Test rig for evaluating active turbine blade tip clearance control concepts

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Lattime, Scott B ^a   Steinetz, Bruce M ^b   Robbie, Malcolm G ^c  

^a OHIO AEROSPACE INSTITUTE   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c ANALEX CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE CLEARANCE CONTROLS; HIGH PRESSURE COMPRESSOR; HIGH PRESSURE TURBINE; MEASUREMENT FEEDBACK; OPERATING CONDITION; PRESSURE AND TEMPERATURE; SPECIFIC FUEL CONSUMPTION; TURBINE BLADE TIP CLEARANCES;

CONTROL SYSTEMS; ENGINES; FUEL CONSUMPTION; GAS TURBINES; PROPULSION; TURBOMACHINE BLADES;

TURBINE COMPONENTS;

EID: 84897767485     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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