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The autogyro La Cierva. This invention due to a Spanish engineer that had produced a great sensation in the scientist institutions of the time, solving several of the most arduous problems in the aviation, such as a perfect stability and the vertical landing at moderate speed. |
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Most of the apparatuses in use towards 1930 were biplanes, that is to say, airplanes with two superposed wings. Between the wings of the typical biplane there was a nacelle that was carefully smoothing in its outside and peaked ahead and behind, to favor that the resistance and the force of drag the device are the lesser possible necessary to fly it by the air. The aviator and the passengers were located in this nacelle , that also contained the motor. The propellers could be located ahead or behind the wings. The airplanes that had the propellers ahead were called "tractors" and those that had it behind were known with the "propulsive" name. The overall length of airplane was generally a little more than half of the wingspan. In the case of the tractors type ones , the nacelle extended backwards of the rear end; but this was not possible in a propulsive type with a helix, because the nacelle or fuselage, as it is also called, would hinder the operation of the helix. This difficulty was solved by the device of Gallaudet, which took part of the fuselage behind the helix on a wide tube that passed through the bucket of it . In such machines, that were familiarly known as cellular kites , the tail was maintained by an armor of three or four props that surrounded the helix. The tail of the apparatus commonly was formed by four surfaces, two horizontals and two verticals ones. There was a horizontal fixed tailplane that helped to maintain the stability, preventing the apparatus to rise, or to descend with too much speed, and a vertical fin located on the fuselage that helped to balance the apparatus. In addition to these mechanisms of stabilization, there were the true control elements: the rudder and the elevator . The elevator was formed generally by two parts, one on each side of the center, to prevent crushing the rudder, but rigidly united, so that they could always maneuver together. The balance of the apparatus was obtained in most of the cases by means of fins (ailerons), or small auxiliary winglets, joined to the rear part of the main wings, near the ends. Sometimes both wings had fins; but more commonly these ones were installed only in the upper wing. The fins were used in the same way that the warp concept used by the Wright brothers, they were tugged downwards in the side that was necessary to elevate, whereas the ones of the opposite side remained raised. Several small apparatuses were still constructed towards 1930 with warping ; but the system had not become general, because it made necessary to debilitate the wings. As it can be seen , the pilot had to take care of three regulations: rudder, elevator and fins. The rudder was handled practically in all the models by a revolving bar moved by the feet, resemblance to the guide of a bicycle. The other two regulations were driven by means of combinations of wheels and handles; a handle was moved forwards when the pilot wanted to descend the airplane, and the inverse movement caused that the apparatus to soar . As the apparatus needed to run some stretch by the ground until reaching great speed it had to be provided with a set of wheels, and as it was important to land on an uneven surface, it was essential that the apparatus had a landing device carefully planned (undercarriage) with own means to cushion the shock. Most of these artifices or devices were made up of two wheels in the front of the fuselage and below it , so that the propeller did not collide with the ground, as well as a short skid in the rear part protecting the tail of the plane of the contact of the ground. The shock absorbers were made of steel some times, but more frequently they were reduced simply to heavy rubber bands. The primitive airplanes were
almost entirely made of wood and steel wires; but later the tendency had
been pronounced to use the steel and the duralumin in tubes, whenever
it was possible, due to the most uniform quality, less deterioration and
in many aspects greater facility to work than the wood. The surprising light and nevertheless powerful motors that has developed the aviation in the beginnings of the aeronautics .
Towards the 1920/30 decade all airplanes flight by gasoline motors that worked according to the cycle of Otto of four times, although several years before, the revolving type of motor seemed the most promising accomplishment of mechanism; but it was left in most of the heavy apparatuses because of the high consumption of combustible, and its application had been confined to light exploratory airplanes and apparatuses used in exhibitions. In the revolving motor, that has only been used in aeronautical applications, the cylinders, seven or nine, were located around the crank, like the wheel radii, and the crank ,instead of rotating as it happens normally, was fixed, whereas the cylinders and the frame that maintain them turn around it. The most popular type used in those times was the ordinary vertical motor or "V" motor, with six, eight or twelve cylinders, and identical in details of construction and disposition, to the motors of the automobiles of those times. These motors were wonderfully light. Before the invention of the automobiles and the airplane. 5.000 kilograms were a very light weight for a machine of 100 horsepower, but soon the same machine happened to weigh only 150 kilograms in average . |
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The image of above right
shows the hydroplane in the firing position on the platform. In the left
image is seen the hidroplane at the moment of leaving the platform hurled
by a powerful catapult moved by compressed air.
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Locating to us temporarily in the beginnings of the XX century, the airplane that was seen with more frequency towards the decade of years 1930s in the airfields was the biplane military tractor of two seats or the commercial modification of the same one. Also similar apparatuses of smaller dimensions for the transport of a single person were constructed. They were used for exploration and war fights and reached speeds in some cases of up to one hundred sixty kilometers per hour. The other extreme was the multi-engine airplane. This type of machine had from two to nine motors and one or more helices, moved by one, two or three motors each one. The greater apparatuses showed to a great variety of construction and dispositions of the wings. They had the advantage of greater duration and cargo capacity for a given crew, and in some cases, due to the possibility of continuing flying after being damaged one or more motors, they were safer than those smaller ones of one motor .The motors could be mounted outside the wings in nacelles, with the helices mounted directly in the motors, or these last ones also mounted in the fuselage and the helices in the wings. Of particular interest for the North Americans were the hydroplanes and the flying boats invented by Mr. Glenn H. Curtiss, by the double property that they had due their utility in the defense of the long coastline of the United States and its application to the sports. These apparatuses lifted off or descended in the water instead of in the Earth, and could be maneuvered surely in a sea that would make navigation to a small yacht difficult. Already in those years they constituted an ideal sports vehicle , because they combined the emotions of the motor boat with those of the airplane, and virtually were safe being the sea easy site of descending in case of failures of the motor or other accidents. They could be transported by boats and be put at sea by means of cranes. In those years several species of catapults had also been invented so that they would send directly the hydroplane to the air from the deck of the ship , if some circumstance prevented it to be put in the water. The introduction of the airplane carrier , a fast ship of great dimensions, with a flight deck free of obstacles so that the airplane could use it to rise and to settle, originated a third type of airplane: the amphibian airplane , that could take off from the Earth and the water. To the terrestrial ordinary type it was also provided with possible floaters of balloon fabric, plenty of air , to be used from the ships. When these floaters were deflated, they were folded inside or to the flank of the fuselage. In the decade of 1920s an airplane reached speeds of up to 320 kilometers per hour, several times quicker than the flight of the fastest birds of which there were news, constituting a very remarkable fact for that time. It had overcome heights superior to 11,200 meters on the Earth surface, and could raise to considerable heights, at the rate of 600 meters per minute. It had conquered the height of the most formidable mountains having crossed the Atlantic and made other remarkable flights, among which they were to mention the trip from England to Australia and from Rome to Tokyo. It had remained in the air for more than twenty-six hours. In the course of World War I, the incursions on enemy territory to drop bombs from airplanes were of almost daily accomplishment . |
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Photo of the express "High-Ball" making the passage between Miami-Bimini.
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The conquest of the air became a reality:
some of the aerial passages to emphasize in the decade of 1920/ 1930,
and that constituted true landmarks in the history of the aeronautics
were:
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