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Wright R-540 Whirlwind

From Wikipedia, the free encyclopedia
Not to be confused withKinner R-540.
R-540 Whirlwind
Wright R-540 Whirlwind installed in aTravel Air 16E at theHistoric Aircraft Restoration Museum
TypeAir-cooled 5-cylinderradial piston engine
National originUnited States
ManufacturerWright Aeronautical Corporation
Major applicationsVarious light aircraft
Manufactured1929-1937
Number builtaround 500

TheWright R-540 Whirlwind was a series of five-cylinder air-cooledradialaircraft engines built by theWright Aeronautical division ofCurtiss-Wright. These engines had adisplacement of 540 in³ (8.85 L) and power ratings of around 165-175 hp (123-130 kW). They were the smallest members of theWright Whirlwind engine family.

Design and development

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Wright introduced the J-6 Whirlwind family in 1928 to replace the nine-cylinderR-790 series. The J-6 family included varieties with five, seven, and nine cylinders. The five-cylinder version was originally known as theJ-6 Whirlwind Five, orJ-6-5 for short. The U.S. government designated it as theR-540; Wright later adopted this and dropped the J-6 nomenclature.

Like all the members of the J-6 Whirlwind family, the R-540 had larger cylinders than the R-790. The pistonstroke of 5.5 in (14.0 cm) was unchanged, but the cylinderbore was expanded to 5.0 in (12.7 cm) from the R-790's bore of 4.5 in (11.4 cm). While the R-790 wasnaturally aspirated, the R-540, like the other J-6 engines, had a gear-drivensupercharger to boost its power output.

Wright gradually refined the R-540, using suffix letters to indicate successive versions. For example, the R-540A had 165 hp (123 kW), while the R-540E of 1931 had power boosted to 175 hp (130 kW) thanks to an improvedcylinder head design. Wright sometimes named these versions according to their power, e.g. "Whirlwind 165" or "Whirlwind 175".[1]

The engine was built inSpain as theHispano-Suiza 5Q orHispano-Wright 5Q without modification apart from the use of Hispano's patented nitriding finishing process.[2]

Operational history

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The R-540 was the smallest, least powerful member of the Whirlwind family and was designed for light aircraft. One of the more popular types to use it was theCurtiss Robin, a light civil utility aircraft. A few were also used in prototype military trainer aircraft that were evaluated by the U.S. Army but not put into production.

The R-540 sold well at first, with over 400 engines being built in 1929.[3] However, with the impact of theGreat Depression, sales plummeted, and only about 100 further examples were built over the next eight years.[3] Wright finally ceased production of five-cylinder Whirlwinds in 1937,[3] concentrating on larger engines and leaving the market for small radials to companies likeKinner andWarner.

Since R-540 engines were found solely in light aircraft, they weren't often used for groundbreaking flights. However, there were a couple of noteworthy exceptions which took advantage of the Whirlwind family's reputation for high reliability. In 1935, the brothersAl and Fred Key set a new flight endurance record of 653 hours, 34 minutes in the Curtiss Robin J-1Ole Miss, flying overMeridian, Mississippi, from June 4 to July 1. Their plane was refueled and resupplied in flight, and they could perform simple engine maintenance by walking out on a small catwalk extending between the cabin and the engine.Douglas "Wrong-Way" Corrigan's famous unauthorized transatlantic flight fromNew York City toDublin,Ireland on July 17–18, 1938, used a Curtiss Robin with an R-540 built from the parts of two used engines.[4]

Applications

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Engines on display

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Wright R-540 engines on display are uncommon, but there is one at theStrategic Air and Space Museum (formerly the Strategic Air Command Museum) nearAshland, Nebraska.[5] Another is on display at the Shannon Air Museum inFredericksburg, Virginia.

Specifications (R-540E)

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Data fromFAAtype certificate data sheet for the R-540E;[6] dimensions from Curtiss-Wright (1983).

General characteristics

  • Type: 5-cylinder supercharged air-cooled radial piston engine
  • Bore: 5.0 in (127 mm)
  • Stroke: 5.5 in (140 mm)
  • Displacement: 540 cu in (8.85 L)
  • Length: 41.1 in (104.4 cm)
  • Diameter: 45.0 in (114.3 cm)
  • Dry weight: 420 lb (191 kg)

Components

Performance

See also

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Related development

Comparable engines

Related lists

References

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Wikimedia Commons has media related toWright R-540 Whirlwind.

Notes

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  1. ^Curtiss-Wright (1940)
  2. ^Lage (2004) pp.152-163
  3. ^abcSummary of Wright Engine Shipments: 1920 to 1963(PDF), archived fromthe original(PDF) on March 3, 2016, retrievedDecember 10, 2009. Transcribed from Wright Aeronautical documents by Robert J. Neal T; available from the Aircraft Engine Historical Society'sreference pageArchived 2010-02-04 at theWayback Machine.
  4. ^Forden (1958) p.84
  5. ^Aircraft Engines, archived fromthe original on 2017-07-28, retrieved2008-09-11. This personal collection of museum aircraft engine photos includes a photo of a Wright R-540 under the SAC Museum section. (The page mislabels it as a "Wright R-540 J-5"—there never was a five-cylinder version of the J-5.)
  6. ^FAA, ATC 23 data sheet

Bibliography

[edit]
Wrightinline engines
Lawranceradials
Wright radials
Whirlwind family
Cyclone family
Others
Turbojets
Turboprops/turboshafts
Ramjets
H (four-bank
H-configuration inline)
IV (inverted-V inline)
L (single-bank inline)
O (opposed)
R (radial)
V (upright-V inline)
V (inverted-V inline)
VG (inverted-V inline)
W (three-bank
W-configuration inline)
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