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Gland Design, Elastomeric O-Ring Seals, General Considerations
- Aerospace Standard
- ARP1231B
- Revised
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. SI unit conversions for U.S. customary units have been provided for reference purposes.
Rationale
Figures 1 and 2 redrawn for better clarity, Reference to ARP1235, ARP1236, and ARP1237 deleted as documents never produced, table 2 redrawn to remove metric dimensions, section added to show reference documents and MIL-H-5606 corrected to MIL-PRF-5606.
Recommended Content
| Aerospace Standard | Gland Design, Elastomeric O-Ring Seals, Static Radial |
| Aerospace Standard | Gland Design, Elastomeric O-Ring Seals, Dynamic Radial, 1500 psi Max |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Table 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 2 |
Issuing Committee
A6C2 is responsible for the development of standards, processes, and practices related to Seals, Scrapers and Bearings used in actuation systems for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, OEMs and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
Reference
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