The Engines
ADEPT Airmotive has recognized the need for modern, fuel-efficient engines to power both existing and new light aircraft. We have developed a range of General Aviation engines specifically tailored to meet our customers’ requirements…
Our competitive advantage stems from significant weight savings, a robust and compact design that allows for installation in a wide range of airframes, superior engine management, fuel efficiency, and reduced maintenance costs. Our engines are suitable for both tractor and pusher applications and are designed to run reliably on readily available unleaded fuels.
ADEPT’s innovative design and engineering approach is unique in the General Aviation sector and would not be considered unusual by those familiar with the high-tech worlds of Motor Racing, Moto GP, or Aerospace and Defense. Our advanced product development, rigorous testing and validation, and practical use of technology, such as engine design and simulation software, are all essential in creating our superior products.
Our design work complies with the certification requirements of an aviation regulatory-approved design organization. Additionally, the use of Rapid Prototyping and Additive Manufacturing has minimized product development lead times, while advanced finite element analysis, computational fluid dynamics, non-destructive testing processes, and casting simulation programs have all contributed to ADEPT’s successful manufacturing and development programs.
The ADEPT engine range features a novel and unique engine architecture in General Aviation. The 120-degree V6 engine layout offers a lightweight, compact engine with high mechanical strength and integrity, excellent balance, uniform cooling, and optimal integration with the engine/propeller speed reduction unit. Fully sequential fuel injection, a unique lubrication system, and anti-backlash and gear cush-drive mechanisms in the PSRU all contribute to creating the smoothest-running piston engine in General Aviation.
Engine Specifications
HORSEPOWER | 250hp |
MAX ENGINE TORQUE | 236ft-lbs |
MAX PROP TORQUE | 491ft-lbs |
MAX ENGINE RPM | 5600rpm |
MAX PROPELLER RPM | 2700rpm (2250rpm Opt.) |
FUEL BURN AT CRUISE (EST.) | 9,9 GPH |
FUEL COMPATIBILITY | 91UL/100LL/E15 |
FUEL SYSTEM | Sequential Fuel Injection |
ENGINE LAYOUT | 120 Degree V6 |
CAPACITY | 3.2 Litre (195cu.in) |
VALVE TRAIN | 24 Valve Quad Cam |
BORE / STROKE | 3.85 x 2.75” |
COMPRESSION RATIO | 10.5:1 |
COOLING | Liquid and Oil Cooled |
IGNITION | Electronic Control |
AVIONICS OUTPUT | RS-232 / CAN |
INDUCTION | Naturally Aspirated |
LUBRICATION | Dry Sump |
DIMENSIONS |
L30" x W30" x H23" |
DRY WEIGHT | 320 lbs |
INSTALLED WET WEIGHT | 421 lbs |
PROJECTED TBO | 2500 Hours |
HORSEPOWER | 280hp |
MAX ENGINE TORQUE | 257ft-lbs |
MAX PROP TORQUE | 535ft-lbs |
MAX ENGINE RPM | 5800rpm |
MAX PROPELLER RPM | 2800rpm (2330rpm Opt.) |
FUEL BURN AT CRUISE (EST.) | 10,7 GPH |
FUEL COMPATIBILITY | 91UL/100LL/E15 |
FUEL SYSTEM | Sequential Fuel Injection |
ENGINE LAYOUT | 120 Degree V6 |
CAPACITY | 3.2 Litre (195cu.in) |
VALVE TRAIN | 24 Valve Quad Cam |
BORE / STROKE | 3.85 x 2.75” |
COMPRESSION RATIO | 10.5:1 |
COOLING | Liquid and Oil Cooled |
IGNITION | Electronic Control |
AVIONICS OUTPUT | RS-232 / CAN |
INDUCTION | Naturally Aspirated |
LUBRICATION | Dry Sump |
DIMENSIONS |
L30" x W30" x H23" |
DRY WEIGHT | 324 lbs |
INSTALLED WET WEIGHT | 426 lbs |
PROJECTED TBO | 2500 Hours |
HORSEPOWER | 320hp |
MAX ENGINE TORQUE | 308ft-lbs |
MAX PROP TORQUE | 640ft-lbs |
MAX ENGINE RPM | 5600rpm |
MAX PROPELLER RPM | 2700rpm (2250rpm Opt.) |
FUEL BURN AT CRUISE (EST.) | 11,7 GPH |
FUEL COMPATIBILITY | 91UL/100LL/E15 |
FUEL SYSTEM | Sequential Fuel Injection |
ENGINE LAYOUT | 120 Degree V6 |
CAPACITY | 3.2 Litre (195cu.in) |
VALVE TRAIN | 24 Valve Quad Cam |
BORE / STROKE | 3.85 x 2.75” |
COMPRESSION RATIO | 8.9:1 |
COOLING | Liquid and Oil Cooled |
IGNITION | Electronic Control |
AVIONICS OUTPUT | RS-232 / CAN |
INDUCTION | Turbocharged |
LUBRICATION | Dry Sump |
DIMENSIONS (INCL TURBO) | L38" x W30" x H23" |
DRY WEIGHT | 348 lbs |
INSTALLED WET WEIGHT | 462 lbs |
PROJECTED TBO | 2500 Hours |
HORSEPOWER | 360hp |
MAX ENGINE TORQUE | 331ft-lbs |
MAX PROP TORQUE | 810ft-lbs* |
MAX ENGINE RPM | 5800rpm |
MAX PROPELLER RPM | 2800rpm (*2330rpm Opt.) |
FUEL BURN AT CRUISE (EST.) | 12,9 GPH |
FUEL COMPATIBILITY | 91UL/100LL/E15 |
FUEL SYSTEM | Sequential Fuel Injection |
ENGINE LAYOUT | 120 Degree V6 |
CAPACITY | 3.2 Litre (195cu.in) |
VALVE TRAIN | 24 Valve Quad Cam |
BORE / STROKE | 3.85 x 2.75” |
COMPRESSION RATIO | 8.9:1 |
COOLING | Liquid and Oil Cooled |
IGNITION | Electronic Control |
AVIONICS OUTPUT | RS-232 / CAN |
INDUCTION | Turbocharged |
LUBRICATION | Dry Sump |
DIMENSIONS (INCL TURBO) | L38" x W30" x H23" |
DRY WEIGHT | 355 lbs |
INSTALLED WET WEIGHT | 467 lbs |
PROJECTED TBO | 2500 Hours |
Concept in Development...
HORSEPOWER | 425hp |
MAX ENGINE TORQUE | 390ft-lbs |
MAX PROP TORQUE | 955ft-lbs |
MAX ENGINE RPM | 5900rpm |
MAX PROPELLER RPM | 2420rpm |
FUEL BURN AT CRUISE (EST.) | 15,9 GPH |
FUEL COMPATIBILITY | 91UL/100LL/E15 |
FUEL SYSTEM | Sequential Fuel Injection |
ENGINE LAYOUT | 120 Degree V6 |
CAPACITY | 3.6 Litre (220 cu.in) |
VALVE TRAIN | 24 Valve Quad Cam |
BORE / STROKE | 4 x 2.91" |
COMPRESSION RATIO | 9.0:1 |
COOLING | Liquid and Oil Cooled |
IGNITION | Electronic Control |
AVIONICS OUTPUT | RS-232 / CAN |
INDUCTION | Twin Turbocharged |
LUBRICATION | Dry Sump |
DIMENSIONS (INCL TURBO) | L40" x W31" x H23" |
DRY WEIGHT | 391 lbs |
INSTALLED WET WEIGHT | 519 lbs |
PROJECTED TBO | 2000 Hours |
320T Torque & HP
vs Engine RPM
Advanced Internal Combustion
Compact and Light Weight
Fuel Efficient
Smooth and Responsive
Advanced Manufacturing Processes
Integrated PSRU
Robust Architecture
Liquid Cooled
Avgas / Mogas / Biofuel Compatible
FADEC
Advanced Materials
High Power Density
PERFORMANCE ADVANTAGE
= COST ADVANTAGE
Fly Further… for Less
Extremely Fuel Efficient
Extended Range
Lower Cost Fuel –
Unleaded and Ethanol Blends
Low Maintenance Costs
Low Service Part Costs
Extended Maintenance Intervals
Designed for Ease of Maintenance
Increased Payload
Substantial Operating Cost Saving
= SAFETY ADVANTAGE
Robust, Reliable Technology
Extended Range and Performance
Fuel Flexibility and Availability
Excellent Power to Weight Ratio
CG Optimization
Low Pilot Workload
Reduced P Factor
Electronic Mixture Optimization
Enhanced Engine / EFIS interface
Responsive Power on Demand
Smooth Engine Operation
Liquid Cooling for Cabin Heat
No Shock Cooling
No Carb Icing
FIXED WING TRACTOR
COMPETITION AIRCRAFT
FIXED WING PUSHER
AMPHIBIAN PUSHER BUSHPLANE
AMPHIBIAN TWIN
HELICOPTER
FLYING CAR
HYBRID APPLICATION
UNMANNED AIRCRAFT
AG FIXED WING
AG HELICOPTER
STOL APPLICATION
Frequently Asked Questions
Here are some frequently asked questions about our engines. If you have any additional queries, please make contact…
What is the cubic capacity of the engine?
Just less than 3.2 liters (195 Cubic Inches).
What is the bore/stroke ratio?
To keep piston velocity low, the engine has a fairly oversquare bore/stroke ratio (98mm / 3,86” x 70mm / 2,75”) in order to keep piston speed low, as well as fairly short con rods. The short rods give higher piston acceleration which helps in effective filling early on the intake stroke. Narrow and light piston/ring components tolerate high acceleration well.
Is the engine suitable for operation in non-certified helicopter applications?
Whilst the company has initially focussed on fixed-wing applications, the engine is ideal for helicopter operation, and can be optimized to provide high power and torque at constant speed as required in rotary-wing applications. The PSRU also is ideally suited to installation in legacy helicopters which use belt drives to the rotors.
Why is the ADEPT Airmotive not a compression ignition (diesel) engine?
Although diesel has certain advantages with regards to fuel consumption and economy, we don’t believe that compression ignition technology is best suited to GA applications.
Among the reasons for this are:
- Poor relationship between torque and power
- If used at high altitudes Jet-A has to be used as it contains an anti-freeze that diesel fuels do not have
- Compression ignition engines have to be heavier to contain higher bearing loads
- Diesel engines have poor power to weight ratios
- Typical harshness of Diesel engines require complex vibration-isolating solutions
- Harsh firing impulses of Compression ignition engines has a negative effect on reduction gearbox and propeller life
- Satisfactory power generation generally requires high turbo boost with related reliability problems
- Diesel fuel weighs more than gasoline
- We can meet the fuel consumption targets by using an efficient gasoline engine
What aircraft use the ADEPT engines?
ADEPT engines are installed / or are currently in process of being installed in a variety of aircraft including Lancairs, Velocity’s, and some exciting new aircraft in development.
As an example, a 320HP engine is fitted to the all-composite SA Ravin 500 (a South African designed and manufactured aircraft similar to the Piper Comanche). The combination of the ADEPT engine and the Ravin airframe results in one of the finest GA aircraft in the world, with an operating radius of over 1900NM (3500Km) and a 12-hour endurance capability.
ADEPT is working with several Non Type Certified airframe OEMs as well as a wide range of aircraft builders and owners flying aircraft ranging from Super Cubs, Lancairs, Velocitys, RV-10s, and aircraft used in crop spraying and humanitarian operations. In addition, the engine is ideal for legacy aircraft engine replacements once certification is obtained.
What advantages does the ADEPT range of engines have over traditional piston engines?
The ADEPT motor utilizes best-practice current engine technology and is therefore extremely economical and reliable. The ADEPT motor offers competitive acquisition costs and affordable operating and maintenance costs.
What is the expected TBO of the ADEPT engine?
The engine has been designed with a targeted TBO in excess of 2000 hours. Our TBO projections are being confirmed during our monitored flight programme.
How does the adept engine achieve such low operating costs?
The ADEPT engine is extremely fuel-efficient, and runs on Autogas/Mogas that is generally far less expensive than Avgas. ADEPT engines are also designed for ease of maintenance, and utilize readily available, modern service components, with far lower costs than traditional aviation service parts. Due to the modern design of the engine, service intervals are also extended in relation to traditional aviation engines.
What is the advantage of a 120° V6 layout?
It is a compact design offering high efficiencies, lightweight, low vibration levels and high structural integrity leading to long engine life.
Does the ADEPT motor rev higher than existing engines – and does this not lead to rapid engine wear?
Current technology gasoline engines are most efficient at higher RPM than the RPM range at which the traditional legacy aviation engines usually operate. The ADEPT engine’s average piston speed is lower than that of conventional GA engines due to the optimum bore/stroke ratio used. The low mass of reciprocating parts also reduces engine wear.
The ADEPT engine uses a PSRU – are these units not a potential source of problems?
The ADEPT PSRU is a robust and thoroughly engineered unit. It is an integral part of the engine structure. The PSRU reduction ratio has been selected to provide low noise and an absence of annoying and dangerous harmonics. Robust gear forms, and the use of a combination of extremely robust roller bearings for radial shaft support, and taper roller bearings for both pusher and tractor thrust loads ensure reliability and durability. The unit also incorporates a gear cush-drive to protect the rest of the engine from prop strikes.
Production Slots Available
PRESS RELEASE
ADEPT Propulsion Technologies Announces Strategic Commercial Agreement with RapidSky LTD at AirVenture 2024…