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Turbomeca Turmo

From Alfawiki
Turbomeca
IndustryAerospace, Engine manufacturing
Headquarters
France
ProductsTurboshaft and turboprop engines (Turmo series)
ParentRolls-Royce (collaboration)
Template:Infobox aircraft engine

The Turbomeca Turmo series comprises French-made turboshaft engines primarily engineered for helicopter use. Originating from the earlier Turbomeca Artouste, the more recent variants achieve power outputs up to . A turboprop configuration was also created for the Bréguet 941 transport aircraft.

Currently, production continues through a collaboration with Rolls-Royce, while licensed manufacturing occurs in China at Changzhou Lan Xiang Machinery Works under the name WZ-6, and in Romania by Turbomecanica, Bucharest, designated as the Turmo IV-CA.

Design and development

Initially, the Turmo featured a single-stage centrifugal compressor, an annular combustion chamber, and a single-stage turbine, producing an initial power output of via a single-stage free power turbine.

During the early postwar period of helicopter advancement, Turbomeca developed the Turmo engine to power gas producers that supplied cold and hot rotor tip-jets. This design utilized the free power turbine to efficiently deliver high mass-flow air.

Variants

Information sourced from Jane's All the World's Aircraft 1957–58

Turmo I
The original model; maximum continuous gearbox output of at 3,000 rpm with a gas generator speed of 33,750 rpm.
Turmo II
An improved version offering maximum continuous output of at a gas generator speed of 34,000 rpm.
Turmo III
Equipped with a two-stage free power turbine and a pressure ratio of 5.7:1; maximum shaft output , continuous rating at 33,400 rpm.
Turmo IIIC series
Includes multiple variants providing up to max output for Super Frelon helicopters in production and military applications.
Turmo IIID series
Turboprop versions designed for STOL transports such as the proposed Breguet Br 942, delivering between and .
Turmo IIIF
Rated at , utilized on high-speed rail vehicles including the Turbotrain and Turboliner.
Turmo IVB/IVC
Versions intended for military (IVB) and civilian (IVC) use respectively.
Turmo IV-CA
Produced under license in Romania.
Turmo VI
A sophisticated turboprop featuring two axial stages plus a centrifugal compressor and dual free power turbines, rated at at 32,000 rpm.
Turmo XII
Capable of producing , employed on Class T 2000 Turbotrain and TGV 001 experimental projects.
WZ-6
Chinese license-built variant manufactured by Changzhou Lan Xiang Machinery Works.

Applications

Turboshaft
Turboprop
Automobile
Train

External links