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[6] [7] In July 1969, this joint venture was superseded by Motoren- und Turbinen-Union GmbH (MTU), which took over the aircraft engine and high-speed diesel engine activities of both MAN Turbo and Daimler-Benz. [6] [7] MTU München was responsible for aircraft engines, while MTU Friedrichshafen was responsible for diesel engines and other gas ...
Korail Diesel Hydraulic Car by "Saemaul" Train, MTU 12V 396TC-13(Early type only) MTU 16V 396TC-13(Mid, late type) MTU 8V 183TC-12( For HEP engine. Mid, late type only) Voith Gravita Locomotive family; New Zealand DL class locomotive; NIR Class 4000; South African Class 45-000, one MTU 20V 4000 R63L engine; Krauss-Maffei ML 4000, two Maybach ...
MTU derives from Motoren- und Turbinen-Union meaning 'Motor (Engine) and Turbine Union'. MTU Friedrichshafen remained a subsidiary of DaimlerChrysler until 2006 when it was sold off to the EQT IV private equity fund, becoming a part of the Tognum Corporation .
Europrop was established in 2002. [2] One year after its inception the TP400 was selected by Airbus Military to design the engine to power the A400M. [9] In 2004, work began on analyzing the engine design, with the initial ground tests taking place a year later.
MTU Turbomeca Rolls-Royce GmbH (MTR) is a multinational engine manufacturer established to develop, manufacture, and service the MTR390 turboshaft engine. It is a joint venture by three European aero-engine manufacturers, Germany 's MTU Aero Engines , France 's Turbomeca and Britain 's Rolls-Royce .
The MTU Turbomeca Rolls-Royce MTR390 is a turboshaft developed for light helicopter applications by MTU Turbomeca Rolls-Royce (MTR). The engine is designed to power helicopters in the weight range of 5-7 tonnes in both single and twin engine configurations. So far the only application is the Eurocopter Tiger. Test runs of the MTR390 began in ...
Together with the German company MTU (Motoren-und-Turbinen-Union), the two companies produced parts for the CF6-50 engine powering the Airbus A300. At the same time, and since the mid-1960s, Snecma began conducting a series of thermodynamic, aerodynamic and acoustic studies to establish the main characteristics of the M56 engine.
The engine requirements to meet the Panavia MRCA specification were significant advances over current engines in thrust-to-weight ratio, fuel consumption and size. The final selection of the engine for the MRCA was made between a new European collaboration, Turbo Union , with the RB199, and Pratt & Whitney who proposed the JTF16. [ 2 ]