The DiNelly eXoGyro System

 

  • ESTOL | SSTOL | STOL
  • TurboProp DiNelly TP 260
  • ROTAX 915is Turbo injection
  • constant speed prop
  • 4,7m² panorama glass
  • 4 doors
  • adjustable rotormast
  • 5,7" EMU glass display
  • 10,4 " glass display
  • 9 x analog instruments
  • up to 3 x bottom hatches
  • bottom windows
  • aerodynamic V-tail
  • up to 5 seats
  • 1,6m³ cargo bay
  • 156l fuel
  • Can Aerospace
  • high efficient rotor system
  • sensorik hatches
  • AC aircondtition
  • 3kW power supply
  • APU fuel cell
  • JET A1 | A | B - fuel

 

Technical specifications of the DiNelly eXoGyro System

 

The model eXoGyro is world´s first professional 4 door UL gyrocopter mission platform, which serially is equipped with minimum 2 hatches at the cargo bay.

Prepared for installing aerial sensing equipment, Lidar sensing, special camera systems, mounts, special sensors,gas leak detection, stretcher, e.g.

Up to 185 kg equipment weight in the cargo bay, additional to the Pilot and Operator in the front. Also the powersupply standard will support 12/28V - 160 A automatic controlled by power management of the APU fuel cell.

The certified Rotax 915is Turbo aircraft engine, works high effcient due to brand new injection technology combined with the turbo. As result the concept of the eXoGyro, perfect aerodynamic, high end rotor system, aerodynmaic V-Tail, adjustable center of gravity coordinated with the Rotax 915is turbo injection engine, you will get low cost operation, high endurance standard up to 10 hrs, ant a maximum operation hight of 23.000 ft.

 

The eXoGyro System is developed, angineered and certified by WAIDHOFER to be the most efficiency low cost mission aerial platform worldwide, which support a cargo bay with 1,6m³ and a payload of 185kg mission operation equippement combined with the safest flight performance according to Clean Sky.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

  • MTOW: 490 -750 kg (depend on national reulations )
  • Certification: ultralight
  • Engine: ROTAX 915is Turbo - 135hp incl. reduction gear
  • side rudder: aerodynamic V-tail
  • elevation stailizer: active V-tail
  • rotor system: 2 blade / 4 blade (in one lever = 1 x CL center lift )
  • ruggedized gear: widht 2,03 meter
  • lenght eXoGyro: 5,70 meter ( nose to V-tail )
  • cabin inside dimesnions: 1,15H x 1,48W x 2,25L meter
  • empty weight: 263kg - 325kg depend on configuration / certification
  • Vne: 217km/h
  • Fuel standard: 156 liter
  • Auxiliary fuel tank: 220 liter
  • Rotor blades: high performance 6,9 meter, 8,4 meter, 8,6 meter
  • Avionic: 9 x analog, 1 x 10,4" glass display, 1 x 5,7" glass EMU
  • Communication EMU - ECU: CanAerospace
  • Propeller: fix pitch, constant speed, (low noise)
  • 4 doors
  • 1,6m³ cargo bay (including attachment points)
  • power supply 14 / 28V - 160
  • Composite high end monocoque (more than carbon or aramid)
  • double fire wall
  • Explosion proof fuel tank

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

  • 4 doors
  • 4,7m² panorama glass
  • 1,6m³ cargo bay
  • cargo bay up to 185 kg payload
  • panorama bottom windows
  • 2 hatches
  • 10,4" master glass display for mission operation
  • 5,7" EMU CANAerospace connected to ROTAX 915is
  • 9 x analog avionic instruments
  • 2 x seats (1 x pilot + 1 x operator)
  • 156 liter fuel tank
  • adjustable center CG (center of gravity)
  • ruggedized gear
  • gear track widht 2,03 meter
  • GCSC - Gyrocopter Comfort Space Cabin (1,15H x 1,48W x 2,25L meter)
  • 14/28V - 160A power supply
  • ergonomic energy absorbing seats (absorbing rotorsystem vibrations)
  • low emission concept (noise, emissions, vibrations)
  • ROTAX 915is Turbo - 135hp ( certified state of the art injection aircraft engine to operate up to 23.000 ft cervice ceiling )
  • TurboProp DiNelly TP 260 (250shp)
  • 3kW poer supply
  • ESTOL | SSTOL | STOL

 

 

  • ESTOL | SSTOL | STOL
  • low operating costs: aprx. $ 150,--/ hrs
  • up to: TurboProp 250shp
  • jump start able / VTOL
  • low infrastructure required
  • maximum wind stability
  • low requirements for pilots
  • low pilot training costs
  • no downwash - no brown out
  • low pilot license upholding costs
  • no STC´s required
  • THE Aircraft of the 21st century

 

The DiNelly eXoGyro family

Emily - recreational flying

Charly - aerial fire fighting

Huxly - aerial sensing

 

 

 

Nelly - military / Gov operation

Molly - transport / logistic

Dusty - agriculture / aerial precision farming

 

 

 

Lucy - police operation

Lilly - trop transporter

eXoDrone - flying taxi

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

Social Media

Facebook

Twitter

YouTube

Google+

Blogger

LinkedIn

Instagram

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

Disclaimer:

 

The information contained in this website is carefully reviewed by DiNelly Aircraft Inc. International Aktiengesellschaft ('DiNelly') and updated on a regular basis. DiNelly asks for forbearance for unintentional and accidental mistakes.

 

Despite the utmost diligence provided by DiNelly, no guarantee is given for the correctness and completeness of the content. Information may be changed, removed or supplemented without notice. No guarantee can be given for completeness, correctness, up-to-dateness and availability.

 

DiNelly declines any liability for incorrect or missing information on the website. Therefore, all decisions based on the information contained on the DiNelly website are solely within the responsibility of the user. In particular, DiNelly is not liable for the content of websites that are reached via links.

 

None of the information provided on the DiNelly website constitutes or is intended to constitute a solicitation to buy or trade in shares of DiNelly. If the DiNelly website contains forward-looking statements, these are based on beliefs and assessments of DiNelly's management and are therefore subject to risks and uncertainties. DiNelly is not required to update such forward-looking statements. Any liability for such statements is expressly excluded.

 

The information contained in this web site or in the accompanying documents is not a legally binding information, but merely an information.

 

Duplication, distribution, reproduction, distribution, downloading, printing, storage and other forms of use of the information contained in this website are subject to approval. Any further use of the information, which may be accessed directly or indirectly from the DiNelly website, requires the express prior consent of DiNelly.

 

All official press releases of DiNelly Aircraft Inc. must be signed in the name of the CEO of DiNelly. Any other press releases mentioning DiNelly's management, employees, products, strategies are void. All rights reserved. Copyright Waidhofer Gwords 2017.