Your Selections

Nickel alloys
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Authors

Publishers

Affiliations

Committees

Events

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Tool wear analysis on drilling process of Inconel 718 superalloy

Federal University of Sao Carlos-Pedro Cabegi Barros, Gustavo Franco Barbosa, Carlos Eiji Hirata Ventura
OSG Sulamericana-Gustavo Roberto Santos
  • Technical Paper
  • 2020-01-0034
To be published on 2020-03-10 by SAE International in United States
The inconel 718 is an alloy based on nickel of high thermal and mechanical resistance, which allows its wide application in the aerospace industry, being generally implemented in aircraft tail cone and engine components. On the other hand, these features become a recurring problem when the machining of this material is performed. For example, in the drilling process of this superalloy, the cutting tools used exhibit excessive wear due to the high temperature and pressure at the cutting edge. However, there are numerous parameters that can influence the cutting tool life, and when analyzed and well defined, determine the types of modifications needed to enable less wear, and consequently an increase of its useful life in service. Given this context and knowing that the study of tool life in the inconel 718 drilling process is extremely relevant in the aerospace sector, this paper presents a wear study in order to evaluate the behavior of different types of cutting tools used to drill the Inconel 718. It was accomplished by the combination of different cutting parameters…
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.
new

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .4375-20 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3254D
  • Current
Published 2020-01-16 by SAE International in United States

Scope is unavailable.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.
new

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .3125-24 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3252E
  • Current
Published 2020-01-16 by SAE International in United States

Scope is unavailable.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.
new

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD,CLOSE TOLERANCE SHANK, NICKEL ALLOY (UNS N07001)165 KSI MIN, .2500-28 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9724E
  • Current
Published 2020-01-07 by SAE International in United States

Scope is unavailable.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.
new

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 74Ni - 15.5Cr - 8.0Fe

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5665P
  • Current
Published 2019-12-17 by SAE International in United States

This specification covers a corrosion and heat resistant nickel alloy in the form of round bars over 2.50 to 4.50 inches (over 63.5 to 114.3 mm), inclusive, in nominal diameter, forgings over 2.50 inches (63.5 mm) in nominal thickness, other bars and forgings, flash welded rings, and stock for forging or flash welded rings (see 8.6).

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.
new

Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing, 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) 0.90Ti - 0.50Al - 18Fe, Consumable Electrode Remelted or Vacuum Induction Melted, 1775 °F (968 °C) Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5589G
  • Current
Published 2019-12-13 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD with nominal wall thickness 0.015 inch (0.38 mm) and over (see 8.6).

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 57Ni - 20Cr - 10Co - 8.5Mo - 2.1Ti - 1.5Al - 0.005B, Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated, Precipitation Heat Treatable

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5915A
  • Current
Published 2019-12-02 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and stock for forging.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Cold Drawn, and Aged

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5834E
  • Current
Published 2019-11-25 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.6).
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Solution Heat Treated and Cold Drawn

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5833E
  • Current
Published 2019-11-25 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.5).
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Nickel-Iron Alloy, Corrosion and Heat-Resistant, Welding Wire 12.5Cr - 42.5Ni - 6.0Mo - 2.7Ti - 0.015B - 35Fe

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5830C
  • Current
Published 2019-11-12 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel-iron alloy in the form of welding wire.
This content contains downloadable datasets
Annotation ability available