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Balancing Machines: Tooling Design Criteria
- Aerospace Standard
- ARP4163
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
ARP4163 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE D1 | Graph-Comparison of Balance Tooling for Aircraft Engines | |
Unnamed Dataset 4 |
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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