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Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图1Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图2Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图3Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图4Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图5Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar图6

Lork Custom AMS 5844/AMS 5845/Uns R30035 Superalloy Rod for Aircraft Engine Fasteners MP35n Cobalt Alloy Bar

Price $50.00
Min Order 50 kg  
Shipping from Henan, China
Quantity
-+
Product details
MP35N rod/bar
Rod
Iron-Nickel-Cobalt Alloy
Low Carbon
100mm
15mm
6
MP35n Bar
4mm - 600mm
1.5mm - 250 mm
as Your Requirments
H9, H11, H13, K9, K11, K13 etc
Free-Sample
Lack, Peeled, Polishing, Bright, Sand Blast, Hl
100kgs
in Stock
LORK
Wooden Package
MP35N rod
China
7219350000
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 %NiCoCrMoTiFeSiMnPBSC
MP35N33-37Bal19-219-10.51 max1 max0.15 max0.15 max0.015 max0.010 max0.010 max0.03 max



Nickel Cobalt Alloy MP35N Mechanical Properties

 
MaterialConditionUltimate Tensile Strength ksi0.2 % Yield Strength ksiElongation %Reduction of Area %Hardness HRC
MP35N
AMS 5844
Solution Heat Treated and Work Strengthened255225125045
MP35N
AMS 5845
Solution Heat Treated and Work Strengthened and Aged26023083538 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

Processing


 

Packaging & Shipping



Company Profile


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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LORK GROUP CO., LTD

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