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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

Inactive Publication Date: 2019-11-19
象限空间(天津)科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] An internal combustion engine is a kind of power machinery. It is a heat engine that directly converts the heat energy released into power by burning fuel inside the machine. In a broad sense, an internal combustion engine includes not only reciprocating piston internal combustion engines, rotary piston engines and free pistons. Type engines, including jet engines with rotary impellers, but internal combustion engines generally refer to piston engines. The ignition timing control system of piston engines uses camshaft position sensors, crankshaft position sensors and signal plates on the engine flywheel. Judging the cylinder and judging the top dead center, if the sensor signal is lost during the generation and transmission process, the control system will not work normally, which will lead to abnormal ignition timing and affect the engine work

Method used

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  • Dual-redundancy rotation speed acquisition ignition timing control system and method for aviation piston engine
  • Dual-redundancy rotation speed acquisition ignition timing control system and method for aviation piston engine
  • Dual-redundancy rotation speed acquisition ignition timing control system and method for aviation piston engine

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Embodiment

[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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PUM

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Abstract

The invention provides a dual-redundancy rotation speed acquisition ignition timing control system and method for an aviation piston engine. The system comprise a shaft head, a flange, a rotation speed sensor, an S-pole magnet, an N-pole magnet, a rotation speed sensor mounting seat, an engine controller, an ignition coil, a high-voltage lead, a high-voltage cap, a spark plug, a cylinder head anda piston. According to the system and the method, the problems that a control system cannot work normally, the ignition timing is abnormal, and the engine fails to work due to the loss of sensor signals in the processes of occurrence and transmission are effectively solved; and the dual-redundancy rotation speed acquisition ignition timing control system and method are low in cost, high in controlaccuracy and fast in responding speed.

Description

technical field [0001] The invention belongs to the field of non-compression ignition control of internal combustion engines, and in particular relates to an ignition timing control system and method for dual-redundant rotational speed acquisition of aviation piston engines. Background technique [0002] An internal combustion engine is a kind of power machinery. It is a heat engine that directly converts the heat energy released into power by burning fuel inside the machine. In a broad sense, an internal combustion engine includes not only reciprocating piston internal combustion engines, rotary piston engines and free pistons. Type engines, including jet engines with rotary impellers, but internal combustion engines generally refer to piston engines. The ignition timing control system of piston engines uses camshaft position sensors, crankshaft position sensors and signal plates on the engine flywheel. Judging the cylinder and judging the top dead center, if the sensor sig...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02P5/15
CPCF02P5/15Y02T10/40
Inventor 宋天一
Owner 象限空间(天津)科技有限公司
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