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BS 3TA28(2009) : 2009

BS 3TA28(2009) : 2009

Current

Current

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AEROSPACE SERIES - SPECIFICATION FOR FORGING STOCK AND WIRE OF TITANIUM-ALUMINIUM-VANADIUM ALLOY (TENSILE STRENGTH 1100-1300 MPA) (LIMITING RULING SECTION 20 MM)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2009

Publisher

British Standards Institution

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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Hardcopy - English
PDF - English
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