Renard Type 100
{{Short description|1920s Belgian piston aircraft engine}}
{{Use dmy dates|date=August 2022}}
{{Use British English|date=August 2022}}
| {{Infobox aircraft begin
| name=Type 100 | image= | caption= }}{{Infobox aircraft engine |type=5-cylinder air-cooled radial piston engine |manufacturer=Société Anonyme des Avions et Moteurs Renard |designer= |national origin=Belgium |first run=1927 |major applications= |produced= |number built= |developed from= |variants with their own articles= }} |
The Renard Type 100 was a five-cylinder, radial piston engine, designed and produced in the late 1920s and early 1930s by Société Anonyme des Avions et Moteurs Renard (Renard) in Belgium.
Design and development
Specifications (Type 100)
{{pistonspecs|
|ref=Jane's all the World's Aircraft 1928{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=3d}}
|type=5-cylinder aircooled radial piston engine
|bore={{cvt|120|mm}}
|stroke={{cvt|140|mm}}
|displacement={{cvt|7.92|L}}
|length=
|diameter={{cvt|1080|mm}}
|width=
|height=
|weight=
|valvetrain=2 cam rings, pushrods and rockers operating one inlet and one exhaust valve per cylinder
|supercharger=
|turbocharger=
|fuelsystem= one carburetor supplying mixture to a crankcase plenum, then by radial pipes to inlet valves
|fueltype=
|oilsystem=dry sump pressure
|coolingsystem=air-cooled
|power=normal:{{cvt|100|hp|order=flip}} at 1,400 rpm; Maximum:{{cvt|120|hp|order=flip}} at 1,580 rpm
|specpower=
|compression=5.2:1
|fuelcon=
|specfuelcon=0.301 kg/(kW hour) (0.495 lb/(hp hour))
|oilcon=
|power/weight=
|designer=
|reduction_gear=direct drive
|general_other=dual ignition system
|components_other=
|performance_other=
}}
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
References
{{Reflist}}