Affiliation:
1. Hamilton Standard Division of United Aircraft Corp., Windsor Locks, Conn.
Abstract
An introduction to the fundamentals of turbine engine multiple fault diagnosis and its relationship to engine parameter selection and measurement requirements is presented. The influence of the type (thermodynamic cycle) of the engine to be diagnosed, and the nature of its expected problems, on the required parameters and the attendant measurement repeatability requirements are discussed.
Cited by
44 articles.
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