Capacitive measurement of compressor and turbine blade tip to casing running clearance

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 5, Issue , 1996, Pages

  Muller D ^a   Sheard, A G ^b,c   Mozumdar, S ^a   Johann, E ^a  

^a ROLLS ROYCE DEUTSCHLAND LTD AND CO KG   (Germany)

^b Techniche Group Ltd   (United Kingdom)

^c BICC Therrnoheat Ltd   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; GAS TURBINES; TURBOMACHINE BLADES;

APPLICATION REQUIREMENTS; CAPACITIVE MEASUREMENTS; ELECTRICAL SIGNAL; ENGINE TESTING; ESTABLISHED FACTS; INVERSE RELATIONSHIP; MEASUREMENT SYSTEM; TURBINE BLADE TIP;

TURBINE COMPONENTS;

EID: 84930453628     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-349     Document Type: Conference Paper

References (5)

1. Chivers J W H,"A Technique for the Measurement of Blade Tip Clearance in a Gas Turbine," Ph.D. Thesis, Imperial College, London, 1989.
2. Chivers J W H,"A Technique for the Measurement of Blade Tip Clearance in a Gas Turbine," 1989, AIAA 89-2916, 1989.
3. ICappler, G.; Moore, R.; Hourmouziadis, Hochleistung-Turbo-Fan-Triebwerke Ein Familienkonzept, DGLR, 92-03-043, 1992.
4. Sheard A G and Killeen B, A Blade by Blade Tip Clearance Measurement System for Gas Turbine Applications. Trans. ASME, J. of Eng. for Gas Turbines & Power, Vol. 117 No. 2, pp 326-331, 1995.
5. Sheard A G and Turner S R, Electromechanical Measurement of Turbomachinery Blade Tip to Casing Running Clearance. ASME 92-CT-SO, 1992