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Warner Scarab

From Wikipedia, the free encyclopedia
(Redirected fromWarner R-500)
American aircraft engine
Scarab
Preserved Warner Scarab
TypeRadial engine
ManufacturerWarner Aircraft Corporation
First runNovember 1927

TheWarner Scarab is an American seven-cylinderradialaircraft engine, that was manufactured by theWarner Aircraft Corporation ofDetroit,Michigan in 1928 through to the early 1940s. In military service the engine was designatedR-420.

Variants

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Scarab S-50
A 7-cyl. air-cooled radial engine introduced in 1928. With a bore and stroke of 4.25 inches and a compression ratio of 5.2:1, the Scarab developed 125 hp (93 kW) at 2,050 rpm from 422 cu in (7 L) with a dry weight of 285 lb (129 kg).
Scarab Junior
A 5-cyl. version introduced in 1930 developing 90 hp (67 kW) at 2,125 rpm from 301 cu in (5 L) with a dry weight of 230 lb (104 kg).
The R-500-7 Super Scarab model 165 displayed atMuseo dell'Aria e dello Spazio in San Pelagio,Due Carrare,Province of Padua.
Super Scarab SS-50/50A
Increased cylinder bore to 4.625 inches to develop 145 hp (108 kW) at 2,050 rpm from 499 cu in (8 L) with a dry weight of 303 lb (137 kg).[1]
Super Scarab SS-165
Increased compression ratio from 5.2:1 to 6.4:1 to develop 165 hp (123 kW) at 2,100 rpm with a dry weight of 341 lb (155 kg).
Super Scarab SS-185
Increased cylinder bore to 4.875 inches, developing 185 hp (138 kW) at 2175 rpm from 555 cu in (9 L), with a dry weight of 344 lb (156 kg).
R-420
Military designation of the Scarab.
R-500
Military designation of the Super Scarab 165.
R-550
Military designation of the Super Scarab 185.
145
Alternative designation for the Warner Super Scarab SS-50/50A .
165
Alternative designation for the Warner Super Scarab 165 .
185
Alternative designation for the Warner Super Scarab 185 (Primarily a helicopter application).

Applications

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Among the many uses for the Scarab, the engine was fitted to theCessna Airmaster and theFairchild 24 (UC-61 or Argus). Notably, in 1942, it was put into use powering theSikorsky R-4, the first helicopter to be put into production.

Many of these reliable engines soldier on today, still powering the aircraft to which they were originally mounted. The Warner 145 and 165 hp engines are the most commonly seen of the small radials for US-built pre-World War II era aircraft, in large part because of good parts availability due to the engines having been used on World War II Fairchild UC-61s and Meyers OTWs.

Warner engines are also in demand as realistically sized, though far more powerful, replacement powerplants for many replica or restored World War I era airplanes which were originally fitted withrotary engines.

Application list

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Specifications (Scarab 50)

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Warner Scarab engine advertisement for 1928 in Aero Digest

Data from FAA Type Certificate Data Sheet (TCDS).,[2] Jane's all the World's Aircraft 1938[3]

General characteristics

  • Type: Seven-cylinder, air-cooled, radial piston engine
  • Bore: 4.25 in (108 mm)
  • Stroke: 4.25 in (108 mm)
  • Displacement: 422 cu in (6.92 L)
  • Length: 29 in (740 mm)
  • Diameter: 36.5625 in (928.69 mm)
  • Height: 36.5 in (930 mm)
  • Dry weight: 292 lb (132 kg)

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cylinder
  • Fuel system: Stromberg NA-5SA carburetor or Holley equivalent
  • Fuel type: 67octaneAvgas
  • Oil system:Dry sump
  • Cooling system: Air-cooled

Performance

See also

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Logo of Scarab engines.

Related development

Comparable engines

Related lists

References

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  1. ^Warner Engine Company."Engine Specifications"(PDF).warnerenginecompany.com.Archived(PDF) from the original on 2022-05-20.
  2. ^TYPE CERTIFICATE DATA SHEET NO. E-2(PDF). DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. Archived fromthe original(PDF) on 2022-05-12.
  3. ^Grey, C.G.; Bridgman, Leonard, eds. (1938).Jane's all the World's Aircraft 1938. London: Sampson Low, Marston & company, ltd. p. 103d.

External links

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Wikimedia Commons has media related toWarner Scarab.
Names
Designations
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)
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