US20040177902A1 - Aluminium wrought alloy - Google Patents

Aluminium wrought alloy Download PDF

Info

Publication number
US20040177902A1
US20040177902A1 US10/798,082 US79808204A US2004177902A1 US 20040177902 A1 US20040177902 A1 US 20040177902A1 US 79808204 A US79808204 A US 79808204A US 2004177902 A1 US2004177902 A1 US 2004177902A1
Authority
US
United States
Prior art keywords
weight
aluminium
elements
group
layer
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.)
Abandoned
Application number
US10/798,082
Other languages
English (en)
Inventor
Robert Mergen
Markus Manner
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.)
Miba Gleitlager Austria GmbH
Original Assignee
Miba Gleitlager Austria 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=32234879&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=US20040177902(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Miba Gleitlager Austria GmbH filed Critical Miba Gleitlager Austria GmbH
Assigned to MIBA GLEITLAGER GMBH reassignment MIBA GLEITLAGER GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MANNER, MARKUS, MEREN, ROBERT
Publication of US20040177902A1 publication Critical patent/US20040177902A1/en
Assigned to MIBA GLEITLAGER GMBH reassignment MIBA GLEITLAGER GMBH CORRECTIVE ASSIGNMENT PREVIOUSLY RECORDED AT REEL; 015080 FRAME: 0782 TO CORRECT ASSIGNOR'S NAME. Assignors: MANNER, MARKUS, MERGEN, ROBERT
Abandoned legal-status Critical Current

Links

Images

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121—Use of special materials
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2204/00—Metallic materials; Alloys
    • F16C2204/20—Alloys based on aluminium
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]

Definitions

  • the invention relates to an aluminium wrought alloy with an aluminium matrix in which a soft phase and hard particles are incorporated, the soft phase being an element from a first group of elements consisting of tin, antimony, indium and bismuth and the hard particles being scandium and/or zirconium and at least one element from a second group of elements consisting of copper, manganese, cobalt, chromium, zinc, magnesium, silicon and iron, as well as scandium and/or zirconium or inter-metallic phases of scandium, zirconium with aluminium or aluminium with the elements from the second group, a base layer for a bearing element made therefrom, which can be disposed between a protective shell and a running layer of the bearing element, as well as a bearing element with a protective shell, a running layer and a base layer disposed in between.
  • This type of bearing generally consists of a protective shell (usually made of steel) designed to absorb mechanical stress, on top of which a layer of the respective bearing alloy is applied.
  • a protective shell usually made of steel
  • Another thin coating also known as an “overlay”
  • This other, very thin layer normally contains a very high proportion of so-called soft phases, such as lead or tin for example, which impart to this layer an ability to adapt to and embed abraded material from the parts to be mounted, such as shafts. Due to the fine thickness of this “overlay”, this layer is also mechanically capable of withstanding a sufficient degree of stress and serves as the so-called running layer.
  • the bearing metal layer underneath ensures that the bearing also remains serviceable even if the running layer is extensively worn, for which purpose this bearing metal layer also contains an appropriate proportion of so-called soft phases.
  • a barrier may be provided between the running and bearing metal to prevent migration, for example of tin. This diffusion barrier may be made from nickel.
  • binding film between the protective shell and the bearing metal, in order to compensate for the properties specific to the materials of the two layers with a view to obtaining sufficient cohesion of the bearing, even when subjected to extensive stress.
  • This binding film may be made from aluminium, for example.
  • a bearing of this type is known from patent specification WO 98/17833 A.
  • This WO-A patent describes in particular an aluminium alloy for a layer, specifically for a plain bearing, which is free of silicon except for the impurities resulting from the melting process, and, in addition to tin, contains as the main alloying element, at least one element each from the group of elements consisting of lead and bismuth on the one hand and from the group consisting of magnesium and zinc on the other.
  • the minimum proportion of tin is 16% by weight. All the other elements in the alloy are limited to a total of at most 11% by weight.
  • the proportion of the respective element from the group which also contains antimony and indium in addition to lead and bismuth is between 10% and 75% of the maximum solubility of the respective element by reference to the total tin content.
  • aluminium alloys for plain bearings which contain tin as the main alloying element should contain an added hard substance selected from at least one element from the group of elements consisting of iron, manganese, nickel, chromium, cobalt, copper, platinum, magnesium and antimony in order to create inter-metallic phases, e.g.
  • aluminides in the boundary regions of the matrix, in which case another element from a second group of elements consisting of manganese, antimony, chromium, tungsten, niobium, vanadium, cobalt, silver, molybdenum and zirconium should be added as a substitute for a part of at least one hard substance from the first group of elements in order to increase almost spherical or cuboid aluminides. This reduces the nicking effect of these hard particles, so that the aluminium alloy can contain a higher proportion of soft phases, which also specifically improves resistance to galling.
  • This aluminium alloy also contains silicon in a quantity of from 0.2% by weight to 2.0% by weight and it is specified that the ratio of the proportion of copper as a percentage by weight to the proportion of nickel as a percentage by weight and the proportion of manganese as a percentage by weight to the proportion of silicon as a percentage by weight should be between 0.6 and 1.5.
  • the silicon increases hardness and reduces susceptibility to corrosive wear, preventing the formation of coarse aluminium-copper-manganese phases, instead of which preferred nickel-copper-aluminides and manganese-silicon aluminides are formed. After a heat treatment at 250° C., these aluminides are also finely distributed.
  • An aluminium-tin alloy containing 7% to 20% of tin is known from patent specification DE 43 32 433 A1.
  • the bearing alloy additionally contains up to 4% silicon along with other alloying elements, such as manganese, magnesium, vanadium, nickel, chromium, zirconium, copper, antimony or titanium, for example.
  • the mechanism whereby silicon causes the matrix to harden is said to be due to the fact that it crystallises out of the aluminium matrix in the form of silicon particles, which thereby increases the strength of the bearing alloy overall. Since the silicon particles are distributed throughout the structure, only the soft aluminium matrix at the surface becomes worn, so that the surface becomes microscopically uneven.
  • the silicon particles left behind as convex particles are capable of withstanding a high load, whilst simultaneously preserving the property of not bonding.
  • the concave parts hold the oil so that the bearing alloys are able to withstand high load provided they have a thin film of oil and are in metal-to-metal contact.
  • the finely distributed silicon particles fulfil another finction in that they wear down minute irregularities and burrs on the co-operating shaft, thereby improving resistance to corrosive wear.
  • An alloy described in both of the above-mentioned documents may contain, for example, 0.15% by weight to 1.0% by weight of scandium, a total of 3% by weight of one of the elements selected from manganese, copper or zirconium, a total of 4% by weight of one of the elements selected from chromium, iron and cobalt as well as tin in a quantity of up to 6.5% by weight.
  • the hardening effect is based on the fact that scandium forms so-called A 3 M phases with aluminium and the finely dispersed distribution of these A 3 M phases imparts a high ductility to these alloys, which nevertheless exhibit no marked hardening behaviour.
  • Patent specification DE 36 40 698 A1 discloses a bearing alloy with an aluminium base, which contains at least one element for the purpose of forming soft phases, selected from the group consisting of lead, tin, indium, antimony or bismuth, as well as silicon as a hard element and other reinforcing elements selected from the group consisting of copper, chromium, magnesium, manganese, nickel, zinc and iron, as well as refining elements from the group consisting of titanium, boron, zirconium, vanadium, gallium, scandium, yttrium and elements selected from the rare earths with atomic numbers 57 to 71.
  • Patent specification DE 43 19 867 A discloses a multi-layer plain bearing, which, in addition to a protective shell of steel and an overlay containing polytetrafluoroethylene, contains 5% by volume to 30% by volume of a metal filler and 5% by volume to 40% by volume of polyvinylidene fluoride, and has a bearing layer of bronze, such as a tin bronze or tin-lead bronze, disposed in between.
  • a bearing layer of bronze such as a tin bronze or tin-lead bronze
  • a comparable multi-layer bearing is known from patent specification EP 0 005 560 A, onto the metal support layer of which a porous base layer is sintered, containing 5% by weight to 25% by weight of lead, 5% by weight to 15% by weight of tin, the rest being copper, with polytetrafluoroethylene in turn deposited in the pores of the base layer.
  • the objective of the invention is to propose a multi-layer plain bearing of simplified structure and at least the same durable, tribological properties as conventional multi-layer plain bearings.
  • the composition of the aluminium alloy proposed by the invention is such that the overlay can be applied directly onto the base layer, which is disposed on the protective shell, which is made from steel for example, which means that the conventionally used binding layer and the nickel barrier can be dispensed with.
  • the composition also obviates the need for the lead bronzes used as standard in high-performance bearings, enabling the use of materials and metals which are as far as possible harmless in terms of their toxicity and suitability for recycling.
  • the use of lead alloys can be dispensed with.
  • the strength and in particular the dynamic strength of the resultant bond can be produced to higher values than is currently possible with standard three-layer bearings and using conventional steel/AlZn4,5 bonding.
  • the tribological properties are also comparable with those of AlSn6CuNi.
  • a further advantage is the high resistance to corrosion in contact with heavy oil and during use in gas-powered engines as well as resistance to cavitation as compared with AlZn4,5.
  • the bond with steel can be produced without the need for an adhesion-imparting intermediate layer.
  • the base layer may also be used for sputter bearings.
  • Yet another advantage is the fact that the cost of manufacturing these types of bearing elements is comparable with that of existing standard multi-layer bearings of the same quality.
  • the aluminium alloy proposed by the invention has the requisite resistance to galling due to its capacity for plastic deformation, enabling it to adapt to geometric faults and variations, i.e. even if faults occur in the overlay due to stress, the bearing element will still continue to be serviceable.
  • An appropriate matrix toughness is obtained by means of the A 3 M phases of scandium and zirconium with aluminium known from the prior art.
  • the proportion of soft phase in the aluminium alloy is at least 0.1% by weight and the proportion of the element(s) from the second group of elements represent(s) at least a total of 0.1% by weight, and the proportion of scandium and zirconium totals at least 0.05% by weight, in particular 0.1% by weight, whilst the proportion of zirconium is in the range of between 0.01% by weight and 0.5% by weight, in particular in the range of between 0.05% by weight and 0.23% by weight, and the proportion of scandium is between 0.05% by weight and 0.5% by weight, in particular in the range of from 0.05% by weight to 0.25% by weight.
  • the base layer is disposed directly on the protective shell, which simplifies the structure accordingly.
  • an alloy with a base of lead, tin, bismuth, indium or copper for the overlay or the overlay may be a layer of plastic, in particular selected from a group consisting of polyamide 6, polyamide 66, POM, silicone, PEK, PI, TPI, PEEK, PPS, PVDF, PTFE, as well as mixtures thereof, enabling the aluminium alloy proposed by the invention and the bearing element containing it to be adapted to a whole range of different applications.
  • the layer of plastic contains a solid lubricant, such as MoS 2 , graphite or similar for example, in which case the bearing properties of this plastic layer will be further enhanced, enabling the bearing element to be used without any or with only the smallest quantities of lubricant, such as a lubricating oil or lubricating grease, for example.
  • a solid lubricant such as MoS 2 , graphite or similar for example
  • the overlay may also be provided in the form of a lubricating varnish.
  • FIG. 1 illustrates a bearing element in the form of a plain bearing half-shell
  • FIG. 2 is a table setting out various aluminium alloys proposed by the invention.
  • FIG. 3 plots a comparison of tension-elongation values for various aluminium alloys.
  • FIG. 1 illustrates a bearing element 1 proposed by the invention in the form of a plain bearing half-shell.
  • bearing elements 1 in the form of plain bearing half-shells and may also be used for other bearing elements 1 of the type made from aluminium alloy, such as thrust rings, for example.
  • bearing elements can be produced not only as half-shells but also as full shells.
  • the bearing element 1 illustrated in FIG. 1 is made up of a protective shell 2 , a base layer 3 proposed by the invention and a running layer 4 .
  • the protective shell 2 is usually made from steel, but may naturally also be made from other similar materials which fulfil the same or a similar function, that is to say will provide the mechanical strength required of the bearing element 1 .
  • the mechanical strength of the bearing element 1 as a whole will depend on the respective application for which it will be used, and, this being the case, a whole variety of copper alloys may be used, such as brass, bronzes, for example.
  • the protective shell 2 also imparts a certain degree of dimensional stability.
  • the base layer 3 is made from the aluminium alloy proposed by the invention. It consists of an aluminium matrix incorporating at least one soft phase as well as hard particles.
  • the at least one soft phase is at least one element selected from a group of elements consisting of tin, antimony, indium and bismuth.
  • the hard particles are at least one element selected from a second group of elements consisting of copper, manganese, cobalt, chromium and iron or the elements scandium and/or zirconium. These hard particles might also be provided in the form of inter-metallic phases comprising the latter elements or the elements from the second group of elements with aluminium or inter-metallic phases comprising said elements.
  • the soft phases on the one hand impart to the base layer 3 the capacity to form a strong enough bond with the running layer 4 disposed on top and on the other hand impart the requisite galling resistance to the bearing element 1 if faults occur in the running layer 4 whilst the bearing element 1 is in operation, thereby enabling the base layer 3 to come into almost direct contact with a component to be supported, such as a shaft, for example.
  • the bearing element 1 is also rendered capable of embedding any hard particles which emerge due to wear when the bearing element 1 is in service. The hard particles impart the requisite mechanical strength to the aluminium alloy.
  • Suitable alloys for the running layer 4 are those with a base of tin, bismuth, indium or aluminium and optionally with a lead base or an alloy with a base of CuPb and a high lead content. Tin alloys with a high content of tin offer particular advantages.
  • Bearing metals with a lead base which might be used include, for example, PbSb10Sn6, PbSb15Sn10, PbSb15SnAs, PbSb14Sn9CuAs, PbSn10Cu2, PbSn18Cu2, PbSn10TiO2, PbSn9Cd, PbSn10.
  • Bearing metals with a tin base include SnSb8Cu4 and SnSb12Cu6Pb, for example.
  • the running layer 4 may also be made from a coating of plastic.
  • plastic particularly advantageous examples are polyamide 6, polyamide 66, polyoxymethylene (POM), various silicones, polyaryl ether ketone (PEK), polyimide (PI), TPI, polyaryl ether ether ketone (PEEK), polyphenylene sulphide (PPS), polyvinylidene difluoride (PVDF), polytetrafluoroethylene (PTFE) and various mixtures thereof.
  • additives may also be used in order to increase the mechanical strength of the plastic layer, such as fibre matrices, such as aramide fibres, for example, or hard substances such as carbides, oxides, nitrides, for example.
  • the plastic layer may also be provided in the form of a so-called lubricating varnish.
  • Said plastics enable running layers 4 with good sliding and anti-galling properties to be obtained, which may also be used dry. They are distinctive due to their low maintenance requirements. It is possible to operate with only a small quantity of lubricant or no lubricant at all. Water may optionally be used for lubricating purposes, which is of particular advantage if the bearing element 1 proposed by the invention is used for pumps, for example. Apart from offering a corresponding weight reduction, susceptibility to nicking has also been found to be low.
  • the bearing element 1 proposed by the invention may also be used for a whole range of other applications and in particular can be used as a plain bearing or as a thrust ring in the automotive industry.
  • the aluminium alloy proposed by the invention contains the element(s) from the first element group in a quantity totalling a maximum of 4.5% by weight, the element(s) from the second group of elements in a maximum quantity of 3.5% by weight, scandium and zirconium in a total quantity of. 0.8% by weight maximum, the rest being aluminium and the usual impurities resulting from the melt.
  • the proportion of soft phase in other words the elements from the first group of elements, represent at least 0.1% by weight.
  • the proportion of the element(s) from the second group of elements represent(s) a total of at least 0.1% by weight.
  • the proportion of scandium and zirconium also represents a total of at least 0.1% by weight.
  • the proportion of zirconium may be in the range of between 0.05% by weight and 0.5% by weight, in particular in the range of between 0.05% by weight and 0.23% by weight, and the proportion of scandium may be between 0.05% by weight and 0.5% by weight, in particular in the range of between 0.05% by weight and 0.25% by weight.
  • Copper is absorbed in the aluminium as a solid solution, resulting in aluminium-rich mixed crystals, producing hardenable composite alloys, which are deformable and readily lend themselves to rolling. Copper also has the effect of strengthening the matrix due to the hardening of the mixed crystals, whereby Al 2 Cu and Al 3 Zr are formed independently of one another, preferably from aluminium and zirconium, so that the resultant nucleus formation is not heterogeneous. These crystallites start to separate more or less at the same time. Using copper increases the resistance of the aluminium alloy to fatigue and also improves the resistance of the aluminium alloy to corrosion due to the corrosive effect of oil-containing substances.
  • Adding cobalt and chromium can also help to harden the aluminium alloy.
  • compositions were made up as set out in table of FIG. 2 and their properties measured.
  • bandwidth is meant that it is possible the adapt the properties to suit a specific purpose, for example by adding one or more elements in a greater or smaller proportion.
  • a larger proportion of copper as specified in example 9 for example, higher toughness can be obtained due to mixed crystal hardening.
  • the toughness behaviour and the properties of the aluminium alloy generally speaking can be optimised to suit the situation in terms of cost by varying the scandium or zirconium contents.
  • An aluminium alloy was also produced on the basis of a composition comprisingAlSn1,3Sc0,2Zr0,26Fe0,1 and its tension-elongation behaviour measured and plotted in comparison with AlSn25CuMn and AlZn4SiPb.
  • the result is set out in FIG. 3, in which the elongation ⁇ is plotted on the X axis and the nominal tensile stress ⁇ z [N/mm 2 ] on the Y axis.
  • the measurements were conducted on strips prepared in accordance with UN EN1002-1 using tension samples E 3 ⁇ 8 ⁇ 30 mm as specified in DIN 50 120.
  • the aluminium alloy proposed by the invention had an elongation of 0.1% compared with AlZn4SiPb (lowermost curve) and exhibited significantly higher values than AlSn25CuMn (middle curve) with effect from an elongation of 0.05%.
  • the alloy proposed by the invention must be exposed to significantly higher forces or tensions, i.e. the aluminium alloy has a correspondingly higher strength than the aluminium alloys with which it was compared.
  • the aluminium alloy and the bearing elements 1 made from it can be produced using methods known from the prior art. Pure elements or highly pure elements are used as the starting materials.
  • the aluminium alloy can be applied to the protective shell by rolling, plating, e.g. electro-plating, for example.
  • the running layer 4 can be disposed on this binding by said methods or alternatively by galvanic processes by spraying, etc..
  • the plastic layer may also be applied by spraying, dipping or by offset printing. Galvanic processes could also be used.
  • auxiliary intermediate layers may naturally also be provided between the individual functional layers, depending on requirements, such as diffusion barriers, pure aluminium layers, a nickel insulation. etc..

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Sliding-Contact Bearings (AREA)
US10/798,082 2003-03-14 2004-03-11 Aluminium wrought alloy Abandoned US20040177902A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ATA404/2003 2003-03-14
AT0040403A AT412284B (de) 2003-03-14 2003-03-14 Aluminiumknetlegierung

Publications (1)

Publication Number Publication Date
US20040177902A1 true US20040177902A1 (en) 2004-09-16

Family

ID=32234879

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/798,082 Abandoned US20040177902A1 (en) 2003-03-14 2004-03-11 Aluminium wrought alloy

Country Status (8)

Country Link
US (1) US20040177902A1 (show.php)
EP (1) EP1475449B1 (show.php)
JP (1) JP2004277883A (show.php)
KR (1) KR100670228B1 (show.php)
CN (1) CN1312304C (show.php)
AT (1) AT412284B (show.php)
BR (1) BRPI0400264B1 (show.php)
DE (1) DE502004010629D1 (show.php)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005033353A3 (de) * 2003-10-08 2006-01-26 Miba Gleitlager Gmbh Legierung, insbesondere für eine gleitschicht
WO2008074344A1 (en) * 2006-12-19 2008-06-26 Mahle International Gmbh Sliding bearing
US20080187260A1 (en) * 2005-09-20 2008-08-07 Ks Gleitlager Gmbh Composite antifriction bearing material
US20110036267A1 (en) * 2008-04-30 2011-02-17 Ulvac, Inc. Water-reactive al composite material, water-reactive al film, process for the production of the al film , and constituent member for film-forming chamber
CN104819209A (zh) * 2014-01-31 2015-08-05 米巴滑动轴承有限公司 多层滑动轴承
US10513766B2 (en) 2015-12-18 2019-12-24 Novelis Inc. High strength 6XXX aluminum alloys and methods of making the same
US10538834B2 (en) 2015-12-18 2020-01-21 Novelis Inc. High-strength 6XXX aluminum alloys and methods of making the same
US11719279B2 (en) 2018-12-05 2023-08-08 Schaeffler Technologies AG & Co. KG Pivot bearing
US11814701B2 (en) 2017-03-08 2023-11-14 NanoAL LLC High-performance 5000-series aluminum alloys
US11885002B2 (en) 2017-03-30 2024-01-30 NanoAL LLC High-performance 6000-series aluminum alloy structures
US11932928B2 (en) 2018-05-15 2024-03-19 Novelis Inc. High strength 6xxx and 7xxx aluminum alloys and methods of making the same
US12492453B2 (en) 2018-06-20 2025-12-09 NanoAL LLC High-performance Al—Zn—Mg—Zr base aluminum alloys for welding and additive manufacturing

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT414128B (de) 2004-08-03 2006-09-15 Miba Gleitlager Gmbh Aluminiumlegierung für tribologisch beanspruchte flächen
DE102005063324B4 (de) * 2005-05-13 2008-02-28 Federal-Mogul Wiesbaden Gmbh & Co. Kg Gleitlagerverbundwerkstoff, Verwendung und Herstellungsverfahren
DE102005059544A1 (de) * 2005-12-13 2007-06-14 Ecka Granulate Gmbh & Co. Kg Sn-haltige hochbelastbare Materialzusammensetzung; Verfahren zur Herstellung einer hochbelastbaren Beschichtung und deren Verwendung
KR101526660B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
KR101526661B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
KR101526656B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
KR101526659B1 (ko) * 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
EP2902647A1 (en) * 2014-02-03 2015-08-05 Siemens Aktiengesellschaft Bearing having a raceway with high chromium content
DE102019000361A1 (de) 2019-01-18 2020-07-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Verschleißbeständige Leichtbaulegierung aus einem Metall-Matrix-Verbundwerkstoff mit einer metallischen Matrix und einer keramischen Hartphase, Verfahren zur Herstellung einer solchen verschleißbeständigen Leichtbaulegierung, und Bremsscheibe mlt einer solchen verschleißbeständigen Leichtbaulegierung
CN110819852A (zh) * 2019-10-30 2020-02-21 全球能源互联网研究院有限公司 一种耐热性好的高导电率软铝单丝及其制备方法
GB2607887B (en) * 2021-06-11 2024-07-03 Mahle Int Gmbh Sliding element with intermediate layer

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6638375B2 (en) * 2000-07-26 2003-10-28 Daido Metal Company Ltd. Aluminum bearing alloy
US6706126B2 (en) * 1998-10-09 2004-03-16 Taiho Kogyo Co., Ltd. Aluminum alloy for sliding bearing and its production method

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0005560B1 (de) * 1978-02-25 1981-08-12 Karl Schmidt Gmbh Gleitlagerwerkstoff
JPS582578B2 (ja) * 1979-09-28 1983-01-17 大豊工業株式会社 アルミニウム軸受合金
GB2067220B (en) * 1980-01-08 1984-04-18 Taiho Kogyo Co Ltd Aluminium-tin base bearing alloy
GB2066846B (en) * 1980-01-08 1984-02-29 Taiho Kogyo Co Ltd Aluminium-tin base bearing alloy
JPS6263636A (ja) * 1985-09-17 1987-03-20 Taiho Kogyo Co Ltd アルミニウム軸受合金
JPS6263637A (ja) * 1985-09-17 1987-03-20 Taiho Kogyo Co Ltd アルミニウム軸受合金
JPS61117244A (ja) * 1985-10-31 1986-06-04 Taiho Kogyo Co Ltd アルミニウム系摺動合金
JP3298635B2 (ja) * 1990-04-27 2002-07-02 大豊工業株式会社 アルミニウム系軸受合金
JPH0483914A (ja) * 1990-07-24 1992-03-17 Taiho Kogyo Co Ltd すべり軸受材料
JP3185219B2 (ja) * 1990-11-30 2001-07-09 大豊工業株式会社 アルミニウム系軸受合金
DE4319867A1 (de) * 1993-06-16 1994-12-22 Kolbenschmidt Ag Mehrschicht-Gleitlagerwerkstoff
JP4063388B2 (ja) * 1998-02-20 2008-03-19 株式会社神戸製鋼所 表面性状に優れた成形加工用Ａｌ−Ｍｇ−Ｓｉ系アルミニウム合金板及びその製造方法
JP3868630B2 (ja) * 1998-07-07 2007-01-17 大豊工業株式会社 すべり軸受用アルミニウム合金及びすべり軸受
AT407404B (de) * 1998-07-29 2001-03-26 Miba Gleitlager Ag Zwischenschicht, insbesondere bindungsschicht, aus einer legierung auf aluminiumbasis
AT407532B (de) * 1998-07-29 2001-04-25 Miba Gleitlager Ag Verbundwerkstoff aus zumindest zwei schichten
EP1229141A1 (de) * 2001-02-05 2002-08-07 ALUMINIUM RHEINFELDEN GmbH Aluminiumgusslegierung
JP4215965B2 (ja) * 2001-04-27 2009-01-28 エヌデーシー株式会社 軸受用アルミニウム基粉末焼結複合材料とその製造方法

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6706126B2 (en) * 1998-10-09 2004-03-16 Taiho Kogyo Co., Ltd. Aluminum alloy for sliding bearing and its production method
US6638375B2 (en) * 2000-07-26 2003-10-28 Daido Metal Company Ltd. Aluminum bearing alloy

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8147981B2 (en) 2003-10-08 2012-04-03 Miba Gleitlager Gmbh Alloy, in particular for a bearing coating
US7879453B2 (en) 2003-10-08 2011-02-01 Miba Gleitlager Gmbh Alloy, in particular for a bearing coating
WO2005033353A3 (de) * 2003-10-08 2006-01-26 Miba Gleitlager Gmbh Legierung, insbesondere für eine gleitschicht
US20110071061A1 (en) * 2003-10-08 2011-03-24 Miba Gleitlager Gmbh Alloy, in particular for a bearing coating
US20080187260A1 (en) * 2005-09-20 2008-08-07 Ks Gleitlager Gmbh Composite antifriction bearing material
WO2008074344A1 (en) * 2006-12-19 2008-06-26 Mahle International Gmbh Sliding bearing
US20100047605A1 (en) * 2006-12-19 2010-02-25 Christiane Knoblauch Sliding bearing
US8715404B2 (en) * 2008-04-30 2014-05-06 Ulvac, Inc. Water-reactive Al composite material, water-reactive Al film, process for the production of the Al film, and constituent member for film-forming chamber
US20110036267A1 (en) * 2008-04-30 2011-02-17 Ulvac, Inc. Water-reactive al composite material, water-reactive al film, process for the production of the al film , and constituent member for film-forming chamber
CN104819209A (zh) * 2014-01-31 2015-08-05 米巴滑动轴承有限公司 多层滑动轴承
US10513766B2 (en) 2015-12-18 2019-12-24 Novelis Inc. High strength 6XXX aluminum alloys and methods of making the same
US10538834B2 (en) 2015-12-18 2020-01-21 Novelis Inc. High-strength 6XXX aluminum alloys and methods of making the same
US11920229B2 (en) 2015-12-18 2024-03-05 Novelis Inc. High strength 6XXX aluminum alloys and methods of making the same
US12043887B2 (en) 2015-12-18 2024-07-23 Novelis Inc. High strength 6xxx aluminum alloys and methods of making the same
US11814701B2 (en) 2017-03-08 2023-11-14 NanoAL LLC High-performance 5000-series aluminum alloys
US11885002B2 (en) 2017-03-30 2024-01-30 NanoAL LLC High-performance 6000-series aluminum alloy structures
US11932928B2 (en) 2018-05-15 2024-03-19 Novelis Inc. High strength 6xxx and 7xxx aluminum alloys and methods of making the same
US12492453B2 (en) 2018-06-20 2025-12-09 NanoAL LLC High-performance Al—Zn—Mg—Zr base aluminum alloys for welding and additive manufacturing
US11719279B2 (en) 2018-12-05 2023-08-08 Schaeffler Technologies AG & Co. KG Pivot bearing

Also Published As

Publication number Publication date
BRPI0400264B1 (pt) 2011-08-23
KR100670228B1 (ko) 2007-01-17
EP1475449A1 (de) 2004-11-10
JP2004277883A (ja) 2004-10-07
BRPI0400264A (pt) 2004-12-28
AT412284B (de) 2004-12-27
CN1312304C (zh) 2007-04-25
KR20040081079A (ko) 2004-09-20
CN1532299A (zh) 2004-09-29
DE502004010629D1 (de) 2010-03-04
EP1475449B1 (de) 2010-01-13
ATA4042003A (de) 2004-05-15

Similar Documents

Publication Publication Date Title
US20040177902A1 (en) Aluminium wrought alloy
JP7606822B2 (ja) 多層滑り軸受けエレメント
JP6326426B2 (ja) 滑り軸受複合材料
US4937149A (en) Overlay alloy used for a surface layer of sliding material, sliding material having a surface layer comprising said alloy and the manufacturing method of the sliding material
US6194087B1 (en) Composite multilayer bearing material
JP5292279B2 (ja) すべり軸受
US6746154B2 (en) Lead-free bearing
KR102250748B1 (ko) 다층 플레인 베어링
JP3249774B2 (ja) 摺動部材
US9708692B2 (en) Sliding bearing
JP5203606B2 (ja) 積層複合体材料、その製造および用途
JP4476634B2 (ja) Ｐｂフリー銅合金摺動材料
KR20110066112A (ko) 내마찰 코팅
US7829201B2 (en) Plain bearing
JP3570607B2 (ja) 摺動部材
US5334460A (en) CU-PB system alloy composite bearing having overlay
GB2264336A (en) Bearings.
GB2250550A (en) Sliding bearing layer composition
JP2007277720A (ja) 軸受要素用滑り層および軸受要素
US6783869B2 (en) Aluminium alloy for an anti-friction element
US5665480A (en) Copper-lead alloy bearing
JP2535105B2 (ja) 複合めっき皮膜を有するすべり軸受
JPH07252693A (ja) 複合めっき皮膜を有するすべり軸受
KR20210061936A (ko) 다층 슬라이딩 베어링 요소
Totten Friction and Wear of Sliding Bearing Materials

Legal Events

Date Code Title Description
AS Assignment

Owner name: MIBA GLEITLAGER GMBH, AUSTRIA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MEREN, ROBERT;MANNER, MARKUS;REEL/FRAME:015080/0782

Effective date: 20040209

AS Assignment

Owner name: MIBA GLEITLAGER GMBH, AUSTRIA

Free format text: CORRECTIVE ASSIGNMENT PREVIOUSLY RECORDED AT REEL; 015080 FRAME;ASSIGNORS:MERGEN, ROBERT;MANNER, MARKUS;REEL/FRAME:016217/0991

Effective date: 20040209

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION