IP Library Granted Patent US 10,400,696
Granted Patent B2
US 10,400,696 · App. 15/437,950 · Granted Sep 3, 2019

Method for starting an internal combustion engine

Inventors: Hugh Blaxill (Novi, MI); Michael Bunce (Plymouth, MI)
Assignee: MAHLE POWERTRAIN, LLC
F02D41/062F02B19/1085F02B19/12F02D37/02F02D41/064F02D41/1454F02D41/3094F02D41/402F02M57/06F02N19/00F02N19/06F02P5/045F02P5/1506F02P13/00F02B19/1009F02N19/08F02N2019/002Y02T10/125Y02T10/44Y02T10/46
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Quick Facts
Patent No.
US 10,400,696
App. No.
15/437,950
Granted
Sep 3, 2019
Kind
B2
Abstract

A method for starting an internal combustion engine comprises the steps of: providing an internal combustion engine having at least one cylinder and a piston supported at a crankshaft for repeated reciprocal movement in the cylinder so as to define a main combustion chamber, the internal combustion engine further having an ignition device arranged in said cylinder with an igniter portion and a fuel injector which are both arranged at a pre-chamber, wherein the pre-chamber has a plurality of orifices for providing fluid communication between said pre-chamber and the main combustion chamber, injecting fuel in the pre-chamber, and igniting the injected fuel in the pre-chamber for pre-heating of the pre-chamber prior to injecting fuel in the main combustion chamber for combusting the injected fuel in the main combustion chamber.

Claims (17)

1. A method for starting an internal combustion engine comprising the steps of:

providing an internal combustion engine having at least one cylinder and a piston supported at a crankshaft for repeated reciprocal movement in the cylinder so as to define a main combustion chamber, the internal combustion engine further having an ignition device arranged in said cylinder with an igniter portion and a fuel injector which are both arranged at a pre-chamber, wherein the pre-chamber has a plurality of orifices for providing fluid communication between said pre-chamber and the main combustion chamber;

injecting fuel in the pre-chamber at the start of an engine cycle so that the lambda value λ in the pre-chamber is less than 1;

subsequently igniting the injected fuel in the pre-chamber, thereby pre-heating the pre-chamber prior to a compression of the piston in the cylinder in said engine cycle, and causing combustion jets to exit the pre-chamber via the plurality of orifices and enter the main combustion chamber; and

subsequent to pre-heating of the pre-chamber, injecting fuel in the main combustion chamber in said engine cycle so that the lambda value λ in the main combustion chamber is less than 1.6, wherein the combustion jets cause combustion of the injected fuel in the main combustion chamber.

2. The method according to claim 1 , wherein the step of injecting fuel in the pre-chamber comprises injecting fuel in the pre-chamber only.

3. The method according to claim 2 , wherein the step of injecting fuel in the pre-chamber comprises multiple injections of fuel via fuel injector in the pre-chamber.

4. The method according to claim 3 , wherein the step of igniting the injected fuel in the pre-chamber is carried out in between subsequent multiple injections of fuel in the pre-chamber.

5. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber are carried out after a predetermined time duration T starting from the injection of fuel in the pre-chamber.

6. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber are carried out after a predetermined angular movement of rotating engine components.

7. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber are carried out prior to a first compression move of the piston in the cylinder.

8. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber are carried out at different individual angular positions of the rotating engine components for a predetermined time interval t.

9. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber is carried out at a continuous range of angular positions a of the crankshaft.

10. The method according to claim 1 , wherein the injection of fuel in the pre-chamber and the ignition of the injected fuel in the pre-chamber are carried out prior to a movement of the crankshaft.

11. The method according to claim 1 , wherein the amount of injected fuel in the pre-chamber is chosen so that the air/fuel ratio λ is less than 1.

12. The method according to claim 1 , further comprising the step of injecting fuel in the pre-chamber comprises the step of simultaneously injecting fuel in the main combustion chamber.

13. The method according to claim 12 , wherein the amount of injected fuel in the main combustion chamber is chosen so that the air/fuel ratio λ is less than 1 in the main combustion chamber.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 29, 2023
From: MAHLE POWERTRAIN, LLC
To: MAHLE INTERNATIONAL GMBH
Reel/Frame 065694/0362 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 30, 2017
From: BLAXILL, HUGH; BUNCE, MICHAEL
To: MAHLE POWERTRAIN, LLC
Reel/Frame 041790/0741 →
Priority Claims (1)
EP 16001518 · Jul 6, 2016 · regional
Continuity (1)
Related Publication 20180010536A1 · Jan 11, 2018
Cited By (1)
US 12,723,537