17-4PH Forged Plate
Specifications Alloy 17-4PH data sheet, Alloy 17-4PH Chemical, 17-4PH Properties Steelmelting (ESR refined), Blooming, Hot forging, Hot rolling, Heat treatment, Straightening, 100% Ultrasonic flaw detection test, Cold working or Machined. All of these mat
| Product parameters | |
| Material Category:: | Martensitic Stainless Steel Series |
| Steel Grade: | Alloy 17-4PH |
| Material Technical Standards:: | ASTM A276, ASTM A693, ASTM A705 |
| Stocklist & Inventory Available:: | Round bar Diam. 3mm ~ 250mm |
| Min. order quantity Per Batch:: | 100 KG |
| Product Shapes:: | Round bar, Flat bar, Hollow bar, Plate, and Forgings. |
| Ultrasonic Test Standard:: | ASTM E2375 / MIL-STD- AMS 2154 / SEP 1923 / GB/T 4162 / EN 10228-3 / EN 10308. |
| Production Lead Time:: | Within 15 days after 30% downpayment. |
| Unified Social Credit Code:: | 91510871777942750J |
| Company ISO Register No:: | UQ211218R0 |
Description
MATERIAL TECHNICAL DATA SHEET - Alloy 17-4PH
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Austenitic high-tensile superalloy & Precipitation hardening steel
HS CODE: 72221100 / 72221900 / 72222000 / 72223000
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.055
Si (％): ≤ 0.40
Mn (％): ≤ 0.60
P (％) ≤: 0.030
S (％) ≤: 0.010
Cr (％): 15.0 ~ 16.0
Ni (％): 3.80 ~ 4.50
Mo (％): -
Nb (%): 0.15 ~ 0.45
Cu (%): 3.00 ~ 3.70
Co (%): -
W (%): -
MECHANICAL PROPERTIES UNDER ROOM TEMPERATURE
Condition: TH1025
Tensile strength, σb/≥ MPa: 1070
Yield strength, σ0.2/≥ MPa: 1000
Elonghation, δ ≥(％): 12.0
Reduction of area, ф ≥ (％): 45.0
Hardness | HB: 35HRC min.
TYPICAL APPLICATIONS
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on.
PRODUCT DESCRIPTION
The alloy is usually produced by AOD / VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution treated + Aged
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Austenitic high-tensile superalloy & Precipitation hardening steel
HS CODE: 72221100 / 72221900 / 72222000 / 72223000
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.055
Si (％): ≤ 0.40
Mn (％): ≤ 0.60
P (％) ≤: 0.030
S (％) ≤: 0.010
Cr (％): 15.0 ~ 16.0
Ni (％): 3.80 ~ 4.50
Mo (％): -
Nb (%): 0.15 ~ 0.45
Cu (%): 3.00 ~ 3.70
Co (%): -
W (%): -
MECHANICAL PROPERTIES UNDER ROOM TEMPERATURE
Condition: TH1025
Tensile strength, σb/≥ MPa: 1070
Yield strength, σ0.2/≥ MPa: 1000
Elonghation, δ ≥(％): 12.0
Reduction of area, ф ≥ (％): 45.0
Hardness | HB: 35HRC min.
TYPICAL APPLICATIONS
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on.
PRODUCT DESCRIPTION
The alloy is usually produced by AOD / VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution treated + Aged
