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Technical Specifications:

The ”eXoGyro System” – high efficiency multi purpose aerial platform.
World´s first 4 door gyrocopter for professional operation ( also as ultralight )
160 hp liquid cooled aircraft injection engine | new DiNelly Tauros
DiNelly Tauros: 160 hp | 250 Nm torque | 2.600 cm³ | reduction gear | liquid cooled
fuel consumption DiNelly Tauros: 4,2 US gallon at 75% power setting | 160Hp
DiNelly Tauros: CANaerospace | double ECU | glass EMU | liquid cooled
CFK propeller: special silent technology | steel edge | constant speed | from 130 hp up to 190hp
world´s first rotorcraft with adjustable center of cravity
4,7 m² glass for your perfect panorama view at mission operation | EASA certified
1,6m³ certified storage compartment + Pilot + Operator | sensing compartment
most modern composite monocoque | fire resistant | 110 KN / mm² | 22,5 kg / 49,6 lbs
engine autark heating system | 2.400 Watt heating power
air condition | 1.800 Watt cooling power | engine autark
156 liter fuel tank standard | 220 liter internal auxiliary fuel tank | up to 22 hrs endurance
stretcher operation | internal stretcher up to 2,02 meter + pilot + doctor
up to 3 hatches | each in a dimension of 40 x 60 centimeter | direct below center of gravity
auxiliary power supply due to fuel cell
avionik: 9 x analog + 1 x 10,4” glass display + 1 x 5,7” EMU + transponder
panorama bottom windows for professional mission operation
specially powerfull rotorblades | low vibration rotor head
fire resistant chassis | monocoque | outside safety fuel tanks
aerodynamic V-Tail | redundant | high efficient
up to 5 seats | 1 x Pilot + 1 x doctor + 1 x stretcher | 1 x pilot + 1 x operator + equipment
up to 200 liter drinking water tank
gyrocopter comfort space cabin | 220 x 148 x 115 centimeter cabin size inside
modular construction | rapid transportation | kit available as standard
low vibration rotor system | 4 blade rotor system
special DiNelly eXoMount for gyrocopter
4 blade rotor system | 4 blades in one level
armored chassis | 7,62 mm | EN 1521
double engine with coaxial propeller | 2 x 80 hp rotary engine EASA certified
Rotax 912is/c in a gyrocopter ( twenty second OEM at BRP Rotax listed ) Ram air charched
EMU (engine management unit) 5,7” glass / flight tracking)
satellite communication | up- downlink | up to 30Mbit/s
eXoMount communicating with flight managment system and EFIS
DiNelly engineering in aviation is according to CLEANSKY philosophy.
fire resistant according to DIN EN 4102 B1 / A1
shock absorbing adjustable design seats
optional fire extinguisher system
safety parts in accordance to EASA Form 1
supplier compliance EASA 145 / Part 21 / ISO:9100
carbon monocoque ISO 9100:2008 (aviation quality standard)
high end engineering | CAD | CFD | CAM | FEM | simulation | rapid prototyping
10,4” glass display with 3D live weather and fleet management system
ergonomic multifunctional dashboard design
engineering & industrial design by DiNelly Aerosystems Ltd | no external design studio involved
available as UAS | UAV | Autopilot

DiNelly at Integeo 2013

Video Gallery / YouTube

DiNelly eXoGyro System
DiNelly eXoGyro System
DiNelly eXoGyro System

Development of eXoGyro