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