ISO 20816-4:2018 機械的振動—機械振動の測定と評価—パート4：3 MWを超えるガスタービン、流体膜ベアリング付き | ページ 2

Foreword

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This document was prepared by Technical Committee ISO/TC 108, Mechanical vibration, shock and condition monitoring, Subcommittee SC 2, Measurement and evaluation of mechanical vibration and shock as applied to machines, vehicles and structures.

This first edition of ISO 20816-4 cancels and replaces ISO 7919-4:2009 and ISO 10816-4:2009, which have been technically revised. It also incorporates the Amendments ISO 7919-4/Amd.1:2017 and ISO 10816-4/Amd.1:2017.

The main change is that the scope has been reduced to exclude large gas turbines with power outputs greater than 40 MW, fluid-film bearings and rated speeds of 1 500 r/min, 1 800 r/min, 3 000 r/min or 3 600 r/min. Such gas turbines are now covered by ISO 20816-2.

A list of all parts in the ISO 20816 series can be found on the ISO website.

Introduction

Documents in the ISO 20816 series have been and are being developed to combine and supersede the ISO 7919 and ISO 10816 series.

ISO 20816-1 is the basic part of the ISO 20816 series that gives the general requirements for evaluating the vibration of various machine types when the vibration measurements are made on both non-rotating and rotating parts. ISO 20816-2 deals with the measurement and evaluation of machine vibration of large gas turbines with certain rotational speeds.

This document provides specific provisions for assessing the vibration of the bearing housings or pedestals and rotating shafts of those gas turbines which are not covered by ISO 20816-2. Measurements at these locations characterize the state of vibration reasonably well. Evaluation criteria, based on previous experience, are presented. These can be used for assessing the vibratory condition of such machines. In those cases where there is a high ratio between the mass of the bearing supports and the rotor, lower values of vibration of the bearing housings or pedestals can be appropriate.

Two criteria are provided for assessing the machine vibration when operating under steady-state conditions. One criterion considers the magnitude of the observed vibration; the second considers changes in the magnitude. In addition, different criteria are provided for transient operating conditions.

The evaluation procedures presented in this document are based on broad-band measurements. However, because of advances in technology, the use of narrow-band measurements or spectral analysis has become increasingly widespread, particularly for the purposes of vibration evaluation, condition monitoring and diagnostics. The specification of criteria for such measurements is beyond the scope of this document. They are provided in greater detail in the relevant parts of ISO 13373 which establish provisions for the vibration condition monitoring of machines.

1 Scope

This document is applicable to land-based gas turbines with fluid-film bearings and power outputs greater than 3 MW and an operating speed under load between 3 000 r/min and 30 000 r/min. In some cases (see the list of exclusions below), this includes other rotating machinery coupled either directly or through a gearbox. The evaluation criteria provided in this document are applicable to the vibration of the main input and output bearings of the gearbox but are not applicable to the vibration of the internal gearbox bearings nor to the assessment of the condition of those gears. Specialist techniques required for evaluating the condition of gears are outside the scope of this document.

This document is not applicable to the following:

• i) gas turbines with power outputs greater than 40 MW at rated speeds of 1 500 r/min, 1 800 r/min, 3 000 r/min or 3 600 r/min (see ISO 20816-2);
• ii) aero-derivative gas turbines (including gas turbines with dynamic properties similar to those of aero-derivatives);

  NOTE ISO 3977-3 defines aero-derivatives as aircraft propulsion gas generators adapted to drive mechanical, electrical or marine propulsion equipment. Large differences exist between heavy-duty and aero-derivative gas turbines, for example, in casing flexibility, bearing design, rotor-to-stator mass ratio and mounting structure. Different criteria, therefore, apply for these two turbine types.

• iii) gas turbines with outputs less than or equal to 3 MW (see ISO 7919-3 and ISO 10816-3);
• iv) turbine driven generators (see ISO 20816-2, ISO 7919-3 and ISO 10816-3);
• v) turbine driven pumps (see ISO 10816-7);
• vi) turbine driven rotary compressors (see ISO 7919-3 and ISO 10816-3);
• vii) the evaluation of gearbox vibration (see this clause) but does not preclude monitoring of gearbox vibration;
• viii) the evaluation of combustion vibration but does not preclude monitoring of combustion vibration;
• ix) rolling element bearing vibration.

This document establishes provisions for evaluating the severity of the following in-situ broad-band vibrations:

• a) structural vibration at all main bearing housings or pedestals measured radial (i.e. transverse) to the shaft axis;
• b) structural vibration at thrust bearing housings measured in the axial direction;
• c) vibration of rotating shafts radial (i.e. transverse) to the shaft axis at, or close to, the main bearings.

These are in terms of the following:

• vibration under normal steady-state operating conditions;
• vibration during other (non-steady-state) conditions when transient changes are taking place, including run up or run down, initial loading and load changes;
• changes in vibration which can occur during normal steady-state operation.

2 Normative references

The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.

3 Terms and definitions

No terms and definitions are listed in this document.

ISO and IEC maintain terminological databases for use in standardization at the following addresses:

Bibliography