РефератыИностранный языкCoControllable Pitch Propeller Essay Research Paper Canada

Controllable Pitch Propeller Essay Research Paper Canada

Controllable Pitch Propeller Essay, Research Paper


Canada is not exactly known for having produced several ground-breaking


inventions or discoveries in her time. However, the period of rapid


technological advancement that she incurred during the third period of the


history of engineering in Canada brought with it several important engineering


inventions which had their roots in Canada. The creation of the controllable


pitch propeller was one such invention which was perfected in Canada and was so


successful that this primarily Canadian development spread throughout the world.


Wallace Rupert Turnball lived in Rothesay and it was there that he carried out


his experiments in aeronautical theory beginning in 1902. His specialty was that


of dihedrals which he studied in a wind-tunnel. He looked at water borne


hydroplanes propelled by motor-driven airscrews. An airscrew the Great Britain


term for a propeller. A standard propeller consists of anywhere from two to four


blades each a section of a helix, the geometric form of a screw thread, hence


the term ?airscrew.? The first plane had two air-screws on each side whereas


the second one had only one, more highly efficient propeller located at the rear


end of craft, near the pilot?s seat. However, both had an uneven torque of


engine that was in fact destructive to the efforts of the propeller. Turnball


experimented with all different types of air-screws; some with a 30? gauge


track that were 300? long for truck. With each air-screw he tested, he


recorded the propeller thrust, rpm and the forward speed. What determines the


forward speed is the distance that a propeller will move in the forward


direction when the shaft of the propeller is rotated 360o. Assuming that there


is no slippage, this distance is termed the geometric pitch. The propellers that


Turnball tested had diameters ranging from 1.5? up to 3.5?, all different


dimensions and shapes. Upon his return to Rothesay in 1918, after the war, he


dove into his research and experimentation on a possible controllable pitch


propeller, an idea that he had been developing since the autumn of 1916. He ran


several tests using rotating electric motor apparatus in order to spin the


blades of his propeller. The finished product was a propeller whose pitch can be


adjusted by the pilot, at different angles, during flight giving the pilot the


ability to command the optimal combination of torque and speed for the situation


at any given moment from his aircraft. By means of a small electric motor


mounted just in front of the propeller, the pitch of the propeller itself could


eventually be adjusted which makes for mor

e efficient take-offs and regular


flight than what would be achieved with an everyday ?fixed blade? propeller


incapable of any pitch change. Under the supervision of both the Ontario


government and the Canadian Air Force, a ground test was run in 1923 on Avro


aircraft at Camp Borden, Ontario only to conclude that more research and


experimentation was necessary. Four years later, on June 6, 1927, again at Camp


Borden on Avro Biplane, Flight Lieutenant G.G. Brookes took Turnball?s


controllable pitch propeller for it?s first air test. Funding was granted


immediately to perfect the invention it was such a success. The news of the


Canadian invention spread rapidly. Turnball wrote a treatise based on his


discoveries and new found technology called ?The Efficiency of Aerial


Propellers? which was published in the Scientific American on April 3, 1909.


His second and third publications on the subject were entitled ?Laws of


Air-Screws? and appeared in The Aeronautical Journal, in the October 1910 and


January 1911 issues. For his studies and discoveries, Turnball was awarded the


Bronze Medal of Royal Aeronautical Society and was, in addition, elected a


?Fellow.? Come 1914, Turnball had published several scientific articles and


found himself one of the world?s authorities on the subject. He sold the


patents to the controllable pitch propeller in December of 1929. The Curtiss


Wright Corporation won the American rights and the Bristol Aeroplane Company,


the English rights. In 1935, the Norseman, the most highly successful bush plane


in the world at the time, was designed in Canada by Robert Noorduyn, an aviation


engineer trained in Holland. The Norseman quickly caught the attention of the


entire world due to the effectiveness of its design. It had a large capacity for


cargo, flexible take-off and landing capabilities, ability to withstand harsh


weather, can be easily flown in either day or night and is capable of flying


great distances. Noorduyn?s Norseman, which utilized Turnbull?s controllable


pitch propeller, was adopted around the world by countries that required short


take off and landing (STOL) planes for their own reasons, most of which involved


mining, lumbering and exploring isolated expanses of land which could not


otherwise be reached quite as easily. W.R. Turnball?s invention of the


controllable pitch propeller was clearly one of the most successful Canadian


innovations in terms of world recognition. Once perfected, it was quickly bought


up by major aircraft manufacturing companies around the world and mass produced


to fulfill the global demand, at the time, for such a development in technology.

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