Unreal Aircraft - Home

Beating Gravity - Bell Model 301 (XV-15)

Enlarge image (will open in a new window)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.


NASA XV-15 Images

Images below are from the
NASA Dryden Flight Research Center at Edwards, California

Open XV-15 gallery on NASA website

Enlarge image (will open in a new window) Enlarge image (will open in a new window) Enlarge image (will open in a new window)



NASA XV-15 Movies

(requires Quicktime - download)

NASA Dryden Flight Research Center website:
XV-15 in flight


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


___________________________________________________________


Site design and maintenance by Andrew McPhee - Macca's Stuff
©2003-2005 www.unrealaircraft.com. All rights reserved.

^ TOP OF PAGE ^

Validate HTML Validate CSS