Ignition system employing plasma spray

An ignition system for a stratified charge internal combustion engine, said engine having at least one combustion chamber subject to high airflow transfer motion of an inducted air supply during the compression cycle, the system comprising:

• (a) walls defining a plasma ionizing chamber having an outlet orifice;
• (b) electrical discharge means effective to apply a high energy electrical discharge of at least 200 millijoules for at least two seconds across the plasma ionizing chamber causing the contents thereof to be shock heated to an ionized condition and sonically released through said outlet orifice as a jet;
• (c) walls defining a shock wave chamber to receive said sonically released jet, said shock wave chamber extending into said one combustion chamber and having openings aligned with said airflow transfer motion;
• (d) fuel injection means effective to inject a conical pattern of comminuted fuel into said shock wave chamber;
• and
• (e) means interrupting said outlet orifice in a manner to form the release of said plasma jet into a hollow cone intersecting with the injected pattern of said fuel.

A method of carrying out combustion in a stratified charge internal combustion engine, said engine having a piston and cylinder effective to define a main combustion chamber into which an air supply is inducted and at least one sonic plasma spark plug effective to selectively provide a high energy electrical discharge across a gap between electrodes to induce a plasma discharge, one of the electrodes being annular and ringing the other electrode, said engine also having a fuel injector effective to spray a pattern of comminuted fuel into a zone to be occupied by a plasma discharge, the improvement comprising:

• (a) axially separating the electrodes of said plug a predetermined distance;
• (b) interposing an inert guide between said electrodes and within said annular electrode to form a hollow, conically shaped plasma discharge;
• (c) sending said electrical discharge across said gap to produce said conically shaped plasma discharge;
• (d) controlling the fuel spray pattern to have a conical pattern complimentary to the conical shape of said plasma discharge;
• and
• (e) directing said plasma discharge to intersect and envelope the fuel spray pattern for ignition.

A method of carrying out combustion in an internal combustion engine, said engine having a piston and cylinder effective to define a variable volume space and a main combustion chamber residing as a cavity in the top face of the piston in communication with the variable volume space, said engine having walls to define an intermediate chamber and to segregate a portion of the variable volume space, said intermediate chamber projecting into said main combustion chamber when the piston is substanally at top dead center, said intermediate chamber having an entrance and an exit aligned with the predetermined circulatory path of gases in said space, the steps comprising:

• (a) inducting air into said variable volume space with a swirling motion about the axis of said cylinder;
• (b) compressing the air within said variable volume space and imparting a high radially inwardly squish motion to the air therein as said piston progressively approaches top dead center, said swirling motion and squish motion combining to define a circulatory path having a transfer motion from said variable volume space into said main combustion chamber defining a central air column which exits from said main combustion chamber along the sides thereof;
• (c) generating a sonic plasma jet having an energy level of at least 200 millijoules and directing said jet through said intermediate chamber so as to penetrate the exit thereof and extend into said main combustion chamber, said plasma jet having a conical pattern formed by interposing an inert guide within the release orifice;
• and
• (d) injecting a conical fuel spray pattern into said intermediate chamber while said plasma jet is resident therein, the axes of said conical spray pattern and conical plasma jet intersecting with a included angle of about 15.degree.-40.degree..