Wright Vertical 4

http://dbpedia.org/resource/Wright_Vertical_4 an entity of type: Software

Wright Vertical 4 foi a designação do segundo modelo de motor produzido pelos irmãos Wright a partir de 1906, e também pela Wright Company a partir de 1909, esse modelo portanto, foi produzido entre 1906 e 1912 tendo sido utilizado para para equipar os aviões Wright desse período. O Wright Vertical 4 tinha 3.932 cc de capacidade, fornecia entre 30 hp nas primeiras versões, chegando a até 40 hp nas últimas, quando passou a ser conhecido também por Wright 4-40 (4 cilindros - 40 hp). Ele foi projetado em 1906 e construído a partir de então para equipar os aviões produzidos pelos Wright até 1912. rdf:langString
The Wright Vertical 4 was an American aircraft engine built by the Wright brothers in the very early years of powered flight. It was a liquid-cooled piston engine with four inline cylinders, mounted vertically. (Earlier Wright engines were mounted horizontally.) It generated about 30–40 horsepower (22–30 kW) from a displacement of 240 cubic inches (3.9 liters) and weighed about 160–180 pounds (73–82 kg). Developed by Orville Wright in 1906, the Vertical 4 was produced by the Wright Company until 1912 and was the most numerous engine they manufactured. Around a hundred Vertical 4 engines were built, according to a Wright test foreman. rdf:langString
rdf:langString Wright Vertical 4
rdf:langString Wright Vertical 4
xsd:integer 30270669
xsd:integer 1068464496
rdf:langString overhead valve, two valves per cylinder, "automatic" intake valve , exhaust valve actuated by camshaft and pushrod
rdf:langString Initially at 1325 rpm, later up to at 1500 rpm.
xsd:gMonthDay --06-12
xsd:integer 4
rdf:langString Liquid-cooled inline-4 piston aero engine
rdf:langString The Wright Vertical 4 was an American aircraft engine built by the Wright brothers in the very early years of powered flight. It was a liquid-cooled piston engine with four inline cylinders, mounted vertically. (Earlier Wright engines were mounted horizontally.) It generated about 30–40 horsepower (22–30 kW) from a displacement of 240 cubic inches (3.9 liters) and weighed about 160–180 pounds (73–82 kg). Developed by Orville Wright in 1906, the Vertical 4 was produced by the Wright Company until 1912 and was the most numerous engine they manufactured. Around a hundred Vertical 4 engines were built, according to a Wright test foreman. The Vertical 4 powered most Wright aircraft during this period, including the Model A and Model B and variants built for the U.S. Army and Navy. This engine was also built under license by in France and by Neue Automobil-Gesellschaft in Germany.
rdf:langString Wright Vertical 4 foi a designação do segundo modelo de motor produzido pelos irmãos Wright a partir de 1906, e também pela Wright Company a partir de 1909, esse modelo portanto, foi produzido entre 1906 e 1912 tendo sido utilizado para para equipar os aviões Wright desse período. O Wright Vertical 4 tinha 3.932 cc de capacidade, fornecia entre 30 hp nas primeiras versões, chegando a até 40 hp nas últimas, quando passou a ser conhecido também por Wright 4-40 (4 cilindros - 40 hp). Ele foi projetado em 1906 e construído a partir de então para equipar os aviões produzidos pelos Wright até 1912.
rdf:langString liquid-cooled
rdf:langString around 100
xsd:nonNegativeInteger 6965

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