HIGH TEMPERATURE ALLOY

Abstract: The invention relates to a high temperature nickel-­ chromium alloy comprising (in weight percent) about: Carbon 1 to 3 Silicon 0,5 to 3 Chromium 20 to 40 Molybdenum 3 to 12 Iron 3 max Columbium 1 to 5 Nickel Balance

Description: Title: High temperature alloy BACKGROUND OF THE INVENTTON 1. - Field of the invention In one aspect this invention relates to high temperature alloys. In a further aspect this invention relates to hard surfacing alloys. In another aspect this invention relates to parts surfaced with or cast from a nickel-chromium alloy with the addition of carbide-forming components. 2. - Prior Art Nickel-chromium alloys are already known which form heat, corrosion and abrasion resistant hard surfaces and which are suitable for use at elevated temperatures. Said known alloys are used, for example, in connection with valves for combustion engines. German Offenlegungsschrift 28 37 196.2 discloses such alloys which avoid the use of the otherwise common but expensive alloy components like cobalt. BRIEF SIIMMARY OF THE INVENTION It is an object of this invention to formulate a temperature resistant alloy which is essentially free of cobalt. It is a further object of this invention to furnish an improved heat, corrosion and abrasion resistant hard facing alloy suitable for use at elevated temperatures. It is yet another object of this invention to provide an alloy with higher resistance to oxidation and lead oxide in an internal combustion engine environment. Another object of the invention is to avoid the coarse acicular carbide formation during re-melt through a control in carbon, chromium, niobium and molybdenum contents. A still further object of the invention is to provide an alloy having mechanical properties, specifically hardness properties, which are maintained through the addition of significant amount of: A) Columbium (Niobium) (Hereunder referred to as EXP 4) B) Columbium plus Vanadium (Hereunder referred to as EXP 2) C) Columbium plus Vanadium plus Tungsten (Hereunder referred to as EXP 1) It is a still further object of this invention to provide an improved nickel-chromium alloy. It is yet another object of this invention to provide a nickelchromium alloy with increased corrosion resistance, without coarse acicular carbide formation during re-melt, while at the same time the mechanical properties are maintained through the addition of niobium and tungsten and/or vanadium in a significant amount. Another object of this invention is to provide a nickel-chromium alloy with a corrosion resistance better than the corrosion resistance of the alloys disclosed in said German Offenlegungsschrift, while at the same time the hardness is at least maintained. The alloy comprises in accordance with one embodiment about 40 to 70 weight percent Nickel, up to 5 weight percent Columbium, 20 to 40 weight percent Chromium, and about 3 to 12 weight percent Molybdenum. In another embodiment, to the above mentioned components up to 5 weight percent Vanadium is added. In a further embodiment to the above mentioned components up to 5 weight percent Vanadium and up to 5 weight percent Tungsten are added. Certain impurities and residual elements in recycled scraps commonly associated with alloys of the main alloying constituents can also be present. Preferably, not more than 3 weight percent iron are present. The amount of carbon present should preferably not exceed 2,5 weight percent. The amount of silicon is preferably not less than 0,7 weight percent. In a further embodiment of this invention a structural element, such as an engine valve, a valve seat or a precombustion chamber, is surfaced with one of the nickel based alloys defined hereinbefore. Such elements have an abrasion resistant surface which performs well at elevated temperatures due to the good high temperature tiar'dri':#s of the alloy. Such structural elements also will have a greatly extended life. Oxidation, sulphidation or corrosion due to lead or other oxides is delayed because of the alloy surface which resists the corrosive effects present in an internal combustion engine. The structural element has these advantages despite being coated with an alloy which is substantially free of cobalt. As a further feature of this invention a structural element can be cast from the alloy described above. BRIEF DESCRIPTION OF THE DRAWING In the accompanying drawing the "Figure" represents a graph of hardness versus temperature for different alloy compositions. EXP 1, EXP 2 and EXP 4 are referring to the present invention. The other ones are existing alloys as described per table I. DESCRIPTION OF THE PREFERRED EMBODIMENTS The alloys of this invention are nickel based alloys containing approximately 40 to 70 weight percent nickel. Nickel as a base metal imparts a good oxidation resistance and high temperature hardness. This is particularly true when combined with the alloying elements used ind the practices of this invention. To the nickel base of this alloy is added a substantial amount of chromium, the chromium generally being present in an amount from about 25 to 32 percent by weight. Chromium is added as an alloying element because if confers good oxidation resistance on the alloy particularly at elevated temperatures, such as 1000 - 16000F. The chromium present helps insure the formation of a tight adherent oxide scale on the surface of the alloy. The oxide adhering to the alloy surface prevents further oxidation of the underlying metal. Molybdenum is present in the alloy in amounts of about 3 to 12 preferably of about 6 to 9 weight percent. Niobium is present in amounts of about 1 to 5 preferably of about 2 to 3 percent; tungsten and/or vanadium are present in amounts of about 1 to 5 preferably of about up to 3 percent. The above elements are strengthening alloying elements providing dispersed hard complex carbide particles and precipitation hardening throughout the alloy making it abrasion resistant, stronger and tougher. Carbon is present in the alloy in amounts from 1 to 3 preferably of about 1,6 to 2,5 weight percent. The preferred alloys have a substantial but controlled amount of carbides which provide good high temperature hardness. There may be high percentages of impurities, up to a total of 10 weight percent or more, present in the alloys of this invention. One example of a common impurity would be cobalt which is present in the common nickel, and chromium scrap in amounts of up to 5 percent. The alloys of this invention can be characterized as substantially free of cobalt despite the presence of residual cobalt. A further impurity is iron which can be present from the use of ferrochrome. The iron is present in amounts less than 3 percent by weight. Other materials will be present in greater or lesser amounts depending on their prevalence in the scrap mix or raw materials used to make the alloy of this invention. A further understanding can be had by referring to the accompanying example in which all parts and percentages are by weight unless otherwise indicated. EXAMPLE The experimental alloys were made by mixing pure elements and/or alloys and melting them in an induction furnace (about 200 Kgms each - open air). The aimed chemistries of embodiments of the invention (EXP 1, EXP 2, EXP 4) are listed in comparison with Stellites and an existing alloy EXP 10 in table I. Table I - Composition in weight - aimed or nominal C Mn Si Cr Ni Mo W V Fe Co Nb Stellite 1 2.8 - - 30.0 - - 12.75 - - Bal. EXP 10 2.8 0.5 1.0 29.0 Bal. 5.0 - - 3.0 Bal. Stellite 6 1.15 - - 28 - - 4.5 - - Bal. - Stellite F 1.75 - - 25 22 - 12 - - Bal. EXP 1 2.0 - 0.6 27 Bal. 8.5 2.5 2.5 3.0 - 2.5 EXP 2 1.8 - 0.6 30 Bal. 8.5 - 2.5 3.0 - 2.5 EXP 4 1.7 - 0.8 26 Bal. 7.0 - - 3.0 - 2.5 Stellite is a trademark of St. Div.-Cabot Corp., Kokomo Ind. USA. After casting of hot hardness test specimens and rods (electrodes) for arc welding, the amount of some key elements was comparatively checked (table III). Table II - Composition in weight (measured for EXP 1, 2, 4 alloys) C Cr Mo Fe Nb W V EXP 1 2.0 26.85 8.86 2.94 2.70 2.43 2.67 EXP 2 1.75 28.0 8.47 2.86 2,97 - 2.78 EXP 4 1.68 25.85 6.58 3.0 2.77 - With the rods (electrodes) five samples each of the alloys listed in table III were prepared as automotive poppet valve hard facings, and some characteristics were checked, in accordance with the test description (see below). Table III 1. - Engine test 2. - Hot impact test mean life (hrs to failure) average life difference in % with material consumption respect to Stellite F (in mm per 100 hrs) Stellite F 420 0 0,15 EXP 10 366 -15% 0,20 EXP 1 365 -13% 0,15 EXP 2 372 -11,5% 0,18 EXP 4 381 - 9,5% 0,20 BRIEF DESCRIPTION OF TESTS The above data were obtained in the following conditions: Test 1 - Engine test Air cooled, 2 It. engine, running on a dynamometer with the setup as hereunder described: rev. per minute: 4.000 Full load wide open throttle temperature: 15% higher than in standard conditions spark advance: 400 before top dead point ratio of air mass vs/fuel mass: 1 (estimated) carburettor fuel max nozzle reduced by 11% in section with respect to standard condition. Test 2 - Hot impact test Special fixture, in which an hydraulically driven test poppet valve was compelled to impact on a seat insert (EMS 202 material) in conditions controlled as hereunder described: temperature: 650 C (oxy-acethylene flame source) impact load: 710 kgms frequency: 10 cycles/sec. test time: 100 hrs metal/metal mating surface reduced by 65% by means of symmetrical reliefs milled on seat insert. Table IV - (Vickers hardness vs/temperature) - Vickers pyramid indenter 10 kg load (HV10) Alloy Room temperature 10000F 12000F 1400 0F 16000F (538 C) (6500C) (7600C) (8700C) EXP 1 470 410 375 313 175 EXP 2 470 410 375 270 150 EXP 4 470 400 350 260 n.d. The above figures can be approximately converted intro Brinell hardness (HBN) by using a conversion table. Inherent values are plotted in the "Figure" and listed hereunder: Table V - (HBN hardness vs/temperature) Alloy Room temperature 10000F 1200 0F 1400 0F 1600 0F (5380C) (6500C) (7600C) (8700C) EXP 1 470 400 370 315 175 EXP 2 470 400 370 270 150 EXP 4 470 390 350 260 n.d. As shown in the "Figure" the alloys of this invention (EXP 1-2-4) have hot hardness figures comparable with Stellite 1 or existing Ni-Cr alloys. The addition of Nb-W and/or V gives a further improvement from this particular standpoint. The peculiarity of the alloys of this invention is nevertheless an improved corrosion resistance in comparison with existing EXP 10 (as per table III) due to the reduction in amount and size of acicular carbides which are quite typical of such kind of alloys and have proved to perform detrimentally as corrosion patterns initiators. It is to be understood that this invention is not to be limited to the example given, being modifications or alterations possible without departing from the spirit and scope of the same. The invention may be summarized as follows: A high temperature nickel-chromium alloy comprising (in weight percent) about: Carbon 1 to 3 Silicon 0,5 to 3 Chromium 20 to 40 Molybdenum 3 to 12 Iron 3 max Columbium 1 to 5 Nickel Balance item 2 An alloy as set forth in item 1 wherein Columbium is present in an amount of 2 to 4 percent by weight. item 3 An alloy as set forth in item 1 or 2 with the addition of about (in weight percent): Vanadium 1 to 5 item 4 An alloy as set forth in item 3 wherein Vanadium is present in an amount of 2 to 4 percent by weight) item 5 An alloy as set forth in one of the preceding claims, particularly as set forth in item 3 or 4 with the further addition of about (in weight percent): Tungsten 1 to 5 item 6 An alloy as set forth in item 5 wherein Tungsten is present in amount of 2 to 4 percent weight. item 7 An alloy as set forth in any of items 1 - 6 wherein the amount of Chromium is from about 25 to 32 percent by weight. item 8 An alloy as set forth in any of items 1 - 7 wherein the amount of Molybdenum is from about 6 to 9 percent by weight. item 9 An alloy as set forth in any of items 1 - 8 wherein the amount of Columbium (Niobium) is from about 2 to 3 percent by weight. item 10 A high temperature nickel-chromium alloy as set forth in any of items 1 - 9 with the following preferred chemistry in weight percent: Carbon 1,6 to 2 Silicon 0,7 to 1,1 Chromium 25 to 28 Molybdenum 6 to 8 Iron 3 max Columbium 2,0 to 3,0 Nickel Balance item 11 An alloy as set forth in any of items 3 - 10 with the following preferred chemistry in weight percent: Carbon 1,5 to 2 Silicon 1,0 max Chromium 29,0 t;t) 32,0 Molybdenum 8,0 to 9,0 Iron 3 max Columbium 2,0 to 3,0 Nickel Balance Vanadium 2,0 to 3,0 item 12 An alloy as set forth in any of items 5 - 11 with the following preferred chemistry in weight percent: : Carbon 2,0 to 2,5 Silicon 1,0 max Chromium 25,0 to 28,0 Molybdenum 8,0 to 9,0 Iron 3 max Columbium 2,0 to 3,0 Nickel Balance Vanadium 2,0 to 3,0 Tungsten 2,0 to 3,0 itern 13 An alloy as set forth in item5 with the following preferred chemistry in weight percent: Carbon 2.0 Manganese Silicon 0,6 Chromium 27 Nickel Bal. Molybdenum 8,5 Tungsten 2,5 Vanadium 2,5 Iron 3,0 Cobalt Niobium 2,5 item 14 An alloy as set forth in item 3 with the following preferred chemistry in weight percent: Carbon 2,0 Manganese Silicon 0,6 Chromium 30 Nickel Bal. Molybdenum 8,5 Tungsten Vanadium 2,5 Iron 3,0 Cobalt Niobium 2,5 item 15 An alloy as set forth in item 1 with the following preferred chemistry in weight percent: Carbon 1,7 Manganese Silicon 0,8 Chromium 26 Nickel Bal. Molybdenum 7,0 Tungsten Vanadium iron 3,0 Cobalt Niobium 2,5 item 16 An alloy as set forth in item 5 with the following preferred chemistry in weight percent: Carbon 2,0 Chromium 26,85 Molybdenum 8,86 Iron 2,94 Niobium 2,70 Tungsten 2,43 Vanadium 2,67 item 17 An alloy as set forth in item 3 with the following preferred chemistry in weight percent: Carbon 1,75 Chromium 28,0 Molybdenum 8,47 Iron 2,86 Niobium 2,97 Tungsten Vanadium 2,78 item 18 An alloy as set forth in item 1 with the following preferred chemistry in weight percent: : Carbon 1,68 Chromium 25,85 Molybdenum 6,58 Iron 3,0 Niobium 2,77 Tungsten Vanadium tim item 19 An article of manufacture comprising a member having a portion which is subjected to abrasion and wear at elevated temperatures said portion being coated with an alloy, as claimed in any of items 1 - 18. item 20 The article of claim 19 where said member is an engine poppet valve and said portion comprises the seating surface thereof. item 21 The article of claim 19 where said member is a pre-combustion chamber for an internal combustion engine. item 22 The article of item 19 where said member comprises a valve member adapted for contact with a valve seat, and said portion comprises the seating surface of said valve member. item 23 The article of item 19 where said member comprises a valve seat adapted for contact with a movable valve member, and said portion comprises the seating surface of said valve seat. item 24 A cast article made from an alloy as claimed in any of items 1 - 18. Claim 25 A cast part of item 24 where said article is a pre-combustion chamber for an internal combustion engine. item 26 An article as per claims 19 - 23 with the alloy as per items 1 - 18 being applied by arc welding.

Claims: Claim 1 CLAIMS A high temperature nickel-chromium alloy comprising (in weight percent) about: Carbon 1 to 3 Silicon 0,5 to 3 Chromium 20 to 40 Molybdenum 3 to 12 Iron 3 max Columbium 1 to 5 Nickel Balance Claim 2 An alloy as set forth in claim 1 wherein Columbium is present in an amount of 2 to 4 percent by weight. Claim 3 An alloy as set forth in claim 1 or 2 with the addition of about (in weight percent): Vanadium 1 to 5 Claim 4 An alloy as set forth in claim 3 wherein Vanadium is present in an amount of 2 to 4 percent by weight) Claim 5 An alloy as set forth in one of the preceding claims, particularly as set forth in claim 3 or 4 with the further addition of about (in weight percent): Tungsten 1 to 5 Claim 6 An alloy as set forth in claim 5 wherein Tungsten is present in amount of 2 to 4 percent by weight. Claim 7 An alloy as set forth in any of claims 1 - 6 wherein the amount of Chromium is from about 25 to 32 percent by weight. Claim 8 An alloy as set forth in any of claims 1 - 7 wherein the amount of Molybdenum is from about 6 to 9 percent by weight. Claim 9 An alloy as set forth in any of claims 1 - 8 wherein the amount of Columbium (Niobium) is from about 2 to 3 percent by weight. Claim 10 A high temperature nickel-chromium alloy as set forth in any of claims 1 - 9 with the following preferred chemistry in weight percent: Carbon 1,6 to 2 Silicon 0,7 to 1,1 Chromium 25 to 28 Molybdenum 6 to 8 Iron 3 max Columbium 2,0 to 3,0 Nickel Balance

Inventors: BAGNATI, ENNIO, RIGAMONTI, FLAVIO
Applicants: EATON AUTOMOTIVE SPA.
Application year: 1981
Main classification: C22C19
IPC codes: C22C19, B23K35