High-Pressure-Turbine Clearance Control Systems: Current Practices and Future Directions

Improved blade-tip sealing in a high-pressure compressor and high-pressure turbine can provide dramatic improvements in specific fuel consumption, time on wing, compressor stall margin, and engine efficiency as well as increased payload and mission range capabilities. Maintenance costs to overhaul l...

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Veröffentlicht in:	Journal of propulsion and power 2004-03, Vol.20 (2), p.302-311
Hauptverfasser:	Lattime, Scott B, Steinetz, Bruce M
Format:	Artikel
Sprache:	eng
Schlagworte:	Turbines
Online-Zugang:	Volltext
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