AMS 5659 (15-5PH)
AMS 5659 (15-5PH) properties and heat treatment forged piece, Including AMS 5659 (15-5PH) application and specifications, We have all specifications,Including AMS 5659 (15-5PH) steel plate, AMS 5659 (15-5PH) sheet, AMS 5659 (15-5PH) square steel, AMS 5659 (15-5PH) flat bar,AMS 5659 (15-5PH) round bar,AMS 5659 (15-5PH) forgings, we can own production and sales.
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forged/hot rolling/ extrusion of steel
We can produce the AMS 5659 (15-5PH) has the following specifications:
Round bar steel: 1mm to 3000mm
Square-shape steel: 1mm to 2000mm
Plate steel:0.1mm to 2500mm
Width: 10mm to 2500mm
Lenth: We can supply any lenth based on the customer's requirement.
Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes
Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.
Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement
Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement
Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.
Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirement
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Chemical composition % of the ladle analysis of grade AMS 5659 (15-5PH) and Standards
15%Cr 5%Ni Precipitation Hardening Stainless Steel
Consumable Electrode Melted (ESR or VAR)
Features & Benefits
• Medium to high strengths developed by appropriate ageing treatment
• Corrosion resistant
• Excellent transverse properties
Applications
• Aircraft structural parts
• Flap Tracks
• Engine pylons
Supply Condition & Availability
• Supplied as solution treated bright machining quality bar
• Also available on request aged to specific “H” conditions
• Stock sizes range 12.7 mm - 250 mm dia.
• Other sections on request
Related specs
1.4545
Z7 CNU15.05
Chemical Composition (Wt %)
Min | Max | |
C | - | 0.07 |
Si | - | 1.00 |
Mn | - | 1.00 |
P | - | 0.030 |
S | - | 0.015 |
Cr | 14.00 | 15.00 |
Mo | - | 0.50 |
Ni | 3.50 | 5.50 |
Nb (Cb) | 5xC | 0.45 |
Cu | 2.50 | 4.50 |
Ta | - | 0.05 |
Final Heat Treatment
Solution treat @ 1038°C. Age @ appropriate
temperature for relevant “H” condition.
(Hxxx condition aged at xxx°F).
Mechanical Properties
Condition | 0.2% Proof Stress MPa |
Tensile Strength MPa |
Elongation % |
Reduction of area % |
Hardness HB |
Min | Min | Min | Min | Min Max | |
Long. Trans. | Long. Trans. | ||||
H900 | 1172 | 1310 | 10 6 | 35 20 | 388 444 |
H1000 | 1069 | 1172 | 10 7 | 38 25 | 375 429 |
H1025 | 1000 | 1069 | 12 8 | 45 32 | 331 401 |
H1050 | 862 | 1000 | 13 9 | 45 33 | 311 375 |
H1100 | 793 | 965 | 14 10 | 45 34 | 302 363 |
H1150 | 724 | 931 | 16 11 | 50 35 | 277 352 |
Specified strength levels refer to both Transverse and Longitudinal directions.
N.B. 1Mpa = 1 N/mm
Machining performance
Download AMS 5659 (15-5PH) the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>
Principal Design Features
One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.
Machinability
Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.
Heat Treatment
CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.
Welding
Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.
Forging
Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.