{"id":1028,"date":"2022-02-20T19:29:21","date_gmt":"2022-02-20T19:29:21","guid":{"rendered":"http:\/\/localhost\/rv10ca\/?page_id=1028"},"modified":"2022-02-20T19:29:22","modified_gmt":"2022-02-20T19:29:22","slug":"engine-theory","status":"publish","type":"page","link":"http:\/\/localhost\/rv10ca\/engine-theory\/","title":{"rendered":"Engine Theory"},"content":{"rendered":"\n
There are a few basic concepts about engine operation you should know as it will make the process for setting up the SDSEFI system clearer. For most pilots, the engine “just works” much the same way as our car engine “just works”. With aircraft engines with electronic ignition, we can tweak the engine control unit (ECU) settings to get better performance over a range of different flight configurations.<\/p>\n\n\n\n
The basics<\/strong> – Cylinder Components<\/strong><\/p>\n\n\n\n Below is a cut away view of a single engine cylinder with key components identified.<\/p>\n\n\n\n Note that the connecting rod is connected to the crankshaft offset from the center of the crankshaft. This means that as the piston moves up or down, it will cause the crankshaft to rotate. This is how a piston moving up or down can rotate the crankshaft which in turn spins the propellor.<\/p>\n\n\n\n The OTTO Cycle<\/strong><\/p>\n\n\n\n Aircraft engines use a 4 stroke Otto cycle. That means the piston in a cylinder goes either up or down 4 times every time a spark plug fires and generates power. The crankshaft to which the piston is connected rotates 180 degrees every time the piston moves fully up or fully down (a stroke). The diagram below shows each of the 4 strokes associated with this movement.<\/p>\n\n\n\n <\/p>\n\n\n\n The 4 strokes are:<\/p>\n\n\n\n Piston \/ Crankshaft Terminology<\/strong><\/p>\n\n\n\n When discussing cylinder movements, we use the rotated position of the crankshaft to describe where the piston is in the cylinder (the crankshaft rotates 3600<\/sup>). For example, when piston is highest in the cylinder, the crankshaft is said to be a 3600<\/sup> (or 00<\/sup>) or TOP DEAD CENTER (TDC). When he piston is at its lowest point in the cylinder and the crankshaft is said to be at 1800<\/sup> or BOTTOM DEAD CENTER (BDC). We can thereby describe where the piston its movement up or down by reference to these two points. For example, a piston moving up where the crankshaft angle is 3360<\/sup> would be said to be 240<\/sup> BEFORE TOP DEAD CENTER (BTC).<\/p>\n\n\n\n It is important that you understand these concepts if you are to understand how the SDSEFI system works. <\/p>\n\n\n\n Referring to the diagrams above, you will notice that certain things happen depending on where the piston is in the cylinder. For example, the intake and exhaust valve opening and closing is controlled by the camshaft which is mechanically linked to the crankshaft. <\/p>\n\n\n\n Control of when the spark plug fires is extremely important. The SDS ECU fires each cylinder’s spark plugs in a specific sequence based on where each cylinder’s piston is in the OTTO cycle. (For clarity, each aircraft cylinder typically has two park plugs which are fired at the same time.)<\/p>\n\n\n\n<\/figure>\n\n\n\n
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