Spherical bearing having a swaged outer ring

Spherical bearings using NiCr19Fe18Nb or X6NiCrTiMoVB25-15-2 superalloys with a swaging process address the mechanical strength and corrosion issues of conventional materials, enabling high-temperature operation.

GB2610270BActive Publication Date: 2025-07-16SKF AEROSPACE FRANCE SAS
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Patent Information

Application Number
GB2022009360
Authority / Receiving Office
GB · GB
Patent Type
Patents
Current Assignee / Owner
Priority Date
2021-07-21
Filing Date
2022-06-27
Publication Date
2025-07-16
Estimated Expiration
2042-06-27

AI Technical Summary

Technical Problem

Conventional spherical bearings made from bronze or stainless steel lose mechanical strength and corrosion resistance at temperatures above 300°C, rendering them unsuitable for high-temperature applications, while split bearings are costly to manufacture.

Method used

Manufacture spherical bearings using NiCr19Fe18Nb or X6NiCrTiMoVB25-15-2 superalloys for the outer ring, which maintain mechanical strength and corrosion resistance under high temperatures, and employ a swaging process to shape the inner and outer rings.

Benefits of technology

The proposed method produces spherical bearings with enhanced mechanical strength and corrosion resistance suitable for high-temperature conditions, overcoming the limitations of conventional materials and manufacturing costs.

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Abstract

A spherical bearing 1 and a method for manufacturing such a bearing is provided. The spherical bearing 1 comprises an outer ring 2 and an inner ring 3 respectively comprising an inner surface 2a and a
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Description

TITLE: Spherical bearing having a swaged outer ring Technical field The present invention relates in general to spherical bearings and, more 10 particularly, to spherical bearings manufactured by swaging of an outer ring onto an inner ring. More specifically, the invention relates to a method for manufacturing a spherical bearing by swaging of an outer ring onto an inner ring, the spherical bearing having mechanical strength and corrosion resistance that are suitable for operation under 15 high-temperature conditions. Prior art Typically, a spherical bearing comprises an outer ring and an inner ring. The outer and inner rings respectively comprise an inner surface and an outer surface that are in contact, forming sliding surfaces for the outer and inner rings to move relative to one 20 another. Depending on their location, some spherical bearings operate under high-temperature conditions, above 300°C. In order to ensure the integrity of the spherical bearings, it is imperative that they retain their mechanical strength under such conditions. 25 According to one particular existing method, the manufacture of a spherical bearing is based on a swaging process. In a first instance, the outer ring and inner ring are assembled, and then the outer ring is swaged directly onto the inner ring, which serves as a die. The shape of the outer surface of the inner ring is imparted to the inner surface of the outer ring. The resulting 30 swaged spherical bearing is referred to in English simply as a “swaged bearing”. Bronze or stainless steels, for example CRES (or “corrosion-resistant steel”) are the materials conventionally used to form the outer ring of a swaged spherical bearing. However, these conventional materials lose their mechanical strength under high-temperature conditions, in particular at temperatures above 300°C. Furthermore, in 35 the case of CRES, the corrosion resistance properties are also reduced. Consequently, swaged spherical bearings cannot be used in applications that involve high temperatures. Other types of spherical bearing can be used at high temperatures. For example, a split spherical bearing is manufactured by assembling an inner ring that is cut into two 5 parts inside an outer ring. A spherical bearing of this kind is referred to in English simply as a “split bearing”. Nonetheless, the process for manufacturing split spherical bearings is costly. Description of the invention The invention therefore aims to remedy these drawbacks and to propose a low-10 cost manufacturing method with which it is possible to obtain a spherical bearing whose properties of mechanical strength and corrosion resistance are suited to applications under conditions of temperatures above 300°C. The invention therefore proposes a method for manufacturing a spherical bearing comprising an outer ring and an inner ring respectively comprising an inner surface and 15 an outer surface that are in contact with one another. Moreover, the material of the outer ring comprises an alloy having the formula NiCrl9Fel8Nb or an alloy having the formula X6NiCrTiMoVB25-15-2. The alloys of formula NiCrl9Fel8Nb and of formula X6NiCrTiMoVB25-15-2 are superalloys whose properties of mechanical strength and corrosion resistance are 20 suitable for withstanding high-temperature conditions, in particular above 300°C. Furthermore, these alloys are advantageously able to undergo a plastic deformation applied to the outer ring during a swaging step that is characteristic of the manufacture of a swaged bearing, without their mechanical properties being affected. According to one exemplary embodiment, the inner surface of the outer ring can 25 be concave spherical, and the outer surface of the inner ring can be convex spherical. The invention relates to a method for manufacturing a spherical bearing, comprising: - a step of positioning an outer ring on an inner ring, the outer and inner rings respectively comprising an inner surface and an outer surface that are in contact with 30 one another; and - a step of swaging the outer ring onto the inner ring, the outer surface of the inner ring being used as the die which imparts its shape to the inner surface of the outer ring. Moreover, the material of the outer ring comprises an alloy having the formula NiCr 19Fel8Nb or an alloy having the formula X6NiCrTiMoVB25-15-2. According to one exemplary embodiment, the outer surface of the inner ring can be convex spherical so as to form a concave spherical inner surface for the outer ring 5 during this swaging step. Advantageously, the manufacturing method may comprise, after the swaging step, a step of machining an outer surface and / or lateral faces of the swaged outer ring. Preferably, the manufacturing method may comprise, after the swaging step, a step of lubricating the inner surface of the outer ring and the outer surface of the inner 10 ring. Preferably, the lubrication step is carried out after the swaging step. Advantageously, the lubricant may comprise molybdenum disulphide or graphite. According to one feature, the manufacturing method may further comprise, prior 15 to the positioning step, a step of manufacturing the outer ring and inner ring. Brief description of the drawings Other aims, advantages and features will emerge from the following description, which is provided purely for illustrative purposes and with reference to the appended drawings, in which: 20 [Fig 1] is a section view of an exemplary embodiment of a spherical bearing comprising an outer ring and an inner ring, which may be manufactured according to the invention; [Fig 21 depicts a method for manufacturing the spherical bearing of figure 1, according to one exemplary embodiment of the invention; [Fig 3] is a section view of the outer ring of the spherical bearing of figure 1, prior to 25 being positioned on the inner ring; [Fig 4] is a section view of the inner ring of the spherical bearing of figure 1, prior to being positioned in the outer ring; [Fig 5] is a section view of the spherical bearing of figure 1, after the outer ring has been swaged onto the inner ring. 30 Detailed description of the invention Figure 1 shows a spherical bearing 1, of axis X, comprising an outer ring 2 and an inner ring 3 onto which the inner ring 3 is swaged. The outer and inner rings 2, 3 are coaxial, of axis X. According to the depicted exemplary embodiment, the spherical bearing 1 is a radial spherical bearing. In one variant embodiment, the spherical bearing may be of a different kind, in particular non-radial or non-spherical, such as an angular- or axial-contact bearing. The outer ring 2 comprises an inner surface 2a that forms a bore, and an outer surface 2b that is radially opposite the inner surface 2a. The outer ring 2 also comprises two mutually opposite radial frontal faces 2c, 2d that axially delimit the inner surface 2a and the outer surface 2b. The inner ring 3 comprises an inner surface 3 a that forms a bore, and an outer surface 3b that is radially opposite the inner surface 3a. The inner ring 3 also comprises two mutually opposite radial frontal faces (no reference) that axially delimit the inner surface 3a and the outer surface 3b. The inner surface 2a of the outer ring and the outer surface 3b of the inner ring are in direct contact with one another in order to allow the inner and outer rings 2, 3 to move relative to one another. In the exemplary embodiment shown, the inner surface 2a of the outer ring and the outer surface 3b of the inner ring are in contact with one another in the radial direction. In the example shown, the inner surface 2a of the outer ring is concave spherical, and the outer surface 3b of the inner ring is convex spherical, so as to form a spherical bearing. The material of the outer ring 2 comprises an alloy having the formula NiCrl9Fel8Nb or an alloy having the formula X6NiCrTiMoVB25-15-2. Preferably, the outer ring 2 is made entirely of an alloy having the formula NiCrl9Fel8Nb or an alloy having the formula X6NiCrTiMoVB25-15-2. The nickel-based alloy having the formula NiCrl9Fel8Nb is for example the material known by the name Inconel® 718. The alloy having the formula X6NiCrTiMoVB25-15-2 is for example the material known by the name A286®. The mechanical strength and corrosion resistance properties of the alloys of formula NiCrl9Fel8Nb and of formula X6NiCrTiMoVB25-15-2 are suitable for withstanding high-temperature conditions above 300°C. Furthermore, they are advantageously able to undergo a deformation applied during a swaging step, without their mechanical properties being affected. A method for manufacturing the spherical bearing 1 is illustrated in figure 2. In a first, positioning step 4, the outer ring 2 comprising an alloy of formula NiCrl9Fel8Nb or an alloy of formula X6NiCrTiMoVB25-15-2 is positioned on the inner ring 3. The outer and inner rings 2 and 3, respectively illustrated in figures 3 and 4, are assembled in such a way that there respective inner and outer surfaces 2a, 3b are arranged facing one another. In a second step 5, the outer ring 2 is directly swaged onto the inner ring 3, the latter being used as the die. The swaging step 5, which in this example is carried out cold, allows the shape of the outer surface 3b of the inner ring 3 to be imparted to the inner surface 2a of the outer ring 2 by plastic deformation. As shown in figure 5, the shape of the inner surface 2a of the outer ring 2, obtained by swaging, is concave spherical provided that the outer surface 3b of the inner ring is convex spherical. The inner surface 2a of the outer ring 2 and the outer surface 3b of the inner ring 3 obtained in this manner are designed to cooperate and to allow the inner and outer rings 2, 3 to move relative to one another. Advantageously, the manufacturing method comprises a subsequent step 6 of machining the outer surface 2b of the swaged outer ring 2. As shown in figure 1, the outer surface 2b of the outer ring 2 has been machined so as to obtain a cylindrical surface. The lateral faces 2c and 2d have also been machined so as to obtain planar faces. Moreover, the manufacturing method may comprise a step 7 of lubricating the inner surface 2a of the outer ring 2 and the outer surface 3b of the inner ring 3. The lubrication step 7 may be carried out prior to or after the swaging step 5. The lubricant is for example a dry lubricant and may comprise molybdenum disulphide or graphite. According to one exemplary embodiment, the manufacturing method may further comprise, prior to the positioning step 4, a step of manufacturing the outer ring and innerring 2, 3. 10

Claims

152025301. Method for manufacturing a spherical bearing (1) comprising:- a step (4) of positioning an outer ring (2) on an inner ring (3), the outer and inner rings (2, 3) respectively comprising an inner surface (2a) and an outer surface (3b) that are in contact with one another; and- a step of swaging (5) the outer ring (2) onto the inner ring (3), the outer surface (3b) of the inner ring (3) being used as the die which imparts its shape to the inner surface (2a) of the outer ring (2),characterized in that the material of the outer ring (2) comprises an alloy having the formula NiCrl9Fel8Nb or an alloy having the formula X6NiCrTiMoVB25-15-2.

2. Manufacturing method according to Claim 1. wherein the outer surface (3b) of the inner ring (3) is convex spherical so as to form a concave spherical inner surface (2a) for the outer ring (2) during this swaging step.

3. Manufacturing method according to Claim 1 or 2, comprising, after the swaging step (5), a step of machining (6) an outer surface (2b) and / or lateral faces (2c, 2d) of the swaged outer ring (2).

4. Manufacturing method according to any one of Claims 1 to 3, comprising, after the swaging step (5), a step of lubricating (7) the inner surface (2a) of the outer ring (2) and the outer surface (3b) of the inner ring (3).

5. Method according to Claim 4, being dependent on Claim 3, wherein the lubrication step (7) is carried out after the swaging step (5).

6. Manufacturing method according to Claim 4 or 5, the lubricant comprising molybdenum disulphide or graphite.

7. Method according to any one of Claims 1 to 6, further comprising, prior to the positioning step (4), a step of manufacturing the outer ring (2) and inner ring (3).

8. Method according to any one of Claims 1 to 7, wherein the swaging step is carried out cold.

Citation Information

Patent Citations

  • Method of manufacturing a spherical bearing arrangement

    EP1816359A2

  • Turbocharger wastegate actuator high temperature rod end with a spherical bearing and a method for operating the actuator

    EP2905445A1

  • A ring for a plain bearing and an attaching device including this ring

    EP3159084A1

  • Improvements in or relating to bearings and the assembly thereof

    GB1146886A

  • Improvements in or relating to methods of swaging generally cylindrical members

    GB1268499A