Annular combustion chamber
This type of combustion chamber consists of a single flame tube, completely annular in form, which is contained in an…
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This type of combustion chamber consists of a single flame tube, completely annular in form, which is contained in an…
There are three main types of combustion chamber in use for gas turbine engines. These are the multiple chamber, the…
Fuel is supplied to the airstream by one of two distinct methods. The most common is the injection of a…
The combustion chamber (fig. 4-1) has the difficult task of burning large quantities of fuel, supplied through the fuel spray…
Materials are chosen to achieve the most cost-effective design for the components in question, in practice for aero engine design…
Where high pressure ratios on a single shaft are required it becomes necessary to introduce airflow control into the compressor…
Each stage of a multi-stage compressor possesses certain airflow characteristics that are dissimilar from those of its neighbour; thus to…
Rotors In compressor designs (fig. 3-10) the rotational speed is such that a disc is required to support the centrifugal…
During operation the rotor is turned at high speed by the turbine so that air is continuously induced into the…
An axial flow compressor (fig. 3-7 and fig. 3-8) consists of one or more rotor assemblies that carry blades of…