GH3536

Объем поставок для авиационной группы

Поковки, круглые прутки, стальные листы, кольца, бесшовные трубы, стальные листы/стальные ленты, сварочные материалы, добро пожаловать на запрос!

1. Introduction to GH3536 Materials

      GH3536 alloy is a nickel-based high-temperature alloy with higher iron content that is mainly strengthened with chromium and molybdenum. The alloy has medium durability and creep strength below 900°C; it has good oxidation and corrosion resistance, good hot and cold processing forming properties and welding properties. It is suitable for manufacturing components such as aircraft engine combustion chambers that are used for a long time below 900℃, as well as high-temperature components that can be used for short-term use at 1080℃.

Стандарты внедрения

      GB/T14992 “Classification and Numbering of High Temperature Materials for High Temperature Alloys and Intermetallic Compounds”

      GJB1952A “Code for Cold Rolled Plate for High Temperature Alloys for Aviation”

      GJB2297A “Specifications for Cold Drawn (Rolled) Seamless Pipe for High Temperature Alloys for Aviation”

      GJB 2612-1996 "Технические условия на холодную вытяжку высокотемпературных сплавов для сварки"

      GJB 3020-1997 "Технические условия на кольцевые билы из высокотемпературных сплавов для авиации"

      GJB 3165-1998 "Технические условия на горячекатаные и кованые стержни для деталей авиационной техники"

      HB5496 “GH536 alloy round cake, ring blank and ring piece”

      HB/Z140 “Heat Treatment Process for High Temperature Alloys for Aviation”

2. Chemical composition of GH3536

3. GH3536 physical properties

Material properties:

      1) Excellent antioxidant properties at up to 1200℃

      2) Good high temperature strength

      3) Very good formability and welding

      4) Very good resistance to stress corrosion cracking

4. GH3536 product features

      It has good oxidation and corrosion resistance, medium durability and creep strength below 900℃, and good cold and hot processing forming properties and welding performance.

      Suitable for manufacturing combustion chamber components and other high-temperature components of aircraft engines, long-term use below 900℃, and short-term working temperature reaches 1080℃. Alloys that can withstand certain stress at high temperatures of 600-1200°C and have oxidation or corrosion resistance.

V. GH3536 application fields

      Industrial and aviation turbines (combustion chambers, rectifiers, structural covers)

      Industrial furnace components, support rollers, gratings, ribbons and radiation tubes

      Spiral tubes in petrochemical furnaces

      High temperature gas cooling nuclear reactor