Impacts of low-pressure (LP) compressors’ fouling of a turbofan upon operational-effectiveness of a military aircraft

Some in-service deterioration in any mechanical device, such as an aircraft’s gas-turbine engine, is inevitable. However, its extent and rate depend upon the qualities of design and manufacture, as well as on the maintenance/repair practices followed by the users. As a result of experiencing deterioration (of the engine as a whole or any of its components individually), an engine will seek a different steady operating point relative to that for an engine with no deterioration. This results in changes in the available thrust from the engine(s) at the same TETs and/or rotational-speeds. Any reduction in the available thrust at specified engine settings, especially maximum available thrust from the engines, will have a significant adverse effect upon the aircraft’s operational-performance. These adverse effects can be reduced by having a better knowledge of the effects of each such deterioration on the aircraft’s operational-performance. Subsequently improvements can be made in the design and manufacture of adversely-affected components as well as in maintenance and repair practices.