Publication 296, 1909, Aeroplanes and motors of the first Paris aeronautical salon
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Original title | Aeroplanes and motors of the first Paris aeronautical salon |
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Simple title | Aeroplanes and motors of the first Paris aeronautical salon |
Authors | |
Date | 1909 |
Countries | US |
Languages | en |
Keywords | airplane, motors, 11th Paris Motor Show |
Journal | Scient. Amer. |
Related to aircraft? | 1 |
Page count | 1 |
Word count | 1857 |
Wikidata id |
Notes from the text version at MS State site (see sources) and other info on this site:
- First Paris Aeronautical Salon = 11th Paris Motor Show
- "The new aeronautic industry has already assumed [notable size] in France,"
- This event was held recently in the Grand Palais at Paris, in conjunction with an exhibition of commercial motor vehicles
- our illustrations show some of the new French aeroplanes
- The aeroplane of greatest interest is the new double surface Blériot machine, shown herewith.
- Blériot has built and flown many flying machines, including several of the Langley following-plane type (possibly meaning tandem biplanes)
- Blériot has recently experimented with monoplanes, which are a more advanced type than biplanes and can go faster.
- On October 31, 1908, he made a monoplane flight of about 18 miles, stopping twice en route
- On November 4, 1908, this dangerous machine was demolished (crashed?)
- Then he constructed a new double surface machine much like the Wright craft. The most important difference is the replacement of the front horizontal rudder by triple vertical rudders, and the use of separate single surface horizontal rudders several feet behind the main planes. These rudders are carried upon triangular vertical trusses, the outermost of which are covered with cloth. The horizontal rudders, when rigged behind the planes as Blériot has arranged them, will be less efficient than if they were in front. The aviator would sit in a comfortable chair on the front edge of the lower plane, and steer and control his machine with an automobile-type steering wheel and a single lever beneath it.
- Each of two horizontal rudders is 8 square meters. They are connected so that moving a lever to inclines one upward and the other downward the same amount, while pushing forward or pulling backward the steering column causes both to act together for directing the machine upward or downward. Turning the steering wheel operates the triple vertical rudders for steering to one side or the other. Thus Blériot accomplishes with two auxiliary horizontal pivoted surfaces-the same number as the Wright aeroplane-what the Wrights have to warp the main planes to accomplish, i e., the maintenance of transverse stability, in addition to the directing of the machine up and down which is the main purpose of these auxiliary surfaces.
- Farman has found the use of vertical partitions connecting the main planes to be advantageous. Blériot has placed one of these on each side of the center part of his new aeroplane, in addition to the triangular vertical portions extending back from the rear edge at the ends. The two central partitions are made of sheet aluminium (not the usual cloth) and serve as radiators to cool the water used in the jackets of the motor. Applied to each surface of the sheet aluminium are a large number of rings of small-sized tubing, connected together by flexible pipes. The cooling water is forced through the large radiating surface thus formed, by a suitable centrifugal pump.
- The motor which will first be used on this new aeroplane is a 50-horse-power Antoinette of the 8-cylinder V type. Later, a 100 horse-power 16 cylinder motor may be tried. The 3-meter (9.8-foot) 4-bladed propeller is placed at the rear of the main planes, which are notched at their center rear edges to allow the propeller to be brought farther forward and to be supported on the central rigid part of the structure. This propeller is driven at 480 R.P.M. by a chain from the motor crankshaft. There is a speed reduction of about 3 to 1 from the engine to the propeller. From his experience with his monoplanes, Blériot evidently believes that the gyroscopic effect of this large 4-bladed propeller will not be sufficient to cause trouble with his new double-surface machine.
- The main planes of the Blériot machine have a spread of 12 meters, and their width from front to back is 2.5 meters. The total supporting surface of the two planes is 60 square meters. The weight is given as 480 kg, or 1,058 pounds. Blériot expects to be able to carry two or three passengers. This would make a total weight of from 1200-1650 pounds. Two passengers are to be carried on the front edge of the machine, and two on the rear. The total length from front to back is 8 meters. The machine rests upon three very small wheels which have large pneumatic tires. On account of the small diameter of the wheels, the lower plane is quite close to the ground, and it will be necessary to alight on an even keel in order not to damage this plane.
- The improvements that Blériot has made upon a machine of the Wright type have caused this to assume a very businesslike appearance. The new machine has sufficiently large radiators to allow it to run for an indefinite period, and the only limit to the length of time it should be able to remain aloft, should be the amount of fuel that can be carried. The 50 horse-power 8-cylinder motor consumes much more fuel per hour than does the 4-cylinder, 25-horse-power motor of the Wright aeroplane, so that in this respect the Wrights doubtless still have a decided advantage. Blériot has had considerable experience with movable wing tips on monoplanes but it is yet to be shown whether the combined horizontal rudders and wing tips in the rear will be as efficient for maintaining the transverse equilibrium of the aeroplane as is the Wright system of warping the main surfaces.
- Melvin Vaniman's new three-decker machine seems to be the first of its kind to make a really successful flight. On December 18, 1908, above the parade ground at Issy-les-Molineaux, it flew a distance of 150 meters. It takes off from a track, with its four wheels running along rails. The aeroplane rose by its own power, and behaved well in the air (see illustration). The Vaniman three-decker has both its horizontal and vertical rudders placed well out in front. The horizontal rudder is about on a level with the middle plane, while the vertical rudder is placed between this plane and the upper one well out in front, and a tail with horizontal and vertical surfaces is placed on the same horizontal line at the rear. There are also auxiliary planes or wing tips at the ends of the middle plane, for the purpose of maintaining the transverse equilibrium. The machine is equipped with an 8-cylinder Antoinette motor of from 60 to 80 horse-power. The two-bladed propeller is direct-connected to the crankshaft. A pair of horizontal radiators are mounted on a level with the top of the motor, one on either side of it. The aviator sits on a seat arranged in front of the motor, and controls the rudders and equalizing planes by two levers. The distinctive feature of this aeroplane is the fact that the framework is constructed of steel tubing. It is the first successful French machine having its framework made of this material. The advantages of the triple-surface aeroplane consist chiefly in the shortening of the planes, and thus in the making of a less cumbersome machine. Vaniman's machine is several feet less wide than the Farman or the Wright aeroplanes. As can be seen from the photograph, it is a very symmetrical and rigid appearing structure. We expect that soon a machine of this type will make successful and extended flights.
- The motor which we illustrate is the new Clement Bayard, 50-horse-power, 7-cylinder aeronautical engine, which has recently been brought out by the Clement firm. The seven cylinders' each of which is provided with a copper water jacket, are evenly spaced about the central crankcase, and have their connecting rods attached to a single crank. Our photograph shows the under side of the motor, which has a centrifugal pump attached to the lower end of its crankshaft and arranged in a casing, the cover of which is removed. This centrifugal pump forces water to the bottom of the water jacket of each cylinder, there being seven separate outlets from the pump for this purpose. Just above the pump there is an annular mixing chamber, from which four large pipes run to the cylinders. Three of these pipes are branched, so that they supply six of the cylinders, while the fourth one (shown at the right) supplies the seventh cylinder only, The carbureter is placed at one side of the casing, the pipe connecting it with the mixing chamber being seen within this casing, to the right of the uppermost cylinder in our illustration. The inlet and exhaust valves are mechanically operated by a rocker arm and single push rod for each pair of valves. The push rods are worked by a cam ring that is concentric with the crankshaft, and that is driven at half the speed of the latter through an idle lay shaft. A high-tension magneto is placed above the cylinders and is gear-driven from the crankshaft, while on the upper end of the lay shaft just mentioned there is a distributor for supplying current to the spark plugs.
- The drawing shown here illustrates a scenario for future naval warfare according to experts in the lighter-than-air craft. The dirigible seen in the foreground has discharged a torpedo from its torpedo-shaped car and hit the warship. The dirigible shown in our illustration has the torpedo-shaped car quite close to the gas bag, and the suspending of this car from a sort of hot-air turbine, by which the car can be swung in any direction when it is desired to fire at the enemy. This dirigible is a recent French invention, which the enthusiastic inventor believes will soon revolutionize warfare on the sea.
- The current issue of the Scientific American Supplement has more about the Paris Aeronautic Salon, including photographs of some of the machines exhibited there, and an article about aeroplane construction.
Sources
- Brockett 1910, page 23, entry 296: Aeroplanes and motors of the first Paris aeronautical salon. Scient. Amer., Vol. 100, No. 4 (Jan. 23, 1909), New York, pp. 81-82, ill. S (296
- Text at Simine Short's Digital Library of Flight