2022
DOI: 10.3390/ma15238432
|View full text |Cite
|
Sign up to set email alerts
|

Optimization of Titanium Alloy Drilling to Minimize the Secondary Burr after Deburring Process

Abstract: The formation of burrs on the edges of machined surfaces is one of the inherent problems during machining. The burrs are formed both on the tool entry surface and exit surfaces. The paper proposes a modification of the drill involving an additional cutting insert located in the shank part. This innovative solution allowed the drill and deburring insert to be integrated, enabling both processes to be performed within one machining operation. The impact of the selected insert geometry and deburring process param… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
5
1

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(3 citation statements)
references
References 26 publications
0
3
0
Order By: Relevance
“…In the above equation, F is the torsion force, V is the linear velocity, and R is the torsion radius. Bringing Equations ( 9) and (10) into Equation ( 8) results in the following equation:…”
Section: Machining Characteristics Of the Pneumatic Spindlementioning
confidence: 99%
See 1 more Smart Citation
“…In the above equation, F is the torsion force, V is the linear velocity, and R is the torsion radius. Bringing Equations ( 9) and (10) into Equation ( 8) results in the following equation:…”
Section: Machining Characteristics Of the Pneumatic Spindlementioning
confidence: 99%
“…Carbon fiber-reinforced plastic composites (CFRP) are very commonly, heavily, and universally used advanced composites in aerospace assembly, processing, and manufacturing, which have a strong representation. Titanium alloys (Ti) also have excellent material properties, and CFRP/Ti stacks composed of the two materials together exhibit excellent mechanical properties and flexible designability, which have been widely used in the manufacturing of components at critical positions of aircraft, providing an important guarantee for the safety, durability, and environmental protection of aircraft [7][8][9][10]. Stacked components need to be assembled by riveting or bolting after the hole-making process.…”
Section: Introductionmentioning
confidence: 99%
“…This may be accomplished by utilising high-efficiency cooling pumps, heat exchangers, and cooling fluids. Further studies are necessary to create effective control mechanisms for specific materials such as Ti6Al4V titanium alloy [86,91].…”
Section: (G) Energy Conservationmentioning
confidence: 99%