25.200 – Heat treatment – PDF Standards Store ?u= Wed, 06 Nov 2024 05:02:56 +0000 en-US hourly 1 https://wordpress.org/?v=6.7.1 ?u=/wp-content/uploads/2024/11/cropped-icon-150x150.png 25.200 – Heat treatment – PDF Standards Store ?u= 32 32 SAE USCAR 8-4:2019 ?u=/product/publishers/sae/sae-uscar-8-42019/ Wed, 06 Nov 2024 05:02:56 +0000 Grain Flow Pattern for Bolts and Screws
Published By Publication Date Number of Pages
SAE 2019-03-14 14
]]> This specification covers the grain flow pattern requirements in headed bolts, screws, and studs. The heading practice in the manufacture of the bolt, screw, or stud sets the grain flow pattern, but it is also greatly influenced by the fastener design.

]]> SAE MAM 5914A:2003 ?u=/product/publishers/sae/sae-mam-5914a2003/ Wed, 06 Nov 2024 05:02:06 +0000 Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Foil 52.5Ni - 19Cr - 3.0Mo - 5.0Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted Precision Cold Rolled, Solution Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 11
]]> This specification covers a corrosion and heat resistant nickel
alloy in the form of sheet, strip, and foil up to 0.38 millimeters
in nominal thickness procured in SI (Metric) units.

AMS 5914 is the inch/pound version of this MAM.

These products have been used typically for the fabrication of
bellows, diaphragms, and other components requiring a combination
of high strength, resistance to heat and corrosion, leak tightness,
and maximum fatigue life, but usage is not limited to such
applications.

]]> SAE MAM 5706C:2003 ?u=/product/publishers/sae/sae-mam-5706c2003/ Wed, 06 Nov 2024 05:02:06 +0000 Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr, Consumable Electrode or Vacuum Induction Melted, 995 to 1040°C Solution Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 9
]]> This specification covers a corrosion and heat resistant nickel
alloy in the form of bars, forgings, flash welded rings, and stock
for forging, flash welded rings, or heading procured in SI (metric)
units.

AMS 5706 is the inch/pound version of this MAM.

These products have been used typically for parts, such as
fasteners, flanges, and rings, requiring high strength up to 815
degrees C and oxidation resistance up to 955 degrees C,
particularly those parts which are formed or welded and then heat
treated to develop required properties, but usage is not limited to
such applications.

]]> SAE MAM 5598C:2003 ?u=/product/publishers/sae/sae-mam-5598c2003/ Wed, 06 Nov 2024 05:02:04 +0000 Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti 0.70Al 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
Published By Publication Date Number of Pages
SAE 2003-03-12 7
]]> This specification covers a corrosion and heat resistant nickel
alloy in the form of sheet, strip, and plate procured in SI
(metric) units.

AMS 5598 is the inch/pound version of this MAM.

]]> SAE MAM 5599C:2003 ?u=/product/publishers/sae/sae-mam-5599c2003/ Wed, 06 Nov 2024 05:02:04 +0000 Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7(Cb + Ta) Annealed
Published By Publication Date Number of Pages
SAE 2003-03-12 6
]]> This specification covers a corrosion and heat resistant nickel
alloy in the form of sheet, strip, and plate procured in SI
(metric) units.

AMS 5599, specified in inch/pound version of this MAM.

These products have been used typically for parts requiring
corrosion and oxidation resistance up to 1095 degrees C,
particularly where such parts may require welding during
fabrication, but usage is not limited to such applications.

]]> SAE MAM 5536B:2003 ?u=/product/publishers/sae/sae-mam-5536b2003/ Wed, 06 Nov 2024 05:02:04 +0000 Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe, Solution Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 7
]]> This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5536 is the inch/pound version of this MAM. These products have been used typically for parts requiring oxidation resistance up to 1205 degrees C and relatively high strength up to 815 degrees C, but usage is not limited to such applications.

]]> SAE MAM 4911B:2003 ?u=/product/publishers/sae/sae-mam-4911b2003/ Wed, 06 Nov 2024 05:02:04 +0000 Titanium Alloy, Sheet, Strip, and Plate, 6Al 4V, Annealed
Published By Publication Date Number of Pages
SAE 2003-03-12 9
]]> This specification covers a titanium alloy in the form of sheet,
strip, and plate procured in metric units.

AMS 4911 is the inch/pound version of this MAM.

These products have been used typically for parts requiring
strength up to 400 degrees C, but usage is not limited to such
applications.

Certain processing procedures and service conditions may cause
these products to become subject to stress-corrosion cracking; ARP
982 recommends practices to minimize such conditions.

]]> SAE MAM 4323B:2003 ?u=/product/publishers/sae/sae-mam-4323b2003/ Wed, 06 Nov 2024 05:02:01 +0000 Aluminum Alloy, Hand Forgings, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 7
]]> This specification covers an aluminum alloy in the form of hand
forgings procured to metric dimensions.

AMS 4323 is the inch/pound version of this MAM.

These forgings have been used typically for parts requiring a
high level of mechanical properties and good resistance to
stress-corrosion cracking, but usage is not limited to such
applications.

]]> SAE MAM 4247B:2003 ?u=/product/publishers/sae/sae-mam-4247b2003/ Wed, 06 Nov 2024 05:02:01 +0000 Aluminum Alloy, Hand Forgings 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T7352) Solution Heat Treated, Stress Relieved by Compression, and Precipitation Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 7
]]> This specification covers an aluminum alloy in the form of hand
forgings procured to metric dimensions. AMS 4247 is the inch/pound
version of this MAM.

These forgings have been used typically for parts requiring a
combination of high strength and resistance to stress-corrosion
cracking and for parts requiring stability during machining, but
usage is not limited to such applications.

]]> SAE MAM 4248B:2003 ?u=/product/publishers/sae/sae-mam-4248b2003/ Wed, 06 Nov 2024 05:02:01 +0000 Aluminum Alloy, Hand Forgings and Rolled Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr Solution Heat Treated, Stress Relieved by Compression, and Precipitation Heat Treated
Published By Publication Date Number of Pages
SAE 2003-03-12 7
]]> This specification covers an aluminum alloy in the form of hand forgings and rolled rings procured to metric (SI) dimensions. These products have been used typically for complex shaped parts requiring moderate strength and good forgeability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element.

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