FOIL BEARING

Abstract

The invention relates to a foil bearing (10) having at least one foil (16, 18), which is arranged and fixed in place inside a bearing bushing (12). In order to simply the production, in particular assembly, of the foil bearing (10), the bearing bushing (12) has at least two openings (20, 22, 24) offset from each other in the circumferential direction of the bearing bushing (12) or depressions (120, 122, 124) made in the inner lateral surface of the bearing bushing, into which openings or depressions two opposing circumferential end sections (16a, 16b, 18a, 18b) of the at least one foil (16, 18) engage.

Claims

1. A foil bearing (10) having at least one foil (16, 18), which is arranged and fixed inside a bearing bushing (12), characterized in that the bearing bushing (12) has at least two openings (20, 22, 24) arranged offset with respect to one another in a circumferential direction of the bearing bushing (12), or has at least two depressions (120, 122, 124) made in an inner lateral surface of the bearing bushing, into which openings or depressions two opposite circumferential end sections (16a, 16b, 18a, 18b) of the at least one foil (16, 18) engage.

2. The foil bearing as claimed in claim 1, characterized in that at least two openings (20, 22) or depressions (120, 122) are arranged offset with respect to one another in a direction of a longitudinal axis (14) of the bearing bushing (12).

3. The foil bearing as claimed in claim 2, wherein the at least two openings include a first opening (20), a second opening (22) and a third opening (24), wherein the at least two depressions include a first depression (120), a second depression (122) and a third depression (124), wherein, in a first circumferential position, the first opening (20) or the first depression (120) is provided, and, in the direction of the longitudinal axis (14) of the bearing bushing (12), the second opening (22) or the second depression (122) is provided, said second opening or second depression being offset with respect to the first opening (20) or first depression (120), and wherein, in a second circumferential position, the third opening (24) or third depression (124) is provided, the third opening or third depression being offset with respect to the first and second openings (20, 22) or depressions (120, 122) in the direction of the longitudinal axis (14) of the bearing bushing (12).

4. The foil bearing as claimed in claim 3, characterized in that, when viewed in the direction of the longitudinal axis (14) of the bearing bushing (12), the third opening (24) or depression (124) is arranged between the first opening (20) or depression (120) and the second opening (22) or depression (122).

5. The foil bearing as claimed in claim 1, characterized in that the at least two openings (20, 22, 24) are bores.

6. The foil bearing as claimed in claim 1, characterized in that the at least two depressions (120, 122, 124) are countersinks.

7. The foil bearing as claimed in claim 1, characterized in that at least one of the circumferential end sections (16a, 16b, 18a, 18b) of the at least one foil (16, 18) has at least one insertion tab (26), which engages in at least one of the at least two openings (20, 22, 24) or at least two depressions (120, 122, 124).

8. The foil bearing as claimed in claim 7, characterized in that the at least one insertion tab (26) tapers in the circumferential direction toward a free end.

9. The foil bearing as claimed in claim 8, characterized in that the at least one insertion tab (26) is at least approximately trapezoidal or triangular or rectangular with a rounded end.

10. The foil bearing as claimed in claim 8, characterized in that the at least one foil (16, 18) includes an upper foil (18) and a lower foil (16), which is arranged between the upper foil (18) and the bearing bushing (12).

11. The foil bearing as claimed in claim 1, wherein the bearing bushing (12) has the at least two openings (20, 22, 24) arranged offset with respect to one another in the circumferential direction of the bearing bushing (12), into which openings the two opposite circumferential end sections (16a, 16b, 18a, 18b) of the at least one foil (16, 18) engage.

12. The foil bearing as claimed in claim 11, characterized in that at least two openings (20, 22) are arranged offset with respect to one another in a direction of a longitudinal axis (14) of the bearing bushing (12).

13. The foil bearing as claimed in claim 12, wherein the at least two openings include a first opening (20), a second opening (22) and a third opening (24), wherein, in a first circumferential position, the first opening (20) is provided, and, in the direction of the longitudinal axis (14) of the bearing bushing (12), the second opening (22) is provided, said second opening being offset with respect to the first opening (20), and wherein, in a second circumferential position, the third opening (24) is provided, the third opening being offset with respect to the first and second openings (20, 22) in the direction of the longitudinal axis (14) of the bearing bushing (12).

14. The foil bearing as claimed in claim 1, wherein the bearing bushing (12) has the at least two depressions (120, 122, 124) made in an inner lateral surface of the bearing bushing, into which depressions the two opposite circumferential end sections (16a, 16b, 18a, 18b) of the at least one foil (16, 18) engage.

15. The foil bearing as claimed in claim 14, characterized in that at least two depressions (120, 122) are arranged offset with respect to one another in a direction of a longitudinal axis (14) of the bearing bushing (12).

16. The foil bearing as claimed in claim 15, wherein the at least two depressions include a first depression (120), a second depression (122) and a third depression (124), wherein, in a first circumferential position, the first depression (120) is provided, and, in the direction of the longitudinal axis (14) of the bearing bushing (12), the second depression (122) is provided, said second depression being offset with respect to the first depression (120), and wherein, in a second circumferential position, the third depression (124) is provided, the third depression being offset with respect to the first and second depressions (120, 122) in the direction of the longitudinal axis (14) of the bearing bushing (12).

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0007] An exemplary embodiment of the invention is illustrated in the drawing and explained in greater detail in the following description. Specifically:

[0008] FIG. 1 shows a foil bearing in a cross section with a bearing bushing and foils arranged therein,

[0009] FIG. 2 shows the bearing bushing in cross section without foils,

[0010] FIG. 3 shows the bearing bushing in a side view,

[0011] FIG. 4 shows a foil in an initial state before being arranged in the bearing bushing,

[0012] FIG. 5 shows a segment of the foil from FIG. 4 in a modified embodiment, and

[0013] FIG. 6 shows a segment of the foil from FIG. 4 in a further modified embodiment.

DETAILED DESCRIPTION

[0014] FIGS. 1 to 6 illustrate a foil bearing 10 with a hollow-cylindrical bearing bushing 12. The bearing bushing 12 is also referred to as a bearing ring and essentially has the shape of a straight, hollow circular cylinder with a longitudinal axis 14. Two foils 16, 18 of the foil bearing 10 are arranged in the interior of the bearing bushing 12. The foil 16 is also referred to as a beam, bump or lower foil and is arranged between the bearing bushing 12 and the foil 18, which is also referred to as a top foil or upper foil. The foil bearing 10 serves for the rotatable mounting of a shaft (not illustrated), which rests against the foil 18.

[0015] The bearing bushing 12 has openings 20, 22, 24, illustrated in FIGS. 1 to 3, in its lateral surface which form a geometry for fixing the foils 16, 18 in the bearing bushing 12. The openings 20, 22, 24 are preferably designed as bores, which are introduced into the bearing bushing 12 from the outside. The openings 20, 22, 24 each have a diameter d.

[0016] As illustrated in FIG. 3, the two openings 20, 22, which are referred to below as the first opening 20 and the second opening 22, are arranged offset with respect to one another in the direction of the longitudinal axis 14 of the bearing bushing 12 on a line L parallel to the longitudinal axis 14. Opening 24 is referred to below as the third opening 24 and is arranged offset with respect to the first and second openings 20, 22 in the circumferential direction of the bearing bushing 12. As illustrated in FIG. 2, there is an angle α between the first and second openings 20, 22 and the third opening 24 with respect to the longitudinal axis 14 of the bearing bushing 12. When viewed in the direction of the longitudinal axis 14 of the bearing bushing 12, the third opening 24 is preferably arranged between the first opening 20 and the second opening 22, in particular at least approximately centrally between the first opening 20 and the second opening 22, as illustrated in FIG. 3. The first opening 20 and the second opening 22 are arranged in a first circumferential position of the bearing bushing 12, and the third opening 24 is arranged in a second circumferential position of the bearing bushing 12.

[0017] Instead of the through openings 20, 22, 24, depressions 120, 122, 124 can also be provided in the inner lateral surface of the bearing bushing 12, as is illustrated by dashed lines in the lower region of the bearing bushing 12 in FIG. 2. However, these depressions 120, 122, 124 must be introduced from the interior of the bearing bushing 12 and may be designed as countersinks, for example.

[0018] In FIG. 4, the foils 16, 18 are shown in an unwound state before they are arranged within the bearing bushing 12. On their two opposite circumferential end sections 16a, 18a and 16b, 18b pointing in the circumferential direction, the foils 16, 18 each have at least one insertion tab 26, which each have a smaller width b than the width B of the foils 16, 18 in the direction of the longitudinal axis 14 of the bearing bushing 12. There are two insertion tabs 26 arranged offset with respect to one another in the direction of the longitudinal axis 14 on one circumferential end section 16a, 18a of the foils 16, 18, and there is only one insertion tab 26 on the other circumferential end section 16b, 18b of the foils 16, 18. Provision can also be made for just one insertion tab 26 or in each case a plurality, also more than two, insertion tabs 26 to be present on both circumferential end sections of the foils.

[0019] The insertion tabs 26 are preferably designed in such a way that they taper toward their free ends, that is to say their width b decreases. As illustrated in FIG. 4, the insertion tabs 26 can be of at least approximately trapezoidal design. Alternatively, as illustrated in FIG. 5, the insertion tabs 26 can also be of approximately triangular or tooth-shaped design or, as illustrated in FIG. 6, approximately rectangular with rounded ends.

[0020] The foils 16, 18 with the insertion tabs 26 can be designed, for example, as metal foils and can be produced by punching. A third foil can also be arranged between the two foils 16, 18.

[0021] In order to arrange the foils 16, 18 within the bearing bushing 12, they are rolled up to a diameter which is smaller than the inside diameter of the bearing bushing 12 and introduced into the bearing bushing 12 in the direction of the longitudinal axis 14. The insertion tabs 26 present on the circumferential end section 16a, 18a of the foils 16, 18 are introduced into the first opening 20 or second opening 22 of the bearing bushing 12, and the insertion tab 26 of the other circumferential end section 16b, 18b of the foils 16, 18 is introduced into the third opening 24 of the bearing bushing 12. During this process, the foils 16, 18 spring apart in the circumferential direction of the bearing bushing 12, and the insertion tabs 26 hook into the openings 20, 22, 24, as a result of which the foils 16, 18 are fixed in the bearing bushing 12 in the radial direction and in the direction of the longitudinal axis 14. Since the insertion tabs 26 are arranged offset with respect to one another in the direction of the longitudinal axis 14, they do not collide with one another and they can be introduced into the openings 20, 22, 24.

[0022] The size of the angle α and of the diameter d of the openings 20, 22, 24, as well as the width b of the insertion tabs 26, are suitably determined in order to enable secure retention of the insertion tabs 26 in the openings 20, 22, 24 and thus secure fixing of the foils 16, 18.

[0023] The shaft belongs, for example, to a rotor (likewise not illustrated) of a turbomachine. The turbomachine is, for example, part of an air supply unit in a fuel cell system. In the fuel cell system, the turbomachine is designed, for example, as a compressor. The compressor comprises a compressor wheel, which is an advantageous component of the rotor.