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NASA NTRS · 20040182413

Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts

Abstract

The objectives of the research presented in this viewgraph presentation are to 1) Design a mechanical ACC system for HPT tip seal clearance management; 2) Design a test rig to evaluate ACC system concepts. We have focused our efforts on designing mechanical ACC systems that articulate the seal shroud via mechanical linkages connected to actuators that reside outside the extreme environment of the HPT. We opted for this style of design due to a lack of high temperature/low profile actuators that are presently available. We have also selected multiple hydraulic actuators for this first generation ACC system. Fuel-draulic actuators are already a well established technology.

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BibTeXRIS

Lattime, Scott B., Steinetz, Bruce M., Robbie, Malcolm G., Erker, Arthur H.. 2004-09-01. Test Rig for Evaluating Active Turbine Blade Tip Clearance Control Concepts. https://ntrs.nasa.gov/citations/20040182413

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