Interference fit bolt and sleeve

• US 5,018,920 A
• Filed: 01/16/1990
• Issued: 05/28/1991
• Est. Priority Date: 01/23/1989
• Status: Expired due to Term

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Speakman, Eugene R.
• Primary Examiner(s): Wilson, Neill R.
• Application Number:
  US07/466,125
• Time in Patent Office: 497 Days
• Field of Search: 411/43, 411/338, 411/339, 411/360, 411/361, 411/383
• US Class Current: 411/43
• CPC Class Codes: B21J 15/02 Riveting procedures
• CPC Class Codes: B23P 9/025 to inner walls of holes by using axially moving tools
• CPC Class Codes: F16B 19/06 Solid rivets made in one piece
• CPC Class Codes: F16B 19/1027 Multi-part rivets
• CPC Class Codes: F16B 19/1054 the pull-mandrel or the like being frangible
• CPC Class Codes: F16B 4/004 Press fits, force fits, interference fits, i.e. fits without heat or chemical treatment F16B4/002 takes precedence
• CPC Class Codes: F16B 5/02 by means of fastening members using screw-thread F16B5/0004 takes precedence; construction of screw-threaded connections F16B25/00 - F16B39/00
• CPC Class Codes: F16B 5/04 by means of riveting rivets F16B19/04

Abstract

In this fastening system two or more layers of material are fastened together by inserting a hollow sleeved fastener such as a rivet or a bolt into the hole in a high interference fit to expand the hole radially. The sleeve is configured either as a collar and a straight shank or as an angled upper portion combined with a shank for counterbored applications. The intersections between either the collar and the shank or the angle portion and the staight shank are designed with an enlarged radius such that when the sleeve is expanded after the insertion of the fastener inside of it, this radius is expanded, which in turn stress coins the adjacent edge of the hole in the layers. This localized stress coining as well as the hoop stress in the hole surrounding the hole dramatically increases the fatigue strength of the fastened layers in a structure assembly.

Claims

1. A interference fit threaded pull bolt fastener system for use with a pull tool securing a plurality of layers having an aligned hole together comprising:

a bolt means comprising a straight walled shank portion having an enlarged head at one end and a threaded portion of a first reduced diameter at its other end with a serrated shaft means of diameter no greater than the first reduced diameter extending beyond the threaded portion, the serrated shaft being adapted to be broken off after pulling the bolt means into the hole;

a hollow sleeve means having a first portion adapted to receive the bolt means head, a straight walled portion of a smaller interior diameter than the exterior diameter of the shank of the bolt means adapted to receive the shank portion in an interference fit and a transition region of the outside surface of the sleeve at the intersection between the first portion and the straight walled portion wherein the transition region is a radiused intersection having a radius of about 0.030 to about 0.040 inches; and

nut means adapted to be torqued onto the threaded portion of the bolt means.