Subject: Single rotor turbo
From: paul
Date: 2/7/2015, 10:54 PM
To: AAA-rotaryengine



Thanks for the input guys.
Your comments have been taken on board. This is the first aircraft that I have built; it is a pioneer 300 microlight or to be precise a champion V by Giuseppe Vidor, scratch built. We are limited in the microlight class in New Zealand to 600kg or 1320lbs all up takeoff weight. I am building a single rotor 13b power plant, and using the Racing Beat side plates, the turbo and fuel injection on a side port seems the best way to go.
Andrew Campbell


How much horsepower do you expect from the single rotor, FI, turbo combination?

Joe Spelz


150 HP would be easy.


The neat think about it is the turbo can be bolted directly to the rotor housing.


Paul Lamar


I am going to mount my turbo behind the engine between the engine and the firewall like a Piper Seneca. If you would go from the 2" rotor output to a Y then to a 3" section of pipe then directly into the turbo inlet you would accomplish 2 important things- the increase in interior volume of the 3" pipe will allow a reduction in pressure and velocity.
The pressure reduction will force a substantial amount of cooling to occur and the decrease in velocity will reduce the exhaust noise. The problem with the rotary turbos has been the excessive heat involved from continuous high HP operation. Moving the turbo downstream a bit will help with this.

I don't know of any certified turbo airplane that has the turbos that close to the engine. The Corvalis TT has then 18 inches away from the cylinders and back toward the firewall and has one smaller one on each side. The Seneca II has one in the center behind the engine fed from both sides and dumped overboard with a single pipe.

There is a known problem with exhaust temp and velocity with these engines, and this is one way to address it.

KA

All true but you lose overall kinetic energy.

The 280 HP third gen RX7 and the 350 HP 20B 3 rotor had the turbo's right up against the rotor housings.
There is a SS heat shield between the turbine housing and the rotor housings.

On an horizontal opposed air cooled aircraft engine the cylinders and the exhaust ports are so far apart it is difficult to design a smooth exhaust manifold for a turbo anywhere near the cylinders.
Even dual turbo's.

Paul Lamar

Owing to the fact that I am only looking for 120 Hp the heat issue should be somewhat less than for a twin or tri rotor. Would anyone have an idea as to the type of turbo that would be suitable? If I was to use a turbo suited to 250 HP perhaps it would cope with the sustained hi power output?
Andrew. CampBell

You could get 120 HP out of a P-port one rotor if you used a 3.12 gear box.
No turbo.

Paul Lamar


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