Wright Vertical 4

{{short description|1900s American piston aircraft engine}}

{{Infobox aircraft begin

| name=Wright Vertical 4

| image=Wright Vertical Four 2.JPG

| caption=Wright Vertical 4 aircraft engine on display at the Steven F. Udvar-Hazy Center. This particular engine was used on the Wright B-1 seaplane that crashed in 1912. A patch was bolted to the side of the crankcase in an attempt to repair the engine.

}}{{Infobox Aircraft Engine

|type=Liquid-cooled inline-4 piston aero engine

|manufacturer=Wright Company

|designer=Orville Wright

|national origin=United States

|first run=

|major applications=Wright Model A
Wright Model B

|produced=

|number built=around 100Hobbs, p. 63.Lippincott, p. 89.

|program cost=

|unit cost=

|developed from=

|variants with their own articles=

}}

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 {{convert|30-40|hp|lk=in}} from a displacement of {{convert|240|in3|L|abbr=off|sp=us}} and weighed about {{convert|160-180|lb}}. 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.Hobbs, p. 34.Lippincott, p. 87. 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 Bariquand et Marre in France and by Neue Automobil-Gesellschaft in Germany.Hobbs, p. 43.

Applications

Engines on display

Specifications

File:Wright Vertical Four-Cylinder Engine.jpg. This engine was originally a keepsake of Orville Wright's.]]

{{pistonspecs|

|ref={{cite web|url=https://airandspace.si.edu/collection-objects/wright-vertical-4-line-4-engine-0|title=Wright Vertical 4, In-line 4 Engine (inventory A19620037000)|publisher=Smithsonian National Air and Space Museum|accessdate=12 June 2018}}

|type=4-cylinder, liquid-cooled inline piston aircraft engine

|bore={{cvt|4.375|in|0}}

|stroke={{cvt|4|in|0}}

|displacement={{cvt|240|in3|L}}

|length={{cvt|40.75|in}}

|diameter=

|width={{cvt|18|in|0}}

|height={{cvt|27|in|0}}

|weight={{cvt|160–180|lb|-1}}Hobbs, p. 62.

|valvetrain=overhead valve, two valves per cylinder, "automatic" intake valve (driven by suction), exhaust valve actuated by camshaft and pushrod

|supercharger=

|turbocharger=

|fuelsystem=

|fueltype=

|oilsystem=

|coolingsystem=liquid-cooled

|power=Initially {{cvt|28|hp}} at 1325 rpm, later up to {{cvt|42|hp}} at 1500 rpm.

|specpower=

|compression=

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=

|designer=Orville Wright

|reduction_gear=

|general_other=

|components_other=

|performance_other=

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

{{Reflist}}

Bibliography

{{cite book |last1=Hobbs |first1=Leonard S. |title=Smithsonian Annals of Flight, No. 5: The Wright Brothers' Engines and Their Design |date=1971 |publisher=Smithsonian Institution Press |location=Washington, D.C. |url=http://www.sil.si.edu/smithsoniancontributions/AnnalsofFlight/pdf_hi/SAOF-0005.pdf}}

{{cite book |author-last=Lippincott |author-first=Harvey H. |editor-last=Wolko |editor-first=Howard S. |title=The Wright Flyer: An Engineering Perspective |chapter=Propulsion Systems of the Wright Brothers |date=1987 |publisher=Smithsonian Institution Press |location=Washington, D.C. |isbn=0-87474-979-4 |pages=[https://archive.org/details/wrightflyerengin00wolk/page/87 87]–89 |url=https://archive.org/details/wrightflyerengin00wolk}}

{{cite book |editor1-last=McFarland |editor1-first=Marvin W. |title=The Papers of Wilbur and Orville Wright, Including the Chanute-Wright Letters and Other Papers of Octave Chanute |volume=Two: 1906–1948 |date=1953 |publisher=McGraw-Hill |location=New York |pages=1215–1216}}