
| A-1 "Triad" introduction |
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| Watch the
A-1 Video Here! (2005) |
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| Photos of
the A-1 under construction (photos soon) |
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| Flying
the A-1. by Jim Poel (2004) |
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| The A-1
retires |
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The A-1 Triad
was the first Seaplane and Amphibian ever made. The name "Triad" stands
for three: Land, Air and Water. Curtiss developed the Triad for the
US Navy and, after much anxst, sold a few to them after it met their
requirements. For example: It had to carry two men aloft for two hours
and fly from the town of Hammondsport to the bluff (about ten miles up
the lake) and back. Jim Poel has flown the A-1 every year since 2003
and it is now "retired" to the museum to allow the "America" to take
center stage. More pictures and articles about the A-1 are on the way
so
check back occasionally for the updated information.
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By Jim Poel
Time Line: On June 30, 1911, Theodore
(Spuds) Ellyson became the first naval aviator when he piloted a
floatplane off Keuka Lake near Hammondsport, N.Y. The aircraft
was a Curtiss Model E pusher mounted on center float with balancing
wingtip floats. The amphibious craft was named the Triad by
it's builder Glenn Curtiss, standing for land, sea and air.
However, the Navy designated it the A-1.
The A-1 Triad which Curtiss
himself had test flown on Feb. 25, 1911, was the first seaplane to fly
in this country, the first amphibious aircraft and the first U.S. Naval
aircraft. It earned Glenn Curtiss the title of "The father of
Naval aviation".
In all, fourteen type A-1s were
built, all with different options available. The Glenn H. Curtiss
museum elected to build a reproduction of the A1 model with all the
extras. Long range fuel tank, Curtiss OX-5 engine, two seats, a
throw over yoke and retractable landing gear. The work was done
under the direction of Art Wilder, and his merry band of
volunteers. Keeping the aircraft as close to original as
possible was the main priority. For this reason, the flying and landing
wires are adjusted by using the original Curtiss motorcycle spoke
turnbuckle system. As bamboo was used in the fuselage of the
original A-1, we also used it. We even purchased it from the same
company that sold it to Glenn Curtiss. And the shoulder yoke control
system was used. (This is where leaning to the left or right
operated the ailerons.) Turning the wheel operates the rudder,
while pushing and pulling it operate the pitch controls which are made
up of a canard and elevators.
It is interesting to note
that because the ailerons are mounted between the upper and lower
wings, there is no asymmetrical drag associated with aileron use.
Sort of set it and forget it in the rudder department.
"When it was decided
that I would be the pilot, I had numerous questions."
1-How
would it handle take off and landing without a stepped hull?
(Curtiss didn't invent the stepped hull for another year and a half.)
2-Where to set the
stabilizer trim and the canard? (I wanted plenty of nose down
authority.) Since it was adjustable, we set it as it was set in
many of the old pictures of the A-1.( This turned out to be just right).3-How was I to maintain pitch awareness with virtually nothing in front of me? 4-How much aileron authority would there be with a shoulder yoke? After overcoming some flotation problems, we felt we were ready to start the trials. An OX-5 engine has to be warmed up before flight to properly vaporize the fuel in the manifold. We devised a system of putting a rope around the two vertical posts just above the float and a little behind the wing. We chose this method in order to decrease the strain on the wing, allow more people to hold on to the rope, and keep them out of the prop blast. When ready, one side would let go and the rope would slide free without hitting the prop. First Flight
September 15, 2004
The day was clear, 80 degrees
Fahrenheit, wind 0-5 knots. The surface of Keuka Lake was light
ripples. While warming up, I check the pitch authority which
responded well. Static RPM was 1360. 90 HP was achieved at
1400 (redline 1450). With the engine warm, the signal given, one
end of the line was released and I began to taxi. Rudder
authority was increased as power was added. I turned and added
full power to step taxi downwind to the take off point. As soon
as I saw the nose come up and the spray move back, I knew it would
fly. While on the step downwind, I again checked flight control
authority. All were good. I found that I had much better
leverage with the shoulder yoke (ailerons) if I gripped the seat frame
with my right hand. I stopped and turned around about a mile down
wind. Slowly I added power and set the rudder to keep my
heading. As I gained speed, holding slight back pressure, the
spray moved back, the nose came up and the aircraft smoothly lifted off
the water in a most delightful manner. There was no popping off
the water or awkward rotation problems that I had been concerned
about. In fact, I wasn't sure exactly when I left the
water. At about fifteen feet I leveled off, noted that the wheel
was set just right to give the neutral pitch setting a comfortable
flying position. Since I was flying into the end of the lake, I
immediately started into the landing phase. The plan was to point
the nose down until I was two or three feet above the surface, then
back off on the power and let it settle on slightly nose high.
This was basically what happened except that with nothing in front of
me, I wasn't real sure of my pitch attitude. The aircraft
basically just landed, beautifully. There was no pitch over
tendency at all, just a smooth settling.
Second Flight
also September 15, 2004
Buoyed by the success of the first flight, I taxied back for another. This time I rotated more
abruptly and the aircraft lifted off more positively. Just as I
was leveling at about fifteen feet, some wind ballooned the
aircraft upward. Despite a few mild attempts to lower the nose, I wound
up about fifty or sixty feet.
I looked around and said, AHoo
boy, a guy could really get hurt coming down from up here. I would push
forward, the aircraft would pitch nose down, but all that happened was
that the speed would build up. At one point there was a mild dutch roll
tendency which was predicted by one of the volunteers, Brian Grigsby,
who is an aeronautical engineer. This was due to the center of lift
moving ahead of the center of gravity as the speed increased.
Now I won't say that the A-1 is
a high drag vehicle, but a pigeon couldn't fly between the wings due to
all the wires. So most flying is done at full throttle.
This being the case, a serious reduction of power in flight should be
reserved for very special occasions.
Well, at fifty feet, speed
increasing, and the lake in front of be rapidly decreasing, I decided
this was one of those special occasions. So I pushed the nose
down and pulled the power. The aircraft glided nicely albeit at
somewhat of a steep pitch angle. Some power was added at the
flair, the wing dropped slightly and we landed right float first, then
the hull. Despite being wing low at touchdown, the landing
was still quite smooth. In retrospect, while concentrating on the glide
and flair, I resorted to conventional controls by turning the wheel
right (right rudder) to pick up the left wing. This caused the
loss of lift in the right wing just before touchdown. Safely back
on the water, I thought that was enough flying for one day.
Third Flight
Sunday, September 19, 2004
Temp 55 degrees Fahrenheit, Wind NE 10-15, Sea Waves 9"-12" with
whitecapsIt was cool and windy.
The engine started easily and ran well. Once warm, I taxied out
in a crosswind. It took some leaning and wingtip flotation to
keep the aircraft level. Once into the wind, I applied full
power. Once again, the nose came up, the spray moved back and we
were airborne in about three aircraft lengths. There was no
tendency to porpoise as the non-stepped float reached across the
waves. Level at ten to fifteen feet, I wondered how landing on
waves would be. Would it porpoise or slam the nose down?
Again, landing was stable and smooth. After settling into
displacement, I tried to turn downwind using power. It didn't
work. At idle, however, I noticed that with each wave the nose
came around further, so I just let it keep coming until I was headed
down wind. I step taxied back to a happy crowd.
Over all, the aircraft was a
delight to fly. It was light and responsive and basically it
wanted to fly. The control system, though quite alien to the
conventional control system that I am used to, worked very well.
Especially not having to work the rudder with every aileron input.
These three short flights were the most memorable I have ever
experienced. Given the location and the aircraft, they were a wonderful
trip back in time to actually experience an historical moment. I feel I
have had the honor of sharing the same thrill in the same place with a
great man-- ninety-three years later..
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By Jim Poel
The Glenn II, Curtiss Museum’s reproduction of the Curtiss A-1 “Triad”
was completed in our restoration shop three years ago. It is one of
three reproductions of the A-1. Only two of these have flown, ours and
one other. The other one built that has flown, had conventional flight
controls and made only one straight, (no turns), flight of less than
one minute. Ours is the only A-1 replica that has flown with the
original flight control, (shoulder yoke), control system, retractable
landing ear, and anti skid panels. It has flown in numerous circles,
lifted off with two pilots and a full tank of gas and even rolled up on
the beach on it’s own wheels. All the things that we know that Glenn
Curtiss did with the original, ours has done it’s 45 minutes of flight
time and thirteen flights. It has been the Star of our show for three
years now having achieved all that we asked of it and more, it has
earned a little rest. Our little A-1 will now be retired for awhile as
we turn our attention towards the 5th Annual Seaplane Homecoming which
will feature the inaugural flight of the 1914 transoceanic flying boat “America”, now under construction in our
restoration shop. Stay tuned. |