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The initial workshare was divided as follows: Turbomeca produced the compressor, gearbox, accessories and control system, Rolls-Royce manufactured the power turbine stage, while MTU was responsible for the combustor, high-pressure turbine, along with the final assembly of the entire first batch of engines. [20]
Data from Rolls-Royce General characteristics Type: Twin-spool turboshaft/turboprop Length: 37.6 inches (96 cm) Diameter: 21.5 inches (55 cm) Dry weight: 201 pounds (91 kg) Components Compressor: Single-stage centrifugal Turbine: 2 stage GP, 2 stage PT Performance Maximum power output: 240–300 shaft horsepower (180–220 kW) Overall pressure ratio: 6.2 Power-to-weight ratio: 0.67 pounds per ...
Rolls-Royce based the 10-stage HP compressor on an 8-stage run in the RB401 in the mid 1970's followed by a 9-stage run in the RJ.500. The V.2500 would use 10 stages, with the first 4 with variable stators, giving a pressure ratio of 20:1. [4] A single-stage booster was also part of the original configuration.
Rolls-Royce is the world's second-largest maker of aircraft engines [3] (after CFM International) [4] and has major businesses in the marine propulsion and energy sectors. Rolls-Royce was the world's 16th largest defence contractor in 2018 when measured by defence revenues. [5]
The Clyde used a two-shaft design, with an axial compressor based on that of the Metrovick F.2 [4] [5] for the low-pressure section, and a single-sided centrifugal compressor scaled up from the Merlin 46 supercharger [6] as the high-pressure stage, both mounted on the HP shaft and driven by a single stage HP turbine. A single stage power ...
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 .
Rolls-Royce RB.203 Trent; Rolls-Royce RB211; Rolls-Royce Trent; T. Turbo-Union RB199; W. Williams EJ22
The Rolls-Royce AE 3007 (US military: F137) is a turbofan engine produced by Rolls-Royce North America, sharing a common core with the Rolls-Royce T406 (AE 1107) and AE 2100. The engine was originally developed by the Allison Engine Company , hence the "AE" in the model number.
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