With reference to Fig. 1, the self-locking fastener assembly 100 comprises a bolt 102, a nut 104, and a compressible polymer locking insert 106. The bolt 102 includes an elongate shank 108 having a dual-lead helical groove 110 formed along at least a portion of its length. The dual-lead groove 110 defines first and second thread leads distributed circumferentially such that two distinct axial load-bearing contact lines 112a, 112b are presented to the engaging nut threads at any given angular position.
As shown in the cross-sectional view of Fig. 2, the nut 104 defines an annular recess 114 formed in the inner bore 116. The polymer locking insert 106, comprising a compressible elastomeric ring, is seated within the annular recess 114 prior to engagement with the bolt 102. Upon tightening of the nut 104 to a target torque as claimed in claim 1, the locking insert 106 deforms radially inward under the compressive load applied by the bolt shank 108, generating a friction-based retention force FR that resists relative rotation of the nut 104 with respect to the bolt 102 under vibratory loading.
Fig. 3 illustrates the dual-lead thread profile in detail. Unlike a conventional single-lead thread, which presents a single helical contact line of contact width W1, the dual-lead profile presents two contact lines 112a, 112b each of width W2, where W2 is at least 0.5 mm measured in the axial direction. The load sharing across two contact lines reduces peak thread stress by approximately 40% as claimed in claim 1.2, thereby improving fatigue resistance of the bolt and nut under cyclic loading.
The polymer material of the locking insert 106 is selected from the group of compressible elastomers, including nitrile rubber (NBR), fluoroelastomer (FKM), and silicone, as recited in claim 1.6. The Shore A durometer of the selected elastomer determines the radial deformation under a given tightening torque and, consequently, the locking torque generated. As shown in Fig. 4, a durometer range of 40–90 Shore A provides a locking torque range of 5–25 Nm across practical tightening conditions, consistent with claim 1.3.
An alternative embodiment employs the assembly in a Method of securing components as claimed in claim 2. In this embodiment, the locking insert 106 is replaced after a defined service interval by applying a radially outward extraction force not exceeding 50 N, without heating or chemical dissolution, as recited in claim 2.4. The replacement insert is installed into the annular recess 114 by hand pressure. This field-serviceability distinguishes the invention from thread-locking adhesives, which require chemical removal, and from prevailing-torque nuts, which are typically single-use by design.