Structure of a main combustion chamber of a diesel engine of a direct injection type

Claim 2

A structure of a main combustion chamber of a diesel engine of a direct injection type in which a main combustion chamber having a peripheral wall and a bottom wall is formed by a hollow at a top of a piston, above peripheral wall includes a plurality of collision walls and guide walls which are disposed alternately to each other in a circumferential direction of the piston, a fuel injection nozzle having a plurality of nozzle holes is disposed in or at the rear of the combustion chamber, the injection nozzle is designed to radiately spray the fuel only against the collision walls, and the sprayed collided fuel is adapted to flow along the guide walls in one direction while forming a swirl; characterized in that; each guide wall includes an upstream portion and a downstream portion with a boundary therebetween with respect to the direction of the swirl, a radial distance from the center of the chamber to the boundary is shorter than a radial distance from the center of the chamber to other portions and each upstream portion has a longer radius of curvature and a circumferential length than each downstream portion so that the inner periphery of the chamber has a pin-wheel-like shape, the upstream portions forms smooth walls along which the fuel after collision flows while forming a film of the fuel, the downstream portions forms walls along which the fuel flows from the boundaries, and the circumferential angle of each collision wall is so determined that the fuel sprayed from the nozzle holes collides only with the collision walls; each said collision wall does not, in combination with the lower portion of a corresponding said guiding wall, constitute a radial pocket operative to retain a mass of fuel, but comprises a lower portion wall forming a support surface contributing to said swirl in fuel flow.

Claim 3

A structure of a main combustion chamber of claim 1 wherein the bottom wall of the chamber is provided with a pyramid like projection of which ridges extend toward the guide walls so that the sprayed fuel from the nozzle holes may not contact the bottom wall before colliding with the collision walls.

Claim 4

A structure of a main combustion chamber of claim 1 wherein a ledge projecting toward the center of the chamber is formed at the upper end of the collision wall.

Claim 5

A structure of a main combustion chamber of claim 1 wherein ledges projecting toward the center of the chamber are formed at the upper ends of the respective collision walls.

Claim 6

A structure of a main combustion chamber of claim 1 wherein the center of the main combustion chamber is shifted away from the center of the piston, the top surface of the piston has a portion which is radially narrower than other portions of the top surface, and a ledge projecting toward the center of the chamber is formed only at the upper end of the collision wall adjacent to the narrow portion of the top surface.

Claim 7

A structure of a main combustion chamber of claim 1 wherein the guide walls include inclined portions which extend to the top of the piston and are inclined at an angle in a range from 5 degree to 15 degree away from the center of the chamber.

Claim 8

A structure of a main combustion chamber of claim 1 wherein a glow lamp is arranged at the near of the upstream side of one of the collision walls in the main combustion chamber.

Claim 9

A structure of a main combustion chamber of a diesel engine of a direct injection type in which a main combustion chamber having a peripheral wall and a bottom wall is formed by a hollow at a top of a piston, above peripheral wall includes a plurality of collision walls and guide walls which are disposed alternately to each other in a circumferential direction of the piston, a fuel injection nozzle having a plurality of nozzle holes is disposed in or at the near of the combustion chamber, the injection nozzle is designed to radiately spray the fuel only against the collision walls, and the sprayed collided fuel is adapted to flow along the guide walls in one direction while forming a swirl; characterized in that; each guide wall includes an upstream portion and an downstream portion with a boundary therebetween with respect to the direction of the swirl, a radial distance from the center of the chamber to the coundary is shorter than a radial distance from the center of the chamber to other portions and each upstream portion has a longer radius of curvature and a circumferential length than each downstream portion so that the inner periphery of the chamber has a pin-wheel-like shape, the upstream portions forms smooth walls along which the fuel after collision flows while forming a film of the fuel, the downstream portions forms walls along which the fuel flows from the boundaries, and the circumferential angle of each collision wall is so determined that the fuel sprayed from the nozzle holes collides only with the collision walls whereby each said collision wall does not, in combination with the lower portion of a corresponding said guiding wall, constitute a radial pocket operative to retain a mass of fuel, and that the lower portion of each said guiding wall forming an active support surface contributing to said swirl in fuel flow; the center of the main combustion chamber is shifted away from the center of the piston, the top surface of the piston has a portion which is radially narrower than other portions of the top surface, and a ledge projecting toward the center of the chamber is formed only at the upper end of the collision wall adjacent to the narrow portion of the top surface.

Claim 10

A structure of a main combustion chamber of a diesel engine of a direct injection type in which a main combustion chamber having a peripheral wall and a bottom wall is formed by a hollow at a top of a piston, above peripheral wall includes a plurality of collision walls and guide walls which are disposed alternately to each other in a circumferential direction of the piston, a fuel injection nozzle having a plurality of nozzle holes is disposed in or at the near of the combustion chamber, the injection nozzle is designed to radiately spray the fuel only against the collision walls, and the sprayed collided fuel is adapted to flow along the guide walls in one direction while forming a swirl; characterized in that; each guide wall includes an upstream portion and an downstream portion with a boundary therebetween with respect to the direction of the swirl, a radial distance from the center of the chamber to the coundary is shorter than a radial distance from the center of the chamber to other portions and each upstream portion has a longer radius of curvature and a circumferential length than each downstream portion so that the inner periphery of the chamber has a pin-wheel-like shape, the upstream portions forms smooth walls along which the fuel after collision flows while forming a film of the fuel, the downstream portions forms walls along which the fuel flows from the boundaries, and the circumferential angle of each collision wall is so determined that the fuel sprayed from the nozzle holes collides only with the collision walls whereby each said collision wall does not, in combination with the lower portion of a corresponding said guiding wall, constitute a radial pocket operative to retain a mass of fuel, and that the lower portion of each said guiding wall forming an active support surface contributing to said swirl in fuel flow; the center of the main combustion chamber is shifted away from the center of the piston, the top surface of the piston has a portion which is radially narrower than other portions of the top surface, and a ledge projecting toward the center of the chamber is formed only at the upper end of the collision wall adjacent to the narrow portion of the top surface.