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Wright R-790 Whirlwind

(Перенаправлен из вихрь Hispano-Suiza J-5 )
R-790 Whirlwind
Wright R-790 (J-5 Whirlwind) в Национальном музее воздуха и космической космос
Тип 9-цилиндровый радиальный поршневый двигатель с воздушным охлаждением
Национальное происхождение Соединенные Штаты
Manufacturer Wright Aeronautical Corporation
Škoda Works (Czechoslovakia)
Avia (Poland)
First run 1923
Major applications Spirit of St. Louis
Fokker Trimotor
Ford Trimotor

Wright R-790 Whirlwind представлял собой серию из девятицилиндровых воздушных охлаждений радиальных авиационных двигателей, построенных Aeronautical Corporation Wright , с общим перемещением около 790 кубических дюймов (12,9 л) и около 200 лошадиных сил (150 кВт). Эти двигатели были самыми ранними членами семьи двигателей Wright Whirlwind .

Дизайн и разработка

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Whirlwind R-790 начался как Lawrance J-1 , девятицилиндровый радиал с воздушным охлаждением, разработанный в 1921 году компанией Lawrance Aero Engine для ВМС США. Военно-морской флот был с энтузиазмом относительно двигателей с воздушным охлаждением, которые он считал лучше подходящим для военно-морского использования, чем жидко-охлаждающие. [ 1 ] Lawrance была небольшой компанией, и военно -морской флот сомневался, что может производить достаточно двигателей для своих потребностей. [ 1 ] Несмотря на пособия со стороны военно-морского флота, крупные производители самолетов США, Райт и Кертисс , были удовлетворены своими двигателями с жидко-охлаждением и не проявляли интереса к строительству двигателей с воздушным охлаждением. [1] Since the Navy was already a major buyer of Wright engines, it pressured Wright into purchasing Lawrance and building the J-1 itself, by informing the company that the Navy would buy no more of its existing engines or spare parts.[1] To retain the Navy's business, Wright complied in 1923 and the Lawrance J-1 became the Wright J-1.[1]

By the time Lawrance merged with Wright, it had already developed the more powerful J-2, a version of the J-1 with slightly enlarged bore and displacement. However, Lawrance decided the J-1 was large enough, and the J-2 never went into production; only two examples were built.[1]

Over the next two years, Wright gradually refined the J-1 engine, introducing the J-3, J-4, J-4A, and J-4B. The changes improved the engine's reliability, cooling, and fuel consumption, but the basic design, dimensions, and performance were unaltered.[1]

The J-4 was the first engine to bear the Whirlwind name; previous engines used only the alphanumeric code.[1]

The J-5 Whirlwind, introduced in 1925, was a complete redesign of the engine with greatly improved cooling and breathing, further increasing its reliability and reducing fuel consumption. Among the visible changes was the much wider separation between the valves, for better cooling airflow, and completely enclosed, instead of exposed pushrods and rocker arms.[1]

The U.S. government later designated the J-5 Whirlwind as the R-790, but it did not apply this designation to the older engines.[2]

All these engines had a bore of 4.5 in (11.4 cm), a stroke of 5.5 in (14.0 cm), and a displacement of 788 in3 (12.91 L).

In a 1928 report on transcontinental aviation, the author disclosed the cost of a typical five-seat commercial aircraft as $12,500, of which $5,000 was for one of the 350 200 hp Whirlwind Engines available that year.[3] The J-5 was the last of the original nine-cylinder Whirlwinds. In 1928, it was replaced by the seven-cylinder Whirlwind J-6.

Operational history

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Many Whirlwind engines were used in U.S. Navy aircraft, mostly in trainers, but also in some ship-based observation and fighter aircraft. As the engines were refined and their reputation for reliability grew, their use expanded to U.S. Army trainers and a wide range of U.S. civil aircraft, including the earliest versions of the Fokker Trimotor and Ford Trimotor airliners.

The reliability of J-5 Whirlwind engines also led aviators to use them for a number of record-setting distance and endurance flights. The most famous of these is Charles Lindbergh's solo transatlantic flight from New York City to Paris on May 20–21, 1927, in the Spirit of St. Louis, powered by a single Whirlwind J-5C. During Lindbergh's flight, the engine ran continuously for 33.5 hours. Lindbergh's achievement greatly boosted the Whirlwind's already good reputation.[4]

Some other historic long-duration flights made in aircraft powered by the J-5 Whirlwind:

Charles L. Lawrance, who developed the original Whirlwind series and became president of Wright, won the 1927 Collier Trophy for his work on air-cooled radial aircraft engines.

License-built versions

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The J-5 Whirlwind was built by Hispano-Suiza in France.[5]

The Whirlwind J-5 was also produced under license in Poland by several makers. Among these were Polskie Zakłady Skody, the Polish branch of Škoda Works, which built about 350 to 400 engines from 1929 to 1931, and the Polish firm Avia, which manufactured a further 300 engines from 1935 to 1938. Polish-built J-5s were used in numerous Polish aircraft, mostly in military training, observation, and liaison aircraft.

Variants

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  • J-1: Lawrance J-1 as built by Wright Aeronautical in 1923.
  • J-3: Wright's first refined version, 1923.
  • J-4: Improved version, 1924. First to be named "Whirlwind".
  • J-4A, J-4B: Further refinements of J-4.
  • J-5 (R-790): Complete redesign with improved reliability and performance, 1925.

Applications

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U.S. aircraft

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Polish aircraft, using Polish-built engines

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Aircraft from other countries

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Engines on display

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Some museums which have J-5 Whirlwinds (or the military R-790 equivalents) on display:

Also on display at the San Francisco International Airport, International Terminal. Older Whirlwinds on display are harder to find. The National Museum of Naval Aviation has two J-4s, one of which is a cutaway.[10] The New England Air Museum in Windsor Locks, Connecticut, has a Lawrance J-1, the Whirlwind's direct predecessor.[13][14]

Specifications (R-790 Whirlwind J-5)

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Data from Type certificate data sheet for the Whirlwind J-5;[15] dimensions from "Model Designations of U.S.A.F. Aircraft Engines" [16]

General characteristics

Components

  • Valvetrain: 2 valves per cylinder, pushrod-actuated
  • Fuel system: single three-barrel carburetor[17]
  • Fuel type: 50 octane

Performance

See also

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Related development

Related lists

References

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Notes

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  1. ^ Jump up to: a b c d e f g h i Wright J-5 "Whirlwind" Archived 2016-03-04 at the Wayback Machine (PDF), by Kimble D. McCutcheon, from the Aircraft Engine Historical Society
  2. ^ Naval Aviation Chronology 1920–1929 Archived 2014-10-15 at the Wayback Machine, from the Naval Historical Center. See entries for 1928, February 1 and 28.
  3. ^ Florabel Muir (4 August 1928). "Blazing New Wing Trails". Liberty Magazine: 20.
  4. ^ Hardesty, Von (2002). Lindbergh: Flight's Enigmatic Hero. New York: Harcourt. p. 78. ISBN 9780151009732.
  5. ^ "Revue Hispano-Suiza" (PDF). dev.museesafran.com (in French). Societe Francais Hispano-Suiza. Archived from the original (PDF) on 20 October 2014. Retrieved 20 October 2014.
  6. ^ Collections Database: Objects: A19791508000, retrieved 2008-09-06.
  7. ^ Wright R-790 Radial, archived from the original on 2013-04-04, retrieved 2017-07-17.
  8. ^ National Museum of the USAF, archived from the original on 2010-07-25, retrieved 2008-09-06. The section "Images from Gary Brossett" has a photo of the museum's R-790.
  9. ^ National Museum of the United States Air Force: Images by Tony Ward, archived from the original on 2012-02-12, retrieved 2008-09-06. This page has several photos of the museum's R-790.
  10. ^ Jump up to: a b Image Galleries by Gary and Janet Brossett: National Museum of Naval Aviation in Pensacola, Florida, archived from the original on 2009-08-27, retrieved 2008-09-06. This page has photos of a J-5 and two J-4s, one a cutaway.
  11. ^ Image Galleries by Gary and Janet Brossett: Experimental Aircraft Association AirVenture Museum – Oshkosh, WI, archived from the original on 2008-12-12, retrieved 2008-09-06. This page has a photo of an R-790A.
  12. ^ Old Rhinebeck Aerodrome – Wright Whirlwind J-5, retrieved 2009-12-13.
  13. ^ New England Air Museum – Engine Profile: Lawrance J-1, archived from the original on 2011-07-17, retrieved 2009-12-13.
  14. ^ New England Air Museum in Windsor Locks, Connecticut, archived from the original on 2010-04-10, retrieved 2009-12-13. The section "Images from Kimble D. McCutcheon" has photos of the museum's J-1.
  15. ^ Approved Type Certificate No. 13 (ATC 13) data sheet[permanent dead link], available from the FAA's Regulatory and Guidance Library Archived 2016-11-12 at the Wayback Machine.
  16. ^ «Модельные обозначения авиационных двигателей США» Архивировали 2008-08-20 в The Wayback Machine , раздел I, с. 11 (TIF Image) Архивировано 2016-03-04 на The Wayback Machine .
  17. ^ Дизайн машины (получен 30 мая 2017 г.)

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