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Balancing Machines: Tooling Design Criteria
- Aerospace Standard
Published August 12, 2021 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document establishes general design criteria, tolerances, and limits of application for tooling, fixtures and accessories for mounting and driving gas turbine engine rotors on horizontal and vertical balancing machines.
For your own safety, while using balancing tooling, regard the safety instructions of the individual supplier.
ARP4163 has been reaffirmed to comply with the SAE five-year review policy.
Data Sets - Support Documents
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|TABLE D1||Graph-Comparison of Balance Tooling for Aircraft Engines|
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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.
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