Inlet system for an internal combustion engine

Patent metadata

Field	Value
Publication number	US-10590890-B2
Application number	US-201716092322-A
Country	US
Kind code	B2
Filing date	May 4, 2017
Priority date	May 9, 2016
Publication date	Mar 17, 2020
Grant date	Mar 17, 2020

Abstract

An inlet system for an internal combustion engine is provided and includes a compressor including a rotor, and an air guide arranged to guide an air flow from an air inlet to at least one cylinder of the engine via the compressor. The inlet system also includes at least two fluid sources, and at least two fluid guiding elements each arranged to guide a fluid from a respective of the fluid sources to the air guide, between the air inlet and an outlet of the compressor, that the fluid guiding elements present a first conduit for guiding a fluid from a first of the fluid sources, and a second conduit for guiding a fluid from a second of the fluid sources, and that a restriction of a flow of the fluid from the first fluid source is provided by a downstream end of the first conduit and the rotor, whereby a downstream end of the second conduit is arranged so that a pressure drop provided by the restriction drives fluid through the second conduit towards the downstream end of the second conduit.

First claim

The invention claimed is:

1. An inlet system for an internal combustion engine, comprising
a compressor comprising a rotor, and
an air guide arranged to guide an air flow from an air inlet to at least one cylinder of the engine via the compressor,
wherein the inlet system comprises at least two fluid sources, and at least two fluid guiding elements each arranged to guide a fluid from a respective of the fluid sources to the air guide, between the air inlet and an outlet of the compressor, and
the fluid guiding elements present a first conduit for guiding a fluid from a first of the fluid sources, and a second conduit for guiding a fluid from a second of the fluid sources, wherein a restriction of a flow of the fluid from the first fluid source is provided by a downstream end of the first conduit and the rotor, whereby a downstream end of the second conduit is arranged so that a pressure drop provided by the restriction drives fluid through the second conduit towards the downstream end of the second conduit.

2. An inlet system according to claim 1 , wherein the restriction is created by the first conduit downstream end being in a vicinity of the rotor.

3. An inlet system according to claim 1 , wherein the restriction is arranged so that a cross-sectional area of a flow through the restriction is smaller than a cross-sectional area of the flow in the first conduit upstream of the first conduit downstream end.

4. An inlet system according to claim 1 , wherein a rotational axis of the rotor extends through the downstream end of the first conduit.

5. An inlet system according to claim 1 , wherein compared to the first conduit, the second conduit extends further downstream in the air guide.

6. An inlet system according to claim 1 , wherein the downstream end of the second conduit is in a vicinity of the restriction.

7. An inlet system according to claim 1 , wherein the distance between the downstream end of the second conduit and the downstream end of the first conduit is within 0-30 mm.

8. An inlet system according to claim 1 , wherein the downstream ends of the first and second conduits form a conduit outlet arrangement for injecting fluid into the air guide.

9. An inlet system according to claim 8 , wherein the conduit outlet arrangement is, as seen in a transverse cross-section of the air guide, centrally arranged in the air guide.

10. An inlet system according to claim 8 , wherein the conduit outlet arrangement is arranged to inject the fluid guided by the first and second conduits towards the centre of the rotor.

11. An inlet system according to claim 1 , wherein a rotational axis of the rotor extends through the downstream end of the first conduit.

12. An inlet system according to claim 1 , wherein the downstream ends of the first and second conduits form a conduit outlet arrangement, a portion of the rotor extending into the conduit outlet arrangement.

13. An inlet system according to claim 1 , wherein at least a part of the first conduit is integrated with at least a part of the second conduit so as to form an integrated fluid guiding element.

14. An inlet system according to claim 1 , wherein the first and second conduits are concentrically arranged.

15. An inlet system according to claim 1 ,
wherein the fluid sources are liquid sources, and the fluid guiding elements are each arranged to guide a liquid from a respective of the liquid sources to the air guide, between the air inlet and the outlet of the compressor.

16. An inlet system according to claim 15 , wherein the inlet system comprises a valve arranged to control the communication between one of the liquid sources and the air guide via one of the fluid guiding elements based on an amount of liquid upstream of the valve.

17. An inlet system according to claim 16 , wherein the valve is a float valve.

18. An inlet system according to claim 1 , wherein one of the fluid sources is a charge air cooler, the air guide being arranged to guide the air flow to the at least one cylinder via the charge air cooler, the charge air cooler being located downstream of the compressor.

19. An inlet system according to claim 1 , wherein one of the fluid sources is a crankcase of the engine or is adapted to communicate with a crankcase of the engine.

20. An inlet system according to claim 1 , wherein one of the fluid guiding elements is a crankcase ventilation conduit ( 501 ) for ventilating a crankcase of the engine.

21. An inlet system according to claim 1 , wherein one of the fluid sources is an oil separator adapted to clean crankcase gas of the engine.

22. An inlet system according to claim 1 , wherein one of the fluid sources is a condensation water trap which may trap condensation water in an exhaust gas recirculation conduit for the engine.

23. An inlet system according to claim 1 , wherein one of the fluid guiding elements forms a part of an exhaust gas recirculation conduit for the engine.

24. An inlet system according to claim 23 , wherein the fluid source, from which the one of the fluid guiding elements is arranged to guide a fluid, is an exhaust gas cooler arranged to cool exhaust gases in the exhaust gas recirculation conduit.

25. An inlet system according to claim 23 , wherein the inlet system comprises in addition to the one of the fluid guiding elements an exhaust gas recirculation bypass conduit arranged to guide exhaust gases from the exhaust gas recirculation conduit to the air guide while bypassing a part of the one of the fluid guiding elements and terminating at the air guide.

26. An inlet system according to claim 25 , wherein the exhaust gas recirculation bypass conduit is less restrictive than the bypassed part of the one of the fluid guiding elements.

27. An inlet system according to claim 25 , wherein the inlet system comprises a valve for controlling the flow through the exhaust gas recirculation bypass conduit.

28. An internal combustion engine system comprising an inlet system according to claim 1 .

29. A vehicle comprising an internal combustion engine system according to claim 28 .

Assignees

• Volvo Truck Corp

Inventors

• Yudanov Sergi

Classifications

• F02M25/06

  adding lubricant vapours · CPC title

• F02B37/00 Primary

  Engines characterised by provision of pumps driven at least for part of the time by exhaust · CPC title

• F02M25/035

  into the charge intakes · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F02M26/09

  Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine · CPC title