초록 ▼

The invention relates to a sealing arrangement for a non-hermetic seal of a gap (11) between a stator and a rotor with a brush seal (13), wherein the brush seal (13) has a bristle package (14) with several bristles (15), the bristles are wound about a core element (16) and fixed to the core element

The invention relates to a sealing arrangement for a non-hermetic seal of a gap (11) between a stator and a rotor with a brush seal (13), wherein the brush seal (13) has a bristle package (14) with several bristles (15), the bristles are wound about a core element (16) and fixed to the core element (16), wherein the brush seal (13) is disposed at least sectionally in an accommodating space, which is bounded by a supporting element (18) and a covering element (19), and wherein the bristles (15) have sealing bristle sections (21), which are at an angle to the bristle shafts (20) and the ends of which run against a sealing surface (22) of the rotor (12). According to the invention, the covering element (19) has a support surface (23) at an end adjacent to the sealing bristle sections (21), wherein the supporting surface (23) contacts the bristle shafts (20) in a defined, locally limited region, so that the radial mobility of the sealing bristle sections (21) is limited in the direction of the rotor (12).

대표청구항 ▼

1. A sealing apparatus for non-hermetically sealing a gap between a stator and a rotor with a brush seal, wherein the brush seal has a bristle package with several bristles, the bristles are wound about a core element and fixed to the core element, wherein the brush seal is disposed at least section

1. A sealing apparatus for non-hermetically sealing a gap between a stator and a rotor with a brush seal, wherein the brush seal has a bristle package with several bristles, the bristles are wound about a core element and fixed to the core element, wherein the brush seal is disposed at least sectionally in an accommodating space defined by a supporting element and a covering element, wherein the bristles have sealing bristle sections, which are at an angle to the bristle shafts, and the ends of which run against a sealing surface of the rotor, the sealing apparatus further comprising: a support surface disposed at an end of the covering element adjacent to the sealing bristle sections, wherein the supporting surface contacts the bristle shafts in a defined, locally limited region, so that the radial mobility of the sealing bristle sections is limited in the direction of the rotor. 2. The sealing apparatus of claim 1, wherein the radial mobility of the sealing bristle sections is limited in the direction toward the rotor in such a manner that the brush seal can move only to the minimum extent necessary to contact the sealing surface of the rotor. 3. The sealing apparatus of claim 1, wherein: the covering element and the bristle package each have a stiffness; andwherein the stiffness of the covering element forming the supporting surface is at least twice the stiffness of the bristle package. 4. The sealing apparatus of claim 1, further comprising: a clamping element affixed over the bristles about the core element; andwherein a section of the covering element, extending between the supporting surface of the covering element and the clamping element of the brush seal, is disposed at a substantially constant distance from the bristle package, thereby forming a straight space relative to the supporting surface. 5. The sealing apparatus of claim 4, wherein the supporting element is disposed opposite to the supporting surface of the covering element, and the supporting element has a bulge formed therein spaced-apart from the bristle package, thereby forming a cavity. 6. The sealing apparatus of claim 5, wherein the cavity on the supporting element side and the straight space on the covering element side include sections that sectionally overlap one another along the bristle package. 7. The sealing apparatus of claims 1, wherein, in relation to an internal diameter (D1) of the bristle package in the region of the supporting surface, a diameter (D3) of the supporting surface is selected so that even when a static eccentricity of the rotor relative to the brush seal occurs, the sealing bristle sections may still touch the sealing surface of the rotor over the whole extent. 8. A brush seal assembly for non-hermetically sealing a gap between a stator and a rotor, the brush seal assembly comprising: a bristle package including a core element and a plurality of bristles; the plurality of bristles being wound about and fixed to the core element;each bristle having a bristle shaft, a sealing bristle section connected to the bristle shaft and disposed at an angle to the bristle shaft, and an end disposed on the sealing bristle section for running against a sealing surface of the rotor;an enclosure defining an accommodating space within which the bristle package is disposed, the enclosure including a supporting element and a covering element; andwherein the covering element has a support surface at an end adjacent to the sealing bristle sections, wherein the supporting surface contacts the bristle shafts in a defined, locally limited region, so that the radial mobility of the sealing bristle sections is limited in the direction of the rotor. 9. The brush seal assembly of claim 8, wherein the position of the supporting surface is selected to limit the radial mobility of the sealing bristle sections in the direction of the rotor such that the ends of the bristles contact the sealing surface of the rotor when the bristles are at the point of maximum movement in the direction of the rotor. 10. The brush seal assembly of claim 8, wherein the covering element and the bristle package each have a stiffness, the stiffness of the covering element being at least twice the stiffness of the bristle package. 11. The brush seal assembly of claim 8, further comprising: a clamping element affixed over the bristles about the core element; andwherein a section of the covering element extending between the supporting surface and the clamping element is disposed at a substantially constant distance from the bristle package, thereby forming an uncurved space between the covering element and the bristle package. 12. The brush seal assembly of claim 11, wherein a portion of the supporting element disposed opposite the supporting surface of the covering element is configured into a bulge at a distance from the bristle package, thereby forming a cavity between the bristle package and the supporting element. 13. The brush seal assembly of claim 12, wherein at least a section of the cavity defined by the supporting element and at least a section of the uncurved space defined by the covering element, overlap in the direction of the bristle shafts. 14. The brush seal assembly of claim 8, wherein: the innermost bristle shafts of the bristle package are disposed at a first diameter (D1) when the ends of the sealing bristle sections are in contact with the sealing surface of the rotor during operation;the supporting surface is disposed at a second diameter (D3); andthe second diameter (D3) is selected to be less than the first diameter (D1) by an amount equal to the static eccentricity of the rotor relative to the brush seal;whereby the sealing bristle sections remains in contact with the sealing surface of the rotor over the whole extent of the sealing surface. 15. A brush seal assembly for sealing a gap between a stator and a rotor, the brush seal assembly comprising: a core element;a plurality of bristles wound about and fixed to the core element, each bristle having a bristle shaft, a sealing bristle section connected to the bristle shaft and disposed at an angle to the bristle shaft, and an end disposed on the sealing bristle section for running against a sealing surface of the rotor;a clamping element affixed over the bristles about the core element;a covering element disposed on one side of the bristle shafts including a supporting surface disposed at an end of the covering element adjacent to the sealing bristle sections; the supporting surface contacting the bristle shafts in a predefined region so that the radial mobility of the sealing bristle sections is limited in the direction of the rotor;a section of the covering element extending between the supporting surface and the clamping element being disposed at a substantially constant distance from the bristle shafts, thereby forming an uncurved gap therebetween; anda supporting element disposed on the opposite side of the bristle shafts from the covering element, a portion of the supporting element disposed opposite the supporting surface being configured into a bulge at a distance from the bristles, thereby forming a cavity between the bristles and the supporting element. 16. The brush seal assembly of claim 15, wherein at least a section of the cavity defined by the supporting element and at least a section of the uncurved space defined by the covering element, overlap in the direction of the bristle shafts. 17. The brush seal assembly of claim 16, wherein: the innermost bristle shafts are disposed at a first diameter (D1) when the ends of the sealing bristle sections are in contact with the sealing surface of the rotor during operation;the supporting surface is disposed at a second diameter (D3); andthe second diameter (D3) is selected to be less than the first diameter (D1) by an amount equal to the static eccentricity of the rotor relative to the brush seal;whereby the sealing bristle sections remains in contact with the sealing surface of the rotor over the whole extent of the sealing surface.