CONNECTION DEVICE FOR AN EXHAUST TURBOCHARGER AND EXHAUST TURBOCHARGER
20200149569 ยท 2020-05-14
Assignee
Inventors
Cpc classification
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L23/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16B7/0453
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L23/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/1805
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16B9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16B7/182
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/243
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16B7/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16B9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L23/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A connection device for an exhaust gas turbocharger includes an essentially bent first element and an essentially bent second element. The first element has a radially extending first clamping arm in a first end region and the second element has a radially extending second clamping arm in the first end region opposite the first clamping arm. The first element is movably connected with the second element in a second end region. The first clamping arm and the second clamping arm may be movably connected by a first connecting element of the connection device. The first element comprises a first supporting portion and the second element comprises a second supporting portion between the two end regions. A stiffening element is formed in a transition region between the clamping arm and the supporting portion for increasing the strength of the connection device.
Claims
1.-11. (canceled)
12. A connection device for an exhaust gas turbocharger, comprising: an essentially bent first element (2); and an essentially bent second element (3), wherein the first element (2) comprises a radially extending first clamping arm (8) in a first end region (13) of the connection device (1) and the second element (3) comprises a radially extending second clamping arm (11) in the first end region (13) opposite the first clamping arm (8), and wherein the first element (2) is formed movably connected with the second element (3) in a second end region (14) of the connection device (1), which faces away from the first end region (13), and wherein the first clamping arm (8) and the second clamping arm (11) may be movably connected by a first connecting element (4) of the connection device (1), and wherein the first element (2) comprises a first supporting portion (6) and the second element (3) comprises a second supporting portion (7) between the two end regions (13, 14), and wherein a stiffening element (27) is formed in a transition region (26) between the clamping arm (8; 11) and the supporting portion (6; 7) for increasing the strength of the connection device (1).
13. The connection device according to claim 12, wherein the two elements (2, 3) comprise the stiffening element (27) in the transition regions (26) at the two end regions (13, 14).
14. The connection device according to claim 12, wherein the stiffening element (27) is formed extending centrally along a center axis (28) of the connection device (1), or wherein the stiffening element is arranged offset relative to the center axis (28).
15. The connection device according to claim 12, wherein the stiffening element (27), is formed asymmetrically relative to the center axis (28).
16. The connection device according to claim 12, wherein the stiffening element (27) is formed as a bead.
17. The connection device according to claim 12, wherein the stiffening element (27) is formed convex or concave.
18. The connection device according to claim 12, wherein the elements (2, 3) are formed profiled exhibiting a cross-sectional profile.
19. The connection device according to claim 18, wherein the cross-sectional profile is formed U-shaped or trapezoidal.
20. The connection device according to claim 12, wherein the first element (2) and the second element (3) are formed movably in the second end region (14) by a second connecting element (5), and wherein the second connecting element (5) is formed as a chain link (5), and wherein at least one of the first element (2) or the second element (3) is formed to be inserted through the chain link (5).
21. An exhaust gas turbocharger, comprising a first casing section and a second casing section, wherein the first casing section and the second casing section are formed connected with each other by the connection device as in claim 12.
22. The exhaust gas turbocharger according to claim 21, wherein a stiffening element (27) of the connection device (1) is formed offset relative to a center axis (28) of the connection device (1), and wherein it exhibits a smaller distance from a leg (25) of the connection device (1), which rests against the first casing section than from a leg (25) which rests against the second casing section.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032]
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[0034]
[0035]
DETAILED DESCRIPTION
[0036] An exhaust gas turbocharger (not shown in detail) comprises a first casing section as a flow-through exhaust gas guide portion which during operation of the exhaust gas turbocharger is flown through by a fluid, generally by exhaust gas. The exhaust gas is generally, but not necessarily, a combustion product of a combustion engine (not shown in detail).
[0037] Furthermore, the exhaust gas turbocharger comprises a second casing section, which is formed as a bearing portion and serves to support the rotor assembly of the exhaust gas turbocharger. The bearing portion is positioned between a flow-through air guide portion (also not shown in detail) of the exhaust gas turbocharger and the exhaust gas guide portion.
[0038] The rotor assembly (not shown in detail) comprises a compressor wheel and a turbine wheel, which are connected non-rotatably with each other via a shaft. The compressor wheel is arranged in a compressor wheel chamber of the air guide portion to take in generally fresh air. The turbine wheel is rotatably accommodated in a wheel chamber of the exhaust gas guide portion.
[0039] During operation of the exhaust gas turbocharger, the turbine wheel is subjected to the exhaust gas flowing through the exhaust gas guide portion and driven by it so that it may perform a rotary movement. This rotary movement may be transferred to the compressor wheel via the shaft, which thereby simultaneously to the rotary movement of the turbine wheel may perform a rotary movement. By means of the compressor wheel and its rotary movement, fresh air is taken in which is compressed in the air guide portion.
[0040] The exhaust gas turbocharger is mechanically and thermodynamically coupled with the combustion engine, and during operation of the combustion engine and thus during operation of the exhaust gas turbocharger, vibrations occur which act on the exhaust gas turbocharger. In addition, the exhaust gas turbocharger is subjected to varying stresses due to varying temperatures of the flowing through exhaust gas with varying elongations in particular of the exhaust gas guide portion.
[0041] The exhaust gas guide portion comprises a first flange surface at its end facing the bearing portion. Opposite this first flange surface, a second flange surface of the bearing portion is formed, wherein the two flange surfaces are formed mainly complementary.
[0042] The two flange surfaces are formed to extend both radially as well as in the circumferential direction relative to a longitudinal axis of the exhaust gas turbocharger, which corresponds to an axis of rotation of the turbine wheel. The exhaust gas guide portion comprises a first portion collar opposite the bearing portion, which is associated with an axially adjacent second portion collar of the bearing portion. The first flange surface and the second flange surface extend over the first portion collar and the second portion collar, respectively.
[0043] The exhaust gas guide portion and the bearing portion are connected with each other by a connection device 1 in the region of the flange surfaces. The connection device 1 comprises a first element 2 which is mainly bent in the circumferential direction and a second element 3 which is mainly bent in the circumferential direction, which on one end are detachably connected with each other by means of a first connecting element 4 and on the other end are movably connected with each other by means of a second connecting element 5, see
[0044] The elements 2, 3 each comprise an essentially bent, in particular segment-shaped supporting portion 6; 7. The first supporting portion 6 of the first element 2 has a radially outwardly extending first clamping arm 8 at its one end and at its end facing away from the first clamping arm 8 a hook-shaped first safety portion 9 which also extends outwardly. It should be noted that outer, outwardly indicates the region which lies on the side of the connection device 1 facing away from a longitudinal axis 10 of the connection device 1. In the following, the region between the connection device 1 and the longitudinal axis 10 will be referred to as inner, inwardly.
[0045] The second supporting portion 7 of the second element 3 has a radially outwardly extending second clamping arm 11 at its one end, and at its end facing away from the second clamping arm 11 a hook-shaped second safety portion 12 which also extends outwardly.
[0046] The two elements 2, 3 are arranged opposite each other in such a manner that they form a more or less circular inner space encompassing it, wherein the two clamping arms 8, 11 opposite form a first end region 13 of the connection device 1 and the two safety portions 9, 12, also opposite, form a second end region 14 of the connection device 1.
[0047] An opening 15 each is formed in the clamping arms 8, 11, through which an insert element 16 of the first connecting element 4, the screw, may be inserted. A head 17 of the insert element 16 is formed to rest on the first clamping arm 8 so that the insert element 16 may bear against the first clamping arm 8. At the insert element end 18 facing away from the head 17, a clamping disk 18 and a safety element 20 are arranged, so that the two elements 2, 3 may be clamped together through a preload force of the first connecting element 4. The first end region 13 comprises the first connecting element 4 which is formed as a form and force-fitting-connecting element and in particular as a screw-nut element.
[0048] The second end region 14 in which the two hook-shaped safety portions 9, 12 of the two elements 2, 3 are formed comprises the second connecting element 5 for a movable connection of the two elements 2, 3, which is formed as a chain link.
[0049] The two clamping arms 8, 11 comprise one stop each at their ends facing away from the supporting portions 6, 7, i. e. the first clamping arm 8 comprises a first stop 21 and the second clamping arm 11 comprises a second stop 22. The two stops 21, 22 serve for an improved force introduction in the circumferential direction of the connection device 1 with the two casing sections being preloaded by means of the connection device 1.
[0050] The two elements 2, 3 are made from a profiled material for a relative adaptation of an inner circumference 23 of the connection device 1 to an outer circumference of the portion collars with legs 25 between a band 24 which exhibits an essentially trapezoidal profile. It could as well exhibit an essentially U-shaped or otherwise designed profile which is suited for the application range.
[0051] To achieve an improved strength of the transition regions 26 formed between the supporting portions 6, 7 and their ends 8, 11, 9, 12, stiffening elements 27 are provided. The transition regions 26 are those places where tensile and compressive stresses occur during operation, because in particular an intensive material reshaping is present in the end regions 13, 14.
[0052] For reducing these tensile and compressive stresses, the first element 2 and the second element 3 are provided with the stiffening elements 27.
[0053] In the first exemplary embodiment which is configured according to
[0054]
[0055] The stiffening elements 27 each are formed in the axial centre of the elements 2, 3. In particular this leads to an increase in stiffness and strength in the highly loaded transition region, such that cracking starting from an outer edge of the respective leg 25 is prevented.
[0056]
[0057] The second connecting element 5 is accommodated in the two safety portions 9, 12, wherein starting from an inner space 29 of the second connecting element 5 the two safety portions 9, 12 extend winding about the second connecting element 5. The bead 27 is formed in the two elements 2, 3 axially protruding into the inner space 29.
[0058]
[0059] Because the stiffening element 27 is formed extending into the inner space 29 of the second connecting element 5 the second connecting element 5 is adapted to the stiffening element 27, see
[0060]
[0061]
[0062]
[0063] It goes without saying that the shape of the stiffening element 27 is not limited to the exemplary embodiments, but may take any design.
[0064]
[0065] In the closed condition as shown in
[0066] The transition regions 26 are to be implemented in such a manner that after a material reshaping of the profiled material a tensile stress or a compressive stress, respectively, just high enough is generated in legs 25 so that an elastic deformation of the transition regions 26 for contact-making between the stops 21, 22 is possible.
[0067] An elasticity of the transition regions 26 which serves to generate an axial force between the legs 25 of the elements 2, 3 is achieved by means of the stiffening elements 27 which are arranged between the legs 25. This means that a variable cross-section 36 in the transition regions 26 is designed in such a manner that an elastic deformation of the supporting portions 6, 7 at a sufficient stiffness of the transition regions 26 at a simultaneous absorption of tensile or compressive stresses, respectively, is possible to introduce a circumferential stress into the supporting portion 6; 7.
[0068] For making a firm and unmovable connection of the two casing sections by means of the connection device 1, the first connecting element 4 is preloaded after positioning of the connection device 1 which is arranged encompassing the two casing sections, wherein the two stops 21, 22 are pressed upon one another until the two clamping arms 8, 11 again lie at an angle relative to one another, wherein, however, a maximum distance is formed between the two clamping arms 8, 11 in the transition region 26.
[0069] The two safety portions 9, 12 are preferably configured in the shape of a crane hook, which means in other words that they accommodate the second connecting element 5 secured against an essentially axial displacement along the center axis 28.
[0070] In an exemplary embodiment (not shown in detail) the stiffening elements 27 are arranged axially offset, which means in other words, that their center lines relative to their longitudinal extension do not coincide with the center axis 28 but are offset from this center line in the direction of the turbine casing.