Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar

Product Details
Customization: Available
Key Words: MP35n Bar
Diameter: 4mm - 600mm
Manufacturer/Factory, Group Corporation
Diamond Member Since 2024

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  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
  • Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
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Overview

Basic Info.

Model NO.
MP35n Bar
Length
as Your Requirments
Diameter Tolerance
H9, H11, H13, K9, K11, K13 etc
Sample
Free-Sample
Surface
Lack, Peeled, Polishing, Bright, Sand Blast, Hl
MOQ
100kgs
Stock
in Stock
Transport Package
Wooden Package
Specification
MP35N rod
Trademark
LORK
Origin
China
HS Code
7219350000
Production Capacity
50000kg/Month

Product Description

Product Description

 

Introduction

LORK is a alloy manufacturer with 20 years of manufacturing experience.
 

MP35N is a multi-phase alloy containing Nickel, Cobalt, Chromium and Molybdenum with a unique range of properties - ultra high strength, toughness, biocompatibility and corrosion resistance. It is produced by vacuum induction melting and vacuum arc re-melting (VIM-VAR) and is then strengthened by work hardening and aging, giving hardnesses of up to 55-60 Rockwell C and strength levels as high as 260-300KSI.

Due to this unique combination of properties, MP35N® has many applications in such industries as oil and gas, aerospace and medical. MP35N can be effectively used at cryogenic temperatures without embrittlement and maintain its properties at temperatures up to 600°F, and is also suitable for medical implants and orthodontic/prosthetic devices.
MP35N is able to resist corrosion to most mineral acid, hydrogen sulfide and seawater environments whilst exhibiting excellent resistance to stress corrosion cracking and hydrogen embrittlement, even at high strength levels. NACE MR0175 allows a hardness of up to 51 HRC for material that has been work strengthened and aged by one of the processes listed in the table below.

Nickel Cobalt Alloy MP35N Applications

  • Fasteners
  • Springs
  • nonmagnetic electrical components
  • medical instruments
  • medical and dental devices
  • seawater
  • oil and gas well
  • chemical applications
  • food processing environments

MP35N Benefits

  • Exceptional Corrosion Resistance: Offers superior performance in harsh, corrosive environments, including resistance to pitting and crevice corrosion.
  • High Strength: Provides one of the highest strength levels among metallic materials, even at elevated temperatures.
  • Outstanding Toughness: Maintains excellent toughness and ductility over a wide range of temperatures, making it ideal for demanding applications.
  • Biocompatibility: Suitable for medical implant devices due to its excellent biocompatibility and resistance to body fluids.
  • Good Fatigue Resistance: Exhibits superior fatigue strength, crucial for cyclic loading applications such as springs and cables.
  • Resistance to Stress Corrosion Cracking: Highly resistant to stress corrosion cracking, especially in environments containing chlorides or hydrogen sulfide.
  • Magnetic Properties: Non-magnetic, which is essential for electronic and certain medical applications where magnetic interference must be minimized.
  • Wear Resistance: Exhibits good wear resistance, beneficial in applications involving friction and material wear.
 

Nickel Cobalt Alloy MP35N Specifications

▪ UNS R30035
▪ AMS 5758 - MP35N VIM-VAR Bar
▪ Solution heat treated 1900-1925°F for 4 to 8 hours
▪ AMS 5844 - MP35N VIM-VAR Bar
▪ Solution heat treated 1900-1925°F for 4 to 8 hours and Work Strengthened
▪ AMS 5845 - MP35N VIM-VAR Bar
▪ Solution heat treated 1900-1925°F for 4 to 8 hours, Work Strengthened & Aged 1000-1200°F for 4 hours
▪ NACE MR0175
▪ ASTM F-562 - Surgical Implant Applications
▪ BS 7252-6 Surgical Implant Applications
▪ ISO 5832-6 Surgical Implant Applications


Nickel Cobalt Alloy MP35N Chemical Composition
 
Weight % Ni Co Cr Mo Ti Fe Si Mn P B S C
MP35N 33-37 Bal 19-21 9-10.5 1 max 1 max 0.15 max 0.15 max 0.015 max 0.010 max 0.010 max 0.03 max



Nickel Cobalt Alloy MP35N Mechanical Properties

 
Material Condition Ultimate Tensile Strength ksi 0.2 % Yield Strength ksi Elongation % Reduction of Area % Hardness HRC
MP35N
AMS 5844
Solution Heat Treated and Work Strengthened 255 225 12 50 45
MP35N
AMS 5845
Solution Heat Treated and Work Strengthened and Aged 260 230 8 35 38 min

Nickel Cobalt Alloy MP35N Characteristics

 
  • Excellent tensile strength, ductility and toughness
  • Excellent resistance to the effects of corrosion
  • Resistant to hydrogen sulphide corrosion, saltwater corrosion and also offers resistance to other chloride solutions and certain mineral acids
  • Resistance to crevice cracking in saltwater environments is also excellent.
Nickel Cobalt Alloy MP35N Fabrication
MP35N alloy can be hot and cold worked and formed by a wide variety of processes. Work strengthening can be accomplished by extruding, rolling, swaging, drawing or a combination of these manufacturing processes. MP35N alloy may be TIG welded, and in general, its weldability is similar to that of Type 304 stainless steel. Joint efficiency is dependent upon the heat treatment / worked condition of the material. The machinability of MP35N is similar to but better than that of Waspaloy, a widely used standard for nickel-cobalt-chromium base alloy machining performance.

Nickel Cobalt Alloy MP35N Heat Treatment
MP35N should be aged at the temperature required to achieve the final properties desired. The amount of cold work in MP35N defines the recommended aging treatments. For AMS 5844 (fully strength/heavily cold worked) material, the alloyshould be ages at 1000ºF - 1200ºF for 4 hours. For optimum sulphide SCC resistance, less-heavily cold worked material can be aged at 1300ºF or 1350ºF for 4 hours or at 1425ºF for 6 hours as indicated in NACE MR-0175. The 425ºF aging treatment provides the best sulphide SCC resistance, but at the expense of strength. Exposure to temperatures much above the recommended aging temperatures may result in significant (and nonrecoverable) loss in strength cause by the reversion of the cold-worked metallurgical structure to the much softer annealed structure.
 

Detection

Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar

Processing

Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
 

Packaging & Shipping


Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar
Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar

Company Profile


Lork Custom ASTM F562/R30035 Co-Ni-Cr-Mo Alloy Rod for Medical Orthopedic Implants MP35n Nickel Cobalt Alloy Bar

FAQ


Q1: Do you accept the trial order ?
A1: Yes,if we have the exactly size in stock.we can delivery even 1 piece/meter .

Q2: Can I have free sample before making orders?

A2: Yes,we can supply free sample as requirement,but buyer needs to pay the freight charges ,the freight fee will return to buyer after making order.

Q3: How do you control the quality ?
A3: MTC and PMI will be sent before shipment,any 3rd party inspection if need .

Q4: How about your delivery time ?
A4: Generally delivery time is 15 working days .

Q5: How can I quickly get the price list ?
A5: Directly click "chat now" or send us email with detail specifications,you will get the official price list in 1 hour .

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