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Mechanics of Preloaded Bolt Tensile Loading With Focus on Load Introduction FactorThe bolt tensile and joint separation loads are directly influenced by the locations at which the external loads enter the clamped members of a preloaded bolted joint (PBJ) and the associated load-paths through the joint. This physical load introduction mechanism affecting the bolt tensile loading is typically represented in the bolt tensile load equation, in part, by a load introduction factor (LIF), which was shown by H.M. Lee of Marshall Spaceflight Center to be a natural product of the bolt tensile load equation using a linear spring stiffness model. This LIF, being a function of load-path stiffness, has subsequently been denoted as the stiffness-based LIF (SBLIF), providing a framework to calculate the LIF using whatever load-path stiffness approximations are appropriate.

Expanding upon the work of Lee, it is shown that the SBLIF and the joint stiffness factor are functions of the stiffnesses of the same load-paths and regions within a PBJ, and thus they should not be treated as independent variables. Mathematical expressions for the SBLIF are presented.

Comparisons are shown between the analytically calculated SBLIF, the analytically calculated geometric LIF (GLIF), which is a simple clamped-member thickness ratio, the experimentally derived LIF, and the LIF determined by finite element analysis (FEA). Using experiment and FEA as a benchmark, the SBLIF, using traditional load-path stiffness approximations, enables a more accurate prediction of bolt tensile loading than the GLIF, although it can be unconservative near joint separation. The GLIF generally attributes more of the externally applied tensile load to the bolt than does the SBLIF, potentially resulting in heavier and/or more
costly bolted joints. Mathematical relationships between the SBLIF and the GLIF are developed.

Supplemental material is provided in the appendixes where the historical practice of using the joint compressive stiffness in place of the joint tensile stiffness is evaluated. The appendixes include step-by-step examples demonstrating the calculation of the SBLIF using traditional stiffness approximations and conclude with the development of the joint diagram in terms of the SBLIF, culminating into formulas for the key features of a joint diagram, which is useful for programming.
Document ID
20250005284
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
John K Ramsey
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 20, 2025
Publication Date
May 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Design, Testing and Performance
Spacecraft Design, Testing and Performance
Launch Vehicles and Launch Operations
Structural Mechanics
Mechanical Engineering
Report/Patent Number
NASA/TM-20250005284
E-20113
Funding Number(s)
WBS: 747797.06.13.06.30.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Professional Review
Keywords
Load Path
Preloaded Bolted Joints
Bolted Joints
Load Introduction Factor
Loading Plane Factor
Compression Zone
Joint Diagram
Bolt Tension Load
Bolt Thermal Load
Fastener Tension Load
Fastener Thermal Load
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