RU94023000A - Nickel-base casting heat-resistant alloy - Google Patents

Nickel-base casting heat-resistant alloy

Info

Publication number
RU94023000A
RU94023000A RU94023000/02A RU94023000A RU94023000A RU 94023000 A RU94023000 A RU 94023000A RU 94023000/02 A RU94023000/02 A RU 94023000/02A RU 94023000 A RU94023000 A RU 94023000A RU 94023000 A RU94023000 A RU 94023000A
Authority
RU
Russia
Prior art keywords
nickel
rhenium
lanthanum
hafnium
niobium
Prior art date
Application number
RU94023000/02A
Other languages
Russian (ru)
Other versions
RU2081930C1 (en
Inventor
А.Г. Копылов
В.А. Дубровский
В.Н. Батуев
Original Assignee
Акционерное общество "Пермские моторы"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Акционерное общество "Пермские моторы" filed Critical Акционерное общество "Пермские моторы"
Priority to RU94023000A priority Critical patent/RU2081930C1/en
Publication of RU94023000A publication Critical patent/RU94023000A/en
Application granted granted Critical
Publication of RU2081930C1 publication Critical patent/RU2081930C1/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

FIELD: metallurgy. SUBSTANCE: the known nickel-base alloy containing carbon, chrome, titanium, aluminium, cobalt, niobium, tungsten, molybdenum, iron, lanthanum, hafnium, boron, cerium and yttrium has additionally tantalum an rhenium at the following ratio of components, wt.-%: carbon 0.12-0.18; chrome 4.3-5.6; titanium 0.9-1.3; aluminium 5.65-6.25; cobalt 8-10; niobium 4.0-4.8; tungsten 10.9-12.5; molybdenum 2.5-3.5; iron 0.1-1.0; lanthanum 0.005-0.05; hafnium 0.01-0.1; boron 0.005-0.015; cerium 0.005-0.025; yttrium 0.005-0.025; tantalum 0.15-0.35; rhenium 0.15-0.35, and nickel - the rest. EFFECT: increased hardness at increased temperature. 1 cl

Claims (1)

Изобретение относится к металлургии, в частности к сплавам, используемым для наплавки деталей, работающих на истирание в условиях высоких температур при значительных циклических и контактных нагрузках, например лопаток газотурбинных двигателей или штампов горячего выдавливания заготовок из труднодеформируемых сталей и сплавов. Цель изобретения - повышение исходной твердости сплава при работе в условиях высоких температур. Для достижения поставленной цели в известный сплав на основе никеля, содержащий углерод, хром, титан, алюминий, кобальт, ниобий, вольфрам, молибден, железо, лантан, гафний, бор, церий и иттрий, дополнительно вводят тантал и рений при следующем соотношении компонентов, мас. %: углерод 0,12 - 0,18, хром 4,3 - 5,6, титан 0,9 - 1,3, алюминий 5,65 - 6,25, кобальт 8,0 - 10,0, ниобий 4,0 - 4,8, вольфрам 10,9 - 12,5, молибден 2,5 - 3,5, железо 0,1 - 1,0, лантан 0,005 - 0,05, гафний 0,01 - 0,1, бор 0,005 - 0,015, церий 0,005 - 0,025, иттрий 0,005 - 0,025, тантал 0,15 - 0,35, рений 0,15 - 0,35, никель - остальное.The invention relates to metallurgy, in particular to alloys used for surfacing parts that work on abrasion at high temperatures under significant cyclic and contact loads, for example, gas turbine engine blades or hot extrusion dies from difficult to deform steels and alloys. The purpose of the invention is to increase the initial hardness of the alloy when operating at high temperatures. To achieve this goal, tantalum and rhenium are additionally introduced into the well-known nickel-based alloy containing carbon, chromium, titanium, aluminum, cobalt, niobium, tungsten, molybdenum, iron, lanthanum, hafnium, boron, cerium and yttrium, in the following ratio of components, wt. %: carbon 0.12 - 0.18, chromium 4.3 - 5.6, titanium 0.9 - 1.3, aluminum 5.65 - 6.25, cobalt 8.0 - 10.0, niobium 4, 0 - 4.8, tungsten 10.9 - 12.5, molybdenum 2.5 - 3.5, iron 0.1 - 1.0, lanthanum 0.005 - 0.05, hafnium 0.01 - 0.1, boron 0.005 - 0.015, cerium 0.005 - 0.025, yttrium 0.005 - 0.025, tantalum 0.15 - 0.35, rhenium 0.15 - 0.35, nickel - the rest.
RU94023000A 1994-06-15 1994-06-15 Nickel-based casting heat resistant alloy RU2081930C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94023000A RU2081930C1 (en) 1994-06-15 1994-06-15 Nickel-based casting heat resistant alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94023000A RU2081930C1 (en) 1994-06-15 1994-06-15 Nickel-based casting heat resistant alloy

Publications (2)

Publication Number Publication Date
RU94023000A true RU94023000A (en) 1997-04-20
RU2081930C1 RU2081930C1 (en) 1997-06-20

Family

ID=20157338

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94023000A RU2081930C1 (en) 1994-06-15 1994-06-15 Nickel-based casting heat resistant alloy

Country Status (1)

Country Link
RU (1) RU2081930C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2546021A1 (en) * 2011-07-12 2013-01-16 Siemens Aktiengesellschaft Nickel-based alloy, use and method
RU2524515C1 (en) * 2013-09-05 2014-07-27 Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" Refractory nickel-based alloy for casting gas turbine working blades
RU2525883C1 (en) * 2013-09-05 2014-08-20 Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" Refractory nickel-based alloy for casting gas turbine working blades

Also Published As

Publication number Publication date
RU2081930C1 (en) 1997-06-20

Similar Documents

Publication Publication Date Title
US4877461A (en) Nickel-base alloy
US5980821A (en) Austenitic nickel-chromium-iron alloy
EP0384433B1 (en) Ferritic heat resisting steel having superior high-temperature strength
KR970070221A (en) Nickel Alloy Used in Turbine Engine Parts
JP2004307999A (en) Ni-BASED SUPER HEAT RESISTANT CAST ALLOY AND TURBINE WHEEL MADE THEREOF
US5932033A (en) Silicide composite with niobium-based metallic phase and silicon-modified laves-type phase
US5942055A (en) Silicide composite with niobium-based metallic phase and silicon-modified Laves-type phase
DE69821493D1 (en) Use of heat-resistant cast steel for components of turbine housings
US3811960A (en) Process of producing nickel chromium alloy products
CA2179214C (en) Forgeable nickel alloy
KR20040089592A (en) Precipitation-strengthened nickel-iron-chromium alloy and process therefor
RU94023000A (en) Nickel-base casting heat-resistant alloy
US5017249A (en) Nickel-base alloy
JPS58120758A (en) High strength nickel base superalloy product
RU94023001A (en) Nickel-base casting heat-resistant alloy
US2746860A (en) High temperature co-cr alloys
US2423738A (en) Forgeable alloy for hightemperature use
JP3424314B2 (en) Heat resistant steel
Freche et al. Cobalt-Base Alloys for Space-Power Systems
US4049432A (en) High strength ferritic alloy-D53
US3393999A (en) High temperature nickel base alloys
RU93026096A (en) POWDER HIGH TEMPERATURE ALLOY ON THE NICKEL BASIS
JPH07331370A (en) Cobalt-chrominum-nickel-aluminum alloy for ultrahigh temperature use
GB1508184A (en) Oxidation resistant iron base alloys
RU2022044C1 (en) Nickel-base heat resistant alloy

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20090616