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Pratt & Whitney R-1690 Hornet

9-cylinder radial engine family

Pratt & Whitney R-1690 Hornet

9-cylinder radial engine family

FieldValue
nameR-1690 Hornet
imageFile:Pratt & Whitney R-1690 Hornet jaypee.jpg
captionPratt & Whitney Hornet, at the Deutsches Museum, Munich.
engine_typeRadial engine
national_originUnited States
manufacturerPratt & Whitney
first_runJune 1926
major_applications
number_built2,944
developed_into

The Pratt & Whitney R-1690 Hornet was a widely used American aircraft engine. Developed by Pratt & Whitney, 2,944 were produced from 1926 through 1942. It first flew in 1927. It was a single-row, 9-cylinder air-cooled radial design. Displacement was 1,690 cubic inches (27.7 L). It was built under license in Italy as the Fiat A.59. In Germany, the BMW 132 was a developed version of this engine. The R-1860 Hornet B was an enlarged version produced from 1929.

Variants

;R-1690-3: 525 hp ;R-1690-5: 525 hp ;R-1690-11: 775 hp ;R-1690-13: 625 hp ;R-1690-S5D1G: 700 hp ;R-1690-52: 750 hp ;R-1690-SDG: ;R-1690-S1EG: 750 hp ;R-1690-S2EG: ;R-1690-25: 850 hp ;R-1690-S1C3G: 1,050 hp ;Fiat A.59 R.: License built in Italy with reduction gearing. ;Fiat A.59 R.C.: License built in Italy with reduction gearing and supercharger. ;BMW Hornet:License production of the Hornet in Germany, independently developed as the BMW 132.

Applications

  • Bach Air Yacht
  • Bellanca 31-40
  • Boeing 80
  • Boeing Model 95
  • Boeing Model 299
  • Burnelli UB-14
  • Douglas O-38
  • Focke-Wulf Fw 200 V1
  • Gee Bee Model R-2 (1933)
  • Gee Bee R 1/2 Super Sportster
  • Granville-Miller-de Lackner R-6H "Q.E.D."
  • Junkers Ju 52
  • Junkers Ju 86
  • Junkers W 34
  • Keystone B-3
  • Lockheed Model 14 Super Electra (L-14H)
  • Lockheed Lodestar (C-56A, C-56B, C-56C, C-56D, C-56E, C-59/Mk 1a)
  • Martin BM
  • Martin XB-14
  • Vought O2U Corsair
  • Sikorsky S-40A
  • Sikorsky S-42
  • Sikorsky S-43
  • Wedell-Williams Model 44

Engines on display

  • There is a R-1690 on display at the New England Air Museum, Bradley International Airport, Windsor Locks, CT.

Specifications (R-1690 S1E-G)

R-1690 with chamber walls cut away to show internal workings

and start a new, fully formatted line with --

  • 789 hp at 2,300 rpm for takeoff
  • 740 hp at 2,250 rpm at 7000 ft |power/weight=0.78 hp/lb

References

Notes

Bibliography

References

  1. link. (2008-01-26 Retrieved: 25 October 2008)
  2. http://neam.org/index.php?option=com_content&view=article&layout=edit&id=1129 "Pratt & Whitney R-1690 Hornet"
  3. Tsygulev. (1939). "Aviacionnye motory voennykh vozdushnykh sil inostrannykh gosudarstv (Авиационные моторы военных воздушных сил иностранных государств)". Gosudarstvennoe voennoe izdatelstvo Narkomata Oborony Soyuza SSR.
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