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SAE AIR1289 Rev A

Evaluation of Helicopter Turbine Engine Linear Vibration Environment
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SAE AIR1289 Rev A

Evaluation of Helicopter Turbine Engine Linear Vibration Environment

PUBLISH DATE 1992
PAGES 14
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This SAE Aerospace Information Report (AIR) outlines a recommended procedure for evaluation of the vibration environment to which the gas turbine engine powerplant is subjected in the helicopter installation. This analysis of engine vibration is normally demonstrated on a one-time basis upon initial certification, or after a major modification, of an engine/helicopter configuration. This AIR deals with linear vibration as measured on the basic case structure of the engine and not, for example, torsional vibration in drive shafting or vibration of a component within the engine such as a compressor or turbine airfoil. In summary, this AIR discusses the engine manufacturer’s "Installation Test Code" aspects of engine vibration and proposes an appropriate measurement method.
SDO SAE: SAE International
Document Number AIR1289
Publication Date March 1, 1992
Language en - English
Page Count 14
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
March 1, 1992 AIR1289A Revision
Sept. 1, 1976 AIR1289 Revision