BS 3TA28(2009) : 2009
Current
The latest, up-to-date edition.
AEROSPACE SERIES - SPECIFICATION FOR FORGING STOCK AND WIRE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 1100-1300 MPA) (LIMITING RULING SECTION 20 MM)
Hardcopy , PDF
English
01-01-2009
Foreword
1 Scope
2 Normative references
3 Technical requirements
Bibliography
Describes requirements for titanium-aluminium-vanadium alloy forging stock and wire with a tensile strength of 1100 MPa to 1300 MPa.
| Committee |
ACE/61/-/49
|
| DevelopmentNote |
Supersedes BS 2TA28(1974) and 09/30193258 DC. (11/2009) 2009 Edition Re-Issued in October 2015 & incorporates AMD 1 2015. Supersedes 15/30324219 DC. (10/2015)
|
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
| 15/30329889 DC : 0 | BS A 266 TO 271 - BOLT, 100 DEGREES COUNTERSUNK HEAD, HI-TORQUE SPEED DRIVE RECESS, UNJF THREAD, SPLIT PIN HOLE OPTION, TITANIUM ALLOY, VARIOUS FINISHES, CLASSIFICATION: 80 TF/IN[2] (1100 MPA) AT TA/+315 DEGREES C |
| BS 2A 266 to 2A 271:2016+A1:2019 | Aerospace Series. Bolt, 100° Countersunk head, Hi-Torque speed drive recess, close tolerance shank, UNJF thread, split pin hole option, titanium alloy, various finishes. Classification: R<sub>m</sub> 1100–1250 MPa (160 000–180 000 lbf/in<sup>2</sup>) at Ambient Temperature | +315 °C |
| BS A101(1969) : 1969 | GENERAL REQUIREMENTS FOR TITANIUM BOLTS |
| PREN 2002-16 : 200P1 | AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 16: NON-DESTRUCTIVE TESTING - PENETRANT TESTING |
| BS EN 4500-004:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules for titanium and titanium alloys |
| BS EN 4050-2:2012 | Aerospace series. Test method for metallic materials. Ultrasonic inspection of bars, plates, forging stock and forgings Performance of test |
| BS 2TA 59:2009 | Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 920-1180 MPa) |
| BS 3TA 10:2009 | Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa) |
| BS 3TA 100:2009 | Procedure for inspection, testing and acceptance of wrought titanium and titanium alloys |
| BS 2TA 56:2009 | Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm) |
| BS EN 4179:2017 | Aerospace series. Qualification and approval of personnel for non-destructive testing |
| BS EN 3310:2011 | Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Not heat treated. Forging stock, for annealed forgings. De ≤ 360 mm |
| BS EN 3312:2012 | Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Forgings De ≤ 150 mm |
| BS 3TA11(2009) : 2009 | AEROSPACE SERIES - SPECIFICATION FOR BAR AND SECTION FOR MACHINING OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 900-1160 MPA) (LIMITING RULING SECTION 150 MM) |
| BS EN 4500-001:2012 | Aerospace series. Metallic materials. Rules for drafting and presentation of material standards General rules |
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