49.025.30 - Titanium
ICS 49.025.30 Details
Titanium
Titan
Titane
Titan
General Information
Frequently Asked Questions
ICS 49.025.30 is a classification code in the International Classification for Standards (ICS) system. It covers "Titanium". The ICS is a hierarchical classification system used to organize international, regional, and national standards, facilitating the search and identification of standards across different fields.
There are 176 standards classified under ICS 49.025.30 (Titanium). These standards are published by international and regional standardization bodies including ISO, IEC, CEN, CENELEC, and ETSI.
The International Classification for Standards (ICS) is a hierarchical classification system maintained by ISO to organize standards and related documents. It uses a three-level structure with field (2 digits), group (3 digits), and sub-group (2 digits) codes. The ICS helps users find standards by subject area and enables statistical analysis of standards development activities.
e-Library Subscription
Create subscription and get permanent access to documents within 49.025.30 - Titanium
Currently subscription includes documents marked with .We are working on making all documents available within the subscription.
This document specifies the characteristics of screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa /315 °C .
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy remelting stock. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard27 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy tubes. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard35 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy plates, sheets and strips. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard37 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy forging stock. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard36 pagesEnglish languagee-Library read for1 day
This document specifies the general requirements for the recycling, by vacuum remelting or cold hearth melting, of titanium and titanium alloy scrap used for the production of ingots.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy wires. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard33 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bars and sections. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard35 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bars and sections. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard35 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy tubes. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard35 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy wires. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard33 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy remelting stock. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard27 pagesEnglish languagee-Library read for1 day
This document specifies the general requirements for the recycling, by vacuum remelting or cold hearth melting, of titanium and titanium alloy scrap used for the production of ingots.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy forging stock. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard36 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy plates, sheets and strips. It is intended to be applied when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard37 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 004 specifies the "Specific rules for titanium and titanium alloys".
- Standard25 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 004 specifies the "Specific rules for titanium and titanium alloys".
- Standard25 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics for screws, 100° countersunk reduced head, offset cruciform recess, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 lubricated, classification 1 100 MPa/315 °C, inch series, for aerospace applications.
- Standard11 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa /315 °C ·
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Bars for machining
D < 300 mm
900 MPa ≤ Rm ≤ 1 160 MPa
for aerospace applications
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Bars for machining
D < 300 mm
900 MPa ≤ Rm ≤ 1 160 MPa
for aerospace applications
- Standard9 pagesEnglish languagee-Library read for1 day
SIGNIFICANCE AND USE
3.1 Because of the tendency of prestressed titanium alloy parts to crack if heated while in contact with certain chemical reagents, it is necessary to ensure that cleaning and maintenance materials will not initiate stress corrosion of titanium alloys under controlled conditions. For test specimens, two common titanium alloys are selected, one that is very susceptible (AMS 4916 or AMS 4919) and one that is not very susceptible (AMS 4911) to stress corrosion cracking.
SCOPE
1.1 This test method establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress corrosion cracking of titanium alloy parts.
1.2 The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of prestressed titanium alloys to crack when subsequently heated to elevated temperatures.
1.3 Test conditions are based upon manufacturer's maximum recommended operating solution concentration.
1.4 Units—The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.
1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific precautionary statements, see 5.3 and 5.6.
1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
- Standard5 pagesEnglish languagesale 15% off
- Standard5 pagesEnglish languagesale 15% off
This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated, for aerospace applications.
Classification: 1 100 MPa /315 °C .
- Standard11 pagesEnglish languagee-Library read for1 day
This document specifies the dimensions of a hose assembly which is in accordance with ISO 7313.
The hose assembly couples to the fittings specified in EN 3274, which are made out of titanium.
The hose is protected either by means of an anti-abrasive, anti-shock and anti-projection sleeve or by means of a fire resistant or fire proof sleeve in accordance with ISO 2685.
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Wires for rivets
1,6 mm ≤ D ≤ 10 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Bar for machining
a or D ≤ 150 mm
Rm ≥ 390 MPa
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Bar for machining
D ≤ 75 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Wires for rivets
1,6 mm ≤ D ≤ 10 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Bar for machining
a or D ≤ 150 mm
Rm ≥ 390 MPa
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Forgings
De ≤ 75 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European standard specifies the characteristics, qualification and acceptance requirements for
bolts with MJ threads in TI-P64001, for aerospace applications.
Strength class: 1 100 MPa1.
It is applicable whenever referenced.
- Standard24 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Bar for machining
D ≤ 75 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Forgings
De ≤ 75 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This standard specifies the characteristics of the pipe coupling adapter, 60° spherical sealing face manufactured in titanium alloy with locking ring, for installing in a boss for aerospace applications.
These adapters shall be installed into port connections manufactured in accordance with EN 2602 using ISO 3601-1 sealing O-rings selected sizes. O-ring material depends on the system fluid and operation conditions. The installation shall be performed in accordance with EN 2608.
Nominal working pressure: up to 28000 kPa.
Temperature range: limited by elastomeric sealing ring, −54 °C to +135 °C
- Standard11 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of thrust wire nuts 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.
- Standard7 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Titanium TI-P99002
Not heat treated
Grade 2 forging stock, for annealed forgings
a or D 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Titanium TI-P99002
Not heat treated
Grade 2 forging stock, for annealed forgings
a or D 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
- Corrigendum2 pagesEnglish languagee-Library read for1 day
This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa ) / 315 °C ).
- Standard10 pagesEnglish languagee-Library read for1 day
This standard specifies the characteristics of screws, 100° countersunk normal head, offset cruciform recess, close tolerance shank, short thread, in titanium alloy, aluminium IVD coated.
Classification: 1 100 MPa 1) / 425 °C 2).
- Standard10 pagesEnglish languagee-Library read for1 day
This European Standard specifies the characteristics of equipped blind ferrules for pipe couplings 8°30’, in titanium alloy, for aerospace applications.
- Standard7 pagesEnglish languagee-Library read for1 day
This European Standard specifies the characteristics of pressure plugs for pipe couplings 8°30’, in titanium alloy, for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This standard specifies the characteristics of elbows 45°, 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.
- Standard6 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to: )
Titanium alloy Ti-4Al-4Mo-2Sn
Solution treated and aged
Forgings
De < or = 150 mm
for aerospace application.
NOTE Other designation: WL: 3.7184
Only the chemical composition of this standard must be considered.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications.
It comprises a series of sheets, by materials or by material family, which:
- indicate the main titles, the typical chemical composition and the main characteristics,
- contain recommendations for welding and brazing,
- indicate a degree of weldability or brazeability for a given process under defined conditions.
It is applicable without restriction for the manufacturing of new parts or for repair.
- Standard26 pagesEnglish languagee-Library read for1 day
This standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Bar and wire for forged fasteners
De £ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Sheet for superplastic forming
a 6 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Sheet for superplastic forming
a 6 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Bar and wire for forged fasteners
De £ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to: )
Titanium alloy Ti-4Al-4Mo-2Sn
Solution treated and aged
Forgings
De < or = 150 mm
for aerospace application.
NOTE Other designation: WL: 3.7184
Only the chemical composition of this standard must be considered.
- Standard8 pagesEnglish languagee-Library read for1 day