AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear

Product Details
Customization: Available
After-sales Service: Support
Warranty: Lifetime Warranty
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  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
  • AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
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  • Overview
  • Product Description
  • Main Material
  • Detailed Photos
  • Company Profile
  • Equipment and Process
  • Application
  • Packaging
Overview

Basic Info.

Model NO.
AMS 6532
Standard
AISI, ASTM, GB, JIS, DIN, BS
Technique
Forged/Hot Rolled/Cold Drawn
Application
Structural Steel Bar, Tool Steel Bar
Surface Treatment
Polished
Alloy
Alloy
Special Use
Free Cutting Steel, Cold Heading Steel
Certificate
ISO, ABS, BV, CCS, Dnv, Lr, Gl, Mill Certificate
Quality Inspection
Ut, Chemical Composition, Physical Properties/SGS
Siz
Dia. 10-1500mm, Length: 3000-6000mm
Heat Treatment
Quenched, Tempered, Annealed
Surface Require
Black, Grinding, Bright, Polish
Delivery Condition
Hot Rolled, Forged, Eaf+Lf+Vd
Transport Package
Seaworthy Packing/Wooden Box or at Client′s Requir
Specification
Customized
Trademark
OEM & ODM
Origin
China
HS Code
722100000
Production Capacity
1000 Ton/Month

Product Description

Product Description


AerMet® 100 is an ultra-high strength type of martensitic (a very hard form of steel crystalline structure) steel alloy.

Is was developed in response to a need for a stronger and tougher material with superior fracture toughness and ductility. The alloy possesses a minimum tensile strength of 280 ksi (1930 MPa) and a minimum fracture toughness of 100 Ksi/in. AerMet is weldable requiring no preheating. Since it is not a corrosion resistant alloy, it must be sealed if used in a moist environment. The exceptional properties of hardness, FTT, tensile strength and ductility make this alloy a candidate for application such as landing gear, armor, fasteners, actuators, ordnance, jet engine shafts, drive shafts and structural tubing. AerMet 100 may be considered for use up to about 800° F (427° C).

 

Chemical Composition:

Element min max
Carbon 0.21 0.25
Manganese - 0.10
Silicon - 0.15
Phosphorus - 0.008
Sulfur - 0.005
Chromium 2.90 3.30
Cobalt 13.00 14.00
Molybdenum 1.10 1.30
Titanium - 0.015
Aluminum - 0.015
Oxygen - 0.0020 (20 ppm)
Nitrogen - 0.0015 (15 ppm)
Nickel 11.00 12.00
Iron - *Balance

Fabrication and Working Instructions:

AerMet 100 can be difficult to machine at HRC 38. In order to mitigate that, carbide tools are recommended at 280 to 350 SFM. After the machining process, stress relieve at 800°F (427°C) is recommended for 1-3 hours.

Forging, on the other hand, should start at a temperature of 2250°F (1232°C) for first break down. Then, the part should be finished starting with a temperature of 1800°F (982°C) and down to 1650° F (899°C) for optimization. After the forging is finished, Steel AerMet 100 should be air cooled to room temperature, followed by annealing and normalizing in order to restore properties to the dead zone.

AerMet 100 is weldable without preheating required.

Typical mechanical properties on longitudinal orientation with heat treatment at 1625°F (885°C), one-hour air cooling to achieve -100°F (-73°C) of the previous temperature, and then aging for 5 hours at 900°F (482°C) are listed in the table below:

Rc UTS Elongation Reduction of Area Charpy V-notch Impact Energy FTT K
53.0/54.0 285 ksi 14% 65% 30 ft-lbs / 40.67 Nm 115 Ksi√ in

Mechanical Properties (Longitudinal)

Property Value
Tensile Strength 290 ksi
Yield Strength at 0.2% Offset 245 ksi
Elongation in 4D 10%
Reduction of Area 50%

Mechanical Properties (Transverse)

Property Value
Tensile Strength 290 ksi
Yield Strength at 0.2% Offset 245 ksi
Elongation in 4D 8%
Reduction of Area 35%

Physical Properties

Property Value
Density 0.285 lb /in3
Modulus of Elasticity 28.2 x 103 ksi
Electrical Resistivity 259.0 ohm-cir-mil/ft at 70.0°F (21°C)
Critical Temperature AC1 - 1065°F (573°C)
AC3 - 1525°F (830°C)
Mean Co of Thermal Expansion Annealed - 6.01 x 10-6 in/in/°F
Heat treated - 6.08 x 10-6 in/in/°F

Mechanical and Physical Properties at a Given Temperature

Properties 70°F (21.1°C) 200°F (93.3°C) 300°F (148.9°C) 400°F (204.4°C) 600°F (316.5°C) 700°F (371.1°C) 800°F (426.7°C) 1000°F (537.8°C)
Ultimate Tensile Strength - 285 ksi 270 ksi 260 ksi 248 ksi 237 ksi 229 ksi -
Yield Strength at 0.2% Offset - 250 ksi 240 ksi 230 ksi 218 ksi 200 ksi 192 ksi -
Reduction of area - 55% 62% 64% 63% 61% 60% -
Elongation - 14% 16% 16% 16% 15% 15% -
Charpy V-notch Impact Energy - 50 ft-lb 52.3 ft-lb 50 ft-lb 33.2 ft-lb 28 ft-lb 27.2 ft-lb -
Modulus of Elasticity 28.2 x 103 ksi - - - - - - -

Specification

Size Round Dia 6-1200mm
Plate/Flat/Block Thickness
6mm-500mm
Width
20mm-1000mm
Heat treatment Normalized ; Annealed ; Quenched ; Tempered
Surface condition Black; Peeled; Polished; Machined; Grinded; Turned; Milled
Delivery condition Forged; Hot rolled; Cold drawn
Test Tensile strength, Yield strength, elongation, area of reduction, impact value, hardness, grain size, ultrasonic test, US inspection, magnetic particle testing, etc. 
Payment terms T/T;L/C;/Money gram/ Paypal
Trade terms FOB; CIF; CNF
Delivery time 20-25 days
Application Structural parts of medium and large cross sections and high surface hardness, e.g., valve and gate valves, cylinders for combustion engines, superheated steam valves and fittings.
 
Quality Assurance
Below inspection will be done in the production.
(1) ray detection---RT;
(2) ultrasonic testing---UT;
(3) Magnetic Particle Testing-MT;
(4) penetration testing-PT; 
(5) eddy current flaw detection-ET

 
Mill′s test certificate
EN 10204/3.1 with all relevant data reg. chem. composition, mech. properties and results of testing.
 
Main Material
 
COLD WORK TOOL STEEL
Grade AISI  /ASTM DIN (W.Nr) JIS EN/ BS GB
DC53 higher than D2   SKD11 XW-5 Cr8Mo2Vsi
D2 D2 1.2379 SKD11 BD2 CR12MO1V1
Cr12MoV         CR12MOV
D3 D3 1.2080 SKD1 BD3 CR12
O1 O1 1.2510 SKS3   9CRWMN
HMD5   HMD5     7CrSiMnMoV
5CrNiMo L6 55NiCrMoV6 SKT4   5CrNiMo
52100 52100 1.3505   EN31 GCR15
HOT WORK TOOL STEEL
H13 H13 1.2344/1.2342 SKD61/DAC 8407 4CR5MOSIV1
FDAC   1.2347 FDAC   FDAC
H11 H11 1.2343 SKD6   H11
3Cr2W8V H21 1.2581/ X30WCrV93 SKD5 BH21 3CR2W8V
PLASTIC MOULD STEEL
P20 P20 1.2311 HPM7/PX88 618 3CR2MO
718 P20+NI 1.2738 PX4/PX5 718 3CR2NIMO
S136 420 1.2083 S-STAR S136 4CR13
NAK80 P21 /P20+S 1.2312 NAK80   15NI3MN
HIGH SPEED STEEL
M2 M2   SKH51   W6MO5CR4V2
M42 M42 S2-10-1-8 SKH59   W2MO9CR4VCO8
           
ALLOY STRUCTURE STEEL 
Grade AISI  /ASTM DIN (W.Nr) JIS EN/ BS GB
5120 5120 1.7027 /21Cr4 SCr420   20Cr
530M40 /5140 530M40 /5140 1.7035 /41Cr4 SCr440   40Cr
5145 5145   Scr445   45CR4
4118 4118 1.7243 /18CrMo4 SCM418 / SCM420   20CrMo
4135 4130 1.7218 /25CrMo4 SCM430 708A25/ 708M25 30CrMo
4140 4140 1.7225 /42CrMo4 SCM440 EN19/ 709M40 42CrMo
4340 4340 1.6582/ 34CrNiMo6 SNCM 439/ SNCM8 EN24/ 817M40 40CrNi2Mo
8620 8620 1.6523/ 21NiCrMo2 SNCM220 805M20 20CrNiMo
CARBON STEEL 
20 1020 C22. CK22 S20C EN3B /070M20 20
35 1035 C35.CK35 S35C   35
45 1045 C45.CK45 S45C EN8D/C45E 45
50 1050 CK53 S50C EN9/070M55 50
Q355   S355J   /ST52   EN14 Q355
30Mn 1030.1033   S30C   30Mn
30Mn2 1330 30Mn5 SMn433h   30Mn2
STAINLESS STEEL 
steel grades: 304, 304L, 316, 316L, 321, 410 430, 431, 2205, 2304, 2507. F53, F55
 
Detailed Photos
AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
Company Profile
AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
Equipment and Process
AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
Application
AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
Packaging
AMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing GearAMS 6478 AMS 6532 Aermet 100 A100 Martensitic Alloy Bar for Aircraft Landing Gear
 

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