Element of an exhaust line comprising valve with added stoppers
US-10167785-B2 · Jan 1, 2019 · US
US10690063B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10690063-B2 |
| Application number | US-201715632694-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 26, 2017 |
| Priority date | Jun 27, 2016 |
| Publication date | Jun 23, 2020 |
| Grant date | Jun 23, 2020 |
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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 ).
Opening claim text (preview).
What is claimed is: 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,
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