Turbomachine

Abstract

A turbomachine may include a turbine arranged in a housing and configured to be acted on with a hot working medium. The turbomachine may include at least one bypass channel for heating the housing through the working medium. The bypass channel may extend completely within the housing and be configured to bypass the turbine.

Claims

1. A turbomachine, comprising: a housing surrounding a turbine chamber; a turbine arranged in the turbine chamber of the housing and configured to be acted on with a working medium; a flow duct coupled to the turbine for conveying the working medium, the flow duct including an upstream duct portion for feeding the working medium to the turbine and a downstream duct portion for discharging the working medium from the turbine; at least one bypass channel configured to heat the housing by transferring heat from the working medium to the housing, the at least one bypass channel structured and arranged to extend completely within the housing and guide the working medium around the turbine, wherein an inlet side of the at least one bypass channel is connected to the upstream duct portion at a first coupling point and an outlet side of the at least one bypass channel is connected to the downstream duct portion at a second coupling point; at least one heat-insulated bypass channel extending at least partially in the housing and configured to bypass the turbine, the at least heat-insulated bypass channel configured to minimize heat transfer of the working medium to the housing; a valve device disposed at the first coupling point and configured to divide a flow of the working medium among the turbine, the at least one bypass channel, and the at least one heat-insulated bypass channel, wherein the valve device is structured and arranged to redirect the flow of the working medium completely to the at least one bypass channel in a bypass mode; at least one heat transfer element arranged in the at least one bypass channel to facilitate heat transfer to the housing, wherein the at least one heat transfer element includes ribs distributed circumferentially to one another about an interior surface of the at least one bypass channel and projecting radially towards a center of the at least one bypass channel with respect to a flow direction of the working medium flowing therethrough to facilitate heating the housing to an operating temperature greater than a condensation temperature of the working medium when the valve device is in the bypass mode; and wherein the at least one bypass channel includes a plurality of bypass channels arranged separate from one another at various locations about the housing and structured to guide the working medium past the turbine, and wherein the plurality of bypass channels extend parallel to one another within the housing between the first coupling point and the second coupling point.

2. The turbomachine according to claim 1, wherein the turbine is an axial impulse turbine.

3. The turbomachine according to claim 1, wherein the first coupling point connected to the inlet side of the at least one bypass channel is arranged within the housing upstream of the turbine and the second coupling point connected to the outlet side of the at least one bypass channel is arranged within the housing downstream of the turbine.

4. The turbomachine according to claim 1, the valve device is switchable between the bypass mode and an operating mode where the valve device directs the working medium to the turbine.

5. The turbomachine according to claim 1, wherein the working medium is a phase change fluid according to the Clausius-Rankine cycle.

6. The turbomachine according to claim 1, wherein the valve device is structured and arranged to redirect the flow of the working medium completely to the at least one heat-insulated bypass channel.

7. An internal combustion engine, comprising: a Clausius-Rankine cycle including a turbomachine integrated therein via a line that conveys a working medium, an exhaust gas heat exchanger operatively connected in a heat- transferring manner to an exhaust gas flow, a condenser, a reservoir for the working medium, and a pump integrated therein via the line, the turbomachine including: a housing surrounding a turbine chamber and provided with an inlet for supplying the working medium to the turbomachine and an outlet for discharging the working medium from the turbomachine; a turbine arranged in the turbine chamber of the housing and operatively connected to the line, the turbine configured to interact with the working medium conveyed in the line; at least one bypass channel configured to heat the housing by transferring heat from the working medium to the housing, an inlet side of the at least one bypass channel coupled to the line at a first coupling point disposed upstream of the turbine and an outlet side of the at least one bypass channel coupled to the line at a second coupling point disposed downstream the turbine, wherein the at least one bypass channel is structured and arranged to extend within the housing and guide the working medium around the turbine from the first coupling point to the second coupling point to bypass the turbine; at least one heat-insulated bypass channel structured and arranged to extend at least partially in the housing and bypass the turbine separate from the at least one bypass channel, the at least one heat-insulated bypass channel configured to minimize heat transfer of the working fluid to the housing; a valve device arranged at the first coupling point configured to divide a flow of the working medium among the turbine and the at least one bypass channel, the valve device switchable between an operating mode where the flow of the working medium is guided from the exhaust gas heat exchanger through the turbine, and a bypass mode where the flow of the working medium is guided from the exhaust gas heat exchanger through the at least one bypass channel and past the turbine towards the condenser arranged downstream of the turbomachine; and wherein the valve device is structured to switch into a position that redirects the flow of the working medium completely to the at least one heat-insulated bypass channel.

8. The internal combustion engine according to claim 7, wherein the turbomachine is arranged in the Clausius-Rankine cycle between the exhaust gas heat exchanger and the condenser, and the exhaust gas heat exchanger is arranged upstream of the turbomachine and downstream of the pump.

9. The internal combustion engine according to claim 7, wherein at least one of the first coupling point and the valve device is disposed within the housing.

10. The internal combustion engine according to claim 7, wherein the valve device is structured and arranged to redirect the flow of the working medium completely to the at least one bypass channel in the bypass mode.

11. The internal combustion engine according to claim 7, wherein the at least one bypass channel includes at least one heat transfer element to facilitate heat transfer of the working medium to the housing, the at least one heat transfer element including ribs distributed circumferentially to one another about an interior surface of the at least one bypass channel and projecting radially towards a center of the at least one bypass channel with respect to a flow direction of the working medium flowing therethrough to facilitate heating the housing to an operating temperature above a condensation temperature of the working medium.

12. The internal combustion engine according to claim 7, wherein the at least one bypass channel includes a plurality of bypass channels arranged separate from one another at various locations about the housing and structured to extend parallel to one another within the housing between the first coupling point and the second coupling point.

13. The internal combustion engine according to claim 12, wherein the at least one bypass channel is connected to the valve device and splits up into the plurality of bypass channels downstream of the valve device.

14. The internal combustion engine according to claim 7, wherein the valve device is structured and arranged to direct the working medium completely to the at least one bypass channel when a temperature of the working medium of the Clausius-Rankine cycle flowing to the turbomachine is below a predefined temperature corresponding to a saturated vapor state of the working medium.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the figures, schematically:

(2) FIG. 1 shows a turbomachine according to the invention,

(3) FIG. 2 shows a turbomachine according to the invention, embedded in a Rankine cycle of an internal combustion engine.

DETAILED DESCRIPTION

(4) According to FIG. 1, a turbomachine 1 according to the invention comprises a turbine 3 which is arranged in a housing 2 and can be acted on with hot working medium. According to the invention, at least one bypass channel 4 for heating the housing 2 or the turbine 3 through the working medium is provided, which bypass extends completely within the housing 2 and bypasses the turbine 3. Through this it is possible during a starting phase of an internal combustion engine 5 (cf. FIG. 2), in which sufficient heat quantity has not yet been transferred to the working medium of the Rankine cycle, to first guide the working medium past the turbine 3 and through the bypass channel 4, which bypass channel contributes to the fact that the housing 2 of the turbomachine 1 is heated up more quickly and therefore the turbine 3 is indirectly heated, so that in particular liquid working medium still situated in the region of the turbine 3 evaporates before the turbine is actually acted on with saturated vapor. Through this it is possible to prevent in particular so-called droplet impingement erosion which can result in damage to the turbine 3 and in particular to the rotor blades arranged therein. By more quickly heating of the housing 2, the turbomachine 1 overall can be brought more quickly to its operating temperature, that is, to a temperature above the condensation temperature of the working medium.

(5) For a better heat transfer from the bypass channel 4 to the housing 2, heat transfer elements 6, which can be formed like ribs, for example (cf. cross-sectional illustration on the bottom right in FIG. 1), can be provided in the bypass channel 4. Also, a cross-section of the bypass channel 4 can be selected individually so that the latter can have a round or angular cross-section. It is also conceivable, of course, that a plurality of bypass channels 4 extending substantially parallel are arranged within the housing 2, as is illustrated for the turbomachine 1 according to FIG. 2, for example.

(6) Optionally, at least one separate and heat-insulated bypass channel 4 can also be provided, which also bypasses the turbine 3, but is not or only marginally connected to the housing 2 in a heat-transferring manner. Also, it is not necessary that the bypass channel 4 extends completely within the housing 2. For example, the turbomachine 1 can be designed as an axial impulse turbine. When viewing again the bypass channel 4 according to the FIGS. 1 and 2, it can be seen that the bypass channel is coupled on the inlet side at a first coupling point 7 and on the outlet side at a second coupling point 8 to a line 9, wherein both coupling points 7, 8 are arranged within the housing 2. As an alternative, these coupling points 7, 8 can also be implemented outside of the housing 2. In the line 9, the working medium heated by an exhaust gas heat exchanger 10 (cf. FIG. 2) or generally by an evaporator flows to the turbomachine 1 and/or flows away again therefrom. At the first coupling point 7, a valve device 11 is arranged which, depending on the position, divides a working medium flow among the turbine 3 and/or the at least one bypass channel 4, wherein the valve device 11 is also arranged within the housing 2. Of course, the valve device 11 also enables to redirect the working medium flow completely to the bypass channel 4, which is arranged separate from the other bypass channels 4 and is not connected in a heat-transferring manner to the housing 2 of the turbomachine 1.

(7) When viewing FIG. 2, an internal combustion engine 5 can be seen there which comprises a Rankine cycle 12 in which the above-described turbomachine 1, for example for power generation, is arranged. Furthermore, the exhaust gas heat exchanger 10 connected in a heat-transferring manner to the exhaust gas flow of the internal combustion engine 5, a condenser 13 for the working medium and a pump 14 are also located in the Rankine cycle 12. In addition, a reservoir 15 for the working medium can be provided.

(8) With the turbomachine 1 according to the invention it is possible to not only increase the service life of a turbine 3 significantly since erosion due to insufficiently heated working medium is no longer a concern, but it is also possible to use the turbomachine 1 earlier because via the at least one bypass channel 4, which is arranged completely within the housing 2, rapid heating of the housing 2 and the turbine 3 is possible.