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CLERGET  9B Specifications


Type

9-cylinder air-cooled rotary engine.

Bore:

120 mm (4.72 in)

Stroke:

160 mm (6.30 in)

Displacement:

16.29 L (993.8 cu in)

Dry weight:

175 kg (385 lb)

Fuel system:

Tampier Bloc-tube carburettor

Cooling system:

Air-Cooled

Ignition system:

2 Magneto's

Power output:

130 hp (96 kW) at 1,250 rpm

Compression ratio:

4.56 : 1

i

CONTENTS


Sample Drawings

1

3

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Clerget 9B Aero Engine

By Pierre Jansen

PJVision

    Visualization Projects, The Netherlands


Clerget-Blin - Société Clerget-Blin et Cie - was a French precision engineering company formed in 1913 by the engineer and inventor Pierre Clerget and industrialist Eugène Blin.

The Clerget-Blin company mainly produced aircraft engines. Their successful rotary engine designs were additionally built in Britain by companies such as Gwynnes Ltd,Ruston Proctor and Gordon Watney, to increase the production in the times of World War I. If any engine could be said to be the standard power unit of the Camel then it was the 130 h.p. Clerget 9B or later the 9BF up until September 1918.


The Clerget 9B Plan set, 120 sheets with full size dimensions in PDF format,
are available for downloading.

Click the Download button below to navigate to the download page.