Precombustion chamber gas engine

Patent metadata

Field	Value
Publication number	US-11143092-B2
Application number	US-201716466553-A
Country	US
Kind code	B2
Filing date	Nov 30, 2017
Priority date	Dec 8, 2016
Publication date	Oct 12, 2021
Grant date	Oct 12, 2021

Abstract

A precombustion chamber gas engine includes a main-chamber forming portion forming a main combustion chamber, a precombustion-chamber forming portion forming a precombustion chamber communicating with the main combustion chamber via a plurality of nozzle holes, and an ignition device disposed in the precombustion chamber and having an ignition portion spaced from a main chamber central axis of the main combustion chamber at a predetermined distance. In a plan view, the precombustion chamber has a near-ignition region including the ignition portion and a far-ignition region opposite to the near-ignition region separated by a borderline passing through a precombustion chamber central axis of the precombustion chamber and perpendicular to a straight line passing through the precombustion chamber central axis and the ignition portion. The distance between the precombustion chamber central axis and a precombustion-chamber-side opening end, connected to the precombustion chamber, of a specific far nozzle hole which is at least one nozzle hole in the far-ignition region is shorter or longer than the distance between the precombustion chamber central axis and a precombustion-chamber-side opening end of a specific near nozzle hole which is at least one nozzle hole in the near-ignition region.

First claim

The invention claimed is:

1. A precombustion chamber gas engine comprising:
a main-chamber forming portion forming a main combustion chamber;
a precombustion-chamber forming portion forming a precombustion chamber communicating with the main combustion chamber via a plurality of nozzle holes; and
an ignition device disposed at an upper portion of an interior of the precombustion chamber and having an ignition portion spaced from a main chamber central axis of the main combustion chamber at a predetermined distance,
wherein, in a plan view, the precombustion chamber has a near-ignition region in which the ignition portion is disposed and a far-ignition region opposite to the near-ignition region, the near-ignition region and the far-ignition region being separated by a borderline passing through a precombustion chamber central axis of the precombustion chamber and perpendicular to a straight line passing through the precombustion chamber central axis and the ignition portion, and
wherein
the plurality of nozzle holes includes a specific far nozzle hole which is at least one nozzle hole in the far-ignition region and a specific near nozzle hole which is at least one nozzle hole in the near-ignition region, and a distance between the precombustion chamber central axis and a precombustion-chamber-side opening end of the specific far nozzle hole connected to the precombustion chamber is shorter than a distance between the precombustion chamber central axis and a precombustion-chamber-side opening end of the specific near nozzle hole; or
the plurality of nozzle holes includes a specific near nozzle hole which is at least one nozzle hole in the near-ignition region and a specific far nozzle hole which is at least one nozzle hole in the far-ignition region, and a distance between the precombustion chamber central axis and a precombustion-chamber-side opening end of the specific near nozzle hole connected to the precombustion chamber is shorter than a distance between the precombustion chamber central axis and a precombustion-chamber-side opening end of the specific far nozzle hole.

2. The precombustion chamber gas engine according to claim 1 ,
wherein the specific near nozzle hole is a nearest nozzle hole having a main-chamber-side opening end connected to the main combustion chamber and closest to the ignition portion among the plurality of nozzle holes in the near-ignition region in a plan view, and
wherein the specific far nozzle hole is a farthest nozzle hole having a main-chamber-side opening end farthest from the ignition portion among the plurality of nozzle holes in the far-ignition region in a plan view.

3. The precombustion chamber gas engine according to claim 1 ,
wherein the distance between the precombustion chamber central axis and the precombustion-chamber-side opening end of the specific far nozzle hole is shorter than an average of distances between the precombustion chamber central axis and respective precombustion-chamber-side opening ends of the plurality of nozzle holes.

4. The precombustion chamber gas engine according to claim 1 ,
wherein the distance between the precombustion chamber central axis and the precombustion-chamber-side opening end of the specific near nozzle hole is shorter than an average of distances between the precombustion chamber central axis Cs and respective precombustion-chamber-side opening ends of the plurality of nozzle holes.

5. The precombustion chamber gas engine according to claim 1 ,
wherein an angle of depression of the specific far nozzle hole is equal to an angle of depression of the specific near nozzle hole.

6. The precombustion chamber gas engine according to claim 1 ,
wherein the main chamber central axis coincides with the precombustion chamber central axis.

7. The precombustion chamber gas engine according to claim 6 ,
wherein the precombustion chamber includes:
a small-diameter-cylinder forming portion forming a small-diameter cylinder chamber having a predetermined inner diameter and connected to the plurality of nozzle holes; and
a large-diameter-cylinder forming portion forming a large-diameter cylinder chamber which has an inner diameter larger than that of the small-diameter cylinder chamber and in which the ignition portion of the ignition device is disposed, and

wherein the main chamber central axis coincides with a precombustion chamber central axis of the small-diameter cylinder chamber.

8. The precombustion chamber gas engine according to claim 7 ,
wherein the large-diameter-cylinder forming portion includes:
a cylindrical enlarged diameter cylinder portion connected to the small-diameter cylinder chamber and having an inner diameter increasing with a distance from the small-diameter cylinder chamber; and
a cylindrical constant diameter cylinder portion connected to the enlarged diameter cylinder portion and having an inner diameter equal to a maximum diameter of the enlarged diameter cylinder portion.

9. The precombustion chamber gas engine according to claim 7 ,
wherein the precombustion chamber central axis is a central axis of the small-diameter cylinder chamber.

10. The precombustion chamber gas engine according to claim 1 ,
wherein the predetermined distance is larger than 10% of a maximum value of an inner diameter of the precombustion chamber.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Nomura Kazutoshi
• Takemoto Daisuke
• Yamada Satoshi
• Yuuki Akihiro
• Sasaki Shunya

Classifications

• F02B19/10 Primary

  with fuel introduced partly into pre-combustion chamber, and partly into cylinder · CPC title

• F02M21/02

  for gaseous fuels · CPC title

• F02M21/0281

  Adapters, sockets or the like to mount injection valves onto engines; Fuel guiding passages between injectors and the air intake system or the combustion chamber · CPC title

• Y02T10/30

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

• F02M21/0218

  Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers · CPC title