DLA MS16624E-2022
DLA · 2022-07-21

Detail Specification Sheet - External Retaining Ring, Basic (Tapered Section Type)

1Key Takeaways

MS16624E DETAIL SPECIFICATION SHEET RING, RETAINING, EXTERNAL, BASIC (TAPERED SECTION TYPE) This specification defines the requirements for external retaining rings of the tapered section type, as detailed in the associated procurement specification MIL-DTL-21248. It is applicable to all Departments and Agencies of th…

2Expert Interpretation

MS16624E is the latest military standard for external retaining rings issued by the U.S. Department of Defense. It covers the technical requirements, material specifications, dimensional tolerances, and protective treatments for tapered-section retaining rings. This standard applies to the design and selection of shaft retaining rings. It offers carbon steel, corrosion-resistant steel, and beryllium copper material options and includes detailed dimension tables and load calculation guidelines.

MS16624E Standard Overview and Technical Evolution

MS16624E is the latest specification document for external retaining rings (tapered cross-section type) in the US military standard system. It was released on July 21, 2022, replacing MS16624D Revision 2 of 2013. As an important technical document in the field of mechanical fasteners, this standard provides unified product technical requirements for various departments and agencies of the Department of Defense.


Standard Structural Framework and Technical Characteristics

The MS16624E standard adopts a modular structural design, which mainly includes five core modules: dimensional specifications, material requirements, hardness standards, protective treatments, and part numbering systems. The tapered cross-section design is a notable feature of this standard, which can maintain nearly constant roundness and pressure on the groove bottom under high-speed rotation conditions, effectively offsetting the influence of centrifugal force.

Same Dimension Range
Technical DimensionsNew Features of MS16624EOld Version of MS16624DTechnical Improvements
Material SpecificationsAdded Chromium-Free Zinc Passivation Coating OptionLimited to Traditional Cadmium Plating and Chromium-Containing PassivationEnvironmental Performance Improvement
Size RangeCovering Shaft Diameters from 0.125 to 10 InchOptimized Tolerance
Safety RequirementsEmphasis on Hydrogen Embrittlement ProtectionBasic Protection RequirementsEnhanced Safety
Application RestrictionsClear List of Prohibited SubstancesFewer Restrictive RequirementsImproved Compliance

In-Depth Analysis of Material Technical Requirements

The standard specifies three primary material systems: carbon spring steel (grades 1060-1095), corrosion-resistant steel (SAE AMS5520), and beryllium copper alloy (C17000/C17200). Material selection depends on the specific application environment. Corrosion-resistant steel is particularly suitable for food processing machinery, fuel lubrication systems, or high-temperature environments above 450°F.

Application Case: In the transmission system of aircraft engine accessories, the external retaining ring with a shaft diameter of 1.000 inches uses the part number MS16624-6100. It is made of carbon steel material with a chromium-free passivated zinc coating, which not only meets the corrosion resistance requirements but also complies with environmental regulations.


Dimension tolerance system and measurement requirements

The standard provides a detailed dimension tolerance table covering the complete shaft diameter range from 0.125 inches to 10.000 inches. Key dimensional parameters include free diameter (ØD), lug height (B), large section height (E), small section height (J), thickness (T), etc. It is worth noting that the thickness tolerance is formulated for unplated rings. For corrosion-resistant steel and plated rings, the maximum tolerance needs to be increased by +0.002 inches.


Mechanical Properties and Load Calculation

The standard provides a complete guide to load calculation methods and safety factors. The allowable thrust load capacity of the snap ring is calculated based on the material's ultimate shear strength, with a recommended safety factor of 4. The allowable compressive load capacity of the groove wall is calculated based on the material's compressive yield strength, with a recommended safety factor of 2.

Calculation Example: For a carbon steel snap ring with a shaft diameter of 1.000 inches, a thickness of 0.042 inches, and a material ultimate shear strength of 150,000 psi, with a safety factor of 4, the allowable thrust load P = π × 1.000 × 0.042 × 150,000 / 4 = 4,950 pounds.


Speed Safety Limits and Application Considerations

The standard provides a table of approximate safety speed limits. For carbon steel and corrosion-resistant steel snap rings, the speed limit is 80,000 RPM for a 0.125-inch shaft diameter, decreasing with increasing shaft diameter. Beryllium copper snap rings have a relatively lower speed limit. During installation, special care should be taken to avoid overexpansion. A gap between the snap ring and the groove diameter indicates overexpansion.


Standard Implementation Recommendations and Best Practices

Based on the requirements of the MS16624E standard, the following implementation recommendations are offered: Chromium-free passivated zinc coating should be preferred during the design phase; specialized tools should be used during installation to prevent snap ring deformation; the fit between the snap ring and the groove should be regularly inspected; speed limits should be strictly adhered to in high-speed applications; and the correct snap ring part number should be used during maintenance and replacement.

The technical evolution of the standard reflects the comprehensive environmental, safety, and performance requirements of modern manufacturing, providing a reliable technical basis for mechanical design engineers. In actual application, the specific working conditions should be combined with comprehensive consideration of material selection, protective treatment and load requirements to ensure the long-term reliable operation of the clamping ring assembly.

3Version History

DLA MS16624E-2022 current

5Citation Network

0
Cite this standard
1
Referenced herein
MIL-DTL-21248

6Frequently Asked Questions

What is DLA MS16624E-2022?
DLA MS16624E-2022 — Detail Specification Sheet - External Retaining Ring, Basic (Tapered Section Type) is an international standard developed by Defense Logistics Agency. MS16624E DETAIL SPECIFICATION SHEET RING, RETAINING, EXTERNAL, BASIC (TAPERED SECTION TYPE) This specification defines the requirements for external retaining rings of the tapered section type, as detailed in the associated procurement specification...
What does DLA MS16624E-2022 cover?
This standard covers: MS16624E DETAIL SPECIFICATION SHEET RING, RETAINING, EXTERNAL, BASIC (TAPERED SECTION TYPE) This specification defines the requirements for external retaining rings of the tapered section type, as detailed in the associated procurement specification MIL-DTL-21248. It is applicable to all...
Who should use this standard?
This standard is intended for organizations, professionals, and stakeholders involved in various industries and sectors. It is applicable to manufacturers, service providers, regulatory bodies, and certification organizations.
What is the latest version of DLA MS16624E-2022?
The current published version is DLA MS16624E-2022, published on 2022-07-21. Always check for amendments or pending revisions.
How do I purchase DLA MS16624E-2022?
You can purchase DLA MS16624E-2022 by visiting our contact page. Click "Get This Standard" to view pricing and send a purchase inquiry. Our team will respond with payment and delivery details.
Shaft Diameter Range (inches)Thickness Tolerance (Unplated)Thickness Tolerance (Plated)FIM Requirements
0.125-0.236±0.001+0.004/-0.002N/A
0.250-0.669±0.002+0.004/-0.002See standard for specific values