NORMSERVIS s.r.o.

SAE AIR1289A

EVALUATION OF HELICOPTER TURBINE ENGINE LINEAR VIBRATION ENVIRONMENT

NORMA vydána dne 1.3.2021

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Informace o normě:

Označení normy: SAE AIR1289A
Datum vydání normy: 1.3.2021
Země: Americká technická norma
Kategorie: Technické normy SAE

Anotace textu normy SAE AIR1289A :


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.

SUBJECT TAXONOMY: Noise, Vibration, Hybrid engines, Turboprop engines, Rotary-wing aircraft
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard