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Balancing Machines - Description and Evaluation Horizontal, Two-Plane, Soft-Bearing Type for Gas Turbine Rotors
- Aerospace Standard
- ARP587C
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
The specific performance requirements preceding each test in Section 9 have been written to define certain characteristics of the machine. Conformance with the tests constitutes what is considered minimum proof that the machine will meet these requirements. The test procedures will not prove conformance with all requirements over the full range of all variables, neither will they measure nor define the exact reasons for nonconformance in a given test.
Failure of a machine to conform may be due to shortcomings in specific components or to more general reasons such as lack of ruggedness, improper leveling or anchoring to the floor, etc.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
Recommended Content
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 | Dimension and Capacity Requirements | |
TABLE 2 | ||
TABLE A1 | Dimensions for Proving Rotor Storage Containers |
Issuing Committee
The SAE EG-1A Balancing committee concerns itself with all balancing methods and procedures as they relate to the interests of the aerospace industry. The group’s scope includes creating, preparing and, maintaining all relevant specifications, recommended practices, standards and, requirements for rotor balance measurement, evaluation and, correction. The SAE EG-1A committee includes OEMs, suppliers, processors, consulting firms, government, academia and others throughout both the commercial and military aerospace industries.
Reference
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