Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 28-May-2020

MARTIN & BROUILLET

(France)


They made a small engine and insufficient to power any aircraft but with an expandable range from 3 to 5 cylinders radials, 6 cylinders in V, 2 opposed cylinders, 3 cylinder fan-shape, etc.

Martin & Brouillet ad
“Martin & Brouillet ad”

-It was presented at the X Lépine Competition within the II Salon de l'Aeronautique, and was announced as an extra-light engine.

-In fact it is an external combustion engine in case of running on steam.

-But it also works with compressed air, carbonic acid (see Serpollet and Vuia).

-And in general with any elastic fluid (as it is said verbatim).

-The proper name of the engines was: "Prima" engines.

-It seems evident that the gaseous fluid opening valve is mechanically controlled by a rod and a rocker arm.

-The simplest solution for this type of engine is the ball valve that is automatically lifted by a stud on the piston head.

CO2 engine concept
“CO2 engine concept” (PiP)

The author of this edition of Aeroengines AtoZ, through Aeroteca, collaborated on Version 2 of this video, which is presented here.

To understand the operation of the connecting rods, the 1929 Continental R 670 single-cylinder engine was chosen.

A demonstration of Version 3, improved at the author's suggestion, is also available on YouTube at a later date. This version shows bronze valve guides, improved valve spring movement, and the split crankshaft counterweights and front bearing balls also move.

The design is from Juan Soler, Sant Cugat, Barcelona

Below we show a flash of version 3

Counting also with the coloboration of JMC of Enginys Mecanics in Mataro, Barcelona