A four-stroke aircraft engine operates through four distinct strokes—intake (fuel-air mixture enters cylinder), compression (mixture is compressed), power (spark ignition forces piston down to produce mechanical power), and exhaust (burned gases exit)—converting fuel and air into rotational power to drive the propeller, with the Cessna 150's Continental O200A engine exemplifying this principle through its horizontally opposed four-cylinder design.
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Added:All right, today we're going to be talking about our Cessna 150. It uses a four-cylinder horizontal horizontally opposed Continental O200A. It's uh operation is based on the four-stroke combustion cycle. Uh this engine converts fuel and air into the mechanical power to turn the propeller.
It is a carbureted naturally aspirated engine, meaning it uses as atmospheric pressure to bring air into the cylinders. The engine is air cooled using air flow and cooling fins to remove. All right. This is a four- stroke cycle. Each cylinder completes four strokes. First stroke is an intake stroke. The intake valve opens, piston moves downward, fuel and air mixture enters the cylinder. Second stroke is compression. Both valve both valves close, piston moves upward, fuel and air mixture is compressed. The third stroke is power. Spark plug ignites and the compre the compressed mixture. Expanding gases forces the piston downward. This produces usable power to rotate the crankshaft and the propeller. And the fourth and final stroke is an exhaust stroke. Exhaust valves open, piston moves upward, burned gases exit the cylinder.
Today we're going to go over the power plant and the prop combination for the Cessna 150. Over here we have the Macau OCM 6984.
The 6984 is for the dimensions of the blade itself. So, it's going to be uh 69 in in length and 48 in in pitch. Right here, this is a fixed pitch propeller. So, no matter what speed, whether it be takeoff, landing, cruise, the pitch of the uh propeller does not change at all.
It'll only change in relations with the RPMs of the engine itself.
Speaking of that, the power plant system for this is going to be the Continental 0200A 200, meaning this is a 200 in U for the power plant of the Cessna 150 is going to be the Continental OAC 200 TAC A uh engine. O meaning horizontally opposed meaning all these pistons right here are moving in opposite directions horizontally from each other and 200 meaning that it is 200 in of displacement when operating on one full cycle.
For the induction system, the Continental O200 operates with a carburetor with a flow type system with a updraft, meaning air is pulled into the carburetor, mixes with a fuel, and flows upward into the cylinder. Once the air fuel mixture comes into the engine, right here to each of these cylinders is the beginning of the four stroke process. So the first stroke is going to be the induction stroke which is going to be pulling the air fuel mixture into the cylinder itself. So when it pulls it in comes from the carburetor up here into the cylinder. Next out on the four stroke process is going to be your compression uh stage. So what's that going to be doing is going to be compressing the air fuel mixture inside of each of these cylinders. And once it gets to the very top, we call that top dead center. It's going to ignite using the magnetos. And speaking to the magnetos, each cylinder has two spark plugs. One at the top, one at the bottom. Same for each cylinder on every side.
With this engine, it has a dual magneto system, meaning it is built for redundancy. As this engine operates, each magneto has one spark plug attached to it to each cylinder. And on each side, one magneto will control two of the spark plugs on the top side of the left side, and the other side will be controlled by the bottom by the same magneto. Therefore, if one of these magnetos goes out, you'll still have another spark plug to be able to operate this engine. And also that lets it work independently of the electrical system.
So as you can look here, there's no battery on it. If this engine were to fail through the electrical system, this engine will still be able to operate.
Last thing we're going to talk about is the last two strokes of the four- stroke system. And that's going to be your power stroke. So once after the compression stroke, that magneto sends a spark to the spark plugs to ignite the air fuel mixture. And after that, as it rotates, that's going to be your power shaft that actually drives power from the piston to the crankshaft to the propeller.
And once that's done, it'll move again for the exhaust stroke. What's going to happen is that after the power stroke, it's going to push the rest of the exhaust gas out of the system. So therefore, it could begin the cycle again. And each side is going to be two cylinders connected to one exhaust manifold. As you can see here and here.
Finally, this propeller and engine combo is based on this fixed pitch propeller design. Meaning that the only way this propeller will turn at a faster RPM is if the engine runs faster as well. So, as the engine runs at a higher RPM, the propeller will run at a higher RPM as well. They do not turn in pitch. It's not constant speed or anything like that. Now, the normal operating range is going to be at 100 horsepower, and that means the engine is going to be operating at RPM of 2,750 rotations per minute.
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