Dual-redundancy rotation speed acquisition ignition timing control system and method for aviation piston engine
A piston engine, ignition timing technology, applied in the direction of internal combustion piston engine, automatic control, automatic control, etc., can solve the problems of the control system not working normally, affecting the engine work, abnormal ignition and other problems, achieving low cost, fast response speed, The effect of high control precision
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[0019] as attached figure 1 As shown, the ignition timing control system and method for double-redundant rotational speed acquisition of an aviation piston engine is characterized in that it includes a shaft head, a flange, a rotational speed sensor, an S pole magnet, an N pole magnet, a rotational speed sensor mounting seat, an engine controller, Ignition coil, high voltage wire, high voltage cap, spark plug, cylinder head, piston.
[0020] The application object of the ignition timing control system and method for dual-redundant speed acquisition and ignition timing control of aviation piston engines is a horizontally opposed 2-cylinder 2-stroke engine, with the attached figure 1 There are two sets of the same 8-13 composition, corresponding to 2 sets of cylinder structures.
[0021] When the aviation piston engine is working, the shaft head drives the flange to rotate. There are two magnets with opposite magnetic polarities on the flange. The angle between the two magnets ...
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