diameter of the main body 44 to locate in the respective sections.
The essential requirement for the war-rings is that they both shall jointly operate to prevent contact between the piston 44 and the interior of the cylinder bore 52 and a sufficiently good degree of sealing is provided by the seal-portion 51 through the useful life of the compressor.
Referring now to the double acting piston and cylinder apparatus as part-shown in Fig. 4, a nondeformable piston core 32 is carried on a spigot 38 of a piston rod 39. A resiliently deformable polytetrafluorethylene wear sleeve 33 is stretched over the periphery of the piston, an inner bead 34 of the sleeve serving to position and retain the sleeve on the piston core by engaging with a matching groove 35 of the core. The sleeve is further provided with two annular deformable seal parts 35, 36 the undeformed shape of which is again shown at 35 and 36. These seal parts are resiliently deformed on assembly to make sealing and sliding contact with the bore 37 of a cylinder as shwon and they are arranged to act in opposing senses in relation to the cylinder bore so that a double acting piston is provided with a single deformable bearing sleeve.
Whilst the piston core of each of the above described embodiments is preferably to be made of aluminium, other suitable substantially non-deformable materials may be used. In the case of suitable plastics material being used the advantages of injection or compression moulding may be enjoyed. Moreover, although the bearing or wear rings or sleeves are made of polytetrafluorethylene, other materials such as polyetheretherketone may be employed.
Claims (11)
1. A piston and cylinder apparatus having a substantially non deformable piston core characterised by a bearing or wear sleeve located thereor before insertion into the cylinder bore, said sleeve being formed of a material offering sliding wear resitance compatible with the cylinder bore and being provided with an integral inwardly resiliently deflectable compression seal slidingly and sealingly engageable with the cylinder bore.
2. Apparatus as claimed in claim 1 characterised by said sleeve comprising an upper-bearing ring and said piston core being provided with a further lower bearing-ring.
3. Apparatus as claimed in claim 2 said bearing-rings being located in respective grooves.
4. Apparatus as claimed in claim 1 characterised in that said sealingly deformable sleeve extends over the full length of a skirt of the piston and being provided with an inward projection located by the piston core.
5. Apparatus as claimed in claim 1 or 4 said sleeve being closed at one end to enclose the hea of the piston core.
6. Apparatus as claimed in claim 4 or 5 said sleeve being provided with at least one axial slot permitting fitting thereof over the piston core priol to insertion into the cylinder.
7. Apparatus as claimed in any preceding clain the piston being rotatably attached to a connecting rod via a gudgeon pin located in the piston core o the piston by means of member passing therethrough.
8. Apparatus as claimed in claim 7 said member comprising a locked screw.
9. Apparatus as claimed in any preceding clain said bearing sleeve being formed of carbon-filled polytetrafluorethylene.
10. Apparatus as claimed in any preceding claim said sleeve being formed of polyetheretherketone material or other wear-resistent plastics material.
11. Apparatus substantially as described hereii with reference to Fig. 1, 2, 3 or 4 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08517272A GB2161242B (en) | 1984-07-07 | 1985-07-08 | Seal/bearing member for piston |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB848417395A GB8417395D0 (en) | 1984-07-07 | 1984-07-07 | Piston and cylinder apparatus |
GB08517272A GB2161242B (en) | 1984-07-07 | 1985-07-08 | Seal/bearing member for piston |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8517272D0 GB8517272D0 (en) | 1985-08-14 |
GB2161242A true GB2161242A (en) | 1986-01-08 |
GB2161242B GB2161242B (en) | 1988-03-30 |
Family
ID=26287962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08517272A Expired GB2161242B (en) | 1984-07-07 | 1985-07-08 | Seal/bearing member for piston |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2161242B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1176310A2 (en) * | 2000-07-26 | 2002-01-30 | Kabushiki Kaisha Toyota Jidoshokki | PEEK compressor coating |
DE102004021589A1 (en) * | 2004-05-03 | 2005-12-01 | Continental Aktiengesellschaft | Piston ring for separating piston guided in cylinder is constructed in one piece and closed, and with recess formed on radially outwards orientated side of piston ring lying opposite rib supported in slot |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1396230A (en) * | 1972-07-21 | 1975-06-04 | Linde Ag | Pistons for reciprocating machines |
GB1424854A (en) * | 1972-03-30 | 1976-02-11 | Panigati P L | Pistons for pressure fluid operated cylinders |
GB1434648A (en) * | 1972-10-18 | 1976-05-05 | Commissariat Energie Atomique | Pump |
GB1559571A (en) * | 1976-09-24 | 1980-01-23 | Avon Ind Polymers | Piston means for piston cylinder arrangements |
-
1985
- 1985-07-08 GB GB08517272A patent/GB2161242B/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1424854A (en) * | 1972-03-30 | 1976-02-11 | Panigati P L | Pistons for pressure fluid operated cylinders |
GB1396230A (en) * | 1972-07-21 | 1975-06-04 | Linde Ag | Pistons for reciprocating machines |
GB1434648A (en) * | 1972-10-18 | 1976-05-05 | Commissariat Energie Atomique | Pump |
GB1559571A (en) * | 1976-09-24 | 1980-01-23 | Avon Ind Polymers | Piston means for piston cylinder arrangements |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1176310A2 (en) * | 2000-07-26 | 2002-01-30 | Kabushiki Kaisha Toyota Jidoshokki | PEEK compressor coating |
EP1176310A3 (en) * | 2000-07-26 | 2004-05-12 | Kabushiki Kaisha Toyota Jidoshokki | PEEK compressor coating |
DE102004021589A1 (en) * | 2004-05-03 | 2005-12-01 | Continental Aktiengesellschaft | Piston ring for separating piston guided in cylinder is constructed in one piece and closed, and with recess formed on radially outwards orientated side of piston ring lying opposite rib supported in slot |
Also Published As
Publication number | Publication date |
---|---|
GB8517272D0 (en) | 1985-08-14 |
GB2161242B (en) | 1988-03-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19960708 |