BASIC DESIGN / ASSEMBLY PARAMETERS
Throughout the aviation community, opinions concerning the best
design approaches are often widely divergent, but there is no disagreement
about the pre-eminence of Safety. And Safety most certainly characterizes
SPORT COPTER designs. For instance, our airframes are completely
triangulated horizontally, vertically and longitudinally with large
diameter-tubing and high-tensile clevises, making them the strongest
gyrocopters in production. Our horizontal/vertical tail assemblies
are big, because that makes our machines stable and controllable.
Likewise, our landing gear is wide-stance and our suspension systems
are specially crafted and combined with the lowest-possible center
of gravity, for maximum stability and controllability. In fact,
the vast majority of what you are going to be reading is about what
we've done to make our machines the most stable, most controllable,
most predictable and therefore the safest in the industry, both
on the ground and in the air.
Recently, there has been a great deal of discussion concerning
High-Profile versus Low-Profile gyrocopter designs, specifically,
the difference between the engine thrust-line and the aircraft's
center of gravity, and the effect this has upon stability under
certain flight conditions. Having built gyrocopters since the mid-fifties,
and having tested them exhaustively in virtually every parameter,
we at SPORT COPTER are truly proud of the handling characteristics
of our machines. We know from long experience that our copters are
stable and forgiving, and they exhibit no penchant for nasty surprises,
such as the problem addressed by the High/Low Profile controversy.
We simply have the best ground and flight characteristics available
on any production gyrocopter.
We also know beyond doubt that a low center of gravity is essential
for safety and stability on the ground, especially when it is obviously
not creating any problems in flight, so that's how we designed our
machines: low to the ground, with wide, beefed-up gear suspension.
. . That's just plain good engineering sense, and it's a big help
when entering and exiting a gyrocopter. These factors are described
in more detail further along in this document.
There is another trait that distinguishes SPORT COPTER designs:
There is no attempt to remain "married" to any one material
or construction practice. Whatever configuration or material is
deemed best for the job is what is selected. For example, the tail
assembly is a riveted aluminum monocoque structure, while the basic
fuselage members are large-diameter aluminum tubing, the cabin enclosure
is molded composite and the fuel tank is one-piece high impact rotor-mold,
specially built for us. By contrast, there are many other aircraft
in production that use the same material and construction methods
for every one of those components, just for the sake of simplicity.
Again, whereas on many gyros you will often find comparatively primitive
construction and less-than-optimum materials used for critical control
and rotor assemblies, SPORT COPTER components are precisely machined
from the finest alloys. It is no exaggeration to say that the engineering,
materials, machining and finish of our components would do justice
for any military aircraft.
While there is no question that the new SPORT COPTER series is
more sophisticated than any gyrocopters now in existence, an essential
part of the sophistication is the fact that they are designed for
total "bolt-together" assembly. This means two things:
1) The time and tools required for assembly are reduced to absolute
minimums. 2) The possibility for errors during kits assembly is
reduced to absolute minimums.
STABILIZED MASS-LOADING AND
ROTORHEAD GEOMETRY
Our airframes are superior to any other gyrocopters flying today.
They're highly versatile and they can accept a variety of engines.
Their geometry allows better flight control, preventing the "rocking"
motion commonly associated with gyrocopters in low-speed flight.
The solution to this problem was actually conceived back in the
late 1950's by Chuck Vanek. He redistributed the geometry and mass-loading
of his airframes, and this company was the first to market this
innovative design.
Here is how it works: The main axle is moved further rearward from
the center of gravity and the pilot's position is moved farther
forward from the center of gravity. During take-off, as the main
rotor is winding up and approaching lift speed, the re-distributed
mass-loading stabilizes the main keel of the aircraft, preventing
rocking back and forth. This eliminates the "porpoising"
tendency so often exhibited by ordinary gyrocopters during take-offs,
landings and slow-flight operations. The improved geometry also
greatly diminishes pilot work-load by requiring far fewer vertical
corrections.
There's yet another very effective geometric refinement to be found
on all new SPORT COPTER rotorheads: The rearward limit of rotorhead
tilt has been increased by several degrees, meaning that the pilot
can tilt the rotor disc farther aft to achieve a more level touch-down
attitude at a complete stop.
SUSPENSION SYSTEM
NOSEWHEEL DESIGN - On most gyros, the nosewheel
and rudder are interconnected, which creates an inherent problem
for cross-wind take-offs and landings: Exceedingly low take-off
and touch-down speeds are true hallmarks of gyrocopter performance;
however, in cross-wind situations, a low forward speed makes any
cross-wind component potentially destabilizing if the nosewheel
is not aligned with the aircraft's actual path when contacting the
ground. With an interconnected nosewheel and rudder, the alignment
of the nosewheel is dictated solely by the position of the rudder,
which means that in typical cross-wind maneuvers (such as forward
slips, pilot-induced aerodynamic skids or "crabbed" lift-offs
and touch downs) the rudder-and therefore the nosewheel-will not
be aligned with the actual ground path, which can result in the
classic ground-loop.
We have an independent system: First, our nosewheel is free-castoring,
so it aligns itself instantly upon ground contact, eliminating any
tendency to ground-loop. Second, our nosewheel features an ingenious
high-viscosity shimmy-dampening system which provides unsurpassed
stabilization at all speeds. Third, our nosewheel uses double swing-arm
suspension with twin-impact compression bosses (which are actually
an integral component of the shimmy-dampening system) giving SPORT
COPTER unrivaled stability and controllability-even at high speeds
and over very rough terrain. In short, our nosewheel system design
is amazingly simple and effective. . . and the only one of its kind.
Finally, there is the matter of steering a SPORT COPTER on the
ground with a free-castoring nose wheel. Traditionally, non-steerable
nosewheels have displayed rather demanding taxiing characteristics,
but in the case of the SPORT COPTER series, steering is easy and
smooth. There are three primary reasons for this:
1) The high-viscosity anti-shimmy mechanism defeats the "hunting"
tendency of a free-castor to amplify or over-steer answers to steering
inputs. The viscosity mechanism instantly "brackets" all
steering commands.
2) Primary steering input is accomplished by independent toe-operated
hydraulic disk brakes, integrally mounted with the rudder pedals
(all four pedals in the two place model). These brakes are thoroughly
effective and show no propensity to fade.
3) It is axiomatic that for any ground vehicle, a properly-designed
steering system will seek to center itself in the absence of any
other input. The SPORT COPTER accomplishes this by a single spring-loaded
centering device which effectively maintains whatever steering input
has already been "bracketed" by the viscous damper.
The net result is not only authoritative steering, but an aircraft
that practically "nails" itself to the runway centerline
during take-offs and landings.
MAIN GEAR DESIGN - We designed
the most impressive telescoping-tripod main-suspension system ever
used on any gyrocopter. It features a unique and ingenious series
of high-impact polymer shock-pads in linear configuration. This
feature alone enables SPORT COPTER to negotiate rough terrain with
amazing stability. Incoming compression spikes are simultaneously
distributed to and absorbed by each polymer unit. The remarkable
virtue in this design lies in the fact that dividing what would
ordinarily be one large shock pad into several individual units
results in an astonishing increase in spike absorption on the magnitude
of better than two-to-one, with absolutely no increase in size or
weight.
Even the strut-rebound design exhibits great attention to detail
and reliability, especially when considered in the light of generally-accepted
industry standards. It's completely enclosed within the upper strut
(safely removed from the elements) and it comprises Teflon bushings
and stainless steel bolts and carriers, where one would normally
expect to find ordinary aircraft steel bolts and aluminum bushings.
The bottom-line of these design innovations is an aircraft that
can sustain realistic, maintenance-free operations from rough fields,
and take truly awesome vertical impacts in stride.
PROGRESSIVE COLLAPSE
We've built special safety features into our aircraft. First, our
basic design philosophy favors time-tested materials for all critical
flight components. This means that there is no compromise in the
selection of alloys for all frame-member tubing. Exotic lighter-weight
alloys have inevitably shorter life expectancies and they're more
brittle. In the event of a hard vertical impact, brittleness is
one of the least desirable characteristics for a frame member, so
only "industry-standard" highest-quality aircraft aluminum
and steel alloys are used.
Meanwhile, a great deal of attention has been focused on seat installation,
to ensure maximum vertical impact protection. The seat bottom is
secured by four stanchions located well along the open spans of
the two upper frame members, providing yet another opportunity for
impact-absorption.
ROLL-OVER PROTECTION
The rotor mast is multi-member-triangulated, affording the strongest
frame/mast assembly in the industry. This means, for example, that
the mast can sustain a rotor strike without catastrophic failure,
an event which is typically far more structurally traumatic than
a roll-over.
All SPORT COPTER seats are provided with 4-point restraint belt
attachments for maximum survivability.
The combination of a generous wheelbase (thanks in part to the
Stabilized Geometry described earlier) a full-beam tripod main suspension
system and massive frame/mast assembly results in roll-over integrity
that far surpasses other gyrocopters, or indeed, almost any low-wing
aircraft.
CYBER SEAT
Despite the fact that we are still discussing safety features, the
new Cyber Seat calls for a separate heading, since it represents
as much a quantum leap in pilot comfort as it does in pilot protection.
Designed by Jim Vanek, it is made of composite material and lined
with a new high-impact cushion. We have been working together with
another company that developed this new cushion material. It has
been jet-sled tested to 14 G's, and is already in operational use
in seats for long-range military transport and in ejection seats
for fighter aircraft.
This remarkable cushioning material actually reconfigures itself
to the shape of the occupant without appreciably varying local pressures
against the occupant. To appreciate this characteristic, picture
lying on your side upon a conventional high-quality foam cushion:
You would of course feel much more cushion-pressure against your
shoulders and your hips than against your waist, because the shoulders
and hips represent considerably more weight and sink much deeper
into the foam, which in turn exerts more pressure against the shoulders
and hips than against the waist. Now if you were to try the same
experiment on this new high-impact material, you would discover
after a few moments that the cushion pressure against your body
feels everywhere the same.
As you can well imagine, this uniform-pressure characteristic translates
into unmatched comfort for extended periods, but even more impressive
is its ability to provide very high-impact cushioning without rebound.
Under impact, the microscopically small individual foam cells exhibit
much the same ideal crash behavior as solid-state rigid styrofoam
cells, requiring very high local pressures before collapsing without
rebound. Of course, the beauty of this new foam is that after a
few moments, it does rebound.
The Cyber Seat is now standard equipment on all SPORT COPTER models,
encapsulating the pilot with full support all the way to the top
of the helmet, and providing unmatched comfort and impact protection.
FUEL CELLS
Many small aircraft have been designed and built utilizing pilot
seats that double as fuel cells. We at SPORT COPTER believe that
although a one-piece seat/fuel cell offers attractive simplicity
and considerably lower manufacturing costs, the concept of combining
two components that ought be as far apart as possible is unacceptably
hazardous. Moreover, there are situations where it is actually desirable
for a pilot seat to partially fail upon impact, while this is certainly
never the case for a fuel cell! Apart from the obvious safety considerations
is the fact that routine spills during filling result in stained
upholstery and intractable fume-odor inside the cabin. Consequently,
our seats are completely separate from the fuel cells, which are
the finest high-impact aircraft quality roto-molded units available.
ENGINES
The "LIGHTNING" is powered by the Rotax 503, with single-carb,
2.58-to-1 gear reduction box, and B-gear drive, producing 47 horsepower
from a highly reliable, easily maintained engine.
The "VORTEX" accepts a wide variety of engines, such
as the Rotax 582, the Rotax 618 or the Subaru four-cylinder Legacy
series, to name a few.
The "SPORT COPTER 2" will be powered by the 2.2 liter,
liquid-cooled, fuel-injected Subaru Legacy engine, with the all-new
gear reduction drive unit and available turbocharging. The complete
engine package is specifically engineered for this two-place machine.
There will be dual ignition, and even a back-up system to ensure
continued fuel flow in the event of a failure in the computer which
controls the fuel injection.
ROTORHEAD DESIGN
Given the critical role of the rotorhead, incorporating refinements
into rotorhead designs is typically an evolutionary process, unlike
the occasional flashes of brilliance that characterize the development
of most other components. The term "evolutionary" implies
the subtle nature of these refinements, often leaving the designer/manufacturer
eager to display them to the public but reluctant to reveal them
to the competition. So please bear with us for the relative brevity
of this section.
SPORT COPTER has somewhat larger rotorheads than other comparable
machines because they were designed for substantially higher loads.
The large size is fairly obvious when you are standing next to one
of our machines. But when you have the opportunity, you might care
to get on a step-ladder and check out one of our rivals' rotorheads.
If you do, you won't find any of the features described here:
First, all SPORT COPTER rotorhead components have built-in, replaceable
bumper-stops (made of a new broad-temperature polymer) which protect
all moving parts from each other as they reach the limits of their
respective movement-arcs. The components of other rotorheads simply
mash into one another when they reach their arc-limits, leaving
dents, scoring and an occasional crack.
Second, the rotorhead itself is actually shock-isolated from the
aircraft by a compression-type shock-mount for the longitudinal
pivot. This isolation is achieved within the longitudinal carry-through
by means of specially-formed polymer and Teflon bushings, compressed
and mounted with machined stainless steel retainers, caps and bolts.
This results in a significant reduction in shock and vibration transfer
between the rotor and the rest of the aircraft. Both the bumper/limit-stops
and the rotorhead isolation are intelligently engineered features
found in no other gyrocopters, but in time they will almost certainly
become accepted design standards throughout the industry.
BODY ENCLOSURE
Our semi-enclosed composite body enhances both appearance and performance.
The one-piece windshield protects the pilot from adverse weather
and provides much better visibility in rain. Pilot fatigue from
pounding wind forces is eliminated, and cross-country flights are
faster, safer and much more enjoyable.
The fully enclosed heated cabin provides complete all-weather utility
and comfort, along with maximum aerodynamic efficiency and elegant
good looks.
FLIGHT CONTROL SYSTEM
In view of the host of innovative features designed into the new
SPORT COPTER series aircraft, it may be surprising to learn that
we consider the flight control system to be the single most important
advancement. To appreciate the assertion, one needs to have a reasonable
understanding of typical rotary-wing control response:
If there is any unbecoming trait that distinguishes rotary-wing
aircraft behavior from that of most fixed-wing machines, it is control
response. Apart from various "fixes" designed into large,
sophisticated helicopters, gyrocopters and helicopters usually are
quite "touchy on the controls", which is an almost universal
complaint of experienced fixed-wing pilots transitioning to rotary-wing
operations. This "over-responsiveness" has generally been
considered to be the "nature of the beast", but it is
not.
The root cause of this "over-responsiveness" lies in
the geometry of the linkage between the control stick and the rotorhead.
Virtually all gyrocopters (and small helicopters) use conventional
push-rods and standard aircraft rod-ends for this purpose. A standard
aircraft rod-end provides a very strong and stable free-gimbal connection,
similar to the human shoulder joint, but unlike a shoulder, it has
a very limited range-of-motion. Even the special High-Range rod-ends
have inadequate movement for this purpose. Owing to this limited
range-of-motion, the over-all distance of any control command must
likewise be limited, since long movements of the push-rods call
for correspondingly large changes in the connector angles, and even
the best aircraft rod-ends simply cannot accommodate such large
angle variations.
The upshot of this mechanical limitation is that since rod-end
angle variation must be kept to a minimum, a little movement has
to go a long way. In other words, small movements at the rotorhead
have to translate into fairly large movements at the control stick,
in order to have sufficient range-of-motion to go around. Consequently,
small control stick movements mean big rotorhead movements, resulting
in a touchy copter . . . and rapid linkage wear, to boot!
What SPORT COPTER conceived to deal with this classic rotary-wing
nemesis may well be its finest achievement to date: The Roto-Control.
The Roto-Control somewhat resembles a human shoulder because that
is basically how it acts. Comprised of a finely-machined, bearing-mounted
aluminum cylinder specially built to accept a standard aircraft
rod-end fitting at either end, the Roto-Control enables those two
rod-ends to act like a pair of real shoulders, with more than enough
range of motion to accommodate any control/response ratio a designer
might wish to select.
So while other gyrocopters (and most helicopters) continue struggling
with over-sensitive controls, SPORT COPTER now has a control system
that provides the response and feel of a high-performance fixed-wing
aircraft, without having added a single pound of weight! Moreover,
the Roto-Control means a SPORT COPTER is more obedient and forgiving,
dramatically easier to master and a joy to fly.
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