PREN 4836 : DRAFT 2017
Withdrawn
Withdrawn
AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH
Published date
02-13-2017
Withdrawn date
11-12-2017
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Foreword
Introduction
1 Scope
2 Normative references
3 Requirements
4 Quality Assurance
5 Designation
6 Marking
7 Packaging
8 Technical Specification
9 REACH
Bibliography
Defines the dimensions, tolerances, required characteristics and the mass of a reducer, flareless tube end EN 6123, ring locked type, for use in 35000 kPa (5080 psi) working pressure systems.
| DocumentType |
Draft
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| Standards | Relationship |
| DIN EN 4836:2017-11 (Draft) | Identical |
| PREN 4832 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| PREN 4835 : DRAFT 2017 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| 14/30310864 DC : 0 | BS EN 4834 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREE CONE UP TO 35000 KPA (5080 PSI) PORT FOR RING LOCKED FITTING - INCH SERIES - GEOMETRIC CONFIGURATION |
| 14/30310862 DC : 0 | BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| PREN 4834 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) PORT FOR RING LOCKED FITTING - INCH SERIES - GEOMETRIC CONFIGURATION |
| PREN 4832 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| PREN 4835 : DRAFT 2017 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| ISO 4287:1997 | Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions and surface texture parameters |
| EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
| EN 6123:2016 | Aerospace series - Fitting end, 24° internal cone, external thread, flareless type - Extra fine thread pitch - Inch series - Design standard |
| EN 4315:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
| SAE AS5551B | Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection, Port Preparation, Installation and Removal of AS5550 and AS5865 |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| PREN 3314 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| SAE AMS5853C | Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution Treated and Work-Strengthened 160 ksi (1103 MPa) Tensile Strength |
| SAE AMS4965L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged |
| SAE AS5550C | FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| ISO 1302:2002 | Geometrical Product Specifications (GPS) — Indication of surface texture in technical product documentation |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| SAE AMS2700E | Passivation of Corrosion Resistant Steels |
| SAE AS5000C | Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for |
| SAE AMS4967L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
Summarise
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