The Bell Boeing Quad TiltRotor (QTR) was a proposed four-rotor derivative of the Bell Boeing V-22 Osprey that Bell Helicopter and Boeing studied jointly as a contender in the United States Army's Joint Heavy Lift program. Bell had developed its model D-322 as a quad tiltrotor concept in 1979, and the two companies disclosed a design in 1999 for a C-130-size V/STOL transport with a payload of up to 25,000 pounds in a hover and about half its parts in common with the V-22. A tandem-wing layout put a V-22 type engine and a 50-foot rotor at each of four wing tips, with a cargo bay that could carry 110 paratroopers or 150 passengers. A 2005 Army contract funded a conceptual design study, and a one-fifth-scale model was tested in the NASA Langley Transonic Dynamics Tunnel in 2006. The study ended in May 2007, but the Department of Defense did not pursue development.
Facts
StatusDesign only (never built) 1 Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Of Make
Source Bell Boeing Quad TiltRotor (Wikipedia)
Sources
1. Bell Boeing Quad TiltRotor (Wikipedia)
Development, background, design disclosure
The Bell Boeing team disclosed a Quad TiltRotor design in 1999
Development, background, 1999 design
This design was to have a maximum takeoff weight of 100,000 lb (45,000 kg)
Lead, aircraft description
The Bell Boeing Quad TiltRotor (QTR) is a proposed four-rotor derivative of the Bell Boeing V-22 Osprey
Lead, development status
is a proposed four-rotor derivative of the Bell Boeing V-22 Osprey
Lead, builder
The Bell Boeing Quad TiltRotor (QTR) is a proposed four-rotor derivative of the Bell Boeing V-22 Osprey developed jointly by Bell Helicopter and Boeing.
In Group: Vertical Takeoff and Landing Research Aircraft, Lead, role of the aircraft
The Bell Boeing Quad TiltRotor (QTR) is a proposed four-rotor derivative of the Bell Boeing V-22 Osprey developed jointly by Bell Helicopter and Boeing.
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