Engine operating method and engine system for improved load step acceptance

Patent metadata

Field	Value
Publication number	US-11280260-B2
Application number	US-202016912285-A
Country	US
Kind code	B2
Filing date	Jun 25, 2020
Priority date	Jun 25, 2020
Publication date	Mar 22, 2022
Grant date	Mar 22, 2022

Abstract

Operating an engine system includes feeding a flow of exhaust to a turbine in a turbocharger, receiving a load step request, and increasing a speed of rotation of the turbocharger based on an increase in a fueling rate initiated in response to the load step request. Operating the engine system further includes limiting dissipation of heat energy of the flow of exhaust to the turbine to hasten an increase in the speed of rotation of the turbocharger, and increasing dissipation of heat energy from the flow of exhaust after satisfaction of the load step request. Varying of the dissipation of heat energy can be achieved by displacing an insulating fluid in the exhaust manifold with a heat exchange fluid such as water and/or engine coolant.

First claim

What is claimed is:

1. A method of operating an engine system comprising:
feeding a flow of exhaust from combustion cylinders in an engine to a turbine coupled to a compressor in a turbocharger;
increasing a fueling rate of the engine based on a load step request;
increasing a speed of rotation of the turbocharger based on the increasing of the fueling rate;
limiting dissipation of heat energy from the flow of exhaust to the turbine to hasten the increase in the speed of rotation of the turbocharger; and
increasing dissipation of heat energy from the flow of exhaust to the turbine after satisfaction of the load step request.

2. The method of claim 1 wherein the limiting of dissipation of heat energy includes insulating an exhaust conduit feeding the flow of exhaust to the turbine.

3. The method of claim 2 wherein the increasing of the dissipation of heat energy includes displacing an insulating material from heat transference contact with the exhaust conduit.

4. The method of claim 3 wherein the displacing of the insulating material includes displacing an insulating fluid from a heat exchange cavity formed in an exhaust manifold of the engine.

5. The method of claim 4 wherein the displacing of the insulating material includes displacing air from the heat exchange cavity with a heat exchange fluid including water and/or engine coolant.

6. The method of claim 1 wherein the feeding of exhaust includes feeding a flow of exhaust produced by combustion of a mixture containing a gaseous fuel and air.

7. The method of claim 6 further comprising supplying gaseous fuel from a first delivery location to the combustion cylinders prior to the receipt of the load step request, and supplying gaseous fuel from a second delivery location to the combustion cylinders after the receipt of the load step request.

8. The method of claim 7 wherein the supplying of gaseous fuel from a first delivery location includes fumigating gaseous fuel into an intake conduit for the engine at a location that is upstream of a compressor in the turbocharger, and the supplying of gaseous fuel from a second delivery location includes port injecting gaseous fuel at locations upstream of the combustion cylinders and downstream of the compressor.

9. The method of claim 6 wherein the feeding of exhaust gases further includes feeding exhaust gases produced by combustion of a gaseous fuel that is delivered by port injection during starting the engine.

10. An engine system comprising:
an engine having a plurality of combustion cylinders formed therein;
a turbocharger including a turbine and a compressor;
an intake system including an intake conduit extending between an air inlet and the compressor, and between the compressor and the plurality of combustion cylinders;
an exhaust system having an exhaust conduit extending between the plurality of combustion cylinders and the turbine;
a fuel system having a first fuel admission valve coupled with the intake conduit at an upstream delivery location, and a second fuel admission valve coupled with the intake conduit at a downstream delivery location;
an insulator forming a heat exchange cavity in heat transference contact with the exhaust conduit between the plurality of combustion cylinders and the turbine; and
a pump structured to feed a heat exchange fluid into the heat exchange cavity to displace an insulating fluid, for varying heat dissipation of a flow of exhaust from the engine to the turbine.

11. The engine system of claim 10 wherein the exhaust system includes an exhaust manifold and the insulator is resident in the exhaust manifold.

12. The engine system of claim 10 wherein the first delivery location is upstream of the compressor.

13. The engine system of claim 12 wherein the fuel system includes a plurality of fuel injectors coupled with the second fuel admission valve and positioned to inject a fuel into a plurality of intake ports in the engine.

14. The engine system of claim 13 wherein the fuel system includes a gaseous fuel system having a low pressure fuel supply fluidly connected to the first fuel admission valve, a compressed fuel storage tank fluidly connected to the second fuel admission valve, and a fuel compressor connected between the low pressure fuel supply and the compressed fuel storage tank.

15. The engine system of claim 14 further comprising a power take-off connection between a crankshaft of the engine and the fuel compressor.

16. A method of accepting a load step in an engine comprising:
receiving a load step request;
increasing a fueling rate of the engine based on the load step request;
boosting a pressure of intake air supplied to the engine with a compressor in a turbocharger based on the increasing of the fueling rate;
operating the engine in a load step acceptance mode at least in part by limiting dissipation of heat energy of a flow of exhaust to a turbine of the turbocharger during the boosting of the pressure of intake air; and
transitioning the engine to a steady state mode after satisfaction of the load step request at least in part by increasing dissipation of heat energy from the flow of exhaust to prevent overheating of the turbine.

17. The method of claim 16 wherein the increasing of the fueling rate of the engine includes initiating port injection of a gaseous fuel to combustion cylinders in the engine.

18. The method of claim 17 wherein the limiting of the dissipation of heat energy from the flow of exhaust to the turbine further includes insulating the flow of exhaust with an insulating fluid.

19. The method of claim 18 wherein:
the insulating of the flow of exhaust with an insulating fluid includes insulating the flow of exhaust with an insulating fluid in a heat exchange cavity in an exhaust manifold of the engine; and
the increasing of the dissipation of heat energy further includes displacing the insulating fluid with a heat exchange fluid.

20. The method of claim 17 further comprising charging a compressed fuel storage tank during the operating of the engine in the steady state mode.

Assignees

• Caterpillar Inc

Inventors

• Wang Paul Sai Keat
• Singh Jaswinder
• Ginter David

Classifications

• Y02T10/30

  Use of alternative fuels, e.g. biofuels · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02D41/0027

  the fuel being gaseous (non-electrical control F02D19/02) · CPC title

• F01P2060/16

  Outlet manifold · CPC title

• F01P3/02

  Arrangements for cooling cylinders or cylinder heads · CPC title