Engineered Propulsion Systems Graflight V-8

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Graflight V-8
Type Liquid-cooled V-8 piston
diesel aircraft engine
National origin United States
Manufacturer Engineered Propulsion Systems
Designer Michael Fuchs and Steven Weinzierl
First run 2014
Major applications Cirrus SR22

The Graflight V-8 is an aircraft diesel engine developed by Wisconsin-based Engineered Propulsion Systems

Design

The Graflight V-8 is a liquid-cooled, flat V-8 with

Cessna TTx and Cessna 206 as possible applications.[2]

The design is a 320–450 hp (240–340 kW), 4.3-liter engine with steel pistons, connecting rods, and crankcase to improve reliability. At 650 lb (290 kg), it weighs 40 to 50 lb (18 to 23 kg) more than a conventional aircraft engine, not including the 30 lb (14 kg) radiator for cooling. It should be 30-40% more expensive to purchase than a comparable avgas engine, but with 30-50% better fuel economy.[3] Its low vibration levels allow the use of composite or aluminum propellers.[1]

The engine's 17:1

brake specific fuel consumption of less than 0.32 lb/(hp⋅h) (195 g/kWh), compared to typical avgas engines with 0.42 lb/(hp⋅h) (255 g/kWh). It is expected that the Graflight V-8 will burn under 11 US gal/h (42 L/h) of fuel at 65% power.[4]

As a direct comparison, the 350 hp (261 kW) version of the Graflight V-8 engine will weigh 30 to 50 lb (14 to 23 kg) more than the comparable

operating costs.[5] At normal 75% cruise power, the Graflight V-8 consumes 77 lb/h (35 kg/h) of fuel, whereas the Continental TSIO-550-E burns 110 lb/h (50 kg/h), a reduction of 30%.[6]

Development

EPS set out to

FAA certification was expected at that time by the end of the year.[2]

Later in 2017 the testing progress was delayed by insufficient funding. By July 2018 it had completed 25 hours of flight testing on a Cirrus Aircraft airplane. At that point the company hoped to attract Fortune 500 investors and planned that a new demonstrator should be ready in the first quarter of 2019.[3] The production version of the engine was shown at AERO Friedrichshafen in April 2019 and work continued on environmental and block testing towards the goal of type certification.[8]

Unable to obtain the needed financing to continue operations, the company filed for

Chapter 11 bankruptcy protection in August 2020.[8]

Applications

Specifications (Graflight V-8)

Data from EPS[1]

General characteristics

Components

  • Fuel type: Jet A, JP-8 or straight diesel
  • Cooling system: liquid cooled

Performance

  • Power output: 350 hp (261 kW)
  • Compression ratio: 17:1
  • Fuel consumption: 9.74 to 17.55 US gal/h (36.9 to 66.4 L/h) from 210 to 350 hp (157 to 261 kW)
  • Specific fuel consumption
    :     0.315 to 0.34 lb/(hp⋅h) (192 to 207 g/kWh)

References

  1. ^ a b c "Engine Overview". Engineered Propulsion Systems.
  2. ^ a b Pia Bergqvist (July 7, 2017). "EPS Diesel Engine Nears Certification". Flying Magazine.
  3. ^ a b c Mark Huber (July 25, 2018). "EPS Continues To Make Progress on Aero Diesel". AIN online.
  4. ^ "EPS Making Progress on Certification of Vision 350 Flat-V Diesel Aero-Engine" (Press release). EPS. July 9, 2013.
  5. ^ Thomas B Haines (October 5, 2015). "DIESEL ROUNDS THE BEND NEW FUNDS SPUR NEXTGEN DIESEL ENGINES". AOPA.
  6. ^ "Fuel Economy". Engineered Propulsion Systems.
  7. ^ Addison Schonland (March 26, 2018). "EPS Diesel Progressing Toward Certification". AirInsight.
  8. ^ a b c O'Connor, Kate (August 11, 2020). "EPS Files For Bankruptcy". AVweb. Archived from the original on August 12, 2020. Retrieved August 12, 2020.
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