Marine engines, cylinder liners for marine engines, and methods and assemblies for forming marine engines

Patent metadata

Field	Value
Publication number	US-11499499-B1
Application number	US-202117494269-A
Country	US
Kind code	B1
Filing date	Oct 5, 2021
Priority date	Oct 5, 2021
Publication date	Nov 15, 2022
Grant date	Nov 15, 2022

Abstract

A marine engine has a cylinder block defining at least one cylinder bore and a cylinder liner providing a running surface for a piston in the cylinder bore. The cylinder liner is non-axisymmetric relative to a center axis of the cylinder liner. The cylinder block defines a pocket that retains the cylinder liner and prevents the cylinder liner from rotating about the center axis. Novel cylinder liners, assemblies and methods are provided for forming a marine engine having the cylinder block with the cylinder liner formed therein.

First claim

What is claimed is:

1. A cylinder liner configured to provide a running surface for a piston in a cylinder bore of a marine engine, the cylinder liner comprising: a liner body configured to fit in the cylinder bore, the liner body having a first end and a second end which is opposite the first end; at least one cylinder liner tab that axially extends from the second end of the liner body; and a radial step that radially extends from the cylinder liner tab and is configured to engage with a corresponding radial shoulder on a mandrel as the first end of the liner body is slid onto the mandrel, wherein engagement between the radial step and the radial shoulder automatically clocks the cylinder liner into a predetermined orientation in the marine engine during formation thereof.

2. The cylinder liner according to claim 1 , wherein the cylinder liner tab is a first cylinder liner tab and further comprising a second cylinder liner tab that axially extends from the second end of the liner body and is diametrically opposite the first cylinder liner tab, wherein the radial step is a first radial step and wherein the radial shoulder is a first radial shoulder, and further comprising a second radial step that radially extends from the second cylinder liner tab and is configured to engage with a corresponding second radial shoulder on the mandrel during forming of the marine engine, wherein said engagement between the second radial step and the second radial shoulder further automatically clocks the cylinder liner into the predetermined orientation in the marine engine during formation thereof.

3. The cylinder liner according to claim 2 , wherein the first radial step extends from an inner diameter of the first cylinder liner tab and wherein the second radial step extends from an inner diameter of the second cylinder liner tab.

4. The cylinder liner according to claim 3 , wherein each of the first and second cylinder liner tabs comprises an axial end surface and a pair of opposing side surfaces that curve away from the axial end surface to the second end of the liner body.

5. The cylinder liner according to claim 4 , wherein the first radial step extends to and between the pair of opposing side surfaces on the first cylinder liner tab and wherein the second radial step extends to and between the pair of opposing side surfaces on the second cylinder liner tab.

6. The cylinder liner according to claim 4 , wherein the first radial step is spaced from and located centrally between the pair of opposing side surfaces on the first cylinder liner tab and wherein the second radial step is spaced from and located centrally between the pair of opposing side surfaces on the second cylinder liner tab.

7. An assembly for forming a marine engine, the assembly comprising: a mold for forming a cylinder block of the marine engine; a mandrel configured for insertion into the mold prior to formation of the cylinder block so as to form a cylinder bore in the cylinder block; and a cylinder liner configured to provide a running surface for a piston in the cylinder bore, the cylinder liner being elongated relative to an axis and being disposed on the mandrel during formation of the cylinder block in the mold, wherein the cylinder liner and the mandrel are configured to engage with each other when the cylinder liner is axially slid onto the mandrel so as to automatically clock the cylinder liner relative to the axis into a predetermined orientation for formation of the cylinder block.

8. An assembly for forming a marine engine, the assembly comprising: a mold for forming a cylinder block of the marine engine; a mandrel configured for insertion into the mold prior to formation of the cylinder block so as to form a cylinder bore in the cylinder block; and a cylinder liner configured to provide a running surface for a piston in the cylinder bore, the cylinder liner being disposed on the mandrel during formation of the cylinder block in the mold, wherein the cylinder liner and the mandrel engage with each other when the cylinder liner is slid onto the mandrel so as to automatically clock the cylinder liner into a predetermined orientation in the cylinder block during formation thereof, wherein the cylinder liner comprises a radial step that radially inwardly extends from the cylinder liner and is configured to engage with a corresponding radial shoulder on the mandrel during forming of the marine engine, wherein engagement between the radial step and the radial shoulder when the cylinder liner is slid onto the mandrel automatically clocks the cylinder liner into the predetermined orientation.

9. An assembly for forming a marine engine, the assembly comprising: a mold for forming a cylinder block of the marine engine; a mandrel configured for insertion into the mold prior to formation of the cylinder block so as to form a cylinder bore in the cylinder block; and a cylinder liner configured to provide a running surface for a piston in the cylinder bore, the cylinder liner being disposed on the mandrel during formation of the cylinder block in the mold, wherein the cylinder liner and the mandrel engage with each other when the cylinder liner is slid onto the mandrel so as to automatically clock the cylinder liner into a predetermined orientation in the cylinder block during formation thereof, wherein the cylinder liner comprises a liner body configured to fit in the cylinder bore, diametrically opposing first and second cylinder liner tabs that axially extend from an end the liner body, and a radial step that radially inwardly extends from the first cylinder liner tab and is configured to engage with a corresponding radial shoulder on a mandrel during forming of the marine engine, wherein engagement between the radial step and the radial shoulder when the cylinder liner is slid onto the mandrel automatically clocks the cylinder liner into the predetermined orientation.

10. The assembly according to claim 9 , wherein the radial step is a first radial step and wherein the radial shoulder is a first radial shoulder, and further comprising a second radial step that radially inwardly extends from the second cylinder liner tab and is configured to engage with a corresponding second radial shoulder on the mandrel during forming of the marine engine, wherein said engagement between the second radial step and the second radial shoulder further automatically clocks the cylinder liner into the predetermined orientation.

11. The assembly according to claim 10 , wherein the first radial step extends along an inner diameter of the first cylinder liner tab, wherein the second radial step extends along an inner diameter of the second cylinder liner tab, and wherein each of the first and second cylinder liner tabs comprises an end surface and a pair of opposing side surfaces that curve away from the end surface to the second end of the liner body.

12. The assembly according to claim 11 , wherein the first radial step extends to and between the pair of opposing side surfaces on the first cylinder liner tab and wherein the second radial step extends to and between the pair of opposing side surfaces of the second cylinder liner tab.

13. The assembly according to claim 11 , wherein the first radial step is spaced from and located centrally between the pair of opposing side surfaces on the first cylinder liner tab and wherein the second radial step extends centrally between the pair of opposing side surfaces of the second cylinder liner tab.

14. The assembly according to claim 8 , wherein the radial shoulder funnels the radial step into a seated position as the cylinder liner is axially slid onto the mandrel.

15.

Assignees

• Brunswick Corp

Inventors

• Hoffman Daniel P
• Monroe Alexander K
• Rasmussen Clayton T
• Roberts Gregory
• Stephany Dennis J

Classifications

• F02F1/10

  for liquid cooling · CPC title

• F02F1/004 Primary

  Cylinder liners (F02F1/08, F02F1/16 take precedence) · CPC title

• B22D19/0009 Primary

  Cylinders, pistons · CPC title

• F02B61/04

  for driving propellers · CPC title