BS EN 4182:2001
Current
The latest, up-to-date edition.
Aerospace series. Pipe coupling 8°30\' in titanium alloy. Tees, reduced
Hardcopy , PDF
English
09-11-2001
Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification
Specifies the characteristics of tees, reduced, for pipe couplings 8 degree 30 minutes, in titanium alloy, for aerospace applications.
Committee |
ACE/12
|
DevelopmentNote |
Supersedes 99/707376 DC (11/2001)
|
DocumentType |
Standard
|
Pages |
12
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This standard specifies the characteristics of tees, reduced, for pipe couplings 8 30\', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: 55 C to 135 C
Standards | Relationship |
SN EN 4182 : 2001 | Identical |
NBN EN 4182 : 2002 | Identical |
NF EN 4182 : 2002 | Identical |
UNI EN 4182 : 2002 | Identical |
NEN EN 4182 : 2001 | Identical |
NS EN 4182 : 1ED 2002 | Identical |
DIN EN 4182:2002-08 | Identical |
EN 4182:2001 | Identical |
I.S. EN 4182:2002 | Identical |
EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
EN 3275:2002 | Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Dynamic beam seal - Metric series - Technical specification |
EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
ISO 5855-3:1999 | Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems |
EN 2424:2008 | Aerospace series - Marking of aerospace products |
EN 3274:2010 | Aerospace series - Pipe coupling 8°30' - Thread end - Geometric configuration |
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