Hill Helicopters' GT 50 engine

riggerrob

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Hill Helicopters announced both their new HX helicopter and GT 50 engine in August of 2020. Hill has chosen the rare path of developing both a new airframe and new engine simultaneously.

The GT 50 gas turbine engine is projected to produce 400 horsepower, similar to the Rolls-Royce Allison 250, PT6A, SAFRAN, etc. engines powering current production light helicopters (2 to 6 seat).

Hill GT 50 is unusual in having three, external, reverse-flow, burner cans arranged radially around the middle of the engine casing. In comparison, RR/Allison uses a single burner can while most other engines have annular combustion chambers that are standard on all larger turbine engines.
What are the advantages of using 1 to 3 burner cans versus annular combustion chambers?
Are burner cans simpler to manufacture?
Are they better suited to small turbine engines (400 horsepower)?

www.hillhelicopters.com
 
I think using three burners instead of one brings the packae closer to an anular combustion chamber. It might be a good compromize which keeps the combustion stability of the burner cans, makes flow distribution easier compared to a single burner and might add reduncy against flame outs.

BTW, the Chrysler turbine car with its can burners could operate with gazoline, Diesel fuel, Channel No.5, Wiskey....

I would like to know the bsfc of it...
 
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I am watching the pre tomorrows event here in my neck of the woods, IWM

cheers hill_helicopters.jpg
 
A centrifugal compressor, reverse flow annular combustor, and a free power turbine. Just like a PT6 from the 1960’s in layout.
 
A centrifugal compressor, reverse flow annular combustor, and a free power turbine. Just like a PT6 from the 1960’s in layout.
Looks more optimized for helicopter use than a small PT6 or 250. Those scroll tubes on the 250 are damage magnets!
 

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