DiNelly THE PIONEER

 

RICHARD WAIDHOFER & HERMANN KÜNKLER ARE PIONEERS AT FIELD OF GYROCOPTER OPERATION & TECHNOLOGY

 

AS A RESULT OF LONG-TERM INVESTMENT IN RESEARCH AND DEVELOPMENT SINCE 2005 OF RICHARD WAIDHOFER

 

In the year 2006 Richard Waidhofer started to design & engineer around the gyrocopter technology. Since then, many international aviation and gyrocopter companies as well as startup companies have commissioned Richard Waidhofer as a consultant or design engineer for gyrocopter projects or took up his services.

 

In the year 2010 joint Dr. Ing. Hermann Künkler as worldwide renmated aviation design engineer of MBB Messerschmitt Bölkow Blohm, EADS, IABG, to the Raecon company of Richard Waidhofer. Due to the united know how of Richard Waidhofer and Hermann Künkler, the project DiNelly eXoGyro moved forward with big steps. These two brains developed and engineered over 54 innovations at the gyrocopter technologies. They calculated, simulated, engineered, together without third party. As result the eXoGyro System was set up innbound one and a half year. Due to their pathbreaking and revolutionary developed technology have recreational gyrocopter manufacturers and pilots try to steal the technology of Richard Waidhofer or copied this illegal. Also partner, employees taken against existing non disclosure agreement the technology of Richard Waidhofer. Otherwise the competitors tried to stop Richard Waidhofer and his project to defamate him with the german gyrocopter-forum.de and using lying press. When Richard Waidhofer started to sue this persons and companies 2014 a lot of projects around the world were stopped by court rulings and had to pay damages to Richard Waidhofer oder DiNelly.

INNOVATIONS | PIONEER PROJECTS | R & D PROJECTS

AT THE FFIELD OF GYROCOPTER AIRCRAFTS

AERIAL SENSING | SURVEY:

  • FIRST PROFESSIONAL AERIAL SENSING MISSION PLATTFORM
  • First AERIAL PRECISION FARMING OPERATION
  • FIRST INGERATED SOMAG MOUNT IN A GYROCOPTER
  • FIRST FLIGHT TESTS WITH SOMAG MOUNT
  • FIRST INTEGRATION OF PHASE ONE CAMERA & INFLIGHT TEST
  • FIRST INTEGRATION OF SOMAG MOUNT CSM 130
  • FIRST INTEGRATION AND INFLIGHT TEST OF SOMAG MOUNT SSM 270
  • FIRST INTEGRATION OF SOMAG MOUNT GSM 3000
  • FIRST INTEGRATION OF SOMAG MOUNT GSM 4000
  • FIRST INTEGRATION OF OPTEECH /TELEDYNE AERIAL SENSING SENSORS / C300
  • FIRST INTEGRATION OF VEXCEL IMAGING CAM SYSTEMS; XP & LP Incl DX; OSPREY; FALCON; EAGLE; CONDOR;
  • FIRST INTEGRATION OF VISIONMAO CAMERA SYSTEMS
  • FIRST INTEGRATION OF ACTIVE HYPERSPECTRAL SCANNER
  • FIRST INTEGRATION OF LIDAR – LASERSCANNER
  • FIRST INTEGRATIO OF RIEGL LASER SCANNER
  • FIRST INTEGRATION OF GAS LEAK DEDECTION SENSORS
  • FIRST INTEGRATION AN INFLIGHT TEST OF PHOTONEN CAMERA SYSTEMS
  • FIRST INTEGRATION AND INFLIGHT TEST OF SENSORIK APU FUEL CELL
  • FIRST INTEGRATION OF LFIR CAM SYSTEMS
  • FIRST INTEGRATION OF WESCAM SYSTEMS
  • FIRST INTEGRATION OF LEICA CAM SYSTEMS
  • FIRST INTEGRATION OF CINEFLEX V1HD CAM SYSTEM
  • FIRST INTEGRATION OF FMS – FLIGH MANAGEMTN SYSTEM – IN STADARD COCKPIT / GLASS DISPLAY
  • FIRST INTEGRATION AT A GYROCOPTER OF PROFESSIONAL DATA UP-DOWNLINK SYSTEM
  • FIRST AERIAL PRECISION FARMING OPERATION
  • AGRICULTURE JOHN DEERE PROJECT
  • AERIAL SENSING PFOTOGRAMMETRY
  • MIL PHOTONEN CAMERA OBSERAVATION
  • AGRICULTURE & FOREST MAPPING
  • FLIR SURVEY OPERATIONXY
  • FLIR SOLARCELL OPERATION
  • HYPERSPECTRAL SENSING OPERATION
  • POWERLINING
  • BOARDER PATROL
  • WILDLIFE SUPPORT

 

ENGINEERING:

  • FIRST INTEGRATION OF A ISO NORM STRETCHER AT UL GYROCOPTER
  • FIRST CALCULATED HIGH EFFICIENT ROTORBLADES
  • FIRST CARBON ROTORBLADES IN PULL BRAIDING TECHNOLOGY NACA8H12 PROFILE
  • FIRST 4 BLADE ROTORSYSTEM ON ONE LEVEL
  • FIRST ADJUSTABLE ROTORMAST (ADJUSTABLE CENTER OF LIFT)
  • FIRST APU FUEL CELL INFLIGHT TESTS COMPLETED
  • FIRST HIGH END LIGHWEIGHT REAL MONOCOQUE CARBON FUSELAGE
  • FIRST LOW VIBRATION ROTORSYSTEM FOR SENSING OPERATION
  • FIRST ENGINE AUTARKT HEATING SYSTEM
  • FIRST HIGH EFFICIENT ENGINE RAM AIR CHARGING SYSTEM (OPERATING WITH PROPELLER SUCTION)
  • FIRST ENGINEERED & SIMULATED V-TAIL
  • 1,6m² CARGO BAY
  • FIRST VIBRATION TESTS AT ROTORSYSTEM; FRAME; CHASSIS; SENSING MOUNT; SCIENTIFICALLY
  • FIRST GYROCOPTER WITH UP TO 3 HATCHES FOR MISSION OPERATION EQUIPMENT AT CG
  • FIRST PROFESSIONAL ENGINEERED DOUBLE ENGINE UL GYROCOPTER
  • FIRST UL GYROCOPTER WITH INTEGRATED CAN AEROSPACE AVIONIK
  • FIRST GYROCOPTER WITH INTEGRATED ROTAX 912iS INJECTION ENGINE
  • FIRST INTEGRATION OF ROTAX 915IS SUPERCHARGED ENGINE
  • FIRST MECHANICAL REDUDANT FLY BY WIRE SYSTEM AT A GYROCOPTER
  • FIRST ENERGY ABSORBING SEATS AT A GYROCOPTER
  • ROTORBLADE COVERED WITH PROTECTIVE FOIL ORACOVER / LANITZ
  • CALCULATION OF REQUIERED PRE ROTATION POWER
  • CALCULATION OF REQUIERED POWERPLANT CONFIGURATION
  • CALCULATION AND ENGINEERING OF TAIL CONFIGURATION
  • INSTALLED CALIBER .50 ABSORBING TESTS

 

NOISE REDUCTION:

  • EXHAUSTING SYSTEM
  • PROPELLER
  • ROTORSYSTEM
  • NOISE ABSORBING COWLING
  • CALCULATING AND ENGINEERING GEAR REDUCTION ACCORDING LOW NOISE PROPELLER

 

SAFETY:

  • ENERGY ABSORBING SEATS
  • HIGH PERFORMANCE LANDING LIGHT
  • RUGGEDIZED GEAR
  • AERODYNAMIC ACTIV V-TAIL
  • FUEL TANK
  • DOUBLE ENGINE VERSION
  • KOAXIAL PROPELLER VERSION
  • FUEL TANK SYSTEM VERTICAL NEXT TO THE CG – CENTER OF GRAVITY
  • AVAILABLE 4 BLADE ROTOR SYSTEM

 

GYROCOPTER AIRCRAFTS:

  • FIRST MedEvac UL GYROCOPTER
  • 4 DOOR UL GYROCOPTER
  • 1,6m² CARGO BAY
  • FIRST 5 SEATER CONFIGURATION AT A UL GYRCOPTER
  • FIRST PROFESSIONAL GYROCOPTER AS MISSION OPERATION PLATFORM
  • FIRST PROFESSIONAL ENGINEERED DOUBLE ENGINE UL GYROCOPTER
  • UG1 – GYROCOPTER MODELL (PROJECT UG-LILLY)
  • XENIA LOW BUDGET SIDE BY SIDE GYROCOPTER
  • SUPERGYRO
  • eXoGyro SYSTEM
  • CargoGyro
  • TroopTransporter GYROCOPTER
  • RECREATIONAL LOW BUDGET SINGLE SEATER
  • ARROWCOPTER PRO (AERIAL SENSING)
  • MAGNI M24 RSR (REMOTE SENSING PLATFORM)
  • ARTUR TRENDAK AVIATION XENON II - ZEN II (AERIAL SENSING PLATFORM)

 

PRODUCTION PROCESS | MATERIALS

  • FIRST ARMORED FUSELAGE ACCORDING ISO NORM
  • FIRE RESISTAND FUSELAGE / COMPOSITE PARTS
  • ISO 9100, PART 21, MANUFACTURING PROCESS
  • MOST MODERN COMPOSITE MATERIALS (MORE THAN CARBON ½ WEIGHT OF CFK

 

CLEAN SKY

  • PRODUCTION PROCESS
  • ASSEMBLING PROCESS
  • STATE OF THE ART INJECTION ENGINES
  • HIGH EFFICIENT PROPELLER
  • HIGH EFFICIENT ROTORSYSTEM
  • MATERIALS
  • EXHAUSTING SYSTEM

 

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

- FIREFIGHTING EQUIPMENT

Social Media

Facebook

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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

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