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THE
DE LACKNER AEROCYCLE –
An early “Flying Platform”
One of the most
prominent concepts in military aviation in the 1950s and 1960s was the
"flying platform." These platforms were designed to carry one
combat-ready soldier to perform reconnaissance missions.
Charles H. Zimmerman,
engineer for the National Advisory Committee on Aeronautics (precursor
to NASA), proposed that if the rotors of a helicopter were placed on the
bottom of the aircraft, a pilot would be able to steer it just by
shifting his weight. This concept became known as 'kinesthetic'
control.
After initial tests by
NACA proved the idea valid, three companies developed prototypes: De
Lackner, Hiller, and Bensen.
First Test Flight of the
Aerocycle – Brooklyn Army Terminal, 1955
The HZ-1 Aerocycle was
designed by De Lackner Helicopter Company of Mount Vernon, New York.
It's first test flight was at Brooklyn Army Terminal with a combat-ready
test pilot.
The tests were
successful, and the US Army ordered twelve of these for further
evaluation.
The Aerocycle was
powered by a 4-cylinder, water-cooled 43hp Mercury outboard motor
located on a circular platform. Just under the platform were two
belt-driven, counter-rotating 15-foot rotor blades.
With a top speed of
more than 70 mph, it was faster than others evaluated by the Army.
Testing at Fort
Eustis – 1956
Captain Selmer Sundby
was the test pilot for this Aerocycle at Fort Eustis in 1956. An Army
pilot with 6 years of experience and more than 1500 hours in fixed and
rotary winged aircraft, Sundby volunteered for numerous test flights,
some lasting seconds long and one almost 43 minutes long.
Designed to require
only about 20 minutes of instruction before actual flight, Sundby said,
". . . it only took me one flight to realize that a non-flyer would have
considerable difficulty operating it."
Standing to the rear of
the center platform, secured by safety belts, Sundby used the
motorcycle-like handlebars to turn, varying the speed of the rotor
blades thereby changing torque. Lift was obtained by increasing the
rotor blade rpms.

Above, then Captain
Sundby testing the Aerocycle, 1956. |
Captain Sundby said, "I
had two accidents while testing this machine - one in free flight from
about 40 feet in the air, doing 30-35 mph, and another during tethered
flight."
"Both accidents were
similar in that the counter-rotating blades flexed and collided,
shattering the blades. This resulted in immediate loss of lift and
control." Further studies could not pinpoint the exact speed or
conditions that caused the blades to flex, and eventually the concept
was abandoned.
For his efforts, Sundby
was awarded the Distinguished Flying Cross by the Chief of Staff of the
Army in 1958.

Sundby as a lieutenant
colonel |
Of the original twelve
ordered by the Army, the only one remaining is the one on exhibit at the
Transportation Museum. |