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Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1. Intake 2. Low pressure compression 3. High pressure compression ...
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The turboprop at its best flight speed gives significant fuel savings over a turbojet even though an extra turbine, a gearbox and a propeller are added to the turbojet's low-loss propelling nozzle. [24] The turbofan has additional losses from its greater number of compressor stages/blades, fan and bypass duct. [clarification needed]
Pages in category "Turbojet engines" The following 2 pages are in this category, out of 2 total. This list may not reflect recent changes. N. Nose bullet; P. PBS TJ80-120
The Soloviev D-30 (now the Aviadvigatel PS-30) is a Soviet two-shaft low-bypass turbofan engine, officially referred to as a "bypass turbojet" [citation needed].It is one of the most powerful turbofan engines developed in the Soviet Union.
Many early turbojet engines used centrifugal compressors as they were robust and simple to design. Pages in category "Centrifugal-flow turbojet engines" The following 49 pages are in this category, out of 49 total.
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