Internal combustion engine arrangement comprising a waste heat recovery system and process for controlling said system

Patent metadata

Field	Value
Publication number	US-9657603-B2
Application number	US-201314893943-A
Country	US
Kind code	B2
Filing date	Jul 15, 2013
Priority date	Jul 15, 2013
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A waste heat recovery system carrying a working fluid in a loop includes an expander, a condenser and a pump, a first and a second line arranged in parallel in the high pressure circuit portion upstream of the expander and joining at a downstream junction point in the high pressure circuit portion. The first line includes a first heat exchanger connected to the exhaust line, and the second line includes a second heat exchanger connected to a line carrying a warm fluid. A first by-pass system prevents not fully evaporated working fluid from the first line to flow through the expander. A second by-pass system connects the second line to the low pressure circuit portion for by-passing the downstream junction point and the expander.

First claim

The invention claimed is:

1. An internal combustion engine arrangement, comprising:
an internal combustion engine;
an exhaust line collecting exhaust gases from the engine;
an additional fluid line, distinct from the exhaust line, carrying a warm fluid;
a waste heat recovery system carrying a working fluid in a closed loop, in which the working fluid is successively pressurized from a low pressure circuit portion to a high pressure circuit portion by a pump, evaporated in the high pressure circuit portion, expanded in an expander from the high pressure circuit portion to a low pressure circuit portion, and condensed in a condenser in the low pressure circuit portion, the waste heat recovery system comprising a first and a second lines arranged in parallel in the high pressure circuit portion upstream of the expander, the first and second lines joining at a downstream junction point in the high pressure circuit portion upstream of the expander, wherein the first line comprises a first heat exchanger thermally connected to the exhaust line, in which the working fluid can be heated by means of the exhaust gases, and the second line comprises a second heat exchanger thermally connected to the additional fluid line, in which the working fluid can be heated by means of the warm fluid;

wherein it further comprises:
a first by-pass system designed to prevent not fully evaporated working fluid from the first line to flow through the expander;

a second by-pass system which connects the second line upstream of the downstream junction point, to the low pressure circuit portion, at a connecting point, for by-passing the downstream junction point and the expander.

2. The engine arrangement according to claim 1 , wherein the second by-pass system comprises at least one by-pass valve which is arranged in the second line between the second heat exchanger and the downstream junction point and which is capable of directing the flow of working fluid from the second heat exchanger either through the second line to the downstream junction point, or to the low pressure circuit portion.

3. The engine arrangement according to claim 1 , wherein the second bypass system is connected to the low pressure circuit portion upstream of the condenser.

4. The engine arrangement according to claim 1 , wherein the second bypass system comprises a secondary line which by-passes the expander and connects the second line upstream of the downstream junction point to a connecting point located in the low pressure circuit portion between the expander and the condenser.

5. The engine arrangement according to claim 2 , wherein the by-pass valve comprises an on-off three-way valve.

6. The engine arrangement according to claim 1 , wherein it comprises a determining device for determining at least one physical parameter of the working fluid in the second line, and a control unit operatively connected to the determining device for controlling the second by-pass system as a function of the physical parameter(s).

7. The engine arrangement according to claim 1 , wherein it comprises at least one pressure reducing valve located upstream from the condenser, and capable of reducing the pressure of the working fluid not having flown through the expander before it enters the condenser.

8. The engine arrangement according to claim 1 , wherein the first by-pass system comprises a first by-pass line having an inlet located between the first heat exchanger and the expander, and an outlet located in the low pressure circuit portion between the expander and the condenser.

9. The engine arrangement according to claim 8 , wherein the outlet of the secondary line is connected to the first by-pass line, between the inlet and the outlet of the first by-pass line, so that the connecting point and the outlet of the first bypass line coincide.

10. The engine arrangement according to claim 8 , wherein the connecting point coincides with the outlet of the secondary line and is distinct from the outlet of the first by-pass line, so that the secondary line forms a second by-pass line distinct from the first by-pass line.

11. The engine arrangement according to claim 7 , wherein the first by-pass system comprises a first by-pass line having an inlet located between the first heat exchanger and the expander, and an outlet located in the low pressure circuit portion between the expander and the condenser, and the outlet of the secondary line is connected to the first by-pass line, between the inlet and the outlet of the first by-pass line, so that the connecting point and the outlet of the first bypass line coincide, and wherein the engine comprises a common pressure reducing valve located in the first by-pass line between the secondary line outlet and the first by-pass line outlet.

12. The engine arrangement according to claim 7 , wherein the first by-pass system comprises a first by-pass line having an inlet located between the first heat exchanger and the expander, and an outlet located in the low pressure circuit portion between the expander and the condenser, and the outlet of the secondary line is connected to the first by-pass line, between the inlet and the outlet of the first by-pass line, so that the connecting point and the outlet of the first bypass line coincide, and wherein the engine comprises:
a first pressure reducing valve arranged in the first by-pass line and capable of reducing the pressure of the working fluid from the first line; and
a second pressure reducing valve, distinct from the first pressure reducing valve, which is arranged in the secondary line and is capable of reducing the pressure of the working fluid from the second line.

13. The engine arrangement according to claim 1 , wherein the first by-pass system comprises a control valve which is arranged in the first line, upstream from the first heat exchanger, and which is capable of preventing the working fluid from flowing into the first heat exchanger.

14. The engine arrangement according to claim 13 , wherein it comprises a derivation line into which the exhaust gases can flow so as to by-pass the first heat exchanger, and a valve for controlling the flow of exhaust gases in the derivation line.

15. The engine arrangement according to claim 13 , wherein it is devoid of any line joining a point located between the first heat exchanger and the expander to the low pressure circuit portion to allow the working fluid from the first line to by-pass the expander.

16. The engine arrangement according to claim 13 , wherein the secondary line forms a second by-pass line having an outlet which coincides with the connecting point.

17. The engine arrangement according to claim 1 , wherein it further comprises a control system for controlling the flow rate (Q 2 ) of working fluid in the second line, in order to regulate the temperature (T 4 ) of the warm fluid in the additional fluid line, between the second heat exchanger and the engine.

18. The engine arrangement according to claim 17 , wherein the control system comprises an electric motor ( 39 ) capable of driving the pump, and a proportional three way valve designed to regulate the sub flow rates of the working fluid in the first and second lines.

19. The engine arrangement according to claim 17 , wherein the pump is mechanically driven by the internal combustion engine, and in that the control system comprises an additional proportional three way valve located between the pump and the second heat exchanger and having a port connected to the low pressure circuit portion, between the

Assignees

• Volvo Truck Corp

Inventors

• Grelet Vincent

Classifications

• F01K23/065 Primary

  the combustion taking place in an internal combustion piston engine, e.g. a diesel engine · CPC title

• F01K23/10

  with exhaust fluid of one cycle heating the fluid in another cycle (F01K17/025 takes precedence) · CPC title