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The Turbomeca TM 333 is a turboshaft engine manufactured by French company Turbomeca and designed for helicopters weighing 4-5 tonnes.[1] It first ran in August 1981 and was introduced commercially in the mid 1980s.[1] It was the first Turbomeca engine to use a single stage turbine, making it more compact than its predecessors.[1] In its original design, the engine was rated at 750 continuous horsepower, though it was designed to allow for future power increases,[1] and the later 2B2 variant made 1,100 horsepower.[2]

TM 333
Type Turboshaft
National origin France
Manufacturer Turbomeca
First run 1981
Major applications HAL Dhruv

Variants


TM 333 2B2
The TM 333 2B2 powered early versions of the HAL Dhruv, though it was replaced by the Shakti engine, which was jointly developed by HAL and Turbomeca.[2]
TM 333 2M2
The TM333 2M2 is used on the HAL Cheetal and Chetan, upgraded versions of the Cheetah and Chetak, respectively.[3]

Applications



Specifications (TM 333 2M2)


Data from EASA TCDS E.030 TM333 Series Issue 05 [4]

General characteristics

Components

Performance


See also


Related lists


References


  1. "TM.333; a new generation turboshaft" (PDF). Flight International. 1 January 1983. Retrieved 13 April 2017.
  2. "Military engines: Local power". Flightglobal. 1 May 2007. Retrieved 13 April 2017.
  3. "Gaining altitude". Flightglobal. 21 February 2006. Retrieved 13 April 2017.
  4. EASA E.030 www.easa.europa.eu - Retrieved: 7 December 2021



На других языках


[de] Turbomeca TM 333

Die Turbomeca Makila ist eine Wellenturbine des französischen Herstellers Turboméca speziell für den Antrieb von Hubschraubern mit einem Gewicht von fünf bis sechs Tonnen.
- [en] Turbomeca TM 333

[fr] Turbomeca TM 333

Le Turbomeca TM 333 est un turbomoteur conçu pour propulser des hélicoptères de 5 à 6 tonnes. Produit à 250 exemplaires, il a trouvé sa première utilisation commerciale dans l'hélicoptère indien Dhruv.



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