Relative performance comparison between baseline labyrinth and dual brush compressor discharge seals in a T-700 engine test

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1994, Pages

  Hendricks, Robert C ^a   Csavina, Kristine R ^b   Griffin, Thomas A ^b   Kline, Teresa R ^c   Pancholi, Arvind ^d   Sood, Dvandra ^d  

^a NASA GLENN RESEARCH CENTER   (United States)

^b JACOBS TECHNOLOGY   (United States)

^c U S ARMY RESEARCH LABORATORY   (United States)

^d GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CARBIDES; COMPRESSORS; ENGINES; FACINGS; GAS TURBINES;

AIRFLOW DISTRIBUTION; CHROMIUM CARBIDE; ENGINE DYNAMICS; ENGINE OPERATIONS; ENGINE PERFORMANCE; LABYRINTH SEAL LEAKAGE; LOWER PRESSURES; RELATIVE PERFORMANCE;

SEALS;

EID: 84926380540     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/94-GT-266     Document Type: Conference Paper

References (0)