Efficiency of a Jet-Powered Rotor Engine

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The discussion centers on the efficiency of a jet-powered rotor engine, comparing it to traditional gas turbines and aeolipiles. It is suggested that jet engines, while capable of impressive thrust, are inefficient due to high fuel consumption, particularly when scaled down. Experiments indicate that using a propeller with a jet engine significantly increases thrust while reducing fuel usage. Concerns about energy loss when converting jet thrust to rotational energy are also raised. Overall, the consensus leans towards the idea that a modern aeolipile may not outperform conventional gas turbines in efficiency or practicality.
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If we make an engine/rotating machine with the use of jets placed around the circumference of a wheel, then how to find its efficiency? This could be something like an Aeolipile (Refer Wikipedia for the same) but without steam.Instead we can use petrol for combustion.Would that make a good engine?
 
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How would your modern aeolipile improve on a conventional gas turbine, for instance? It seems like the G.T. would be a simpler machine to construct, and it could run at higher speed than the aeolipile.

As always, thermal efficiency = work output / heat input
 
Without any of the math, my guess is it would be very inefficient. Jets consume a lot of fuel. While their thrust can be impressive, when you scale them down to the size of a loaf of bread they become rather ineffective at producing thrust compared to a propeller.

Energy loss might also be an issue. Using the thrust from jets to spin a wheel in order to turn something might mean your output is significantly lower than your input, since the little jets are gas guzzlers.

As an example, I ran a small jet engine in a lab, about half the size of a football (American). We used kerosene as fuel, and it produced about 4 to 5 lbs as max thrust. When we took the same jet and slapped a propeller on the front of it, it produce about 20 lbs. It also went through a gallon of fuel (3.8L) in just over 20 minutes of run time (I'm sure however there are much better designs, by no means was it a state of the art engine).
 
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stinsonbr said:
Without any of the math, my guess is it would be very inefficient. Jets consume a lot of fuel. While their thrust can be impressive, when you scale them down to the size of a loaf of bread they become rather ineffective at producing thrust compared to a propeller.

Energy loss might also be an issue. Using the thrust from jets to spin a wheel in order to turn something might mean your output is significantly lower than your input, since the little jets are gas guzzlers.

As an example, I ran a small jet engine in a lab, about half the size of a football (American). We used kerosene as fuel, and it produced about 4 to 5 lbs as max thrust. When we took the same jet and slapped a propeller on the front of it, it produce about 20 lbs. It also went through a gallon of fuel (3.8L) in just over 20 minutes of run time (I'm sure however there are much better designs, by no means was it a state of the art engine).


Thank you! It's great that you experimented on the idea.So i am getting the feel that Aeolipile is just a toy after all. But still I would like to know the equation of efficiency for the same. I am an electrical Engineer so I am not able to derive the your thermodynamic equations & all.
 
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