Engineering:Turbomeca TM 333
From HandWiki
Short description: 1970s French turboshaft engine
| TM 333 | |
|---|---|
| Type | Turboshaft |
| National origin | France |
| Manufacturer | Turbomeca |
| First run | 1981 |
| Major applications | HAL Dhruv |
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]
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
- HAL Dhruv
- HAL Cheetah
- HAL Chetak
Specifications (TM 333 2M2)
Data from EASA TCDS E.030 TM333 Series Issue 05 [4]
General characteristics
- Type: Twin-spool turboshaft
- Length: 1,045 mm (41.1 in)
- Diameter: 454 mm (17.9 in) (width), 745 mm (29.3 in) (height)
- Dry weight: 162.5 kg (358.3 lb)
Components
- Compressor: Two-stage axial, single-stage centrifugal
- Combustors: Annular,reverse flow
- Turbine: Single-stage compressor turbine, single-stage power turbine
Performance
- Maximum power output: 736 kW (987 shp) (maximum continuous)
- Power-to-weight ratio:
See also
Related lists
References
- ↑ 1.0 1.1 1.2 1.3 "TM.333; a new generation turboshaft". Flight International. 1 January 1983. https://web.archive.org/web/20170414082241if_/https://www.flightglobal.com/FlightPDFArchive/1983/1983%20-%200023.PDF.
- ↑ 2.0 2.1 "Military engines: Local power". Flightglobal. 1 May 2007. https://www.flightglobal.com/news/articles/military-engines-local-power-213590/. Retrieved 13 April 2017.
- ↑ "Gaining altitude". Flightglobal. 21 February 2006. https://www.flightglobal.com/news/articles/gaining-altitude-204846/. Retrieved 13 April 2017.
- ↑ EASA E.030 www.easa.europa.eu - Retrieved: 7 December 2021
External links
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