Armengaud-Lemale gas turbine

In 1901, Charles Lemale obtained a patent for a gas turbine and in 1903 he founded the Société Anonyme des Turbomoteurs with Rene Armengaud.

The society proposed a number of new technologies including hollow turbine blades, combustion reheat and compressor stage inter-cooling.

The air fuel mixture was fired by a hot wire with combustion products cooled by water spray.

Exhaust gasses were expanded in a nozzle before acting on a modified 25 hp (19 kW) de Laval steam turbine with a 6 in (152 mm) wheel which ran at 20,000 rpm.

[6] Kerosene was injected and burned in a compressed air stream increasing the pressure actuating the torpedo's propelling engine.

Diagram of the Armengaud-Lemale water cooled combustion chamber: A -Oil enters under pressure and is atomised B -Air inlet C -Combustion chamber E -Cooling water inlet G -Combustion Chamber Housing H -Nozzle K -Turbine wheel