Hall-Scott A-7

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Template:Short description

A-7
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Hall-Scott A-7a at the National Air and Space Museum
Type Piston aero engine
National origin United States of America
Manufacturer Hall-Scott Motor Car Company
First run 1910s

The Hall-Scott A-7 was an early liquid-cooled aircraft engine manufactured by the Hall-Scott company of Berkeley, California. Using a straight-4 configuration, the engine developed 90 horsepower (67 kW) as the A-7 and 100 horsepower (75 kW) as the A-7a. In service these engines suffered from reliability problems and were prone to catch fire while in operation.

Variants

Applications

In 2017 about seven A-7a engines were still in use in Edwardian racing cars, mostly in the United Kingdom.

Engines on display

A Hall-Scott A-7a on display at the Hiller Aviation Museum
A Hall-Scott A-7a aircraft engine on display at the Hiller Aviation Museum

Specifications (A-7a)

File:Hall-Scott A-7A.jpg
Hall-Scott A-7a at the Museum of Flight

Data from Airplane Engine Encyclopedia [1]

General characteristics

Components

  • Valvetrain: 1 intake and 1 exhaust valve per cylinder, SOHC
  • Fuel system: Miller or Zenith carburetors
  • Cooling system: Water

Performance

See also

Related lists

References

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  1. ↑ a b c Script error: No such module "citation/CS1".

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  • Gunston, Bill. (1986). World Encyclopaedia of Aero Engines. Patrick Stephens: Wellingborough. p. 73

External links

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Template:Hall-Scott aeroengines