SAE AMS2801B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Heat Treatment of Titanium Alloy Parts
Hardcopy , PDF
09-10-2022
English
02-27-2014
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGEMENT
7 REJECTIONS
8 NOTES
Includes engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors.
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This specification covers the engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors, of parts (See 1.1.2) made from the following titanium alloys:
| MS27225 Revision C:2007 | Nipple Assembly 45 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines |
| SAE AMS4289 | Aluminum Alloy Castings 7.0Si - 0.55Mg - 0.12Ti (F357.0-T6) Solution and Precipitation Heat Treated |
| SAE AS7102B | National Aerospace and Defense Contractors Accreditation Program Requirements for Heat Treating |
| ASTM F 3302 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Standard Specification for Titanium Alloys via Powder Bed Fusion |
| SAE AMSH81200D | Heat Treatment of Titanium and Titanium Alloys |
| ASTM F 2924 : 2014 : REDLINE | Standard Specification for Additive Manufacturing Titanium-6 Aluminum-4 Vanadium with Powder Bed Fusion |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA MSFC SPEC 3717 : 2017 | SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
| ASTM F 3001 : 2014 : REDLINE | Standard Specification for Additive Manufacturing Titanium-6 Aluminum-4 Vanadium ELI (Extra Low Interstitial) with Powder Bed Fusion |
| MS27223 Revision C:2007 | Nipple Assembly 90 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines 1/4 Inch through 2 Inch Tube Sizes |
| ASTM F 3301 : 2018 | Standard for Additive Manufacturing – Post Processing Methods – Standard Specification for Thermal Post-Processing Metal Parts Made Via Powder Bed Fusion |
| SAE AMS4914F | Titanium Alloy Cold Rolled Sheet and Strip 15V - 3Al - 3Cr - 3Sn Solution Heat Treated |
| SAE AMS2368D | Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock |
| SAE AMS 4938 : 2013 | FORGINGS, TITANIUM ALLOYS HEAT-TREATED, FINISHED-PART PROPERTIES: SHORT-TRANSVERSE TENSILE, FRACTURE TOUGHNESS, AND LONGITUDINAL TIME-DEPENDENT-TENSION |
| SAE AMS4938A | Forgings, Titanium Alloys Heat-Treated, Finished-Part Properties: Short-Traverse Tensile, Fracture Toughness, and Longitudinal Time-Dependent-Tension |
| BB-H-1168 Revision D:2010 | HELIUM, TECHNICAL |
| MIL-PRF-27407 Revision D:2014 | PROPELLANT PRESSURIZING AGENT, HELIUM |
| MIL A 18455 : C | ARGON, TECHNICAL |
| SAE AMS2750E | Pyrometry |
| SAE AMS4901T | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| SAE ARP 1962 : 1995 | TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL |
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