TurboProp

at

DiNelly GYROCOPTER

 

The TurboProp engine will be installed at the DiNelly Gyrocopter models: eXoGyro, SuperGyro, UG1,

(System will be available 2017)

 

DiNelly has in-house expertise and know-how in the field of turbines and jet engines development. Hermann Künkler has done his doctoral thesis in the field of jet turbines and rocket propulsion technology around NASA.

 

 

 

 

 

 

 

The TurboProp engine offers the following benefits:

 

  • small buildup dimensions
  • low weight
  • high static thrust

 

The TurboProp engine is designed for use in push configuration. Thnaks to its low weight and 190 kW output the engines is an ideal solution for powering the professional DiNelly mission operation platforms. Unique flight performance up to 29.500ft supported by this engine.

 

At this time, no other gyrocopter offers you so much performance, safety. This great turbine is fully controlled by FADEC and connected over CANAerospace with the redundant 5,7" glass display to increase your comfort.

 

The turboprop engine is especially suited to small aircraft and unmanned aerial vehicles. The main advantage of this engine is its low weight with a power of 180 kW and its capacity to achieve flight levels of 9.000m with a maximum starting height of 6.000m. The system is designed so that the engine can be placed in the aircraft either pusher or tractor mode.

 

 

MAIN FEATURES:

 

  • Excellent power-to-weight ration
  • Installation in pusher or tractor mode
  • Gearbox design offers the possibility to install an alternator with output power 1,6kW
  • Modular design features a gas generator, power turbine and gearbox
  • Standard completion; fuel-oil system, control system, ignition unit and connection cables
  • Small installation dimensions, low weight and high static power

 

 

TECHNICAL PARAMETERS

 

 

 

Output shaft speed

2,158 RPM

2,158 RPM

Gas generator speed (100%)

56.200 RPM

56,200 RPM

Power supply

28 V DC

28 V DC

Electrical power output

720 W

720 W

 

 

 

DIMENSION & WEIGHT

 

 

Heigth x width (without exhaust)

398 x 330 mm

15,67 x 13,00 in

Lenght

891 mm

35,08 in

Engine weight

61,6 kg

135,8 lbs

 

 

 

POWER

 

 

Take-off (max-5 min)

180 kW

260 HP

Maximum continuous

160 kW

214 HP

Normal cruise

140 kW

188 HP

 

 

 

FUEL CONSUMPTION (SFC)

 

 

Take-off (max 5 min.)

0.515 kg/kW/h

0,847 lb/HP/hr

Maximum continouos

0.525 kg/kW/h

0,863 lb/HP/hr

Normal cruise

0.548 kg/kW/h

0,901 lb/HP/hr

 

 

 

OTHER DATA

 

 

Max. EGT

650 C

1.202 F

Amount of air intake

1,5 kg/sec

3.3lb/sec

Fuel

JET A, A1, B of DERD 2494 standard

TS-1, T2, RT of GOST 10227-86 standard

JET A, A1, B of DERD 2494 standard

TS-1, T2, RT of GOST 10227-86 standard

Oil

according to MIL-L-23699

( Mobil Jet oil II, AERSHELL 390)

according to MIL-L-23699

( Mobil Jet oil II, AERSHELL 390)

 

 

 

OPERATING RANGE

 

 

Max. operating altitude

9.000 m

29.500 ft

Max. starting altitude

6.000 m

19.700 ft

Temperature operating range (0 m)

-50 C to ISA +30 C

-58 F to ISA +54 F

Ambient temperature for start (0)

-30 C to ISA +30 C

-22 F to ISA +54 F

 

 

 

DiNelly Management, Richard Waidhofer, Peter, Göllner, Jörn follmer, DiNelly TurboProp,

 

In case of interest contact us by the following form:

 
 
 
 
 
 

DiNelly Aircraft Inc.

302A W. 12th St. # 308

New York, NY 10014

U.S.

 

Mail: contact@dinelly-exogyro.com

Web: www.dinelly-exogyro.com

 

Director: Mr. Richard Waidhofer

CEO: Mr. Richard Waidhofer

 

Aviation design engineer: Mr. Richard Waidhofer

 

Richard Waidhofer Licensor of:

DiNelly - eXoGyro System

DiNelly - Emily

DiNelly - Huxly

DiNelly - UG1- Lilly

DiNelly - LPOA -Lucy

DiNelly - JLTA - Nelly

DiNelly - Molly

DiNelly - Charly

DiNelly - Rotorblades

Field of activity of DiNelly

- AEROSPACE

- DEFENSE

- COMMERCIAL

- EMERGING TECHNOLOGIES

- AIRCRAFT CONSTRUCTIION

- INNOVATION

- OFF-SITE SERVICE

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Perry DiClemente
Hermann Künkler - WAIDHOFER-exogyro
Peter Göllner - WAIDHOFER eXoGyro

Peter Göllner

Aerial Sensing | CASO

Geodesy engineer

Perry DiClemente

Aircraft design

Aviation engineer

Hermann Künkler

Engineering | certification

Aviation engineer

Jörn Follmer - WAIDHOFER-exogyro

Jörn Follmer

Sales executive | CSO

MBA business economist

Richard Waidhofer

Richard Waidhofer

Product Owner | CEO

Aviation design engineer

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