BELL DESIGNS INNOVATIVE COMPOUND HELICOPTER CONCEPT FOR
LOCKHEED MARTIN UCAR PROGRAM
OWEGO, NY, September 27, 2004
Bell Helicopter, a key member of the Lockheed
Martin Unmanned Combat
Armed Rotorcraft (UCAR) team,
has successfully completed preliminary design of a novel air
vehicle to conduct reconnaissance and combat missions
without sending aircrews into harm's way.
During a two-year, multimillion dollar effort
funded by the Defense Advanced Research Projects Agency (DARPA)
for the U.S. Army, Bell analyzed 13 concepts from advanced,
slowed rotor helicopters through very high-speed vertical
takeoff and landing (VTOL) fan-in-wing configurations. Bell
chose a heavy fuel advanced compound helicopter concept to
obtain efficient vertical lift and speed capabilities in
excess of 170 knots. The 5,500 pound gross weight aircraft
is designed to meet emerging Army hot-day performance
requirements of 6,000 feet altitude on a 95 degree-day
Fahrenheit and still maintain a capability to climb at 500
feet per minute and an altitude ceiling of 18,600 feet. This
was accomplished while staying inside the structural limits
normally associated with all types of rotorcraft and using
turbine engine fuel available on the battlefield such as
JP-5, JP-8 and diesel.
“We are delighted with the advanced technical
achievements of this design. It will revolutionize the
helicopter industry for years to come,” said Mike Redenbaugh,
chief executive officer of Bell Helicopter in Fort Worth,
TX. “In today’s world, protection of U.S. interests at home
and abroad are paramount and this system fills a gap in our
strategic and tactical systems. It is an honor to serve the
U.S. Army in this way,” Redenbaugh added.
The main rotor concept is an advanced rotor
with cambered blades, a product of Bell’s 60 years
experience in producing high performance, safe rotor
systems. The Propulsive Anti-Torque System (PATS) is a
technically advanced, high-bypass propulsion system within
the tail cone that provides an anti-torque capability
comparable to modern helicopter designs, with the added
synergistic benefit of forward propulsive thrust. This
provides the benefit of compounding without the weight
penalties normally associated with compound helicopters.
The
concept also provides high levels of safety, as there is no
exposed rotating tail rotor. Absence of a tail rotor and
slowed main rotor contribute to achieving significantly
lower noise levels and vastly improved survivability
attributes over standard helicopters. Bell considered using
a turbocharged internal combustion engine to achieve an even
greater endurance than the maximum nine hours, but found
that the empty weight penalties associated with these
concepts outweighed the advantages.
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“Our design simplicity, use of man-rated
helicopter components and specifications, combined with our
fully integrated redundant flight control system provides a
significant improvement in performance, safety and
reliability compared to standard UAV systems with single
thread or nonintegrated dual redundant flight control
systems,” said Charles H. Jacobus, director of Advanced
Technology Programs for Bell.
The Lockheed Martin UCAR team
includes Lockheed Martin Systems Integration – Owego,
Lockheed Martin Aeronautics Company Advanced Development
Programs, Lockheed Martin Advanced Technology Laboratories,
Lockheed Martin Simulation and Training Systems, Lockheed
Martin Missiles and Fire Control, Bell Helicopter, a Textron
company, Raytheon Company, the Charles Stark Draper
Laboratory, Whitney, Bradley & Brown, L-3 Communications,
DRS Technologies and Harris Corporation.
Headquartered in Bethesda, MD, Lockheed Martin employs about
130,000 people worldwide and is principally engaged in the
research, design, development, manufacture and integration
of advanced technology systems, products and services.
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Media
Contacts:
Jan
Gottfredsen, Lockheed Martin, (607) 751-2598; e-mail,
janet.gottfredsen@lmco.com
For additional
information, visit our websites:
http://www.lockheedmartin.com
http://www.bellhelicopter.textron.com
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