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Search Results for Riveting
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Image
Published: 01 August 2012
Fig. 14.1 Illustration of the principle of punch riveting. Source: Ref 14.1
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Image
Schematic diagram of self-piercing riveting with semitubular rivet. Source:...
Available to PurchasePublished: 01 August 2012
Image
Cross section of components used during semitubular self-piercing riveting....
Available to PurchasePublished: 01 August 2012
Fig. 14.3 Cross section of components used during semitubular self-piercing riveting. Source: Ref 14.4
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Image
Published: 01 August 2012
Fig. 14.4 Operational sequence of the hydro-self-piercing riveting process. Source: Ref 14.7
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Book Chapter
Mechanical Joining by Forming
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 August 2012
DOI: 10.31399/asm.tb.smfpa.t53500289
EISBN: 978-1-62708-317-1
... Abstract This chapter describes joining by forming processes including riveting, clinching, crimping, and dieless joining techniques. It also discusses the fatigue behavior of clinched joints and the results of fatigue tests that compare clinched and spot welded joints. clinching...
Abstract
This chapter describes joining by forming processes including riveting, clinching, crimping, and dieless joining techniques. It also discusses the fatigue behavior of clinched joints and the results of fatigue tests that compare clinched and spot welded joints.
Book Chapter
Failure of a Tail Rotor Blade in a Helicopter
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270107
EISBN: 978-1-62708-301-0
... Abstract A helicopter lost the outboard rib on a tail rotor blade in flight and was forced to land because of the resulting vibrations. The investigation that followed is described in this chapter along with key findings. As shown in a sketch, the rib is held in place by a set of six rivets...
Abstract
A helicopter lost the outboard rib on a tail rotor blade in flight and was forced to land because of the resulting vibrations. The investigation that followed is described in this chapter along with key findings. As shown in a sketch, the rib is held in place by a set of six rivets. All of the rivets on the failed blade were missing and sections of skin were torn from most of the rivet holes. One such rivet hole was examined in a SEM, revealing corrosion on one of the tear surfaces and dimples (characteristic of ductile overload failure) on the other. In addition, the inner surface of the skin nearest the rib was found to be coated with soot, the paint on the leading edge of the top skin was abraded, and the skin in that area had thinned. Based on their findings, investigators concluded that the outboard rib separated because of stress-corrosion cracking around the rivets, and erosion may have contributed.
Image
Corrosion failure of 100-year-old riveted steel water transmission main. Co...
Available to PurchasePublished: 01 October 2011
Fig. 15.2 Corrosion failure of 100-year-old riveted steel water transmission main. Courtesy of S. Paul, CorrTech, Inc.
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Image
Fatigue life of riveted joints with different tension (T)/shear (S)/bearing...
Available to Purchase
in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture: Understanding the Basics
Published: 01 November 2012
Fig. 3 Fatigue life of riveted joints with different tension (T)/shear (S)/bearing (B) ratios. Source: Ref 3
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Image
Published: 01 August 1999
Fig. 1 Galvanic corrosion in an aluminum-copper riveted assembly
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Image
Typical aerospace structural fasteners, (a) rivets, (b) pin and collar, (c)...
Available to PurchasePublished: 01 October 2012
Fig. 8.52 Typical aerospace structural fasteners, (a) rivets, (b) pin and collar, (c) bolts and nuts, (d) blind fasteners. Source: Ref 8.1
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Image
Fracture surface on one-half of the stud showing the rivet holes. Note the ...
Available to Purchase
in Failure of a Throttle End Fitting in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH1.1 Fracture surface on one-half of the stud showing the rivet holes. Note the taper of one of the holes and noncentering of the other.
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Image
in Failure of a Throttle End Fitting in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH1.3 SEM fractograph of region A of Fig. CH1.1 , close to the rivet hole, showing tearing mode of fracture
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Image
(a) Solid and (b) tube rivets in a joint, before and after upsetting. Solid...
Available to PurchasePublished: 01 July 2009
Fig. 24.13 (a) Solid and (b) tube rivets in a joint, before and after upsetting. Solid line, before upsetting; dashed line, after upsetting. Source: Messler 1993b
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Image
in Failure of a Tail Rotor Blade in a Helicopter
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH18.2 A typical tear in a rivet hole of a blade
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Image
in Failure of a Tail Rotor Blade in a Helicopter
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH18.5 Cracks emanating from a rivet hole in a blade
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Image
Low-cycle fatigue cracking induced by thermal strains in the rivet slot of ...
Available to PurchasePublished: 01 March 2002
Fig. 14.19 Low-cycle fatigue cracking induced by thermal strains in the rivet slot of a nickel-base superalloy disk
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Image
Carriage body of the Trans Europa Express (TEE) in riveted and spot-welded ...
Available to PurchasePublished: 01 December 2006
Fig. 2.12 Carriage body of the Trans Europa Express (TEE) in riveted and spot-welded ALMgSi sheets with longitudinal and transverse stiffeners in extruded sections of the same alloy in the heat treated temper
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Image
An aluminum plate riveted to a steel plate resulted in a galvanic couple an...
Available to PurchasePublished: 30 November 2013
Fig. 4 An aluminum plate riveted to a steel plate resulted in a galvanic couple and crevice corrosion that produced a significant amount of corrosion products between the two plates. The stresses generated as a result of the volume change of the corrosion products were sufficient
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Image
Published: 30 June 2023
Fig. 10.21 Typical automotive joint combining adhesive bond with self-piercing rivets
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