Boeing Vertol YUH-61

YUH-61

Boeing Vertol YUH-61A
Role	Utility transport helicopter
Manufacturer	Boeing Vertol
First flight	29 November 1974
Status	Program terminated
Primary user	United States Army
Number built	3

The Boeing Vertol YUH-61 (company designation Model 179), was a twin turbine-engined, medium-lift, military assault/utility helicopter. The YUH-61 was the runner-up in the United States Army Utility Tactical Transport Aircraft System (UTTAS) competition in the early 1970s to replace the Bell UH-1 Iroquois helicopter. At the end of the flyoff program, Sikorsky Aircraft was awarded a contract to develop and build its UH-60A entry.

Development

Under a contract awarded in August 1972, Boeing Vertol designed and delivered three prototypes to compete UTTAS program.^[1] When Boeing Vertol failed to win the Army competition, it pinned its hope on winning civil orders and the US Navy's LAMPS III program. In the end, a variant of the Sikorsky design, the SH-60B, won the Navy contract, and the civil orders received were canceled.^[1]

Three aircraft were built and a further two were cancelled and not completed. An attack helicopter design, using the YUH-61's dynamic system (engines, rotor systems and gearboxes), was proposed for the Advanced Attack Helicopter competition, much as the dynamic system of the earlier UH-1 Iroquois had been adapted into the AH-1 Cobra gunship, but did not make the downselect that resulted in the Bell YAH-63 and Hughes YAH-64 being built. The Boeing Vertol AAH design was unique in that the crew were seated in a laterally staggered tandem configuration.^[2]

Design

The YUH-61 was designed to meet the UTTAS requirements for improved reliability, survivability and lower life-cycle costs, resulting in features such as dual-engines with improved hot and high altitude performance, and a modular design (reduced maintenance footprint); run-dry gearboxes; ballistically tolerant, redundant subsystems (hydraulic, electrical and flight controls); crashworthy crew (armored) and troop seats; dual-stage oleo main landing gear; ballistically tolerant, crashworthy main structure; quieter, more robust main and tail rotor systems; and a ballistically tolerant, crashworthy fuel system.^[3]

Transport aboard the C-130 limited the UTTAS cabin height and length.^[4] This also resulted in the main rotor being mounted very close to the cabin roof.

While Sikorsky chose a fully articulated rotor head with elastomeric bearings, Boeing Vertol chose a rigid main rotor design, based upon technology supplied by MBB, which was partnered with Boeing Vertol at the time.^[5] Boeing Vertol also selected to use a tricycle landing gear and a pusher tail rotor, as opposed to the tail wheel configuration and canted tractor tail rotor that Sikorsky chose, meaning that the thrust produced by the tail rotor was directed away from the vertical stabilizer, while the Sikorsky's flowed around it. Not to be confused with a pusher propeller used for forward propulsion, as used in some helicopters and airplanes).

Variants

Model 237: naval version of the YUH-61 for the USN's LAMPS II competition (ship-based multi-purpose helicopter) and lost out to Sikorsky SH-60 Seahawk; no models built
Model 179: civilian 14–20 passenger utility helicopter later canceled; 1 model built

Survivors

Two of the three aircraft (73-21656 and 73-21658) built are preserved at the United States Army Aviation Museum in Fort Rucker, Alabama.

Specifications (YUH-61A)

Data from Modern Military Aircraft^[1]

General characteristics

Crew: Minimum 2 pilots
Capacity: 14–20 passengers
Length: 60 ft 8.5 in (18.504 m)
Height: 15 ft 6 in (4.72 m)
Empty weight: 9,750 lb (4,423 kg)
Max takeoff weight: 17,700 lb (8,029 kg)
Powerplant: 2 × General Electric T700 turboshaft engines, 1,536 hp (1,145 kW) each
Main rotor diameter: 49 ft (15 m)
Main rotor area: 1,885 sq ft (175.1 m²)

Performance

Maximum speed: 155 kn; 286 km/h (178 mph)

References

1 2 3 Gunston, Bill: The Illustrated Encyclopedia of the World's Modern Military Aircraft, page 205. Crescent Books, New York, NY USA, ca. 1978. ISBN 978-0-517-22477-9
↑ http://www.helis.com/h/bo_aah.jpg helis.com, Retrieved: June 14, 2011.
↑ Leoni 2007, pp. 42–48.
↑ Leoni 2007, pp. 39, 42–43.
↑ Leoni 2007

Bibliography

Leoni, Ray D. Black Hawk, The Story of a World Class Helicopter. American Institute of Aeronautics and Astronautics, 2007. ISBN 978-1-56347-918-2.

External links

Wikimedia Commons has media related to Boeing Vertol YUH-61.

UTTAS program—YUH-61 origins

Boeing Vertol/Boeing Helicopters/Boeing Rotorcraft

Transport rotorcraft	CH-46/BV 107 CH-47/Model 234/Chinook HC Model 360 YUH-61 XCH-62 V-22

Attack/reconnaissance helicopters	ACH-47A AH-64/WAH-64 RAH-66 MELB/AH-6

United States helicopter designations, Army/Air Force and Tri-Service systems

Numerical sequence used by USAAC/USAAF/USAF 1941–present; US Army 1948–1956 and 1962–present; US Navy 1962–present

Main sequence
(1941–1962)

Prefix R-, 1941–1948	R-1 R-2 R-3 R-4 R-5 R-6 R-7 R-8 R-9 R-10 R-11 R-12 R-13 R-14 R-15 R-16

Prefix H-, 1948–1962	H-5 H-6 H-9 H-10 H-11 H-12 H-13/J H-15 H-16 H-17 H-18 H-19 H-20 H-21 H-22 H-23 H-24 H-25 H-26 H-27 H-28 H-29 H-30 H-31 H-32 H-33 H-34 H-35 H-36¹ H-37 H-38¹ H-39 H-40 H-41 H-42 H-43 H-44¹ H-45¹

Main joint sequence
(1962–present)

1962 redesignations	OH-13/UH-13J UH-19 CH-21 OH-23 UH-25 CH-34 CH-37 HH-43

New designations	CH-46/HH-46/UH-46 CH-47 UH-48 XH-49 QH-50 XH-51 HH-52 CH-53/HH-53/MH-53/CH-53E/CH-53K CH-54 TH-55 AH-56 TH-57 OH-58 XH-59 UH-60/SH-60/HH-60/HH-60J YUH-61 XCH-62 YAH-63 AH-64 HH-65 RAH-66 TH-67 MH-68 H-69¹ ARH-70 VH-71 UH-72 H-73 to H-89¹ MH-90 H-91¹ VH-92

1962 redesignations
reusing old numbers

¹ Not assigned

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