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Air Force the Official Service Journal - Air Force Historical Studies ...

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R.6<br />

I:>:CJ: <strong>the</strong> AAF<br />

S helicopter, <strong>the</strong><br />

accepted<br />

Sikorsky<br />

delivery of its first successful<br />

XR--I-, in <strong>the</strong> spring of 19-1-),<br />

three new models have been added to our whirligig family.<br />

The most unllSu;l] design among <strong>the</strong> newcomers is that<br />

of <strong>the</strong> Plutt-Lcf'agc XR-I, a twin-rotor craft weighing 4,800<br />

pounds. Far from being rcadv to appear in qua ntitv, <strong>the</strong><br />

XR-I is just coming out of <strong>the</strong> experimental stage. Its<br />

couvcntionallv shaped fuselage has tandem scats with sliding<br />

canopies and <strong>the</strong> bottom of <strong>the</strong> compartments is of transparent<br />

plastic. The high stnbilizcr and rudder empennage<br />

of <strong>the</strong> tail arc similar to those of <strong>the</strong> normal airplane tail<br />

assembly. There arc no elevators,<br />

At each end of <strong>the</strong> pvlous, which project from <strong>the</strong> fuselage<br />

like \\'ings. is a three-bladed rotor, each hlacle approximately<br />

15 feet long. These rotors neutralize torque bv<br />

rotating in opposite directions. thcrcbv eliminating <strong>the</strong><br />

need for <strong>the</strong> tail rotor used on <strong>the</strong> Sikorskv-tvpc helicopters.<br />

A -I-50-hp Pratt and \\'hitnev radial engine powers <strong>the</strong><br />

XR-l. /\lthough ordered earlier than <strong>the</strong> first experimental<br />

R-4, <strong>the</strong> XR-l was not succcssfullv flight tested until <strong>the</strong><br />

summer of 19-1-).<br />

An improved version of <strong>the</strong> original R--1-helicopter has<br />

been designated <strong>the</strong> R-b. The "Six" looks like an 0\'('[sized<br />

squash gourd with rotors and wheels. The square<br />

corners of <strong>the</strong> R--I- h;l\c been eliminated in its successor.<br />

A small nosc-who;-] protects <strong>the</strong> plexiglas nose of <strong>the</strong> craft.<br />

O<strong>the</strong>r new materials used in <strong>the</strong> R-b include a paper-based<br />

cowling that encloses <strong>the</strong> engine and rotor shaft. The cabin<br />

is constructed of plastic impregnated glass fiber cloth. The<br />

OCTOBER,1944<br />

OUR NEW HELICOPTERS<br />

slender tail cone has a covering of tough magnesiulll skin.<br />

Powered with a 2-1-5-hp Franklin six-cvlindcr horizontullvopposed<br />

engine, <strong>the</strong> R- ') has a top speed in excess of I rio<br />

mph, a normal useful load capacity of approximutclv half a<br />

ton and can climb to 5.900 feet in less than seven minutes.<br />

E\'aeuation litters can be installed on each side of <strong>the</strong><br />

fuselage. Pilots and observer sit sidc-bv-sidc.<br />

The R-,) helicopter is <strong>the</strong> big bro<strong>the</strong>r of <strong>the</strong> "Six." In<br />

configuration <strong>the</strong> craft resembles <strong>the</strong> R-b and R--I- helicopters,<br />

having one main three-bladed rotor and a vertical<br />

tail rotor. The main rotor is <strong>the</strong> largest ever built. measuring<br />

-1-8feet across <strong>the</strong> disc. The R-S's nine-evlinder aircooled<br />

Pratt and \\-hitnev engine den-lops -I-50-I;p.<br />

Fuselage of <strong>the</strong> R-:; measures approximately 40 feet<br />

from nose to tail. It is built in three sections. The center<br />

section. supportiug <strong>the</strong> eugine. is made of welded steel<br />

tubing, cowlcd with plastic-impregnated molded plywood.<br />

The tail section is a wooden monoeoque cone to snpport<br />

<strong>the</strong> tail rotor. A long shaft atop <strong>the</strong> cone's exterior is geared<br />

to <strong>the</strong> engine for turning <strong>the</strong> solid wood, seven-foot blades<br />

of <strong>the</strong> vertical rotor. The nose section is an aluminum .rllov<br />

channel superstructure mounted on an aluminum mOJ1(jcoque<br />

floor. This forward section houses <strong>the</strong> plexiglas-enclosed<br />

cabi».<br />

The R-,) has a convcnt ional landing gen. The observer<br />

sits in <strong>the</strong> nose with <strong>the</strong> pilot directly behind him. Stick<br />

and rudder controls arc dual. Space is available for cameras,<br />

radio accessories and o<strong>the</strong>r auxiliarv equipment in cockpits.<br />

Four litters, two on a side, em he carried hy <strong>the</strong> R-5. * 53<br />

..•

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