词条 | Wright R-2600 Twin Cyclone | ||||||||||||||
释义 |
The Wright R-2600 Cyclone 14 (also called Twin Cyclone) was an American radial engine developed by Curtiss-Wright and widely used in aircraft in the 1930s and 1940s. HistoryIn 1935, Curtiss-Wright began work on a more powerful version of their successful R-1820 Cyclone 9. The result was the R-2600 Twin Cyclone, with 14 cylinders arranged in two rows. The {{convert|1,600|hp|kW PS|lk=on|abbr=on}} R-2600-3 was originally intended for the C-46 Commando (being fitted to the prototype CW-20A) and was also the original engine choice for the F6F Hellcat; a running change (one which would not stop production) for the CW-20A, and one in late April 1942 for the second XF6F-1, led to the adoption of the {{convert|2,000|hp|kW PS|abbr=on}} Pratt & Whitney R-2800 in its place for both designs. The Twin Cyclone went on to power several important American-designed World War II aircraft, including the A-20 Havoc, B-25 Mitchell, TBF Avenger, SB2C Helldiver, and PBM Mariner. Over 50,000 R-2600s were built at plants in Paterson, New Jersey, and Cincinnati, Ohio. Variants
Applications
Specifications (GR-2600-C14BB){{pistonspecs| |type=14-cylinder supercharged air-cooled two-row radial engine |ref=Jane's.[1] |bore=6 {{frac|1|8}} in (155.6 mm) |stroke=6 {{frac|5|16}} in (160.3 mm) |displacement=2,604 in3 (42.7 L) |length=62.06 in (1,576 mm) |diameter=55 in (1,397 mm) |width= |height= |weight=2,045 lb (930 kg) |valvetrain=Two pushrod-actuated valves per cylinder with sodium-cooled exhaust valve |supercharger=Single-stage two-speed centrifugal type supercharger, impeller diameter 11 in (280 mm), blower ratio 7.06:1 at slow speed and 10.06:1 at high speed |turbocharger= |fuelsystem=Stromberg PR48A downdraft carburetor with automatic mixture control |fueltype= |oilsystem=Dry sump with one pressure pump and two scavenge pumps |coolingsystem=Air-cooled |power=
|specpower=0.67 hp/in³ (30.6 kW/L) |compression=6.9:1 |fuelcon= |specfuelcon= |oilcon= |power/weight=0.86 hp/lb (1.40 kW/kg) }} See also{{aircontent|see also=
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}} References{{Commons category}}Notes1. ^Jane's 1998, p. 317. 2. ^Witold Liss (1967). The Lavochkin La 5 & 7, number 149. Profile publications Ltd., P.O. Box, 1a North Street, Leatherhead, Surrey, UK. p. 3 Bibliography
3 : Radial engines|Wright aircraft engines|Aircraft piston engines 1930–1939 |
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