The Bell Boeing V-22 Osprey is an
aircraft of American Air force which is designed to combine the functionality
of a helicopter AND A turboprop aircraft. The osprey is the world's first
production TILTROTOR aircraft, with one three-bladed prop rotor, turboprop
engine, and transmission nacelle mounted on each wingtip.
V22 OSPREY |
DESIGN AND FEATURES:
THE AIRCRAFT IS DESIGNED TO MEET BOTH THE CAPABILITIES OF
HELICOPTER AND TURBOPROP AIRCRAFT.
1. For Takeoff And Landing, It Typically
Operates As A Helicopter With The Nacelles vertical and rotors horizontal.
2. Once airborne, the nacelles rotate forward
90° in as little as 12 seconds for horizontal flight, converting the V-22 to a
more fuel efficient, higher speed turboprop aircraft.
3. FOR STOL (SHORT TAKEOFF AND LANDING)
rolling-takeoff and landing capability is achieved by having the nacelles
tilted forward up to 45°.
V22 OPSREY |
The V-22's two engines are connected by drive shafts to a
common center gearbox so that one engine can power both proprotors if an engine
failure occurs. However, if a proprotor gearbox fails that proprotor cannot be
feathered, and both engines must be stopped before an emergency landing. The
aircraft's autorotation characteristics are poor partly because the rotors have
low inertia.
The V-22 is equipped with integrated threat
countermeasures, terrain-following radar, forward-looking infrared sensor and
other advanced avionics systems that allow it to operate at low altitude in
adverse weather conditions and medium- to high-threat environments.
The
osprey’s Work has been split evenly between Bell and Boeing. Bell Helicopter
manufactures and integrates the wing, nacelles, rotors, drive system, tail
surfaces, and aft ramp, as well as integrates the Rolls-Royce engines and
performs final assembly. Boeing Helicopters manufactures and integrates the
fuselage, cockpit, avionics, and flight controls.
THE V-22 OSPREY
PROVIDES UNIQUE CAPABILITIES OFFERING:
·
Increased
speed because it's twice as fast as a helicopter.
·
Much
longer range resulting in greater mission versatility than a helicopter.
·
Multi-mission
capability: amphibious assault, combat support, long-range special ops
infiltration and exfiltration, transport, search and rescue, medevac, and, in
the future, tanker capability.
THE V-22 OSPREY
AIRCRAFT:
·
Can
transport 24 combat troops, 20,000 pounds of internal or up to 15,000 pounds of
external cargo using its medium lift and vertical takeoff and landing
capabilities
·
Meets
U.S. navy requirements for combat search and rescue, fleet logistics support,
and special warfare support
·
Matches
the U.S. Special operations command's requirement for a high-speed, long-range,
vertical lift aircraft
·
Can be
stored aboard an aircraft carrier or assault ship because the rotors can fold
and the wings rotate
·
Has
air-to-air refueling capability, the cornerstone of the ability to self-deploy
V22'S COCKPIT |
General Characteristics
Primary Function: Special operations forces long-range infiltration, exfiltration and resupply
Crew: Four (pilot, copilot and two flight engineers)
Power Plant: Two Rolls Royce-Allison AE1107C turbo shaft engines
Thrust: More than 6,200 shaft horsepower per engine
Wingspan: 84 feet, 7 inches (25.8 meters)
Length: 57 feet, 4 inches (17.4 meters)
Height: 22 feet, 1 inch (6.73 meters)
Speed: 277 miles per hour (241 knots) (cruising speed)
Ceiling: 25,000 feet (7,620 meters)
Maximum Vertical Takeoff Weight: 52,870 pounds (23,982 kilograms)
Maximum Rolling Takeoff Weight: 60,500 pounds (27,443 kilograms)
Armament: 1 x .50 Cal Machine gun on ramp
Range: combat radius of 500 nautical miles with 1 internal auxiliary fuel tank ; unlimited range with aerial refueling
Payload: 24 troops (seated), 32 troops (floor loaded) or 10,000 pounds of cargo Unit cost: $89 million (fiscal 2005 dollars)
Primary Function: Special operations forces long-range infiltration, exfiltration and resupply
Crew: Four (pilot, copilot and two flight engineers)
Power Plant: Two Rolls Royce-Allison AE1107C turbo shaft engines
Thrust: More than 6,200 shaft horsepower per engine
Wingspan: 84 feet, 7 inches (25.8 meters)
Length: 57 feet, 4 inches (17.4 meters)
Height: 22 feet, 1 inch (6.73 meters)
Speed: 277 miles per hour (241 knots) (cruising speed)
Ceiling: 25,000 feet (7,620 meters)
Maximum Vertical Takeoff Weight: 52,870 pounds (23,982 kilograms)
Maximum Rolling Takeoff Weight: 60,500 pounds (27,443 kilograms)
Armament: 1 x .50 Cal Machine gun on ramp
Range: combat radius of 500 nautical miles with 1 internal auxiliary fuel tank ; unlimited range with aerial refueling
Payload: 24 troops (seated), 32 troops (floor loaded) or 10,000 pounds of cargo Unit cost: $89 million (fiscal 2005 dollars)
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