Imagine a new airliner design that has slower, safer take off and approach speeds yet can fly at Mach .95 with little drag. Imagine an airliner that takes the engines away from the wings and places them out of the way of bird strikes at the tail of an advanced airfoil body. Imagine a plane that can carry twice the load yet get the same fuel economy as others with 1/2 this load. Now imagine your airfare actually going down.
Not possible? Actually, the design has been around since the early 60's jet age. Propeller designs go back even further. With today's improvements in engine design, materials and advanced airfoil design, this plane is entirely possible. It has even been compared to NASA's X-43 hypersonic designs.
Composites capable of holding pressure in any shape - PRSEUS - Proven structural integrity 2015.
Supercritical airfoil design, high speed, low drag, improved fuel economy - Proven mid-70's.
Lifting fuselage design, higher load capacity, stability and safety - Proven in flight testing 1920's thru' 1950's.
References:
Composites - http://www.compositesworld.com/articles/prseus-update-hybrid-wing-body-passenger-cabin-takes-shape
Supercritical Airfoil Design - https://en.wikipedia.org/wiki/Richard_T._Whitcomb
Lifting Fuselage - http://www.burnelliaircraft.com/
http://www.meridian-int-res.com/Aeronautics/Burnelli.htm
Advanced Design - http://www.meridian-int-res.com/Aeronautics/Burnelli_AIAA.pdf
This aircraft will out perform all tube and wing designs and even rival and, in some cases, exceed the performance the BWB or HWB Hybrid Wing Body all for lesser cost in manufacturing and complexity. This is the future of large aircraft be it airliners, cargo planes, military transports, bombers or fuel tankers. Join me in promoting the greatest design in aviation history that promises savings in production, fuel costs and pollution as well as reduced air traffic and a marked increase in comfort and safety.
I'm workin' on it.
Video
Voting
-
ABOUT THE ENTRANT
- Name:Larry Pope
- Type of entry:individual
- Software used for this entry:CAD
- Patent status:none