Turbine Troubles

Jet turbine engines are designed with multiple redundancies to ensure safety and reliability during operation.

These redundancies include multiple compressor and turbine stages, which allow the engine to continue functioning even if one stage underperforms or fails.

Dual or triple-redundant fuel systems ensure a consistent fuel supply, while separate hydraulic and electrical systems maintain control over essential functions.

Modern jet engines also feature redundant computer systems, such as FADEC (Full Authority Digital Engine Control), to monitor and adjust engine performance.

Additionally, engines are built with fail-safe mechanisms like containment rings to prevent debris from escaping in the event of a turbine blade failure.

These redundancies are critical for maintaining engine performance and safety, especially during long flights or adverse conditions.