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The '''Pratt & Whitney R-2270''' was an American air-cooled ] ]. Displacing {{convert|2270|cuin|L|abbr=on}}, it was ]'s first two-row radial engine,<ref name="AAHS">''AAHS Journal'', 1971, p.118</ref> developed using parts from existing ] and ] engines to produce an experimental engine.<ref name="Schlaifer">Schlaifer and Heron 1950, p.686</ref> Design of the engine was begun in January 1929;<ref name="Schlaifer"/> it first ran on May 14, 1930, and in April 1931<ref name="Schlaifer"/> was test-flown in a ] aircraft.<ref name="AAHS"/> The R-2270 was intended as a purely experimental engine;<ref name="Schlaifer"/> studies indicated a smaller engine would be more favored by the market,<ref name="AAHS"/> began development of the ] engine in April 1931.<ref name="Schlaifer"/> The '''Pratt & Whitney R-2270''' was an American air-cooled ] ]. Displacing {{convert|2270|cuin|L|abbr=on}}, it was ]'s first two-row radial engine,<ref name="AAHS">''AAHS Journal'', 1971, p.118</ref> developed using parts from existing ] and ] engines to produce an experimental engine.<ref name="Schlaifer">Schlaifer and Heron 1950, p.686</ref> Design of the engine was begun in January 1929;<ref name="Schlaifer"/> it first ran on May 14, 1930, and in April 1931<ref name="Schlaifer"/> was test-flown in a ] aircraft.<ref name="AAHS"/> The R-2270 was intended as a purely experimental engine;<ref name="Schlaifer"/> studies indicated a smaller engine would be more favored by the market,<ref name="AAHS"/> and Pratt & Whitney began development of the ] engine in April 1931.<ref name="Schlaifer"/>


== Applications == == Applications ==

Revision as of 01:25, 18 December 2024

1930 14-cylinder radial piston engine by Pratt & Whitney

R-2270
Type Radial engine
National origin United States
Manufacturer Pratt & Whitney
First run 1930
Number built 1

The Pratt & Whitney R-2270 was an American air-cooled radial aircraft engine. Displacing 2,270 cu in (37.2 L), it was Pratt & Whitney's first two-row radial engine, developed using parts from existing Wasp and Hornet engines to produce an experimental engine. Design of the engine was begun in January 1929; it first ran on May 14, 1930, and in April 1931 was test-flown in a Boeing Model 40B aircraft. The R-2270 was intended as a purely experimental engine; studies indicated a smaller engine would be more favored by the market, and Pratt & Whitney began development of the R-1830 engine in April 1931.

Applications

See also

Related development

Related lists

References

Notes

  1. ^ AAHS Journal, 1971, p.118
  2. ^ Schlaifer and Heron 1950, p.686

Bibliography

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
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: