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Quad TiltRotor (QTR) aircraft development contract awarded
By Mike Hanlon
September 23, 2005
6 Pictures
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Quad TiltRotor (QTR) aircraft development contract awarded
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September 24, 2005 The team of Bell Helicopter and Boeing has been awarded a $3.45 million contract by the U.S. Army to perform conceptual design and analysis of its Quad TiltRotor (QTR) aircraft for the Joint Heavy Lift (JHL) Program. "The Bell Boeing team is exceptionally pleased to have been one of the teams chosen by the Joint Service Team to take the first step in providing a truly transformational vertical lift cargo aircraft," said Mike Redenbaugh, chief executive officer of Bell Helicopter. "The critical need for long range, high speed, heavy lift without access to runways is being highlighted around the world every day."
"We view this as an important first step toward defining the next generation of high-speed, heavy-lift rotorcraft," said Ron Prosser, Boeing Phantom Works vice president and general manager of Integrated Defense Advanced Systems. "This Bell Boeing effort is a great opportunity to demonstrate the utility of cutting edge technology in meeting joint service needs."
Bell Boeing's QTR is an evolutionary application of its tiltrotor technology utilized in the V-22 Osprey. The QTR is a tandem-wing, four-proprotor aircraft with a large cargo fuselage and a rear-loading ramp. Four turboshaft engines, each mounted in one of four tilting wingtip nacelles, power the proprotors through interconnected transmissions for redundancy.
The QTR design will be sized, refined and analyzed over the next 18 months to determine program requirements and feasibility of further development. Bell Helicopter , a subsidiary of Textron Inc., is a leading producer of commercial and military helicopters and the pioneer of the revolutionary tiltrotor aircraft.
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Bell developed its model D-322 as a quad tiltrotor concept in 1979. The Bell Boeing team disclosed in 1999 a Quad TiltRotor design the companies had been investigating for the previous two years. The design was for a C-130-size V/STOL transport for the US Army's Future Transport Rotorcraft program and would have 50% commonality with the V-22. This design was to have a maximum takeoff weight of 100,000 lb (45,000 kg) with a payload of up to 25,000 lb (11,000 kg) in a hover.[2][3] The design was downsized to be more V-22-based and to have a payload of 18,000 to 20,000 lb (8,200 to 9,100 kg). This version was referred to as "V-44".[2][4] Bell received contracts to study related technologies in 2000. Development was not pursued by the US Department of Defense.[2]
During 2000-06, studies of the aerodynamics and performance of a Quad Tilt Rotor were conducted at the University of Maryland, College Park. This effort was initially funded by NASA/AFDD and subsequently by Bell. An experimental investigation in helicopter mode with ground effect found that it was possible to reduce the download on the aircraft from 10% of the total thrust to an upload of 10% of the thrust.[5] A parallel Computational Fluid Dynamics (CFD) study confirmed these findings.[6]
Joint Heavy Lift studies
In September 2005 Bell and Boeing received a cost-sharing contract worth US$3.45 million from the U.S. Army's Aviation Applied Technology Directorate for an 18-month conceptual design and analysis study lasting through March 2007, in conjunction with the Joint Heavy Lift program.[7][8] The contract was awarded to Bell Helicopter, which is teaming with Boeing's Phantom Works. The QTR study is one of five designs; another of the five is also a Boeing program, an advanced version of the CH-47 Chinook.[1]
During the initial baseline design study, Bell's engineers are designing the wing, engine and rotor, while the Boeing team is designing the fuselage and internal systems.[9] A similar arrangement is used on the V-22
By Mike Hanlon
September 23, 2005
6 Pictures
Tweet

Quad TiltRotor (QTR) aircraft development contract awarded
Image Gallery (6 images)
September 24, 2005 The team of Bell Helicopter and Boeing has been awarded a $3.45 million contract by the U.S. Army to perform conceptual design and analysis of its Quad TiltRotor (QTR) aircraft for the Joint Heavy Lift (JHL) Program. "The Bell Boeing team is exceptionally pleased to have been one of the teams chosen by the Joint Service Team to take the first step in providing a truly transformational vertical lift cargo aircraft," said Mike Redenbaugh, chief executive officer of Bell Helicopter. "The critical need for long range, high speed, heavy lift without access to runways is being highlighted around the world every day."
"We view this as an important first step toward defining the next generation of high-speed, heavy-lift rotorcraft," said Ron Prosser, Boeing Phantom Works vice president and general manager of Integrated Defense Advanced Systems. "This Bell Boeing effort is a great opportunity to demonstrate the utility of cutting edge technology in meeting joint service needs."
Bell Boeing's QTR is an evolutionary application of its tiltrotor technology utilized in the V-22 Osprey. The QTR is a tandem-wing, four-proprotor aircraft with a large cargo fuselage and a rear-loading ramp. Four turboshaft engines, each mounted in one of four tilting wingtip nacelles, power the proprotors through interconnected transmissions for redundancy.
The QTR design will be sized, refined and analyzed over the next 18 months to determine program requirements and feasibility of further development. Bell Helicopter , a subsidiary of Textron Inc., is a leading producer of commercial and military helicopters and the pioneer of the revolutionary tiltrotor aircraft.
===============
Bell developed its model D-322 as a quad tiltrotor concept in 1979. The Bell Boeing team disclosed in 1999 a Quad TiltRotor design the companies had been investigating for the previous two years. The design was for a C-130-size V/STOL transport for the US Army's Future Transport Rotorcraft program and would have 50% commonality with the V-22. This design was to have a maximum takeoff weight of 100,000 lb (45,000 kg) with a payload of up to 25,000 lb (11,000 kg) in a hover.[2][3] The design was downsized to be more V-22-based and to have a payload of 18,000 to 20,000 lb (8,200 to 9,100 kg). This version was referred to as "V-44".[2][4] Bell received contracts to study related technologies in 2000. Development was not pursued by the US Department of Defense.[2]
During 2000-06, studies of the aerodynamics and performance of a Quad Tilt Rotor were conducted at the University of Maryland, College Park. This effort was initially funded by NASA/AFDD and subsequently by Bell. An experimental investigation in helicopter mode with ground effect found that it was possible to reduce the download on the aircraft from 10% of the total thrust to an upload of 10% of the thrust.[5] A parallel Computational Fluid Dynamics (CFD) study confirmed these findings.[6]
Joint Heavy Lift studies
In September 2005 Bell and Boeing received a cost-sharing contract worth US$3.45 million from the U.S. Army's Aviation Applied Technology Directorate for an 18-month conceptual design and analysis study lasting through March 2007, in conjunction with the Joint Heavy Lift program.[7][8] The contract was awarded to Bell Helicopter, which is teaming with Boeing's Phantom Works. The QTR study is one of five designs; another of the five is also a Boeing program, an advanced version of the CH-47 Chinook.[1]
During the initial baseline design study, Bell's engineers are designing the wing, engine and rotor, while the Boeing team is designing the fuselage and internal systems.[9] A similar arrangement is used on the V-22

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