| 词条 | Turbomeca TM 333 | ||||||||||||||
| 释义 |
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.[5] Variants
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]
The TM333 2M2 is used on the HAL Cheetal and Chetan, upgraded versions of the Cheetah and Chetak, respectively.[3] Applications
References1. ^1 2 3 {{cite web | url=https://www.flightglobal.com/FlightPDFArchive/1983/1983%20-%200023.PDF | title=TM.333; a new generation turboshaft | publisher=Flight International | date=1 January 1983 | accessdate=13 April 2017}} 2. ^1 {{cite web | url=https://www.flightglobal.com/news/articles/military-engines-local-power-213590/ | title=Military engines: Local power | publisher=Flightglobal | date=1 May 2007 | accessdate=13 April 2017}} 3. ^{{cite web | url=https://www.flightglobal.com/news/articles/gaining-altitude-204846/ | title=Gaining altitude | publisher=Flightglobal | date=21 February 2006 | accessdate=13 April 2017}} External links
3 : Turboshaft engines 1970–1979|Turbomeca aircraft engines|Mixed-compressor gas turbines |
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