Is StarRotor's Novel Engine Design the Future of Efficient Energy?

AI Thread Summary
StarRotor's Brayton Cycle engine design aims to offer a simpler and potentially more efficient alternative to traditional engines, with claims of improved efficiency. However, concerns arise regarding its low 6:1 compression ratio, which may result in lower efficiency compared to conventional Otto cycle engines. The discussion highlights challenges such as the corrosive nature of hot gases and issues related to thermal expansion and leakage. While some participants express optimism about the feasibility of the design, skepticism remains due to the absence of a working prototype and the inherent difficulties in engine development. Overall, the potential for the Brayton Cycle engine to revolutionize energy efficiency in vehicles is acknowledged, but significant hurdles must be overcome.
Kenneth Mann
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I decided to try my hand at initiating a discussion. In particular, I'm interested in what others think about the rather novel (Brayton Cycle) engine design at (www.starrotor.com) and its claims? It's, in principle, the same type of continuous burn engine as in jet aircraft, but with somewhat simpler design and less requirement for exotic materials. Note in particular, their efficiency claims. If it works as planned, it might be interesting.

KM
 
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The link works just fine!

KM
 
Maybe its just for the prototype, but a 6:1 compression ratio means pretty low efficiency - worse than a regular car (otto cycle) engine. Regardless, they are still pretty early in the development. We'll need to wait and see. I'm definitely in favor of brayton cycle engines in cars if its feasible though.
 
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Actually I think that you're applying the limitations of an Otto cycle to the Brayton cycle. Gas turbines and jet engines have low compression ratios but high volume flows.

KM
 
A higher compression ratio is still better.

KM
 
Interesting concept. I think it seems like it will eventually be quite feasible, if not soon. It would be cool to see this go into production. :cool:
 
It looks pretty good. But hot gas is corosive. Also heat make things expand, which would spoil close fit. Lots of leakage! They don't have a prototype running, which tells you how hard it is. Pistons with piston rings is hard to beat! Wes Hughes
 
Lets not forget the original rotor engine. Those are harder to beat, fewer moving parts = longer life. Plus better efficiency. Rotor engines have been in use for decades, the starrotor just looks like an American redesign. About time, too, sometimes we're pretty slow on the uptake.
 
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Deleted previous message: As I'm talking rubbish and thinking of something else altogeher.

Interesting idea, the efficiency claims aren't outside the realm of possibility either.
 
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Wesley Hughes said:
But hot gas is corosive. Also heat make things expand, which would spoil close fit. Lots of leakage!
Isn't a Brayton cycle isobaric?
The combustion chamber is open to the output turbine - there isn't anything to seal.
 
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FYI...this thread is like 5 years old...LOL!

CS
 
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Balls! Can't believe I didnt notice that.
 
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Wow! Has it been that long. I feel old.

KM
 
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