Rolls-Royce Holdings plc RB199 Jet Engine

Description
The RB199 is a 3-shaft reheated turbofan engine, with three low pressure (LP), three intermediate pressure (IP) and six high pressure (HP) compressor stages, powered by two single-stage turbines (HP and IP) and a 2-stage LP turbine. The combustion system is of annular vaporising design. Engine control is by a Full Authority Digital Engine Control (FADEC) system and features an integral thrust reverser
Description
The RB199 is a 3-shaft reheated turbofan engine, with three low pressure (LP), three intermediate pressure (IP) and six high pressure (HP) compressor stages, powered by two single-stage turbines (HP and IP) and a 2-stage LP turbine. The combustion system is of annular vaporising design. Engine control is by a Full Authority Digital Engine Control (FADEC) system and features an integral thrust reverser

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Description
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RB199 Jet Engine -  - Rolls-Royce Holdings plc
London, United Kingdom
RB199 Jet Engine
RB199 Jet Engine
The RB199 is a 3-shaft reheated turbofan engine, with three low pressure (LP), three intermediate pressure (IP) and six high pressure (HP) compressor stages, powered by two single-stage turbines (HP and IP) and a 2-stage LP turbine. The combustion system is of annular vaporising design. Engine control is by a Full Authority Digital Engine Control (FADEC) system and features an integral thrust reverser

The RB199 is a 3-shaft reheated turbofan engine, with three low pressure (LP), three intermediate pressure (IP) and six high pressure (HP) compressor stages, powered by two single-stage turbines (HP and IP) and a 2-stage LP turbine. The combustion system is of annular vaporising design. Engine control is by a Full Authority Digital Engine Control (FADEC) system and features an integral thrust reverser

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Technical Specifications

  Rolls-Royce Holdings plc
Product Category Combustion Engines
Product Name RB199 Jet Engine
Fuel Type Jet Fuel
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