This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses cam operated specially designed bilaterally operated double action scotch-yoke mechanism which facilitates two phase suction and compression of fuel and facilitates separation of fuel valve from ignition chamber. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.

Methods and systems are provided for an injector. In one example, the injector comprises at least two passages, wherein outlets of each of the passages are differently shaped than corresponding inlets of the passages. Further, in one or more examples, each of the outlets may be shaped and sized differently with respect to each other.

Methods and systems are provided for an injector. In one example, the injector comprises at least two passages, wherein outlets of each of the passages are differently shaped than corresponding inlets of the passages.

The method for injecting an oxidiser-fuel gaseous fuel mixture (1) of a pilot charge (39) into an ignition prechamber (2) is to measure the angular position of a crankshaft (7) then, using a filling electrical current profile (22) which imposes a filling lift law (23) on a gaseous fuel mixture injector (9) which opens into said prechamber (2), using a recovery variable (25) which sets the offset between the ignition (41) of the pilot charge (39) in the ignition prechamber (2) and the end of the injection of said charge (39), using a triggering variable of the the filling electrical current profile (26), using a richness variable (27), in order to generate, for each operating point of an internal combustion engine (4), an injection data set (28), then to execute said set (28).