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  • Chapter 1: Aircraft Engines › Combustion Section › Exhaust Section

    main path of flow by passing through the clearance between the turbine disc and the inner cone. The exhaust cone assembly is the terminating component of the basic engine. The remaining component (the exhaust nozzle) is usually considered an airframe ... units. For this reason, some means of insulation had to be devised. There are several suitable methods of protecting the fuselage structure; two of the most common are insulation blankets and shrouds…

  • Glossary

    turbocharger uses a small radial inflow turbine in the exhaust system to drive a centrifugal-type air compressor on the turbine shaft. The compressed air is directed into the engine cylinders to increase power. Turbo-compound engine. A reciprocating engine ... that has power recovery turbines in its exhaust system. The power extracted from the exhaust by these turbines is directed into the engine crankshaft through a fluid coupling. Turbofan engine. A type of gas turbine engine that…

  • Chapter 1: Aircraft Engines › Gas Turbine Engines › Types & Construction

    reflected in the applicable maintenance manuals. One of the greatest single factors influencing the construction features of any gas turbine engine is the type of compressor or compressors for which the engine is designed. Four types of gas turbine engines ... power aircraft. They are the turbofan, turboprop, turboshaft, and turbojet. The term “turbojet” was used to describe any gas turbine engine used in aircraft. As gas turbine technology evolved, these other engine types were developed to take the place…