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SAE - SAE AMS5686 - STEEL, CORROSION RESISTANT, RIVET WIRE, 18CR - 11.5NI (SAE 30305) SOLUTION HEAT TREATED - UNS S30500 Organization: SAE
Date: 2001-04-01
Description: Application: This wire has been used typically for fabricating into rivets, but usage is not limited to that application.
SAE - SAE J1200 - BLIND RIVETS - BREAK MANDREL TYPE Organization: SAE
Date: 2017-01-01
Description: This SAE Standard establishes the dimensional, mechanical, and performance requirements of inch and metric break mandrel blind rivets suitable for use in joining the component parts of an assembly
SAE/TP - 2009-01-3155 - SLUG RIVET MACHINE INSTALLS 16 RIVETS PER MINUTE DRILL-RIVET-SHAVE Organization: SAE/TP
Date: 2009-11-10
Description: The E6000's fastening cycle is capable of forming and shaving 16 rivets per minute. Head alignment is maintained by two independent four axis heads using a combination of controls and kinematics.
SAE/TP - 2010-01-1843 - SIMULATION OF THE SOLID RIVET INSTALLATION PROCESS Organization: SAE/TP
Date: 2010-09-28
Description: Afterwards, the clearance fit between the rivet shank and the borehole, the rivet grip, and the squeeze force have been numerically studied in order to determine their effect on the joint.
NAVISTAR - MPAPS S-GM-90.101-GS/PL - BREAK MANDREL BLIND RIVETS – METRIC SERIES (NOUN CODE – 7220) Organization: NAVISTAR
Date: 2015-06-01
Description: This specification contains the essentials of the SAE Standard. A break mandrel blind rivet is a blind fastener with a self-contained mandrel which during the setting operation is pulled into or against the rivet body forming an upset on the blind end and expanding the body until the mandrel breaks.
SAE - SAE J663 - RIVETS FOR BRAKE LININGS AND BOLTS FOR BRAKE BLOCKS - TRUCK AND BUS Organization: SAE
Date: 2013-06-01
Description: This SAE Standard specifies the dimensions of semitubular rivet and bolts for brake linings/blocks.
SAE/TP - 2011-01-2706 - NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE MECHANICAL PROPERTIES OF RIVETED JOINTS CONSIDERING THE INSTALLATION PROCESS Organization: SAE/TP
Date: 2011-10-18
Description: It deals with the transfer of the stress and strain state resulting from the rivet installation, obtained by a two-dimensional, rotational symmetric model, to a full 3D simulation of a single lap shear tests. The rivet installation simulation has been presented on last years' SAE-conference The method to include the stress state originating from the rivet installation into the numerical investigation of riveted joints is applied to a well known lap shear joint configuration.
SAE/TP - 2010-01-1844 - REFURBISHMENT OF 767 ASAT DRILL-RIVET-LOCKBOLT MACHINES Organization: SAE/TP
Date: 2010-09-28
Description: Name: Richard Wilkes; Affiliation: Boeing Co. Meeting Details: Name: SAE Aerospace Manufacturing and Automated Fastening Conference and Exhibition Location: Wichita, Kansas, USA Date: 09-28-2010
SAE-ITC - SAE ITC TS39 - MANUFACTURING AND INSPECTION REQUIREMENTS FOR RIVET, BLIND, SELF-PLUGGING, FLUSH BREAK, MECHANICALLY LOCKED STEM, ALUMINIUM ALLOYS AS46784 TO AS46787 - ISSUE 2; FORMERLY ADS TS39 Organization: SAE-ITC
Date: 1992-05-01
Description: These Standards are produced by the SAE ITC with the assistance of, and for the benefit of the Aerospace Industry, as part of a continuous programme of Standardisation for Aerospace application under the control of the Technical Standards Committee (TSC) of the SAE ITC. SAE ITC Standards are published as part of the series of SAE ITC Aerospace Industry Standards, and where appropriate, additional manufacturing and inspection requirements are issued as Reference Sheets (RS) or Technical Specifications (TS).
GMNA - GMP.PA66.015 - NYLON 66 - HIGH IMPACT MODIFIED, HEAT STABILIZED - ISSUE 7; DO NOT USE ON NEW PROGRAMS; REPLACED BY GMW16447 - GMW16447P-PA66-T2 Organization: GMNA
Date: 2015-12-01
Description: Typical applications include the following: Emission canisters, brackets, push rivet fasteners.
SAE/TP - 2009-01-3185 - THE UNDERAPPRECIATED FASTENER Organization: SAE/TP
Date: 2009-11-10
Description: Don't underestimate the power of something as simple as the rivet for a repair to resolve a discrepant condition. Hole drilling discrepancies can occur daily on time sensitive parts which can cause scrapped parts, delays, extra expenses and angry customers.
SAE/TP - 2011-01-2774 - AUTOMATED COAXIAL SQUEEZE RIVETER Organization: SAE/TP
Date: 2011-10-18
Description: This process utilizes an innovative coaxial riveting head design in which the drill spindle and rivet driver share a common servo axis, with a simple toggle mechanism to switch which tool is active.
SAE/TP - 2009-01-3089 - NEW JIG MOUNTED WING PANEL RIVETERS, AERAC 2 Organization: SAE/TP
Date: 2009-11-10
Description: These machines employ several new technologies to achieve this including Electroimpact's latest generation rivet injector, an integrated headstone load cell, and GE Fanuc's customer board. The new rivet injector grips the rivet axially and maintains positive control of the rivet from magazine to panel.
SAE/TP - 2011-01-2756 - RIVETLESS NUTPLATE DEVELOPMENTS FOR AEROSPACE APPLICATIONS Organization: SAE/TP
Date: 2011-10-18
Description: Within this paper, the AIRBUS approach on the development of rivetless nutplates as an alternative to riveted anchor nuts is described. Within the frame of a wider analysis, it was identified that currently used riveted anchor nut elements does have disadvantages with negative impact on an optimized cost-efficient and lead-time driven design and manufacturing environment.
SAE/TP - 2008-01-2283 - TRAVELING COLUMN MACHINES FOR AUTOMATED DRILLING AND FASTENING OPERATIONS ON DIFFERENT AIRCRAFT STRUCTURAL COMPONENTS Organization: SAE/TP
Date: 2008-09-16
Description: Application examples are shown for drilling and installation of two-piece and blind rivet fasteners on box-type and barrel-type aircraft structures at Airbus Deutschland.
SAE/TP - 2006-01-3176 - DUAL ELECTRIC SPINDLE RETROFIT FOR WING RIVETERS Organization: SAE/TP
Date: 2006-09-12
Description: The Boeing Company (Renton Division) had a requirement for a 30,000 RPM spindle to provide improved surface finish when milling 2034 ice box rivets in hydraulic wing riveters. Electroimpact supplied an electrical spindle which fit into the same cylinder block as the hydraulic spindle.
SAE/TP - 2009-01-3208 - DEVELOPMENT AND IMPLEMENTATION OF SOL-GEL COATINGS FOR AEROSPACE APPLICATIONS Organization: SAE/TP
Date: 2009-11-10
Description: Use of the novel coating as a surface pretreatment for the exterior of commercial aircraft has enabled environmental, health, and safety benefits due to elimination of hexavalent chromium, and flight test and early fleet survey data support the laboratory observations that the sol gel coating reduces the occurrence of "rivet rash" adhesion failures. Modifications of the basic inorganic/organic hybrid network have yielded multifunctional coatings with promise for applications such as corrosion control and oxidation protection.
SAE/TP - 2009-01-3157 - AUTOMATED FASTENING OF AIRCRAFT CARGO DOOR STRUCTURES WITH A STANDARD ARTICULATING ROBOT SYSTEM Organization: SAE/TP
Date: 2009-11-10
Description: Our customer's application required a completely new type of end-effector; installing solid rivets and capable of operating within the inner structure of the cargo doors.
SAE/TP - 2009-01-3172 - ECONOMICAL REPAIR OF DAMAGED AND DISCREPANT HOLES IN METALS AND COMPOSITES Organization: SAE/TP
Date: 2009-11-10
Description: Bushing the hole back to nominal size using press or shrink fit bushings; often in conjunction with doublers or local riveted patches, are not very effective and can change the local stiffness of the structure.
SAE/TP - 2008-01-2301 - CHISEL EDGE EFFECT ON DELAMINATION WHEN DRILLING THICK COMPOSITE MATERIALS WITH A TWIST DRILL Organization: SAE/TP
Date: 2008-09-16
Description: The drilling process is currently applied for bolt or rivet assembly of composite structures. As for metallic structures, the twist drill is the most commonly used cutter.

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