Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 15-May-2020

A project proposed by Edouard Maillet. It is an X-engine, with a "double connecting rod".

Motor Maillet, front view
“Maillet, front view”

-It has 16 cylinders in total, and it had the main advantage of suppressing the lateral reactions of the piston on the cylinder wall.

Motor Maillet, side view
“Maillet, side view”

Classic connection-rod system
“Classic connection-rod system”

-The Maillet system, we see in two stages in "B" and "C".

Maillet's connection-rod system
“Maillet's connection-rod system”

-A schematic representation of the "connection" between each piston can be represented as in the following figure.

Maillet, rod-piston connections
“Rod-piston connections”

-It consisted of two crossed-over 8-cylinder engines. The engine was air cooled and used the 2-stroke cycle with the intention of complying with the “Coupe Deutsch de la Meurthe” rules.

-With a gearbox the 5,000 rpm of the engine was reduced to 2,140 rpm for the propeller.

-The estimated power was 1,425 hp but the real power was 1,280 hp. The two centrifugal compressors to fill the cylinders already consumed 130 hp.

Engines of MAILLET

Model: 16 cyl. X-engine

Arquitecture: 2-stroke16-cylinder X-engine
Cooling:
Total Displacement:
Bore / Stroke:
Power: 1280 CV @ 5000 rpm
Weight:

Other details:
Maillet engine front view

"Maillet engine front view"