IO Aircraft - Chippewa 350 14 Passenger VTOL Fixed Wing Aircraft

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Chippewa 350 - 14 Passenger Medium Lift VTOL Fixed Wing Aircraft

 

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Passengers:

14 Commercial

21 Military
Total Length: 45'

Total Span:

38' 5"

Power:

2 X U-GTG Turbine (H2/Kero)

88 X 2.5KW Fuel Cells

Motors:

4 X Super Magnetic Graphene Based

Range:

1,000+ NM Kero or H2 Exclusively

2,000 NM, Both Simultaneously

Performance:

 

350 KT Cruise

Safety:

 

Aircraft also equipped with a BRS (Ballistic Recovery System)
  Estimate Price in Production $8 Million Fly Away Price

 

Chippewa 350 - 14 Passenger Medium Lift VTOL Fixed Wing Aircraft

21 Passenger in Military Configuration

 

*This aircraft design is not a graphics concept, but ready to be built and begin certification processes leading into serial production

 

This aircraft is designed as a super vtol medium lift. In the class of UH-60 Blackhawk's and the new Sikorsky V-280, except in military configuration double the capacity and a smaller footprint and substantially heavy passenger lift capabilities, along with a rear payload door.  This is not really a concept, since we have developed all the technologies incorporated into this aircraft and is ready to be built and go into serial production.

The rotors on this aircraft are not props, but articulating, and able to cycle through Mach 2 blade tip speeds with elimination of the supersonic shock entirely.  Instead of the "chop" it is just a "woosh" so to speak. As the aircraft transitions to forward flight, rotor velocity reduces to subsonic since loads are reduced dramatically.

Control surface on the wings are not hinged, but wing warping surfaces with precision control, allowing for advanced flow of the air stream for optimized performance.

The entire airframe for this aircraft is produced using GRAPHENE which is 33X stronger then titanium but 1/50th the weight, it is also bulletproof. The entire airframe stripped, could be lift by hand from 1 person. Overall, the aircraft weight far less then another aircraft it's scale.

Motors for this aircraft are highly proprietary, but are graphene based as well, which is 10-20 times more conductive then copper, which means the motors for this aircraft have a minimum of double the shaft horsepower vs others it's size.  Also, each nacelle is 2 motors, ensuring if failure ocurrs with one motor, the other motor takes up the load.

The turbines for this aircraft are called U-GTG aka Unified Gas Turbine Generators, that are also thrust producing. This is also highly proprietary, but the entire core of the turbines are the generators, not operating under shaft to generators.  The nozzles also transition for VTOL operations.

Turbines can operate on Compressed Hydrogen or Kero, or a combine of both simultaneously.
 

 

*Commercial Version Only, can be configured for Fuel Cell only, turbines removed and replaced with additional hydrogen fuel cells, for very quiet operation

 

  • Folding Wings for minimal ground footprint when parked or stored, including maritime operations

  • Rear Payload Door

  • 6 - 9 Stretchers Configured for Medivac

  • Graphene Airframe (lower costs then aluminum, 33X stronger then Titanium, 1/50 the weight

  • Dual Kero and Hydrogen Fueled, can operate on either, or both

  • If turbine failure occurs then the 88 Fuel Cell Stacks provides several minutes to land safely, or vice/versa

  • Ballistic Recovery System Built In.

  • Advanced fly by wire system providing high performances capabilities

 

  • Can land and take off in STOL configuration with the wing rotated from 30-45°, which means it can land in forward flight at only 30-40 KTS, or vertically land.
     

Because of the Graphene airframe composition and High Pressure H2 tanks; this aircraft in maritime operations cannot sink, if catastrophic failure occurs, resulting in impact with water or ditching the aircraft remains boyant.

 

 

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