49.025.15 有色金属合金综合 标准查询与下载
共找到 497 条与 有色金属合金综合 相关的标准，共 34 页
本标准规定了 GH4169合金棒材、锻件、闪光焊环形件的技术要求、质量保证规定、交付条件、确认、拒收、采购订单及质量证明书等。本标准适用于GH4169合金棒材、锻件和闪光焊环形件。
GH4169 alloy bars, forgings and rings
- ICS
- 49.025.15
- CCS
- J32
- 发布
- 2014-05-06
- 实施
- 2014-12-01
Aerospace series. Steel X5CrNiCu15-5 (1.4545). Consumable electrode remelted (ESR or VAR). Solution treated and precipitation treated (H1025). Bars for machining. a or D ≤ 250 mm. 1 070 MPa ≤ Rm ≤ 1 200 MPa. Premium quality (pq)
- ICS
- 49.025.15
- CCS
- 发布
- 2023-10-31
- 实施
- 2023-10-31
Aerospace series. Heat-resisting nickel base alloy NiCr20Co3Fe3. Rm ≥ 650 MPa. Sheets and strips, cold rolled. 0,25 mm < a ≤ 3 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2023-09-30
- 实施
- 2023-09-30
本文件规定了航空发动机紧固件用GH4738合金冷拉棒材的术语和定义、标记和编码、尺寸、外形、重量、技术要求、订货内容、取样、试验方法、检验规则、质量证明书、包装、运输和贮存。 本文件适用于航空发动机紧固件用直径不大于25mm的GH4738合金冷拉棒材。
Cold drawn GH4738 alloy bars for aircraft engine fastener
- ICS
- 49.025.15
- CCS
- C348
- 发布
- 2022-06-30
- 实施
- 2022-07-01
1 Scope This document specifies the requirements relating to: Heat-resisting alloy CO-PH4101 (CoCr20W15Ni) Vacuum melted Solution treated Forgings D e ≤ 100 mm for aerospace applications.
Aerospace series. Heat resisting alloy CO-PH4101 (CoCr20W15N1) -Vacuum melted. Solution treated. Forgings. De < 100 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2022-05-31
- 实施
- 2022-05-31
This document specifies the requirements relating to heat resisting nickel base alloy (NI-P101HT), cold worked and solution treated, bars for machining for fasteners, 3 mm ≤ D ≤ 50 mm for aerospace applications.
Aerospace series - Heat resisting nickel base alloy (NI-P101HT) - Cold worked and solution treated - Bars for machining for fasteners - 3 mm ≤ D ≤ 50 mm; German and English version EN 2960:2020
- ICS
- 49.025.15
- CCS
- 发布
- 2021-03-01
- 实施
Aerospace series - Heat resisting alloy CO-PH4101 (CoCr20W15N1) - Vacuum melted - Solution treated - Forgings - ≤ 100 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2020-11-00
- 实施
BS EN 4842. Aerospace series. Steel X5CrNiCu15-5 (WL 1.4545). Consumable electrode remelted (ESR or VAR). Solution treated and precipitation treated (H1025). Bars for machining. a or D ≤ 250 mm. 1 070 MPa ≤ Rm ≤ 1 200 MPa. Premium quality (pq)
- ICS
- 49.025.15
- CCS
- 发布
- 2020-09-15
- 实施
- 2020-09-15
What is BS EN 3018- Aerospace series: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) wires about? BS EN 3018 is a metallic material standard that serves technical specifications for the Aerospace series: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) wires that enhance load-bearing capacity and heat resistance in aerospace applications. BS EN 3018 specifies the requirements relating to Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) in wire form. BS EN 3018 specifies a cold drawn method of production and a consumable electrode method as a method of melting. BS EN 3018 sets a limit dimension of D ≤ 3 mm for aerospace applications.
Aerospace series. Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1). Consumable electrode remelted. Cold drawn wire for the manufacture of thread inserts. D ≤ 3 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2019-12-31
- 实施
- 2019-12-31
What is BS EN 2400- Nickel base alloy NI-P96-HT for aerospace applications about? BS EN 2400 is a metallic material standard that covers heat resisting nickel base alloy NI-P96-HT for aerospace applications which ensures the operational safety and thermal resistance of components at high temperatures. BS EN 2400 specifies the requirements relating to heat resisting nickel base alloy Ni-P96-HT wires. These wires should satisfy the use condition as cold drawn, and precipitation treated. It covers nickel alloy wires limit dimension of D ≤ 10 mm for aerospace applications. Who is BS EN 2400- Nickel base alloy NI-P96-HT for aerospace applications
Aerospace series. Heat resisting nickel base alloy NI-P96-HT. Cold drawn and precipitation treated. Wire. D ≤ 10 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2019-12-31
- 实施
- 2019-12-31
What is BS EN 3844 ‑ 3- Flammability of non-metallic materials in aerospace applications about? BS EN 3844 ‑ 3 is part third of a multi-series standard that covers technical specifications for the determination of resistance of material to flame and glow propagation and to flame penetration which facilitates planning and designing of interior structure of aircrafts that complies with required regulations. BS EN 3844 ‑ 3 specifies the test for the determination of the resistance of non-metallic materials in part or in whole to flame and glow propagation and to flame penetration. BS EN 3844 ‑ 3 test method is also used for testing non-metallic materials which have to meet the test criteria for the 45° Bunsen burner test. BS EN 3844 ‑ 3 is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents. Note: BS EN 3844 ‑ 3 is n...
Aerospace series. Flammability of non-metallic materials. Small burner test, 45°. Determination of the resistance of material to flame and glow propagation and to flame penetration
- ICS
- 49.025.15
- CCS
- 发布
- 2019-09-30
- 实施
- 2019-09-30
What is BS EN 3844 ‑ 1- Flammability of non-metallic materials in aerospace applications about? BS EN 3844 ‑ 1 is the first part of a multi-series standard that serves technical specifications for the determination of vertical flame propagation that enables planning and designing of the interior structure of aircraft that complies with required regulations. BS EN 3844 ‑ 1 specifies the test method for the determination of the vertical flame propagation and after flame time of non-metallic materials in part or in whole.
Aerospace series. Flammability of non-metallic materials. Small burner test, vertical. Determination of the vertical flame propagation
- ICS
- 49.025.15
- CCS
- 发布
- 2019-09-30
- 实施
- 2019-09-30
What is BS EN 4842- Aerospace series: X5CrNiCu15-5 (1.4545) bar for machining about? BS EN 4842 is a metallic material standard that covers technical specifications for the Aerospace series: X5CrNiCu15-5 (1.4545) bar for machining that enhances the structural integrity and corrosion resistance. BS EN 4842 specifies the requirements relating to X5CrNiCu15-5 (1.4545) bars for machining with consumable electrode remelted (ESR or VAR) as the method of melting. BS EN 4842 specifies delivery condition requirements as solution treated and precipitation treated (H1025).
Aerospace series. X5CrNiCu15-5 (1.4545). Consumable electrode remelted (ESR or VAR). Solution treated and precipitation treated (H1025). Bar for machining. a or D ≤ 250 mm. 1 070 MPa ≤ Rm ≤ 1 200 MPa. Premium quality (pq)
- ICS
- 49.025.15
- CCS
- 发布
- 2019-06-30
- 实施
- 2019-06-30
This European Standard specifies the requirements relating to: Heat resisting Nickel base alloy Ni-Cr20Co3Fe3 Annealed Bars for aerospace applications.
Aerospace series - Heat resisting - Nickel base alloy Ni-Cr20Co3Fe3 - Annealed - Bars; German and English version EN 2306:2017
- ICS
- 49.025.15
- CCS
- 发布
- 2018
- 实施
Aerospace series. Heat resisting. Nickel base alloy Ni-Cr20Co3Fe3. Annealed. Bars
- ICS
- 49.025.15
- CCS
- 发布
- 2017-11-17
- 实施
- 2017-11-30
Aerospace series - Heat resisting - Nickel base alloy Ni- Cr20Co3Fe3 - Annealed - Bars
- ICS
- 49.025.15
- CCS
- 发布
- 2017-10-01
- 实施
Aerospace series - Metallic materials@ Filler metal for brazing - Technical specification
- ICS
- 49.025.15
- CCS
- 发布
- 2017-08-01
- 实施
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
Nickel Alloy@ Corrosion and Heat-Resistant@ Seamless Tubing 74Ni - 15.5Cr - 8.0Fe Annealed (UNS N06600)
- ICS
- 49.025.15
- CCS
- 发布
- 2015-07-01
- 实施
This specification covers a corrosion and heat-resistant nickel alloy in the form of forgings 3.25 inches (82.6 mm) and under, and forging stock of any size. (See 8.5).
Nickel Alloy@ Corrosion and Heat Resistant@ Forgings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1825 to 1900 ��(996 to 1038 �� Solution@ Stabilization@ and Precipitation Heat Treated
- ICS
- 49.025.15
- CCS
- 发布
- 2015-01-01
- 实施
Cette Norme européenne spécifie les exigences relatives à :Alliage résistant à chaud à base de nickel NiCr20Co3Fe3RecuitFilD < ou = à 10 mmpour les applications aérospatiales.
Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D < or = 10 mm
- ICS
- 49.025.15
- CCS
- 发布
- 2014-12-26
- 实施
- 2014-12-26
