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Gland Design, Elastomeric O-Ring Seals, General Considerations
- Aerospace Standard
- ARP1231A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document establishes general gland design criteria for static and dynamic O-ring seal applications used in fluid systems and at fluid pressures common to the aerospace industry. Detailed discussion of design criteria and tables of recommended gland dimensions are contained in the documents listed in Table 1. S.I. unit conversions for U.S. customary units have been provided for reference purposes.
Rationale
ARP1231A has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Aerospace Standard | General Gland Design Criteria for Static and Dynamic O-Ring Seal Applications Specifically for Engines and Engine Control Systems |
Technical Paper | Compatibility and Filterability of Hydraulic Fluids |
Aerospace Material Specification | Rings, Sealing, Synthetic Rubber Phosphate Ester Hydraulic Fluid Resistant, Butyl Type 70-85 |
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
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