|
Beating Gravity - Bell Model 301 (XV-15)
Bell,
having considerable experience in rotary-wing and tilt-rotor aircraft, was selected
in 1973 as a prime contractor for a research program to prove the operational
practicality of the tilt-rotor concept. The program was launched by the US Army's
Air Mobility Research and Development Laboratory and NASA.
Drawing on their experience with the Bell Model 200,
the Model 301 was developed. Further funding in the later 1970s allowed construction
of two XV-15 prototypes. The first XV-15 prototype flew on 3rd May, 1977. After initial trials in VTOL
mode it was used for wind-tunnel tests. The second prototype first flew in April 1979, and achieved the XV-15's first
free-flight transition between vertical and horizontal flight that July.
The aircraft's layout was more or less conventional; a streamlined fuselage with
tricycle undercarriage, high-mounted cantilever wing, and an upswept tail unit
with endplate vertical surfaces. Advanced proprotors were located on swivelling
nacelles at the wing tips. These nacelles housed individual turboshaft engines.
Tranverse cross-shafting enabled either engine to drive both rotors in the event
of single-engine failure.
The design provided for vertical takeoff and a 12-second transition to wing-borne
forward flight as the proprotors tilted through 90 degrees. The XV-15 program was very successsful, and provided a sound background for development
of the Osprey and other subsequent VTOL aircraft.
| Bell Model 301 (XV-15) data: |
POWERPLANT:
Two Avco Lycoming LTC1K-4K
turboshafts, each rated at
1,550 shp (1156
kW).
MAX. TAKEOFF WEIGHT:
13,000 lb (5897 kg)
PAYLOAD:
Up to nine passengers, or freight.
SPAN:
57 ft 2 in (17.42 m) overall,
35 ft 2 in (10.72 m) including nacelles.
PROPROTOR DIAM.:
25 ft. 0 in (7.62 m)
LENGTH:
47 ft 1 in (12.83 m)
HEIGHT:
15 ft 4 in (4.67 m) |
MAXIMUM SPEED:
382 mph (615 km/h)
at 17,000 ft (5180 m)
CRUISING SPEED:
349 mph (581 km/h)
at 16,300 ft (4970 m)
INITIAL CLIMB:
3,150 ft (960 m) per min.
SERVICE CEILING:
29,000 ft (8840 m)
HOVERING CEILING:
10,500 ft (3200 m) in ground effect,
8,650 ft (2635 m) out of
ground effect
OPERATIONAL RANGE:
512 miles (825 km) |
More 301 (XV-15) links:
http://avia.russian.ee/vertigo/bell_xv-15-r.html
|