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History:  Helicopters | UAVs | Compound | Geeps | Heavy Lift | Future | Piasecki first

History - tandem helicopters

M O D E L   YH-16,   M O D E L   YH-16A

      In 1964, development of the H-16 was initiated in response to a U.S. Air Force requirement for a long range (1432 mi.) Rescue helicopter to pick up (1-1/2 way mission) bomber crews. The YH-16 became the largest helicopter in the world, having a rotor diameter of 82 feet and an overall length (rotors turning) of 134 feet. The fuselage was as large as that of a four-engine airliner and could accommodate three light trucks loaded through a rear ramp.

        Initially powered with two P&W R-2180-11 radial engines (each in an engine room), the YH-16 was the first twin engine helicopter. Later, the YH-16 became the world’s first twin turbine helicopter.

        The three blades in each rotor were all aluminum alloy step taper milled skins keeping a ± .002 inch tolerance through their 41 foot radius by a special process developed by Piasecki. The bonded blade was made in four pieces, with two outer skins, a honeycomb filler and a leading edge balance weight which was almost a mechanical fastener of the leading edges of the skins.

        The first flight of the YH-16 was 23 October 1953. The slow turning speed of the rotors (125 rpm) almost made the blades visible in their rotation and in-flight vibration was loping in character.

        The size of the YH-16A fit the power output of the existing 1800 HP Allison T-38 gas shaft turbine. However, the T-38 was not a free-wheeling turbine and thus not ideally suited for multi-turbine interconnection. A concept was developed to tune the two fixed shaft turbines to act in consonance. (This concept was later utilized in Air Geep II).

        The U.S. Army saw the H-16 as an answer to several of its military transport missions and joined in the project. The tall landing gear version was of particular interest since it allowed the rapid attachment of external loads or pods.

 

YH-16 frst flt (94838 bytes)

YH-16 First flight:  23 October 1953;  H.Peterson, pilot      P.Camerano, copilot

 

YH-16A frst flt (71524 bytes)

YH-16A First flight:  1955;  H.Peterson, pilot       G.Callahan, copilot

 

yh16a.gif (113068 bytes)

 

H-16 hgh lndng gear (160242 bytes)

YH-16 on high landing gear to accept the belly mounting of a detachable container

        The detachable pod could carry equipment and the troops could ride in main fuselage. In this way, both troops and their equipment could be landed simultaneously.

        The fuselage was designed with a flat bottom to permit slugging a container or other external payload thus eliminating payload swing. Various pods were designed for special functions, including a field operating room, an electronics center, and a mobile repair center.

        The YH-16A became the world’s first twin turbine helicopter and established an unofficial speed record of 166 mph in 1956.

 

Model YH-16

Mission    Rescue & Transport
Crew    3
Passengers    40 or 32 Litters
Engines    (2) P&W R 2180-11
hp    1650 each
Rotor diameter    82 ft
Fuselage length    78 ft
Weight empty    32,000 lb
Useful load    14,000 lb
Max. speed    123 mph
Cruising speed    110 mph
Range    230 miles
Ceiling with normal load    18,000 FT

Model YH-16A

Mission    Rescue & Transport
Crew    3
Passengers    40 or 32 Litters
Engines    (2) Allison YT38-A-10
hp    1,800 each
Rotor diameter    82 ft
Fuselage length    78 ft
Weight empty    22,506 lb
Useful load    11,071 lb
Max. speed    146 mph
Cruising speed    140 mph
Range    230 miles
Ceiling with normal load    19,100 ft

 

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