Misplaced Pages

Pratt & Whitney R-1690 Hornet

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
(Redirected from Fiat A.59) "Pratt & Whitney Hornet" redirects here. For the Pratt & Whitney R-1860 Hornet B, see Pratt & Whitney R-1860.
This article includes a list of general references, but it lacks sufficient corresponding inline citations. Please help to improve this article by introducing more precise citations. (April 2018) (Learn how and when to remove this message)
R-1690 Hornet
Pratt & Whitney Hornet, at the Deutsches Museum, Munich.
Type Radial engine
National origin United States
Manufacturer Pratt & Whitney
First run June 1926
Major applications Boeing 80
Lockheed Lodestar
Sikorsky S-42
Vought O2U Corsair
Number built 2,944
Developed into Pratt & Whitney R-1860
BMW 132
Mitsubishi Kinsei

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

For the R-1860 Hornet B series, see Pratt & Whitney R-1860.
R-1690-3
525 hp (391 kW)
R-1690-5
525 hp (391 kW)
R-1690-11
775 hp (578 kW)
R-1690-13
625 hp (466 kW)
R-1690-S5D1G
700 hp (520 kW)
R-1690-52
750 hp (560 kW)
R-1690-SDG
R-1690-S1EG
750 hp (560 kW)
R-1690-S2EG
R-1690-25
850 hp (630 kW)
R-1690-S1C3G
1,050 hp (780 kW)
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

Engines on display

Specifications (R-1690 S1E-G)

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

Data from

General characteristics

  • Type: Nine-cylinder single-row supercharged air-cooled radial engine
  • Bore: 6+1⁄8 in (155.6 mm)
  • Stroke: 6+3⁄8 in (161.9 mm)
  • Displacement: 1,690.5 cu in (27.7 L)
  • Length: 50.98 in (1,295 mm)
  • Diameter: 54.41 in (1,382 mm)
  • Dry weight: 1,014 lb (460 kg)

Components

Performance

See also

Related development

Comparable engines

Related lists

References

Notes

  1. Pratt & Whitney - R-1690 page Archived 2008-01-26 at the Wayback Machine 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) (in Russian). Moscow: Gosudarstvennoe voennoe izdatelstvo Narkomata Oborony Soyuza SSR. Archived from the original on 2009-03-24.

Bibliography

  • Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.

External links

Pratt & Whitney aircraft engines
Radial engines
H piston engines
Free-piston gas turbines
Turbojets
Turbofans
Turboprops/Turboshafts
Propfans
Rocket engines
Aeroderivative gas
turbine engines
Subsidiaries
Key people
Joint development aeroengines
See also: Pratt & Whitney Canada aeroengines
Fiat aircraft engines
Piston engines
Turbine engines
United States military piston aircraft engine designation system
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)
Categories: