Internal combustion engine having a split crankcase

1. An internal combustion engine comprising:

a crankcase having a first crankcase portion fastened to a second crankcase portion, the first crankcase portion being joined to the second crankcase portion along a first plane,

the first crankcase portion having a first wall defining a first crankshaft support aperture,

the second crankcase portion having a second wall defining a second crankshaft support aperture;

a crankshaft having a first end portion, a second end portion and a central portion, the crankshaft being rotatably supported inside the crankcase,

the crankshaft being rotatable about a crankshaft axis, the crankshaft axis being normal to the first plane,

the first end portion being received in the first crankshaft support aperture, the second end portion being received in the second crankshaft support aperture;

a cylinder block fastened to the crankcase, the cylinder block defining two cylinders, each of the two cylinders having a cylinder axis;

two pistons operatively connected to the crankshaft, the two pistons being disposed in the two cylinders;

a cylinder head fastened to the cylinder block, the cylinder block being disposed between the cylinder head and the crankcase;

a crankshaft support defining a third crankshaft support aperture,

the third crankshaft support aperture being coaxial with the first crankshaft support aperture, the second crankshaft aperture and the crankshaft axis,

the central portion of the crankshaft being received in the third crankshaft support aperture; and

at least one fastener fastening the crankshaft support to the cylinder block, the at least one fastener being perpendicular to the crankshaft axis and being disposed in a second plane, the second plane being one of coplanar with and parallel to the first plane.

2. The engine of claim 1 , wherein the at least one fastener fastens the crankshaft support to the cylinder block and the cylinder head.

3. The engine of claim 1 , wherein the at least one fastener is parallel to a third plane, the third plane containing the cylinder axes and the crankshaft axis.

4. The engine of claim 1 , wherein the at least one fastener is two fasteners disposed on both sides of a third plane, the third plane containing the cylinder axes and the crankshaft axis.

5. The engine of claim 1 , wherein the first plane is disposed between the two cylinders.

6. The engine of claim 1 , wherein the second plane is disposed between the two cylinders.

7. The engine of claim 1 , wherein the second plane is coplanar with the first plane.

8. The engine of claim 1 , further comprising at least one lubrication passage defined in the crankshaft support.

9. The engine of claim 8 , wherein the crankshaft support defines at least one spray aperture fluidly communicating with the at least one lubrication passage, the at least one spray aperture being adapted to spray lubricant on a least one of the two pistons.

10. The engine of claim 1 , wherein the crankshaft support has a first part defining a portion of the third crankshaft support aperture and a second part defining another portion of the third crankshaft support aperture; and

wherein the first part is fastened to the second part.

11. The engine of claim 10 , wherein the at least one fastener is at least one first fastener; and

the engine further comprising at least one second fastener fastening the first part to the second part, the at least one second fastener being perpendicular to the crankshaft axis and being disposed in the second plane.

12. The engine of claim 11 , wherein the first part is disposed between the second part and the cylinder block; and

wherein the at least one second fastener is inserted through the second part and into the first part.

13. The engine of claim 12 , wherein the at least one first fastener is inserted into the first part and is not inserted into the second part.

14. The engine of claim 11 , wherein the at least one second fastener is parallel to a third plane, the third plane containing the cylinder axes and the crankshaft axis.

15. The engine of claim 14 , wherein the at least one first fastener is parallel to the third plane.

16. The engine of claim 15 , wherein the at least one first fastener is two first fasteners disposed on both sides of the third plane;

wherein the at least one second fastener is two second fasteners disposed on both sides of the third plane; and

wherein the two second fasteners are closer to the third plane than the two first fasteners.

17. The engine of claim 11 , wherein the at least one second fastener is two second fasteners disposed on both sides of the third crankshaft support aperture.

18. The engine of claim 1 , wherein:

the first crankcase portion defines a first counterbalance shaft support aperture in the first wall,

the second crankcase portion defines a second counterbalance shaft support aperture in the second wall,

the crankshaft support defines a third counterbalance shaft support aperture,

the engine further comprising:

a counterbalance shaft having a first end portion, a second end portion and a central portion, the counterbalance shaft being rotatably supported inside the crankcase,

the first end portion of the counterbalance shaft being received in the first counterbalance shaft support aperture, the second end portion of the counterbalance shaft being received in the second counterbalance shaft support aperture, and the central portion of the counterbalance shaft being received in the third counterbalance shaft support aperture.

19. The engine of claim 18 , wherein:

the counterbalance shaft is a first counterbalance shaft,

the first crankcase portion defines a fourth counterbalance shaft support aperture in the first wall,

the second crankcase portion defines a fifth counterbalance shaft support aperture in the second wall,

the crankshaft support defines a sixth counterbalance shaft support aperture,

the engine further comprising:

a second counterbalance shaft having a first end portion, a second end portion and a central portion, the second counterbalance shaft being rotatably supported inside the crankcase,

the first end portion of the second counterbalance shaft being received in the fourth counterbalance shaft support aperture, the second end portion of the second counterbalance shaft being received in the fifth counterbalance shaft support aperture, and the central portion of the second counterbalance shaft being received in the sixth counterbalance shaft support aperture.

20. The engine of claim 19 , wherein the first and second counterbalance shafts are disposed on opposite sides of the third plane.