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Here you can find the specifications for each one of the products in PAPIZTURBINE®
Prometeo Turboprop 300Hp
Turboprop designed to be use in medium size both single and twin engine aircrafts been able to deliver constant 300sHP with a very similar consumption to a regular and same power piston engine making it a unique engine. Its simplicity and sturdiness frame in combination with last generation materials like TITANIUM, INCONEL; CERAMIC and others make of this engine an indispensable element for all category and type of plane that its performance or flight type requires such a engine.
Description:
Turboprop engine made from a PAPIZTURBINE own design pure reactor with own planetary and helical gear box to be used both in tractor and pusher propellers types. The products are a high performance reliable and low consumption engines with plus long TBO and special materials as any reactor engine.
These engines were designed and prove to avoid the dangerous non aeronautical piston engines and answering to real aeronautical needs for a very reliable engine for small and medium size aircrafts and to introduce an economical engine in price and operability according to the global actual economic reality.
The Materials for these engine were carefully selected end prove to give the best result for these type of engine without a high cost and being able to use more spacing services time giving to the pilot the freedom of flight passing the less time possible in the workshop.
The engine is made of 1 step ensuring its simplicity and efficiency; it has a very unique injection system in perfect harmony between the mechanical and electronic closing the circle to achieve the new engine generation.
The patented injections system was prove and calibrated to use 3 type of fuel as JP or Jet A1, Diesel fuel and Biodiesel fuel making automatic corrections without losing any power solving the problem of refueling only in airports and according to the global crisis using cheap type of fuel. These characteristics make true the possibility to have a turbine power plant in small and medium size aircraft with the same consumption as the piston engine.
Technical specifications:
| DataSheet | Advanced |
| Type: dual busters 1 stage Turboprop engine | Turbine RPM max: 65.000 |
| Nominal Power: 300 sHP | Propeller RPM max: 2750 |
| Residual Power: 10% aprox | Gear Box: 2 State Own Design Planetary Gear Box. |
| Engine Diameter: 240mm | Control Systems: ECU instrument with 7” touch screen for parameters. |
| Normal Gear Box Option Total Diameter: 480mm | Start Sequence : to avoid the human error in the start sequence the ECU make a perfect automatic start with only press a button. |
| Length without exhaust and propeller : 800mm | TBO Time: 3500hs |
| Max Power Estimated Consumption: 85 lts/h | Service Time scheme: 100, 250, 500, 750 y 1200hs |
| Cruise Power Estimated Consumption (75%): 73 lts/h | Estimated Weight: 110kg |
| IDLE Power Estimated Consumption : 28 Lts/h | Recommended Propellers: AVIHEL propellers, 2 blades fix pitch and variable pitch composite propeller, 3 blade fix pitch and variable pitch composite propeller Variable pitch propeller PAPIZ-AVIHEL systems. |
| Admitted Fuel Types: JP, Diesel and Biodiesel | |
| Injection System: Mechanical and Electronic |
Quasar Turboprop 180Hp
Turboprop designed for medium size airplane or small ones with special characteristics like STOL airplane and others. As every engine design by PAPIZTURBINE Company, this engine has a very low consumption, the capacity of use 3 type of fuel like JP or jet A1, diesel and biodiesel bringing safety, reliability and savings to this kind of airplanes.
This turboprop unlike the PRETORIAN 100hp uses an direct shaft to make the acceleration faster, use another systems for ensure to the pilot to have the power when he need it and how he need it..
Description:
Turboprop engine made from a PAPIZTURBINE own design pure reactor with a own planetary and helical gear box to be used both in tractor and pusher propellers types. The products are a high performance reliable and low consumption engines with plus long TBO and special materials as any reactor engine.
These engines were designed and prove to avoid the dangerous non aeronautical piston engines and answering to real aeronautical needs for a very reliable engine for small and medium size aircrafts and to introduce an economical engine in price and operability according to the global actual economic reality.
The Materials for these engine were carefully selected end prove to give the best result for these type of engine without a high cost and being able to use more spacing services time giving to the pilot the freedom of flight passing the less time possible in the workshop.
The engine is made of 1 step ensuring its simplicity and efficiency; it has a very unique injection system in perfect harmony between the mechanical and electronic closing the circle to achieve the new engine generation.
The patented injections system was prove and calibrated to use 3 type of fuel as JP or Jet A1, Diesel fuel and Biodiesel fuel making automatic corrections without losing any power solving the problem of refueling only in airports and according to the global crisis using cheap type of fuel. These characteristics make true the possibility to have a turbine power plant in small and medium size aircraft with the same consumption as the piston engine.
Technical specifications:
| DataSheet | Advanced |
| Type: dual busters 1 stage Turboprop engine | Turbine RPM max: 65.000 |
| Nominal Power: 180 sHP | Propeller RPM max: 2750 |
| Residual Power: 10% aprox | Gear Box: 2 State Own Design Planetary Gear Box |
| Engine Diameter: 200mm | Control Systems: ECU instrument with 7” touch screen for parameters |
| Planetary Gear Box Option Diameter: 250mm | Start Sequence : to avoid the human error in the start sequence the ECU make a perfect automatic start with only press a button. |
| Length without exhaust and propeller : 700mm | TBO Time: 3500hs |
| Max Power Estimated Consumption: 40 lts/h | Service Time scheme: 100, 250, 500, 750 y 1200hs |
| Cruise Power Estimated Consumption (75%): 35 lts/h | Estimated Weight: 80kg |
| IDLE Power Estimated Consumption : 20Lts/h | Recommended Propellers: AVIHEL propellers, 2 blades fix pitch and variable pitch composite propeller, 3 blade fix pitch and variable pitch composite propeller Variable pitch propeller PAPIZ-AVIHEL systems. |
| Admitted Fuel Types: JP, Diesel y Biodiesel | |
| Injection System: Mechanical and Electronic |
Pretorian Turboprop 100Hp
Turboprop design for small size aircraft, ULTRALIGH types, LSA or regular conventional aircrafts types with a very broad range of types, shape, cost and characteristics. Manufactured with the same materials that all PAPIZTURBINE engines but with a free shaft system turbine and hydraulic clutch that allows the engine a smooth start with no load ensuring a good time of useful life and presenting the same low consumption as all engines of this company that allows to put this type of engine without making several modification in the plane and in the flight.
Design with forced lubrication in the gear box and special ball bearings that confer a very low wear and long TBO time.
Description:
Turboprop engine made from a PAPIZTURBINE own design pure reactor with an own planetary and helical gear box to be used both in tractor and pusher propellers types. The products are high performance reliable and low consumption engines with plus long TBO and special materials as any reactor engine.
These engines were designed and prove to avoid the dangerous non aeronautical piston engines and answering to real aeronautical needs for a very reliable engine for small and medium size aircrafts and to introduce an economical engine in price and operability according to the global actual economic reality.
The Materials for these engine were carefully selected end prove to give the best result for these type of engine without a high cost and being able to use more spacing services time giving to the pilot the freedom of flight passing the less time possible in the workshop.
The engine is made of 1 step ensuring its simplicity and efficiency; it has a very unique injection system in perfect harmony between the mechanical and electronic closing the circle to achieve the new engine generation.
The patented injections system was prove and calibrated to use 3 type of fuel as JP or Jet A1, Diesel fuel and Biodiesel fuel making automatic corrections without losing any power solving the problem of refueling only in airports and according to the global crisis using cheap type of fuel. These characteristics make true the possibility to have a turbine power plant in small and medium size aircraft with the same consumption as the piston engine.
Technical specifications:
| DataSheet | Advanced |
| Type: dual busters 1 stage Turboprop engine | Turbine RPM max: 80.000 |
| Nominal Power: 100 sHP | Propeller RPM max: 2750 |
| Residual Power: 10% aprox | Gear Box: 2 State Own Design Planetary Gear Box |
| Engine Diameter: 180mm | Control Systems: ECU instrument with 7” touch screen for parameters |
| Planetary Gear Box Option Diameter: 360mm | Start Sequence : to avoid the human error in the start sequence the ECU make a perfect automatic start with only press a button. |
| Length without exhaust and propeller : 700mm | TBO Time: 3500hs |
| Max Power Estimated Consumption: 25 lts/h | Service Time scheme: 100, 250, 500, 750 y 1200hs |
| Cruise Power Estimated Consumption (75%): 18 lts/h | Estimated Weight: 50kg |
| IDLE Power Estimated Consumption : 10 Lts/h | Recommended Propellers: AVIHEL propellers, 2 blades fix pitch and variable pitch composite propeller, 3 blade fix pitch and variable pitch composite propeller Variable pitch propeller PAPIZ-AVIHEL systems. |
| Admitted Fuel Types: JP, Diesel y Biodiesel | |
| Injection System: Mechanical and Electronic |
E-olo Turbofan
Developing Turbofan Engine using the PAPIZTURBINE hi power reactor as a base with a smooth gear box and a hydraulic clutch with a perfect actual used materials for this company and composite parts combination.
Description:
Meant for a subsonic own designed prototype for 2 and 4 seats, a high performance jet plane, and usual planes with similar takeoff and landing parameters. It has an excellent cruise speed above 600km/h and with a range near to 1500km.
Developing Turbofan Engine using the PAPIZTURBINE hi power reactor as a base with a smooth gear box and a hydraulic clutch with a perfect actual used materials for this company and composite parts combination.
E-OLO Turbofan
Developing Turbofan Engine using the PAPIZTURBINE hi power reactor as a base with a smooth gear box and a hydraulic clutch with a perfect actual used materials for this company and composite parts combination.
Description:
Meant for a subsonic own designed prototype for 2 and 4 seats, a high performance jet plane, and usual planes with similar takeoff and landing parameters. It has an excellent cruise speed above 600km/h and with a range near to 1500km.