Opposed piston engine with pistons having conical recesses therein

Patent metadata

Field	Value
Publication number	US-9970350-B2
Application number	US-201415513046-A
Country	US
Kind code	B2
Filing date	Sep 29, 2014
Priority date	Sep 29, 2014
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

An opposed piston engine includes a cylinder having a cylinder wall, and a pair of opposed pistons, Each face of each piston of the pair of opposed pistons has a top plane and a recess formed therein, each recess comprising a first surface defining part of a cone, the cone defined by the first surface of at least one of the recesses having a longitudinal axis that defines an angle equal to at least one half of a cone angle of the cone with the top plane.

First claim

What is claimed is:

1. An opposed piston engine, comprising:
a cylinder having a cylinder wall; and
a pair of opposed pistons, each piston of the pair of opposed pistons having a face, the pair of pistons being disposed in the cylinder and movable between first positions in the cylinder in which faces of the opposed pistons and the cylinder wall define a maximum volume and second positions in the cylinder in which the faces of the opposed pistons and the cylinder wall define a minimum volume,
wherein each face of each piston of the pair of opposed pistons has a top plane and a recess formed therein, each recess comprising a first surface defining part of a cone, the cone defined by the first surface of at least one of the recesses having a longitudinal axis that defines an angle equal to at least one half of a cone angle of the cone with the top plane, wherein each recess comprises a U-shaped base surface at a widest end of the cone, and wherein the base surface has a concave, partially toroidal portion and includes a center protrusion at a center of a toroid defined by the toroidal portion.

2. The opposed piston engine as set forth in claim 1 , wherein the longitudinal axis of the cone of the first surface of the recess of a first piston of the pair of opposed pistons defines a non-zero angle with the longitudinal axis of the cone of the first surface of the recess of a second piston of the pair of opposed pistons when viewed along an axis of the cylinder.

3. The opposed piston engine as set forth in claim 1 , wherein the longitudinal axis of the cone of the first surface of the recess of a first piston of the pair of opposed pistons aligned with the longitudinal axis of the cone of the first surface of the recess of a second piston of the pair of opposed pistons when viewed along an axis of the cylinder.

4. The opposed piston engine as set forth in claim 3 , wherein the cone of the first surface of the recess of the first piston widens in an opposite direction from the cone of the first surface of the recess of the second piston.

5. The opposed piston engine as set forth in claim 3 , wherein the cone of the first surface of the recess of the first piston widens in a same direction as the cone of the first surface of the recess of the second piston.

6. The opposed piston engine as set forth in claim 1 , wherein the first surface defines half of the cone.

7. The opposed piston engine as set forth in claim 1 , wherein, for at least one piston of the pair of opposed pistons, the cone defined by the first surface is disposed below the top plane.

8. The opposed piston engine as set forth in claim 1 , wherein the cone defined by the first surface of the recess in a first piston of the pair of opposed pistons has a different shape than the cone defined by the first surface of the recess in a second piston of the pair of opposed pistons.

9. The opposed piston engine as set forth in claim 1 , wherein the cone defined by the first surface of the recess in a first piston of the pair of opposed pistons has a different cone angle than the cone angle of the cone defined by the first surface of the recess in a second piston of the pair of opposed pistons.

10. The opposed piston engine as set forth in claim 1 , wherein, for each piston of the pair of opposed pistons, the angle defined by the longitudinal axis of the cone defined by the first surface with the top plane is equal to at least one half of the cone angle of the cone.

11. The opposed piston engine as set forth in claim 1 , comprising a pair of fuel injectors in the cylinder wall, each fuel injector being configured to inject fuel into the cylinder in a shape of a fuel jet cone having a fuel jet cone angle substantially equal to the cone angle.

12. The opposed piston engine as set forth in claim 11 , wherein each fuel injector of the pair of fuel injectors is arranged to inject fuel in the shape of the fuel jet cone along the longitudinal axis of the cone of the first surface of the recess of a respective one of the pair of opposed pistons.

13. The opposed piston engine as set forth in claim 11 , wherein each fuel injector comprises a plurality of spray orifices adapted to produce multiple spray plumes to form the fuel jet cone as an envelope cone.

14. The opposed piston engine as set forth in claim 11 , wherein each fuel injector comprises a single spray orifice with a central pintle adapted to form the fuel jet cone as a hollow or solid cone.

15. The opposed piston engine as set forth in claim 11 , wherein the pair of fuel injectors are of different size.

16. The opposed piston engine as set forth in claim 11 , wherein the pair of fuel injectors are arranged to supply different amounts of fuel.

17. The opposed piston engine as set forth in claim 11 , wherein the pair of fuel injectors are arranged to supply fuel at different times.

18. An opposed piston engine, comprising:
a cylinder having a cylinder wall; and
a pair of opposed pistons, each piston of the pair of opposed pistons having a face, the pair of pistons being disposed in the cylinder and movable between first positions in the cylinder in which faces of the opposed pistons and the cylinder wall define a maximum volume and second positions in the cylinder in which the faces of the opposed pistons and the cylinder wall define a minimum volume,
wherein each face of each piston of the pair of opposed pistons has a lop plane and a recess formed therein, each recess comprising a first surface defining part of a cone, the cone defined by the first surface of at least one of the recesses having a longitudinal axis that defines an angle equal to at least one half of a cone angle of the cone with the top plane, wherein each recess comprises a U-Shaped base surface at a widest end of the cone, and wherein the longitudinal axis of the cone of the first surface of the recess of a first piston of the pair of opposed pistons defines a non-zero angle with the longitudinal axis of the cone of the first surface of the recess of a second piston of the pair of opposed pistons when viewed along an axis of the cylinder.

Assignees

• Volvo Truck Corp

Inventors

• Morton Richard Kellogg
• Li Jian
• Brandt Richard

Classifications

• F02B75/287

  with several pistons positioned in one cylinder one behind the other · CPC title

• F02B75/16

  Engines characterised by number of cylinders, e.g. single-cylinder engines (F02B75/26 takes precedence) · CPC title

• F02B23/066

  the injector being located substantially off-set from the cylinder centre axis · CPC title

• F02B75/28 Primary

  Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders (arranged oppositely relative to main shaft F02B75/24) · CPC title

• F02B75/26

  Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis · CPC title