2005
DOI: 10.1361/105994905x75466
|View full text |Cite
|
Sign up to set email alerts
|

Candidate Materials for High-Strength Fastener Applications in Both the Aerospace and Automotive Industries

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4

Citation Types

0
11
0
2

Year Published

2007
2007
2022
2022

Publication Types

Select...
5
2
1

Relationship

0
8

Authors

Journals

citations
Cited by 55 publications
(13 citation statements)
references
References 4 publications
0
11
0
2
Order By: Relevance
“…Structural materials such as commercially pure (CP) titanium and its alloys are extremely important in a number of sectors, particularly in the transport, chemical, energy generation and biomaterial industries [1][2][3][4][5]. Although CP titanium possesses interesting properties, especially a good strength-to-weight ratio, high biocompatibility and enhanced corrosion resistance, its mechanical strength is relatively limited.…”
Section: Introductionmentioning
confidence: 99%
“…Structural materials such as commercially pure (CP) titanium and its alloys are extremely important in a number of sectors, particularly in the transport, chemical, energy generation and biomaterial industries [1][2][3][4][5]. Although CP titanium possesses interesting properties, especially a good strength-to-weight ratio, high biocompatibility and enhanced corrosion resistance, its mechanical strength is relatively limited.…”
Section: Introductionmentioning
confidence: 99%
“…To overcome such restrictions, CP titanium was substituted by titanium alloys, particularly, the classic grade 5, i.e., Ti-6Al-4V alloy. The Ti-6Al-4V α + β-type alloy, the most worldwide utilized titanium alloy, was initially developed for aerospace applications [12,13]. Although this type of alloy is considered a good material for surgically implanted parts, recent studies have found that vanadium may react with the tissue of the human body [2].…”
mentioning
confidence: 99%
“…The applications of titanium as a fastener material began in the mid-1960s [8] derived by the reduction of weight of aircraft such as the Airbus A380, which replaced the fastener material with titanium alloy [9,10]. A lot of β-Ti alloys have been used as fastener, such as Ti-5Al-5Mo-5V-3Cr-0.5Fe (wt%, Ti-5553) and Ti-10V-2Fe-3Al (wt%, Ti-1023) [11,12] due to higher strengths than the traditional α-β alloys.…”
Section: Introductionmentioning
confidence: 99%
“…The reason for higher strengths than the traditional α-β alloys is that the α phase in β-Ti alloys can be very fine, undeformable particles with a high volume fraction. Over the years, the need for reliable high-strength titanium fasteners for aircrafts has significantly increased [8]. Besides the strength, the volume change caused by vibration and wearing could also influence the behavior of the fastener, especially at high temperatures [2,3].…”
Section: Introductionmentioning
confidence: 99%