Inconel Alloy X-750 Forging Rings For High Pressure Turbine Engine Aerospace

Name: Inconel Alloy X-750 Forging Rings For High Pressure Turbine Engine Aerospace
Brand: Hunan Dinghan New Material Technology Co., LTD

Price Negotiable

Price: Negotiable

MOQ: Negotiable

Delivery Time: (Sample order) 7 days

Brand: DINGSCO

Product Description

Inconel Alloy X-750 Forging Rings for High Pressure Turbine Engine Aerospace

High Pressure Turbine (HPT) engines are critical components in both aerospace and power generation sectors, operating under extremely high temperatures and pressures. Nickel alloy forging rings play a pivotal role in these engines due to their superior strength, corrosion resistance, and thermal stability. Here are details concerning nickel alloy forging rings used in High Pressure Turbine engines:

Composition:

Nickel alloy forging rings for HPT engines are made from specialized nickel-based superalloys. These superalloys often include additional elements such as chromium, cobalt, molybdenum, and aluminum to enhance their high-temperature strength, durability, and corrosion resistance. Common superalloys include Inconel, Hastelloy, Waspaloy, and Rene alloys.

Properties:

High-Temperature Capability: Nickel alloy forging rings can withstand the extreme temperatures found in HPT engines, often exceeding 1000°C.
Creep Resistance: They retain their mechanical properties under high stress for long periods at high temperatures, resistance to creep is crucial for maintaining engine integrity.
Corrosion and Oxidation Resistance: The inclusion of chromium and aluminum provides excellent resistance against oxidation and corrosion caused by fuel combustion.
Fatigue Resistance: These alloys are designed to resist fatigue cracking under the cyclic stresses of engine operation.

Applications:

In HPT engines, nickel alloy forging rings are utilized in components such as:

Turbine disks
Seals and casing segments
Compressor rings
Rotor and stator assemblies

Grade	UNS	Density	Tensile Strength (MPa min)	Yield Strength (MPa min)	Reduction of Area min (%)	Elongation min (%)	Hardness (HRC)
INCONEL X-750	N07750	8.28	1170MPa min	790MPa min	18%	18% min	HRC35 max
INCONEL 625	N06625	8.44	827MPa min	414MPa min	/	30% min	HRC35 max
INCONEL 718	N07718	8.19	1275MPa min	1034MPa min	15%	12% min	HRC35-40

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Company Hunan Dinghan New Material Technology Co., LTD

Location No. 2319, Building 2, Dongfang Furong Garden, No. 582 Yuanda 1st Road, Hehuayuan Street,Furong District, Changsha, Hunan Province, China.

Contact Person Julia Wang

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Inconel Alloy X-750 Forging Rings For High Pressure Turbine Engine Aerospace

Composition:

Properties:

Applications:

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