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UNS S15700 Stainless Steel Special Alloys For Aerospace And Defense High Performance

Categories Special Alloys For Aerospace And Defense
Brand Name: CMMC
Model Number: As per specification and drawing
Certification: AS, PED, ISO, API etc.
Place of Origin: CMMC in CHINA
MOQ: Negotiable
Price: Negotiable
Payment Terms: D/P, L/C, T/T
Supply Ability: 300 metric tons per month
Delivery Time: 60-90 days
Packaging Details: Water prevent, seaworthy transport, mill's export standard packing
Material: UNS S15700, a chromium-nickel-molybdenum-aluminum semi-austenitic, precipitation-hardening stainless steel
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UNS S15700 Stainless Steel Special Alloys For Aerospace And Defense High Performance

UNS S15700 (PH15-7Mo®, AISI 632) stainless steel for aircraft components requiring high strength at elevated temperature


1 PRODUCT

UNS S15700 (PH15-7Mo®, AISI 632) stainless steel for aircraft components requiring high strength at elevated temperatures.

UNS S15700 is available in product forms as plate, sheet, strip, pipe, tube, bar (round, flat, hexagon, square, shapes), wire (profile, round, flat, square), forgings, etc.


2 EQUIVALENT DESIGNATION

Type 632(ASTM), 0Cr15Ni7Mo2Al (GB/T), SUS 632(JIS), ATI 15-7™, PH15-7Mo®


3 APPLICATION

S15700 is mainly used for applications requiring high strength and a moderate level of corrosion resistance.

S15700 is particularly beneficial for a wide range of applications that include retaining rings, springs, diaphragms, aircraft bulkheads, welded and brazed honeycomb paneling and other aircraft components requiring high strength at elevated temperatures.


4 OVERVIEW

S15700 stainless steel is a chromium-nickel-molybdenum-aluminum semi-austenitic, precipitation-hardening stainless steel that provides high strength and hardness, good corrosion resistance and minimum distortion on heat treatment.

The S15700 alloy is similar to S17700 precipitation hardening SS. S15700 is designed with substitution of approximately 2.0 percent molybdenum for 2.0 percent chromium in the S17700. This results in somewhat higher room and elevated temperature strength for the S15700.

S15700 is easily formed in the annealed condition and develops an effective balance of properties by simple heat treatments.

For applications requiring exceptionally high strength, S15700 stainless steel in Condition CH 900 is particularly useful for applications with limited ductility and workability.

In its heat-treated condition, this alloy provides excellent mechanical properties at temperatures up to 900 °F (482 °C). Its corrosion resistance is superior to that of the hardenable chromium types.

In some environments, corrosion resistance approximates that of the austenitic chromium-nickel stainless steels. Fabricating practices recommended for other chromium-nickel stainless steels can be used for S15700 stainless steel.


5 CHEMICAL COMPOSITION (wt%):

FeNiAlCrMoCMnSiPS
Balance6.50-7.750.75-1.5014.0-16.02.0-3.0≤0.09≤1.00≤1.00≤0.040≤0.030

6 PHYSICAL PROPERTY

Physical propertiesCondition
ATH 1050RH 950
Densitylbs./in3. (g/cm3)0.282 (7.804)0.277 (7.685)0.277 (7.680)
Modulus of elasticityksi. (GPa)29.0 x 103 (200)29.0 x 103 (200)
Electrical resistivityµΩ•cm808283
Magnetic permeability H/m@ 25 oersteds5.114265
@ 50 oersteds5.2147118
@ 100 oersteds5.19487
@ 200 oersteds4.75553
Maximum5.3150119
Thermal conductivity, BTU/hr./ft2./°F (W/m/K)70 °F (21 °C)104 (15.1)104 (15.1)
200 °F (93 °C)112 (16.2)112 (16.2)
400 °F (204 °C)124 (17.9)122 (17.6)
600 °F (316 °C)136 (19.7)136 (19.7)
800 °F (427 °C)146 (21.1)144 (20.8)
900 °F (482 °C)150 (21.7)
1000 °F (538 °C)158(22.8)
Mean coefficient of thermal expansion in./in./°F (μm/m/K)70–200 °F (21–93 °C)8.0 x 10-6 (14.4)6.1 x 10-6 (11.0)5.0 x 10-6 (9.0)
70–400 °F (21–204 °C)8.0 x 10-6 (14.4)6.1 x 10-6 (11.0)5.4 x 10-6 (9.7)
70–600 °F (21–316 °C)8.5 x 10-6 (15.3)6.1 x 10-6 (11.0)5.6 x 10-6 (10.1)
70–800 °F (21–427 °C)8.9 x 10-6 (16.0)6.3 x 10-6 (11.3)5.9 x 10-6 (10.6)
70–900 °F (21–482 °C)9.2 x 10-6 (16.6)6.5 x 10-6 (11.7)6.0 x 10-6 (10.8)
70–1000 °F (21–538 °C)9.4 x 10-6 (16.9)6.6 x 10-6 (11.9)6.1 x 10-6 (11.0)

7 MECHANICAL PROPERTIES

Typical room temperature mechanical properties

PropertyCondition
ATTH 1050A 1750R 100RH 950CCH 900
UTS, ksi. (MPa)130(896)145(1000)220(1517)150(1034)180(1241)245(1689)220(1517)265(1828)
0.2% YS, ksi. (MPa)55(372)90(620)205(1413)55(372)125(862)215(1482)190(1310)260(1793)
Elongation % in 2"3376127652
Rockwell HardnessB88C28C45B85C40C49C45C50

8 CORROSION RESISTANCE

The general level of corrosion resistance of S15700 stainless steel in Conditions TH 1050 and RH 950 is superior to standard hardenable types of stainless such as Types 410, 420 and 431, but is not quite as good as Type 304.


Corrosion resistance and compatibility in Rocket fuels

Oxygen – While oxygen is highly reactive chemically, liquid oxygen is noncorrosive to most metals. The precipitation hardening stainless steels experience no problem.

Ammonia –S15700 stainless steel is satisfactory for handling ammonia.

Hydrogen – Liquid hydrogen and gaseous hydrogen at low temperatures are noncorrosive.

Nitrogen Tetroxide – Static tests in nitrogen tetroxide containing 3.2% by weight water lasting from 3 to 27 days, S15700 stainless steel, Condition RH 950, has shown very low corrosion rates up to 165°F (74°C). Under circulating conditions at 79°F (26°C) to 88°F (31°C) for 100 hours, it has shown no corrosion.


9 HEAT TREATMENT

S15700 stainless steel requires three essential steps in heat treating:

1) Austenite conditioning

2) Cooling to transform the austenite to martensite

3) Precipitation hardening

Standard heat treatments

It presents the procedures for heat treating material in condition A to conditions TH 1050 and RH 950.

Condition A

For in-process annealing (mill annealing), the alloy should be heated to 1950 ± 25°F (1066 ± 14°C) for three minutes for each 0.1 in. (2.5 mm) of thickness, and air cooled. This treatment may be required to restore the ductility of cold-worked material so that it can take additional drawing or forming. Although most formed or drawn parts do not require

re-annealing prior to hardening, annealing is required on severely formed or drawn parts to be heat treated to Condition TH 1050 if full response to heat treatment is required. Annealing is unnecessary in the case of the RH 950 heat treatment.

Procedure from condition A to conditions TH 1050

Procedure from condition A to conditions RH 950


Procedure from condition A to conditions CH 900


10 FORMABILITY

S15700 stainless steel in Condition A can be formed comparably to Type 301. It work hardens rapidly, and may require intermediate annealing in deep drawing or in forming intricate parts. Springback is similar to that of Type 301.

This alloy is extremely hard and strong in Condition C. Therefore, fabrication techniques for such materials must be used.


11 STANDARD SPECIFICATION

AMS 5520 Sheet, Strip and Plate

AMS 5657 Bars and forgings

AMS 5812 Welding wire

AMS 5813 Welding wire

ASTM A461 Bars, Forgings and Forging Stock

ASTM A564 / ASTM SA564 Bars, wire and shapes

ASTM A579 Forings

ASTM A693 / ASME SA693 Sheet, Plate and Strip

ASTM A705 / ASME SA705 Age hardening stainless steel forgings

MIL S-8955 Plate, Sheet and Strip


12 COMPETITIVE ADVANTAGE

(1) More than 50 years experience of research and develop in high temperature alloy, corrosion resistance alloy, precision alloy, refractory alloy, rare metal and precious metal material and products.
(2) 6 state key laboratories and calibration center.
(3) Patented technologies.

(4) Ultra-purity smelting process: VIM + IG-ESR + VAR

(5) Excellent high performance.


13 BUSINESS TERM

Minimum Order QuantityNegotiable
PriceNegotiable
Packaging DetailsWater prevent, seaworthy transport, mill’s export standard packing
MarkAs per order
Delivery Time60-90 days
Payment TermsT/T, L/C at sight, D/P
Supply Ability300 metric tons per month

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