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Bentley BR1

Aircraft Engines

The Bentley BR.1, first known as the A.R.1 for Admiralty Rotary and later as the Bentley Rotary, was a nine-cylinder air-cooled rotary aircraft engine of the First World War. W. O. Bentley, then a Royal Navy officer acting as liaison between the Royal Naval Air Service and the engine builders, had been sent to improve the licence-built Clerget 9B, which tended to overheat and seize. At Humber's works he reworked the design with aluminium cylinders, shrunk-in liners that let ordinary piston rings replace the fragile obturator rings, and a longer stroke, lifting output to about 150 horsepower. The engine was standardised for the Sopwith Camel in Royal Naval Air Service squadrons and powered most of the Camels they flew, although supply never allowed it to replace the Clerget across British service. It cost the Admiralty far less than the Clerget and led directly to the larger BR.2.

Facts
Classification
Configuration
Rotary 1
Cylinder Count
9 1
Connections

Invented By

W. O. Bentley, Figures
Source Bentley BR1 (Wikipedia)

Of Make

Source Bentley BR1 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Bentley BR1 (Wikipedia)Design and development
Quote, Design and development
At Humber's works, Bentley was able to implement his ideas resulting in a rotary engine
Sources
1. Bentley BR1 (Wikipedia)
  • Specifications, cylinders
    Type: 9-cylinder air-cooled rotary engine
  • Invented By: W. O. Bentley, Lead
    Designed by the motor car engine designer W. O. Bentley
  • Of Make: Bentley, Design and development
    but later called the BR.1 ("Bentley Rotary")
  • Part Of: Sopwith Camel, Lead, vehicle
    BR.1s powered the majority of Sopwith Camels flown by the Royal Naval Air Service (RNAS)
  • In Group: Piston Aero Engines, Lead, group
    The Bentley BR.1 is a British rotary aircraft engine of the First World War.
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