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Cessna bringing Jet A fuel engine to piston market; 30-40% more fuel efficient than avgas engines

28 July 2012

Cessna Aircraft Company, a Textron Inc. company, is introducing a single-engine airplane—the new Turbo 182 Skylane—equipped with the first engine of its kind in the single-engine industry designed to run on Jet A aviation fuel.

SAF01406
SMA SR 305-230 engine on the stand at Le Bourget 2007 SAFRAN. Intended for general aviation piston engine that operates on a diesel cycle and uses a standard fuel Jet A/1A. Click to enlarge.

The new Turbo 182 is a result of market research and has already undergone extensive reliability testing, as well as flight testing. The Safran-made SMA engine (SMA SR305-230E) is engineered specifically for aviation and is already FAA and EASA certified. The four-cylinder, four-stroke engine uses 11 gallons per hour of the typically lower-cost Jet A fuel at the estimated maximum cruise speed of 155 knots.

The 230 horsepower Jet A engine offers customers increased range and greater payload capacity and does not sacrifice performance. This plane offers significantly lower direct operating costs due to the fact that Jet A fuel is typically more affordable and much more widely available.

—Jeff Umscheid, Cessna 172, 182, 206 business leader

The fuel technology used in the engine eliminates concerns about carbon monoxide emissions, fuel mixtures, propeller control and exhaust gas. The engine operates at a lower propeller speed. As a result, the turbocharger technology delivers a quieter flight line and reduces noise pollution. There are zero lead emissions and zero CO emissions. Flight at the maximum cruise speed demonstrates greater fuel efficiency, and will burn approximately 30% to 40% less fuel than comparable avgas engines.

The new Turbo 182 has a seating capacity for four and an estimated range at max cruise speed of 1,025 nautical miles (1,898 kilometers). The certified ceiling is 20,000 feet (6,096 meters). The Garmin G1000 avionics suite is pilot-friendly and highly-functional, bringing great levels of situational awareness to the cockpit. The engine diagnostics display on the primary flight display and the multi-function flight display. Fuel capacity is 87 gallons (329 liters), with an estimated useful load of 1,000 pounds (454 kilograms).

July 28, 2012 in Brief | Permalink | Comments (9) | TrackBack (0)

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Over 30% increase in fuel efficiency and less noise will be appreciated by users and by people living in the neighborhoods. Some of the small aircraft make more noise than an Airbus A-380.

First, I will say that I do think that this is an improvement over the lycoming or Continental gasoline engines that are normally found in these planes.

However, why someone would build an air-cooled engine and use mechanical injection is beyond understanding. I first saw this engine at the Oshkosh airshow about 10 years ago (2001?) For the same power, you build a lighter and more reliable engine using liquid cooling and you could save even more fuel and run cleaner and smoother with electronic injection.

I am currently building an experimental plane with a liquid-cooled Rotax 914. I would rather have a diesel engine but not an air-cooled engine. Anyway, this engine is too heavy and has too much power anyway for my use. I need about 100 to 140 hp.

This engine seems to come from two realities:

"Av gas is now more expensive than beer." That high octane lead fuel economic is intolerable.

Limited av gas supplies are so rare in some areas that it can cost $20/gal to be imported.

Jet A fuel flying at a fraction of current av gas rates will win out, besides the 30%+ higher efficiency.

Air cooling and mechanical injection have one major virtue:  they either can't fail, or tend to fail gently.

Delta Hawk has been working on a liquid-cooled aerodiesel for a very long time.  I have no idea how far along they are toward their goal of FAA certification.

@ HarveyD

" Some of the small aircraft make more noise than an Airbus A-380."

Oh really, care to mention which ones?

In this picture the Safran SMA engine shape reminds me of the OPOC engine, by EcoMotors (http://www.greencarcongress.com/2010/03/ecomotors-20100310.html).
Just wonder if the OPOC Engine could be used in aircraft. The designers said the first application to be for trucks, although it naturally looks as an aircraft engine, and would probably have less packaging issues than in trucks.

Mono-engine on floats (all of them) can be heard taking off and climbing from many miles. We hardly hear the A-380 taking off from 10 Km away. People living close to airports with flying schools want to sell but can't find buyers.

Engineer-Poet

I would disagree with you on the failure mode both on air-cooled engines and mechanical injectors. Air-cooled engines often fail catastrophically with a valve or piston failure leading to basically an engine explosion. Even in the best case, a valve is burned or a piston is holed.

Electronic injectors use a high pressure pump and a common rail. It is easy to provide a second pump for backup. I believe that the new electronic injection (gasoline) Rotax 912 has a complete independent injection system. With mechanical injection, the pump supplies both the pressure and the timing.

Electronic injectors stop working when the electrical system does.  The whole point of using magnetos on an engine is that they are independent of the rest of the aircraft's electrical system; building a compression-ignition engine dependent on bus power to run makes the powerplant far less reliable than before.

I was a member of a flying club.  We had engines experience difficulties due to mechanical failure, but the aircraft was still flyable and did not have to make an emergency landing.  That's the difference between partial and total failure.

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