49.025.30 钛 标准查询与下载

ASTM F945-22 航空发动机清洁材料对钛合金应力腐蚀的标准试验方法

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.

Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials

KS W 1161-2022 阳极处理 钛及钛合金 溶液pH 13或更高

Anodic treatment－Titanium and titanium alloy－Solution pH 13 or higher

KS W 1201-2022 航空航天 钛合金棒材、丝材、锻件、环件和拉拔型材 6Al 4V 退火、可热处理

Aerospace－Titanium alloy bars, wire, forgings, rings, and drawn shapes 6Al－4V annealed, heat treatable

KS W 1162-2022 钛及钛合金的热处理

Heat treatment of titanium and titanium alloys

21/30439943 DC BS EN 3311 航空航天系列 钛合金TI-P64001（Ti-6Al-4V） 退火 机加工用棒材 直径<300毫米 900兆帕≤Rm≤1160兆帕

BS EN 3311. Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bars for machining. D < 300 mm. 900 MPa ≤ Rm ≤ 1 160 MPa

prEN 3311-2021 航空航天系列 - 钛合金 TI-P64001 (Ti-6Al-4V) - 退火 - 机加工棒材 - D < 300 mm - 900 MPa ≤ Rm ≤ 1160 MPa

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bars for machining - D < 300 mm - 900 MPa ≤ Rm ≤ 1160 MPa

DIN 65083:2020 航空航天系列. 钛和钛合金铸件的热处理

This document specifies the terms and definitions for annealing, stress relieving, hot straiphtening and hot isostatic sealing. In addition to the general indications to be observed for the heat treatment of castings made from titanium and titanium alloys it defines the requireme

Aerospace series - Heat treatment of castings of titanium and titanium alloys

BS EN 3378:2019 航空航天系列 钛 TI-P99002 退火 铆钉用线材 1.6 毫米 ≤ D ≤ 10 毫米

What is BS EN 3378- Aerospace series: Titanium TI-P99002 wires for rivets about?   BS EN 3378 is a metallic material standard that covers technical specifications for the Aerospace series: Titanium TI-P99002 wires for rivets that enhance the vibration resistance and mechanical strength in aerospace applications.   BS EN 3378 specifies the requirements for Titanium TI-P99002 wires for rivets with the annealed delivery condition. BS EN 3378 sets a limit dimension range of 1.6 mm ≤ D ≤ 10 mm for aerospace applications.   Who is BS EN 3378- Aerospace series: Titanium TI-P99002 wires for rivets for?

Aerospace series. Titanium TI-P99002. Annealed. Wires for rivets. 1,6 mm ≤ D ≤ 10 mm

BS EN 3460:2019 航空航天系列 钛 TI-P99002 退火 机加工用棒材 a或D≤150毫米 Rm≥390兆帕

1   Scope This document specifies the requirements relating to: Titanium TI-P99002 Annealed Bar for machining a or D ≤ 150 mm R m ≥ 390 MPa for aerospace applications.

Aerospace series. Titanium TI-P99002. Annealed. Bar for machining. a or D ≤ 150 mm. Rm ≥ 390 MPa

ASTM F945-12(2019) 航空发动机清洁材料对钛合金应力腐蚀的标准试验方法

Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials

BS EN 3314:2019 航空航天系列 钛合金TI-P64001 固溶处理和老化 机加工用棒材 直径≤75毫米

What is BS EN 3314 - Titanium alloy for aerospace about ?   BS EN 3314 is a European metallic material standard for aerospace applications and specifies the requirements relating to:   Titanium alloy TI-P64001   Solution treated and aged    Bar for machining  

Aerospace series. Titanium alloy TI-P64001. Solution treated and aged. Bar for machining. D ≤ 75 mm

BS EN 3315:2018 航空航天系列 钛合金TI-P64001 固溶处理和老化 锻件 深度≤75毫米

What is this standard about? This European Standard specifies the requirements relating to:   Titanium alloy TI-P64001 Solution treated and aged Forgings De ≤ 75 mm   for aerospace applications.

Aerospace series. Titanium alloy TI-P64001. Solution treated and aged. Forgings. De ≤ 75 mm

BS EN 3451:2017 航空航天系列 钛TI-P99002 未经热处理 2级锻件坯料，用于退火锻件-a或D300mm

Aerospace series. Titanium TI-P99002. Not heat treated. Grade 2 forging stock, for annealed forgings - a or D 300 mm

EN 3451:2017 航空航天系列-钛 TI-P99002-未热处理-退火锻件的 2 级锻坯 -a 或 D ▲300 mm

Aerospace series - Titanium TI-P99002 - Not heat treated - Grade 2 forging stock@ for annealed forgings - a or D ��300 mm

DIN EN 331:2016 航空航天系列. Ti-6Al-4V型钛合金. 退火. 锻件. D<(下标)e> <小于 => 150 mm; 德文和英文版本EN 3312-2012

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Forgings - D_e 150 mm; German and English version EN 3312:2012

SAE AMS4982F-2015 钛合金丝 44.5 Cb（UNS R58450）

The specification covers a titanium alloy in the form of wire.

Titanium Alloy Wire 44.5 Cb (UNS R58450)

SAE AMS2775C-2015 钛和钛合金的表面硬化

This specification covers the engineering requirements for producing a carbon-oxygen-nitrogenbearing case on titanium and titanium alloys by means of a molten salt bath, and the properties of the case.

Case Hardening of Titanium and Titanium Alloys

SAE AMS4924H-2015 钛合金棒材 锻件 和环-15 5Al 2.5Sn 超低间隙退火（UNS R54521）

This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides, and stock for forging and flash welded rings of any size.

Titanium Alloy Bars@ Forgings@ and Rings-15 5Al - 2.5Sn@ Extra Low Interstitial Annealed (UNS R54521)

SAE AMS4931E-2015 钛合金杆 锻件 和环 6Al 4V 超低间隙（ELI）双相退火 断裂韧性（UNS R56400）

This specification covers a titanium alloy in the form of bars 6.000 inches (152.40 mm) and under in nominal diameter or least distance between parallel sides, forgings and flash welded rings 6.000 inches (152.40 mm) and under in thickness, and stock for forging and stock for flash welded rings of any size.

Titanium Alloy Bars@ Forgings@ and Rings 6Al - 4V Extra Low Interstitial (ELI) Duplex Annealed@ Fracture Toughness (UNS R56400)

SAE AMS4984F-2015 钛合金锻件 10V 2Fe 3Al 自耗电极熔化 固溶热处理和时效 173 ksi（1193 MPa）抗拉强度（UNS R56410）

This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size.

Titanium Alloy Forgings 10V - 2Fe - 3Al Consumable Electrode Melted@ Solution Heat Treated and Aged 173 ksi (1193 MPa) Tensile Strength (UNS R56410)