EP0692068A1 - Piston alternatif d'un moteur a combustion interne dont la surface d'usure comporte un renforcement au moins partiel - Google Patents

Piston alternatif d'un moteur a combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Info

Publication number
EP0692068A1
EP0692068A1 EP94911087A EP94911087A EP0692068A1 EP 0692068 A1 EP0692068 A1 EP 0692068A1 EP 94911087 A EP94911087 A EP 94911087A EP 94911087 A EP94911087 A EP 94911087A EP 0692068 A1 EP0692068 A1 EP 0692068A1
Authority
EP
European Patent Office
Prior art keywords
reciprocating piston
piston according
piston
reinforcement
film
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.)
Withdrawn
Application number
EP94911087A
Other languages
German (de)
English (en)
Inventor
Jürgen Ellermann
Manfred Ziegler
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.)
Mahle GmbH
Original Assignee
Mahle GmbH
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 Mahle GmbH filed Critical Mahle GmbH
Priority to EP96120559A priority Critical patent/EP0768458B1/fr
Publication of EP0692068A1 publication Critical patent/EP0692068A1/fr
Withdrawn legal-status Critical Current

Links

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 
    • F02F3/10—Pistons  having surface coverings
    • 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
    • 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
    • F05C2201/00—Metals
    • F05C2201/04—Heavy metals
    • F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
    • 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
    • F05C2201/04—Heavy metals
    • F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0448—Steel
    • 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
    • F05C2203/00—Non-metallic inorganic materials
    • F05C2203/08—Ceramics; Oxides
    • F05C2203/0865—Oxide ceramics
    • F05C2203/0882—Carbon, e.g. graphite

Definitions

  • Aluminum pistons with tread reinforcement are known per se. In many cases, such reinforcements are applied galvanically and consist, for example, of iron, nickel or chrome layers. The application of such layers is technically complex and is therefore associated with relatively high costs.
  • Another type of reinforcement consists of synthetic resin-bonded graphite layers, which can be applied, for example, using the screen printing process.
  • the invention deals with the problem of creating a tread reinforcement for a piston in a way that is as cost-effective as possible and that has a long service life while being inexpensive to manufacture.
  • FIG. 1 is a view of a piston with a local tread coating of the piston skirt
  • FIG. 2 shows a view of a piston with an additional coating in the region of the piston ring webs, including the top land,
  • FIG. 3 shows a view of a piston with a locally foil-coated piston shaft
  • FIG. 5 shows a view of a section of a film provided with different perforations
  • FIG. 6 is a view of a piston with a plate-shaped reinforcement part anchored to the shaft with a positive fit
  • Fig. 7 is a view of the reinforcement part 6 before assembly on the piston
  • FIG. 9 is a view of a piston with a plate-shaped reinforcement part in another embodiment
  • Fig. 11 is a view of the plate-shaped
  • FIG. 13 is a view of a piston head with molded hubs and a self-supporting reinforcement part anchored in them;
  • Fig. 14 is a half section through the hubs of the piston in Fig. 14 along the line XV - XV.
  • Fig. 15,16 a piston on the side Ends of cast-in plate-shaped reinforcement elements, partly in view, partly in section in directions perpendicular to one another
  • 26 shows a section through the piston along line XXVI-XXVI in FIG. 24
  • the reinforcements according to the invention are shown in dotted lines in all the embodiments described below, ie as layers, foils or reinforcement plates in a view or plan view, and are therefore not identified by a special reference number in all of the drawings.
  • a tread layer is applied to the wings of a correspondingly pre-machined piston skirt.
  • This consists of a synthetic resin into which metal particles are introduced. These metal particles can consist of nickel, iron, bronze, chromium, copper or silver, and these can be present individually or in combination with one another. Metal oxides, other metallic compounds or substances which have a favorable sliding and wear behavior are also included.
  • the synthetic resin can be, for example, a curable polyimide or polyamideimide, and solid lubricants such as graphite can also be contained in the layer.
  • the layer has a thickness of about 15 to 25 microns.
  • the diameter of the metal particles in the layer should not be more than about 15 micrometers, so that the metal particles are completely embedded in the layer.
  • the metal particles can expediently also be lamellar with a total length of at most about 50 micrometers. The width of these slats is limited to about 15 microns.
  • the layer surface should no longer be processed after it has been applied.
  • the layer can be applied, for example, in the screen printing method known per se to a correspondingly pre-processed piston. In cases where the ring lands and possibly also the fire land contact the cylinder running surface in a piston, these areas can be coated with, as shown in FIG. 2.
  • the tread reinforcement consists of a glued-on, relatively thin film with a thickness between approximately 20 and 40 micrometers.
  • the bonding can be carried out using an adhesive system known per se for heat-resistant bonding.
  • the piston base material is aluminum in all cases of the exemplary embodiments described.
  • the film to be glued can consist, for example, of nickel, iron, chromium, steel or bronze, the individual elements being present alone or in combination with one another in the form of alloys.
  • Precision foils in which the thickness is subject to extremely small tolerances, are to be used in particular as foils.
  • the foils should only be applied locally on the piston skirt, specifically on the wings on the pressure and counterpressure side of the piston skirt.
  • the foils can be perforated in various ways or can be embossed on one side in order to improve the tribology.
  • the piston skirt should not be reworked after the foils have been stuck on.
  • a precision film with a precisely defined and maintained thickness must be used.
  • the adhesive layer must not cause dimensional inaccuracies.
  • the surface on the aluminum base material to which the film is to be glued is jagged and the glue is applied so that it only comes into contact with the film in the valleys of the fissure while the The rest of the film rests on the outer tips of the fissure.
  • the fissure is expediently formed by a turning profile which is produced on a lathe with the aid of a correspondingly set feed with the turning tool. Rotary profiles of this type are defined by roughness values.
  • the turning profile should be determined by roughness values between 5 and 50 meters.
  • FIG. 4 shows how a film should lie on the tips of a rotary profile according to the invention.
  • the rotary valleys are filled there with an adhesive contacting the film.
  • the adhesive to be used should be heat resistant at least to 180 degrees Celsius.
  • a plate-shaped reinforcement part is provided, which is anchored on the piston shaft in a form-fitting manner by means of a spring lock.
  • the resilient parts of the spring lock are integrated in the plate-shaped reinforcement part.
  • tabs of the reinforcement part lying at the top and bottom in the stroke direction of the piston are designed as spring hooks according to FIG.
  • the plate-shaped reinforcement part is snapped into receiving slots (FIG. 10) of the piston skirt via horizontally attached tabs.
  • the starting form of the plate-shaped conveyor shown in FIG. 12 The actual reinforcement part is shown in FIG. 12.
  • the assembly takes place in such a way that the plate-shaped reinforcement part is simply inserted into the corresponding receiving slots of the piston shaft, as a result of which the reinforcement part adapts to the outer shape of the shaft.
  • the piston shaft is formed exclusively by a reinforcement part inserted into the hubs.
  • the piston skirt is composed of two parts, one of which is anchored on the pressure side and the other on the counter pressure side in the hubs of the piston head.
  • the reinforcement parts in question are designed and anchored in terms of strength so that they can safely absorb the transverse forces acting on the piston during engine operation.
  • the reinforcement parts each consist of spring steel, so that the spring-loaded anchoring can be camouflaged.
  • the thickness of the spring steel used is between 0.3 and 1.0 mm.
  • a reinforcement plate is cast in laterally in the area of the hubs when the piston is cast. In the area of the hub bores, an opening is recessed in each of these reinforcement plates.
  • the two reinforcement plates each protrude into the support sides of the piston skirt, where, however, they end circumferentially at a distance from one another.
  • the reinforcement plates must have sufficient strength to absorb the piston side forces.
  • the thickness of the reinforcement plates is approximately one Range of 2 mm.
  • the reinforcement plates of the piston which can also be called strips, are machined on the outer surface.
  • the shape of the outer surface corresponds to the shape of the piston.
  • a reinforcement plate lies on the piston base material on the pressure / counterpressure side of the piston skirt, each with an anchoring within the piston base material in the hub area.
  • This anchoring is achieved in casting the piston by casting the horizontal ends of the reinforcement plates, which for this purpose are bent approximately at right angles and provided with undercuts as seen in the radial direction.
  • the undercuts can be achieved by appropriate shaping of the reinforcement plates, which for this purpose are wave-shaped or can be provided with holes.
  • the reinforcement plates run practically over the entire shaft height and can have lateral recesses. As a result, they can have the shape of a double-T profile with horizontal T-bars lying at the top and bottom of a piston-shaft support side shown in the view. It is important for the function that with the piston alone the reinforcement plates contact the cylinder barrel structure of the engine. This means that the piston base material must be radially recessed in the lateral recesses of the reinforcement plates.
  • the piston according to FIGS. 21-23 differs from that according to FIGS. 18-20 practically solely in that the reinforcement plates in the bearing areas of the piston rest frame-like on the piston base material only on their edges, while the piston base material is recessed within these frame areas. In these areas that are spared from the piston base material, the reinforcement plates must be able to absorb the piston lateral forces alone, ie the force is transferred to the piston base material solely via the support edge areas of the reinforcement plates.
  • the edge support area of the reinforcement plates on the piston base material is further reduced by the fact that there is no horizontal support at the lower end of the piston.
  • the reinforcement plates are anchored laterally over their entire height in the base material of the hub area.
  • the reinforcement plates can each have recesses in a circumferential area. These recesses are expediently located laterally at some distance from the area in which the connecting rod oscillation plane intersects the shaft jacket contour, so that the shaft can have a bearing function with respect to the cylinder raceway in this cutting area.
  • the piston designs according to the invention are particularly suitable for use in engines in which the cylinder running surface and the piston base material are aluminum in equal measure.
  • reinforcement of an aluminum piston is imperative.
  • the previously applied galvanic metal layers are technically functional, but are associated with a high cost-intensive manufacturing effort.
  • the alternatives according to the invention are considerably cheaper to produce with at least the same good function. bar,

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)

Abstract

L'invention vise à réaliser un renforcement économique et résistant pour la surface d'usure du piston alternatif d'un moteur à combustion interne, notamment un piston alternatif dont le matériau de base est un alliage d'aluminium et qui est destiné tout particulièrement à un moteur dont la surface d'usure du cylindre est réalisée dans un alliage d'aluminium. Il s'agit à cet effet de remplacer les revêtements en fer, en nickel ou en chrome appliqués par galvanisation utilisés jusqu'à maintenant, par une couche de graphite liée par une résine synthétique, qui comporte des particules de métal incorporées. Les particules de métal peuvent être du nickel, du fer, du bronze, du chrome, de l'argent ou des alliages de ces différents métaux. La couche d'usure peut également consister en une pellicule de métal collée. Une autre possibilité consiste à réaliser la couche d'usure à l'aide de plaques de métal ancrées mécaniquement ou fondues sur la tige du piston.
EP94911087A 1993-03-31 1994-03-28 Piston alternatif d'un moteur a combustion interne dont la surface d'usure comporte un renforcement au moins partiel Withdrawn EP0692068A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP96120559A EP0768458B1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur à combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE4310491 1993-03-31
DE4310491A DE4310491A1 (de) 1993-03-31 1993-03-31 Hubkolben eines Verbrennungsmotors mit einer zumindest teilweisen Laufflächenbewehrung
PCT/DE1994/000351 WO1994023193A1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur a combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Related Child Applications (1)

Application Number Title Priority Date Filing Date
EP96120559A Division EP0768458B1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur à combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Publications (1)

Publication Number Publication Date
EP0692068A1 true EP0692068A1 (fr) 1996-01-17

Family

ID=6484343

Family Applications (2)

Application Number Title Priority Date Filing Date
EP94911087A Withdrawn EP0692068A1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur a combustion interne dont la surface d'usure comporte un renforcement au moins partiel
EP96120559A Expired - Lifetime EP0768458B1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur à combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP96120559A Expired - Lifetime EP0768458B1 (fr) 1993-03-31 1994-03-28 Piston alternatif d'un moteur à combustion interne dont la surface d'usure comporte un renforcement au moins partiel

Country Status (5)

Country Link
EP (2) EP0692068A1 (fr)
JP (1) JPH08508324A (fr)
BR (1) BR9406242A (fr)
DE (2) DE4310491A1 (fr)
WO (1) WO1994023193A1 (fr)

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US5469777A (en) * 1994-07-05 1995-11-28 Ford Motor Company Piston assembly having abradable coating
DE19919725A1 (de) 1999-04-30 2000-11-02 Mahle Gmbh Kolbenmotor mit einem Zylinder aus Leichtmetall
US6662773B2 (en) 2000-05-26 2003-12-16 Audi Ag Cylinder crankcase for an internal combustion engine
DE10026290B4 (de) * 2000-05-26 2007-05-24 Audi Ag Zylinderkurbelgehäuse für eine Brennkraftmaschine
US7171936B2 (en) * 2003-10-23 2007-02-06 Mahle Technology, Inc. Piston having a patterned coating and method of applying same
US7051645B2 (en) * 2004-06-30 2006-05-30 Briggs & Stratton Corporation Piston for an engine
US8240676B2 (en) 2006-02-28 2012-08-14 Nippon Piston Ring Co., Ltd. Piston ring
EP2184477B1 (fr) * 2007-08-24 2013-04-17 Honda Motor Co., Ltd. Piston d'un moteur à combustion interne
DE102008006854A1 (de) * 2008-01-31 2009-08-06 Bayerische Motoren Werke Aktiengesellschaft Kolben mit Drahtkissenkörper
DE202009015247U1 (de) 2009-11-09 2010-03-04 Schreiner Group Gmbh & Co. Kg Schichtverbund zur Aufbringung auf planaren oder gekrümmten Oberflächen
JP5642624B2 (ja) * 2010-09-09 2014-12-17 本田技研工業株式会社 摺動部材の製造方法及び摺動部材
US9181897B2 (en) 2011-04-06 2015-11-10 Honda Motor Co., Ltd. Sliding member and method for producing sliding member
JP5763390B2 (ja) * 2011-04-06 2015-08-12 本田技研工業株式会社 摺動部材の製造方法及び摺動部材
JP5840485B2 (ja) * 2011-12-28 2016-01-06 本田技研工業株式会社 内燃機関用ピストン
DE112012005520B4 (de) 2011-12-28 2022-11-17 Honda Motor Co., Ltd. Kolben für Verbrennungsmotor
JP5815399B2 (ja) * 2011-12-28 2015-11-17 本田技研工業株式会社 内燃機関用ピストンの製造方法
JP6144907B2 (ja) * 2012-12-13 2017-06-07 株式会社シンク・ラボラトリー 摺動面被覆用微細金属パターンシートの製造方法
JP6476817B2 (ja) * 2014-12-12 2019-03-06 アイシン精機株式会社 内燃機関用ピストンおよび内燃機関用ピストンの製造方法
DE102016205627A1 (de) * 2016-04-05 2017-10-05 Elringklinger Ag Kolben und Kolbenvorrichtung
FR3061756B1 (fr) * 2017-01-11 2019-05-10 H.E.F. Piston pour machine thermique, machine thermique comprenant un tel piston, et procedes
CN109113891A (zh) * 2017-06-26 2019-01-01 华晨汽车集团控股有限公司 一种增压发动机曲柄连杆系统
DE102019122878A1 (de) * 2019-08-27 2021-03-04 Man Energy Solutions Se Kolben und Zylinder einer Brennkraftmaschine und Brennkraftmaschine

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See also references of WO9423193A1

Also Published As

Publication number Publication date
WO1994023193A1 (fr) 1994-10-13
EP0768458B1 (fr) 2000-06-07
DE59409395D1 (de) 2000-07-13
DE4310491A1 (de) 1994-10-06
EP0768458A3 (fr) 1997-05-02
BR9406242A (pt) 1996-02-06
EP0768458A2 (fr) 1997-04-16
JPH08508324A (ja) 1996-09-03

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