Exhaust gas flap

Abstract

An exhaust gas flap, especially for the exhaust gas stream of an internal combustion engine, includes a flap tube (24), a flap diaphragm (26). The flap diaphragm (26) is carried in the interior of the flap tube (24) on a pivot shaft (18), rotatable about a pivot axis (A). The flap diaphragm (26) has at least one flap diaphragm part (28, 30) and a mounting area (40) enclosing the pivot shaft (18) in at least some areas. A wing stop (42, 44) is provided at an inner circumferential area of the flap tube (24) in association with at least one flap diaphragm part (28, 30). A recess (60, 62, 64, 66) at the flap diaphragm (26), receiving a circumferential end area (48, 50) of a wing stop (42, 44), is provided in at least one axial end area of the mounting area (40).

Claims

1. An exhaust gas flap for an exhaust gas stream of an internal combustion engine, the exhaust gas flap comprising: a flap tube; a pivot shaft in an interior of the flap tube and rotatable about a pivot axis; and a flap diaphragm carried in the interior of the flap tube, having a mounting area enclosing the pivot shaft in some areas and being mounted on the pivot shaft, the flap diaphragm comprising two separate flap diaphragm parts of identical configuration, each separate flap diaphragm part being of a one piece configuration and comprising a flap wing and a curved mounting area section of the mounting area, the curved mounting area sections enclosing the pivot shaft in some areas thereof, the two separate flap diaphragm parts being fixed to the pivot shaft with the respective curved mounting area section thereof independently from each other; two wing stops, each one of the two wing stops associated with a respective one of the two separate flap diaphragm parts, each one of the two wing stops comprising a ring segment fixed to an inner circumferential area of the flap tube in association with the two separate diaphragm parts and providing a stop surface, the stop surfaces of the two wing stops being offset in relation to each other in a direction of a flap tube longitudinal axis and being oriented to face away from each other; and a recess is provided in each axial end area of the curved mounting area sections of each one of the two separate flap diaphragm parts, each recess for receiving the respective wing stop associated with the flap wing of the other one of the two separate flap diaphragm parts, each recess of a respective one of the two separate flap diaphragm parts being open both in a diametrical direction of the flap tube and in one circumferential direction around the pivot shaft from the respective one of the two separate flap diaphragm parts toward the other one of the two separate flap diaphragm parts.

2. An exhaust gas flap in accordance with claim 1, wherein: in each axial end area of the mounting area, the flap wings extend in a diametrical direction of the flap tube beyond the mounting area to the area of the recess, or extend up to an outer circumference of the pivot shaft, or extend in the diametrical direction of the flap tube beyond the mounting area to the area of the recess and extend up to the outer circumference of the pivot shaft.

3. An exhaust gas flap in accordance with claim 1, wherein: each of the curved mounting area sections and the two separate flap diaphragm parts together partially enclose the pivot shaft.

4. An exhaust gas flap in accordance with claim 1, wherein: the mounting area of the flap diaphragm partially encloses the pivot shaft.

5. An exhaust gas flap in accordance with claim 1, wherein: both the curved mounting area sections of the two separate flap diaphragm parts enclose the pivot shaft at circumferential areas essentially located opposite one another, and the flap wings of the two separate flap diaphragm parts are arranged offset in relation to each other in the direction of a flap tube longitudinal axis when the flaps wings are in contact with the associated wing stops; the wing stops provided in association with the two flap wings are arranged essentially not offset in relation to each other in the direction of the flap tube longitudinal axis on both circumferential sides in relation to the pivot shaft, the wing stops providing stop surfaces for the associated flap wings on sides located opposite one another in the direction of the flap tube longitudinal axis; the wing stops are separate structure from the flap tube; an axial length of the wing stops along the flap tube longitudinal axis is equal to the offset of the the two separate flap diaphragm parts.

6. An exhaust gas flap in accordance with claim 1, wherein: each recess of a respective one of the two separate flap diaphragm parts is provided by a stepped structure of an axial end area of the respective curved mounting area.

7. An exhaust gas flap in accordance with claim 1, wherein: the pivot shaft is carried, rotatably about the pivot axis at the flap tube, in each of a first axial end area and a second axial end area; the two wing stops extend, without interruption in a circumferential direction relative to an inner circumference of the flap tube, from a first circumferential end area thereof, which is positioned in an area of the first axial end area of the pivot shaft, to a second circumferential end area, which is positioned in an area of the second axial end area of the pivot shaft, each stop surface configured for abutment of a respective one of the flap wings.

8. An exhaust gas flap in accordance with claim 7, wherein: each wing stop, in at least one of the first circumferential end area and the second circumferential end area, has a circumferential distance to the associated axial end area of the pivot shaft forming a gap; and each gap, which is formed by the circumferential distance between the pivot shaft and each one of the wing stops, is essentially completely overlapped in the circumferential direction by one of the flap wings when the flap wing is in contact with the respective stop surface of the associated wing stop.

9. An exhaust gas flap in accordance with claim 1, wherein: the curved mounting area sections of the two separate flap diaphragm parts enclose the pivot shaft at circumferential areas essentially located opposite one another; or the flap wings of the two separate flap diaphragm parts are arranged offset in relation to each other in the direction of the flap tube longitudinal axis when the flaps wings are in contact with the associated wing stops; or both the curved mounting area sections of the two separate flap diaphragm parts enclose the pivot shaft at circumferential areas essentially located opposite one another and the flap wings of the two separate flap diaphragm parts are arranged offset in relation to each other in the direction of the flap tube longitudinal axis when the flaps wings are in contact with the associated wing stops.

10. An exhaust gas flap in accordance with claim 9, wherein the wing stops provided in association with the two flap wings are arranged essentially not offset in relation to each other in the direction of the flap tube longitudinal axis on both circumferential sides in relation to the pivot shaft, the wing stops providing stop surfaces for the associated flap wings on sides located opposite one another in the direction of the flap tube longitudinal axis.

11. An exhaust gas flap for an exhaust gas stream of an internal combustion engine, the exhaust gas flap comprising: a flap tube; a pivot shaft rotatably arranged in an interior of said flap tube about a pivot axis; a first flap diaphragm part having a first curved mounting area and a first flap wing, said first curved mounting area and said first flap wing being formed as a one-piece configuration, said first curved mounting area being arranged on said pivot shaft to at least partially enclose said pivot shaft, said first curved mounting area defining a a first recess by an edge of said first curved mounting area extending along said pivot axis, and by another edge extending in a rotational direction of said pivot shaft; a second flap diaphragm part having a second curved mounting area and a second flap wing, said second curved mounting area and said second flap wing being formed as a one-piece configuration, said second curved mounting area being arranged on said pivot shaft to at least partially enclose said pivot shaft, said second curved mounting area defining a second recess by an edge extending along said pivot axis, and by another edge extending in the rotational direction of said pivot shaft; said first flap diaphragm part and said second flap diaphragm part being of identical configuration, being separate from each other, and being fixed to said pivot shaft independently from each other; a first wing stop comprising a first ring segment fixed to a first inner circumferential area of said flap tube, said first wing stop having a first stop surface, said first flap diaphragm part being rotatable with said pivot shaft to cause said first flap wing to contact said first stop surface, and partially block said flap tube; a second wing stop comprising a second ring segment fixed to a second inner circumferential area of said flap tube, said second wing stop having a second stop surface, said second flap diaphragm part being rotatable with said pivot shaft to cause said second flap wing to contact said second stop surface, and partially block said flap tube; said first and second stop surfaces being arranged facing in opposite axial directions of said flap tube, and being arranged to face away from each other.

12. An exhaust gas flap in accordance with claim 11, wherein: said first and second flap diaphragm parts are spaced from each other.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the drawings:

(2) FIG. 1 is a lateral view of an exhaust gas flap for an exhaust system of an internal combustion engine with a flap drive;

(3) FIG. 2 is a partially exploded in a perspective view showing the exhaust gas flap from FIG. 1;

(4) FIG. 3 is a sectional view of the exhaust gas flap from FIG. 1, cut along a line III-III in FIG. 1;

(5) FIG. 4 is a detail view of the exhaust gas flap from FIG. 1 in the adjoining area of a pivot shaft carrying a flap diaphragm at a flap tube of the exhaust gas flap; and

(6) FIG. 5 is a view corresponding to FIG. 4 of an alternative embodiment.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

(7) Referring to the drawings, an exhaust gas flap which can be used, for example, in an exhaust system of an internal combustion engine is designated by 10 in FIG. 1. A flap drive 12, which operates, for example, by means of an electric motor, is associated with the exhaust gas flap 10. A drive element 14, for example, drive shaft, of the flap drive 12 is coupled to the exhaust gas flap 10 via a coupling element 16, which is configured, for example, as a bow spring made of wire material, for the joint rotation with a pivot shaft 18. The pivot shaft 18 is carried pivotably about a pivot axis A in its two end areas 20, 22 via bearings, not shown, at a flap tube 24.

(8) A flap diaphragm, which is generally designated with 26, is carried at the pivot shaft 18 in the interior of the flap tube 24, which has an essentially circular cross section and correspondingly circular inner contour in this exemplary embodiment. In the exemplary embodiment of FIGS. 1 through 4, the flap diaphragm 26 comprises two flap diaphragm parts 28, 30, which have, e.g., a one-piece configuration. Each of the two flap diaphragm parts 28, 30 in turn comprises a flap wing 32, 34 as well as a mounting area section 36, 38. Each of the two mounting area sections 36, 38 has a curved configuration adapted to the outer contour of the pivot shaft 18 and each encloses the pivot shaft 18 in a partial area of the outer circumference thereof. The two mounting area sections 36, 38 thus together form a mounting area 40 for the flap diaphragm 26. The flap diaphragm parts 28, 30 can be mounted, for example, by welding at the pivot shaft 18 in this mounting area 40 or in the area of the mounting area sections 36, 38.

(9) A wing stop 42, 44 having a ring-segment-like configuration is provided at the flap tube 24 in association with each of the two flap wings 32, 34 or with each flap diaphragm part 28, 30. The two wing stops 42, 44 may be fixed, for example, by connection in substance at the inner circumference 46 of the flap tube 24, but may also be provided with the flap tube 24 as an integral component of same. As is illustrated in FIG. 1, for example, on the basis of the wing stop 44, this wing stop 44 extends without interruption along the inner circumference 46 of the flap tube 24 starting from a first circumferential end area 48 located close to the first axial end area 20 of the pivot shaft 18 to a second circumferential end area 50 located close to the second axial end area 22 of the pivot shaft 18. The wing stop 42 provides a stop surface 54 for the flap wing 28 on a side 52 oriented in the direction of a flap tube longitudinal axis L. Correspondingly, the wing stop 44 provides a stop surface 58 for the flap wing 34 on a front side 56 oriented in the direction of the flap tube longitudinal axis L. It is seen in FIG. 3 that the two wing stops 42, 44 are arranged essentially in the same axial area in relation to the flap tube longitudinal axis, so that the two stop surfaces 54, 58, which are oriented in a direction away from one another, are offset in relation to each other in the direction of the flap tube longitudinal axis L.

(10) In order to leave as few gaps as possible in the adjoining area of the circumferential end areas 48, 50 at the pivot shaft 18, each of the wing stops 42, 44 is brought as close as possible to the pivot shaft 18 in these circumference end areas 48, 50. In order to make this possible, the flap diaphragm 26 or each flap diaphragm part 28, 30 in the respective mounting area section 36, 38 has a recess 60, 62, 64, 66 at the end areas thereof located oriented in the direction of the pivot axis A. This recess may be provided by the mounting area sections 36, 38 being shorter in the direction of the pivot axis A than the flap wing 32, 34 connected to each of these sections. This means that the flap wings 32, 34 in the axial end areas of the flap diaphragm parts 28, 30 project axially over that area of the mounting area sections 36, 38, in which the recesses 60, 62, 64, 66 are provided.

(11) It can be seen in FIG. 1 and in FIG. 4 that the wing stop 44 extends with its first circumferential end area 48 so close to the pivot axis 18 that the first circumferential end area 48 meshes with the recess 60 of the flap diaphragm part 28 present in this area, at least when the flap wing part 28 or the mounting area section 36 thereof also pivots about the pivot axis A by rotating the pivot shaft 18 about the pivot axis A, and the flap wing 32 of the flap wing part 28 approaches the first circumferential end area 48 of the wing stop 44 in the circumferential direction in relation to the pivot axis A. Since the flap wing 34 of the flap wing part 30 located behind the wing stop 44 in FIG. 4 and interacting with same extends up to the pivot shaft 18, a gap 68, which is nonetheless unavoidably formed between the first circumferential end area 48 of the wing stop 44 and the pivot shaft 18, is essentially completely overlapped by the flap wing 34 in the circumferential direction. To keep this gap 68 as small as possible, the wing stop 44 may have a concave configuration in its first circumferential end area 48, adapted to the circular outer circumferential contour of the pivot shaft 18, and thus enclose the pivot shaft 18 in some areas in the circumferential direction.

(12) The functionality shown above with reference to the first circumferential end area 48 of the wing stop 44 is correspondingly also achieved in all other circumferential end areas of the wing stops 42, 44. It is thus ensured that as few flow leaks as possible occur especially in the adjoining area of the wing stops 42, 44 at the pivot shaft 18 in the blocked position, shown in FIG. 1 and also in FIG. 3, of the flap diaphragm 26, in which the two flap wings 32, 34, which are arranged offset in relation to each other in the direction of the flap tube longitudinal axis L, are in contact with their associated stop surfaces 54, 58 and thus block the flap tube 24 essentially against flow. This avoids disturbing noises, on the one hand, and provides an essentially noise-proof configuration, on the other hand. The embodiment of the flap diaphragm 26 with two flap diaphragm parts 28, 30 further makes possible a tolerance compensation between the flap diaphragm parts 28, 30 and the wing stops 42, 44 associated with same when the flap diaphragm parts 28, 30 are mounted with their mounting area sections 36, 38 during assembly. In this connection, the flap diaphragm parts 28, 38 can be positioned with their flap wings 32 34 being in contact with the associated wing stops 42, 44 and are subsequently connected to the pivot shaft 18 essentially independently of one another.

(13) FIG. 5 shows an alternative embodiment. FIG. 5 shows a configuration, in which the flap diaphragm 26 has a one-piece configuration. The flap diaphragm 26 comprises a mounting area 40, which is tubular and encloses the pivot shaft 18, from which mounting area 40 the flap wings 32, 34 extend on both sides of the pivot shaft 18. In the axial end areas, the flap wings 32, 34 extend beyond the mounting area 40, so that recesses, which can be seen in FIG. 5 on the basis of a recess 60, are formed in each of the areas located between the two flap wings 32, 34. The circumferential end areas, which can be seen in FIG. 5 on the basis of the first circumferential end area 48 of the wing stop 44, extend into these recesses up to close to the pivot axis 18, so that the gap 68 is formed between them. This gap 68 is overlapped by the flap wing 34, which is located behind the wing stop 44 in FIG. 5, wherein the flap wing 34, in its area extending axially beyond the mounting area 40, extends up to the outer circumference of the pivot shaft 18. This configuration may be provided in the adjoining area of each circumferential end area of the two wing stops 42, 44 at the pivot shaft 18. In this case, the two flap wings 32, 34 are preferably located in one plane and are thus not offset in relation to each other in relation to the flap tube longitudinal axis in case of positioning the flap diaphragm 26 in the blocked position. Hence, it is necessary to arrange the two wing stops 42, 44 or the stop surfaces provided at same correspondingly axially offset in relation to each other, but oriented facing each other.

(14) Also with the configuration shown in FIG. 5, the possibility is offered to bring the wing stops in their circumferential end areas very close to the pivot shaft 18 and to almost completely overlap a gap 68 formed between them in the circumferential direction in relation to the flap tube longitudinal axis and in the direction of the pivot axis A of the pivot shaft 18.

(15) While specific embodiments of the invention have been shown and described in detail to illustrate the application of the principles of the invention, it will be understood that the invention may be embodied otherwise without departing from such principles.