Skip Nav Destination
Close Modal
Search Results for
Studs
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Book Series
Date
Availability
1-20 of 86 Search Results for
Studs
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
Image
Published: 01 November 2007
Fig. 16.9 (a) Fractured studs due to cadmium-induced LME during service at 315 °C (600 °F), and (b) optical micrograph showing intergranular cracks at the cross section of a fractured stud. Source: Ref 46
More
Image
Published: 01 December 2004
Fig. 7 Wedge-test details for studs. D , diameter of stud; C , clearance of wedge hole; R , radius; T , thickness of wedge at short side hole; W , wedge angle
More
Image
in Failure of an LP Turbine Disc in an Aircraft Engine
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH44.9 (a) Two sheared mounting studs. (b) Close-up view of one of the sheared studs. Note the direction of pulling of the studs.
More
Image
Published: 01 November 2011
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2011
DOI: 10.31399/asm.tb.jub.t53290079
EISBN: 978-1-62708-306-5
... Abstract This chapter discusses the fusion welding processes, namely oxyfuel gas welding, oxyacetylene braze welding, stud welding (stud arc welding and capacitor discharge stud welding), high-frequency welding, electron beam welding, laser beam welding, hybrid laser arc welding, and thermit...
Abstract
This chapter discusses the fusion welding processes, namely oxyfuel gas welding, oxyacetylene braze welding, stud welding (stud arc welding and capacitor discharge stud welding), high-frequency welding, electron beam welding, laser beam welding, hybrid laser arc welding, and thermit welding.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270180
EISBN: 978-1-62708-301-0
... Abstract The nose landing gear on an aircraft malfunctioned during landing roll. After the incident, two fractured studs were found in the retraction jack support beam. Based on visual examination and the results of SEM fractography, investigators concluded that the studs failed by fatigue...
Abstract
The nose landing gear on an aircraft malfunctioned during landing roll. After the incident, two fractured studs were found in the retraction jack support beam. Based on visual examination and the results of SEM fractography, investigators concluded that the studs failed by fatigue, a vulnerability because of the way they were mounted. A sketch showing the correct mounting configuration is included in the report.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270065
EISBN: 978-1-62708-301-0
... Abstract An aircraft was heavily damaged when it was forced to land due to a throttle malfunction. Investigators determined that one of the studs linking the throttle to the engine fractured from fatigue, initiated by cracks formed during a riveting procedure. This chapter provides a summary...
Abstract
An aircraft was heavily damaged when it was forced to land due to a throttle malfunction. Investigators determined that one of the studs linking the throttle to the engine fractured from fatigue, initiated by cracks formed during a riveting procedure. This chapter provides a summary of the investigation, which included the use of scanning electron fractography, along with recommendations on acceptable hole patterns for rivets.
Image
Published: 01 November 2011
Fig. 4.4 Stud arc welding process: (a) gun is properly positioned; (b) trigger is depressed and stud is lifted, creating an arc; (c) arcing period is completed and stud is plunged into molten pool of metal on base material; (d) gun is withdrawn from welded stud and ferrule is removed. Source
More
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270168
EISBN: 978-1-62708-301-0
... and subjected to further damage. Some of the dovetail mounting regions were also found sheared. The region that had suffered minimum damage was the locking plate region. The two mounting studs were found pulled outward and sheared ( Fig. CH44.9 ), along with the locking plate. The region showed no other damage...
Abstract
During cyclic spin tests, the turbine disc in an aircraft engine broke apart with a loud noise, followed by a fire. Based on a detailed examination and the results of SEM fractography and hardness measurements, failure analysts concluded that a locking plate became dislodged due to the shearing of the screws that hold it in place. They also provided recommendations to remediate the problem.
Image
Published: 01 November 2011
Fig. 4.3 Typical integrated power/control system for stud arc welding. Source: Ref 4.3
More
Image
Published: 01 November 2011
Fig. 4.5 Macrosection of low-carbon steel stud weld. Source: Ref 4.3
More
Image
Published: 01 November 2011
Fig. 4.7 Typical current-versus-time curves for the three capacitor discharge stud welding methods. Source: Ref 4.4
More
Image
Published: 01 November 2011
Fig. 4.8 Methods used for capacitor discharge (CD) stud welding, (a) initial-gap; (b) initial-contact; (c) drawn-arc. Source: Ref 4.4
More
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. CH1.1 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.
More
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. CH1.2 Fracture surface of the mating half of the stud, from inside the tube with rivets still in position
More
Image
in Failure of an LP Turbine Disc in an Aircraft Engine
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH44.10 SEM fractograph of the stud. Elongated dimples indicate failure due to shear loads.
More
Image
in Failure of a Nose Undercarriage Retraction Jack Support Beam
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH49.1 Fracture surface of the failed stud showing the fatigue zone
More
Image
in Failure of a Nose Undercarriage Retraction Jack Support Beam
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH49.4 Sketch showing the location of leading thread in the stud
More
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060195
EISBN: 978-1-62708-355-3
... Wedge angles for tensile testing of fasteners Table 2 Wedge angles for tensile testing of fasteners Nominal product diam, mm Degrees Fasteners (a) Studs and flange fasteners 5–24 10 6 Over 24 6 4 (a) For heat-treated fasteners that are threaded one diam or closer...
Abstract
This chapter focuses on tensile testing of three types of engineering components that undergo significant loading in tension, namely, threaded fasteners and bolted joints; adhesive joints; and welded joints. It describes the standardized tensile test for externally threaded fasteners and provides a brief background on relationships among torque, angle-of-turn, tension, and friction. The chapter also describes the test methods covered in the ASTM F 606M standard, namely, product hardness; proof load by length measurement, yield strength, or uniform hardness; axial tension testing of full-sized products; wedge tension testing of full-sized products; tension testing of machined test specimens; and total extension at fracture testing. Finally, the chapter covers tensile testing of adhesive and welded joints.
Image
Published: 01 December 2018
Fig. 6.81 (a) Close-up view at leakage location with leakage in the form of tiny pinholes and smooth outer surface with erosion marks where the studs had worn out. (b) Bent location showing scale deposits. (c) Inner surface view brick red in color indicating absence of protective magnetite
More
1