Device and method for separating dirt particles from the working medium of a turbine
09970327 ยท 2018-05-15
Assignee
Inventors
- Andreas Wengert (Backnang, DE)
- Hans-Christoph Magel (Reutlingen, DE)
- Nadja EISENMENGER (Stuttgart, DE)
- Frank Ulrich Rueckert (Stuttgart, DE)
Cpc classification
B01D45/16
PERFORMING OPERATIONS; TRANSPORTING
F05D2260/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D45/14
PERFORMING OPERATIONS; TRANSPORTING
F01D9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K11/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K25/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D25/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K11/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K25/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D45/14
PERFORMING OPERATIONS; TRANSPORTING
B01D45/16
PERFORMING OPERATIONS; TRANSPORTING
F01D5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention relates to a device and a method for separating dirt particles from the working medium of a turbine (10). The turbine (10) comprises at least one rotor (11) which is arranged in a housing (17). A swirl generator (20) is provided that sets the working medium and the dirt particles in a spiral-shaped rotational movement along a principal axis (22) by means of the geometry of the swirl generator (20) and thereby separates the dirt particles from the working medium. The swirl generator (20) is designed in such a way that the working medium experiences a reversal of the speed component parallel to the principal axis (22) within the swirl generator (20).
Claims
1. A device for separating dirt particles from a working medium of a turbine (10), the turbine (10) comprising at least one rotor (11) which is arranged in a housing (17), the device comprising a swirl generator (20) configured to set the working medium and the dirt particles in a spiral-shaped rotational movement having a speed component along a first direction parallel to a principal axis (22) by means of a geometry of the swirl generator (20) and thereby separate the dirt particles from the working medium, characterized in that the swirl generator (20) has at least one reflection surface by means of which the speed component of the working medium is reversed within the swirl generator, wherein the reflection surface faces the rotor, is perpendicular to the principal axis, and is configured to redirect the working medium along a second direction that is opposite to the first direction.
2. The device according to claim 1, characterized in that the swirl generator (20) includes a hollow body (24) which is approximately rotationally symmetrical and into which a pipe (26) protrudes, the pipe being a connection to the turbine (10).
3. The device according to claim 2, characterized in that the pipe (26) which protrudes into the hollow body (25) of the swirl generator (20) is formed by the housing (17) of the turbine (10).
4. The device according to claim 2, characterized in that the swirl generator includes an inlet line (28) configured to pass the working medium into the hollow body of the swirl generator (20), the swirl generator (20) configured such that the working medium has a further speed component tangential to an inner wall (25) of the hollow body (24).
5. The device according to claim 4, characterized in that an inside radius of the hollow body (24) decreases along the principal axis (22) between the inlet line (28) and an outflow wall (27) located opposite the pipe, wherein the outflow wall (27) includes the reflection surface.
6. The device according to claim 5, characterized in that at least one outlet line (23) for dirt particles is disposed on the outflow wall (27).
7. An internal combustion engine comprising the device according to claim 1, wherein the turbine (10) is disposed in a system for heat recovery (30) in the internal combustion engine (31), in which system the working medium passes through a circuit, wherein at least one heat exchanger (32), the turbine (10), at least one condenser (34) and at least one pump (36) are disposed in succession.
8. The device according to claim 1, wherein the housing (17) forms a pipe (26) that extends into the swirl generator (20), wherein the reflection surface is configured to redirect the working medium into the pipe (26) along the second direction.
9. The device according to claim 8, wherein a nozzle (13) is disposed within the housing (17) between the pipe (26) and the rotor (11).
10. The device according to claim 1, wherein the reflection surface is flat.
11. The device according to claim 1, wherein the device includes an outlet wall that includes the reflection surface, wherein the device further includes at least one outlet line (23) having an inlet opening in the reflection surface, wherein the inlet opening is configured such that the dirt particles enter the inlet opening along the first direction and the working medium moves along the opposite, second direction.
12. A method for separating dirt particles from a working medium of a turbine (10), the turbine (10) comprising at least one rotor (11) which is disposed in a housing (17), the method comprising providing a swirl generator (20) configured to set the working medium and the dirt particles into a spiral-shaped rotational movement (7, 9) having a speed component along a first direction parallel to a principal axis (22) and thereby separate the dirt particles from the working medium, and causing the working medium to experience a reversal of the speed component parallel to the principal axis (22) by means of at least one reflection surface of the swirl generator (20), wherein the reflection surface faces the rotor, is perpendicular to the principal axis, and is configured to redirect the working medium along a second direction that is opposite to the first direction, whereas the dirt particles are separated through an outlet line (23) due to a higher inertia thereof in comparison to the working medium.
13. The method according to claim 12, characterized in that the swirl generator (20) includes a hollow body (24) that is approximately rotationally symmetrical and the working medium is caused to flow with a further speed component tangentially to an inner wall (25) of the hollow body (24).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) An exemplary embodiment of the invention is depicted in the drawings and is explained in detail in the following description.
(2) In the drawings:
(3)
(4)
(5)
DETAILED DESCRIPTION
(6) A turbine 10 comprising a rotor 11, which is disposed in a housing 17, is shown in
(7) A nozzle arrangement 13 can be disposed upstream of the rotor 11. This can be a laval nozzle which leads to an acceleration of the working medium prior to striking the rotor 11.
(8) A swirl generator 20 is disposed directly on the input side of the turbine 10. The swirl generator 20 is formed from a hollow body 24 which is approximately rotationally symmetrical and which is fastened to the front face of the housing 17 of the turbine 10. The hollow body 24 has an inlet line 28. The working medium can move into the hollow body 24 of the swirl generator 20 by means of the inlet line 28. On account of the inlet line 28, the rotational symmetry is interrupted in at least one region of the hollow body 24.
(9) The inlet line 28 can be designed such that the working medium has at least one further speed component parallel to an inner wall 25 of the hollow body 24.
(10) A pipe 26, which constitutes a connection to the turbine 10, is disposed within the hollow body 24. The pipe 26 can be formed by the housing 17 of the turbine 10. The pipe can, however, also be a separate component of the swirl generator 20, which is flanged to the housing 17 of the turbine 10 by means of a connection that is as impermeable as possible. Working medium which has flowed into the swirl generator 20 moves through the pipe 26 into the supply line 12 of the turbine 10.
(11) An outlet line 23 is disposed on an outflow wall 27 located opposite the pipe 26. The outlet line 23 can be connected to the hollow body 24 via a bore in the center of the outflow wall 27. Further positions of the bore within the outflow wall 27 are also possible. Said positions can be selected as a function of the geometry of the hollow body 24.
(12) The device shown in
(13) In order to remove the dirt particles from the working medium of the turbine 10, the working medium containing the dirt particles is led via the inlet line 28 into the swirl generator 20 directly upstream of the turbine 10.
(14) By way of example,
(15) Centrifugal forces act on the working medium and the dirt particles by means of the spiral-shaped rotational movement, said centrifugal forces produce a radial force that is directed outwards on the working medium and the dirt particles. Due to the different size and thickness of the particles of the working medium and the dirt particles, a spatial separation of the working medium from the dirt particles occurs during this spiral-shaped rotational movement.
(16) The working medium experiences a reflection on at least one reflection surface of the hollow body 24 which leads to a reversal of the speed component parallel to the principal axis 22 and therefore to a change in sign of the corresponding speed component so that an inner partial vortex 9 forms which is in the opposite direction of the outer main vortex 7. In contrast, the dirt particles do not experience a reversal of the speed component parallel to the principal axis 22 so that they continue to move in the direction of the outlet line 23. This causes a separation of working medium and dirt particles. While the working medium and the dirt particles are still situated in the outer main vortex, the proportion of dirt particles in the inner partial vortex is greatly reduced.
(17) The at least one reflection surface can be formed by any wall of the hollow body 24. An arrangement according to
(18) The inner partial vortex 9 moves with a spiral-shaped rotational movement in the opposite direction of the outer main vortex 7. Furthermore, the radius of the inner partial vortex 9 is smaller than the radius of the outer main vortex 7 so that a mixing of the working medium from the outer main vortex 7 and the inner partial vortex 9 hardly occurs.
(19) The working medium of the inner partial vortex 9 moves in the direction of the pipe 26, through which the working medium passes into the supply line 12 of the turbine 20, due to the opposite speed component with respect to the main vortex 22.
(20) In contrast, the dirt particles move in the direction of the outlet line 23 and can be removed from the swirl generator through said outlet line 23.
(21) The hollow body 24 is formed by a cone in the depiction in
(22) A schematic depiction of a system for heat recovery 30 in an internal combustion engine 31 is shown in
(23) The working medium passes through the system for heat recovery 30 within the framework of a circular process and, in so doing, is not exchanged. This leads to a permanent accumulation of dirt particles in the working medium so that, precisely here, the device and the method for separating dirt particles from the working medium take on a great deal of importance.