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NZ270219A - Spark plug electrode of intermetallic compound - Google Patents

Spark plug electrode of intermetallic compound

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Publication number
NZ270219A
NZ270219A NZ270219A NZ27021994A NZ270219A NZ 270219 A NZ270219 A NZ 270219A NZ 270219 A NZ270219 A NZ 270219A NZ 27021994 A NZ27021994 A NZ 27021994A NZ 270219 A NZ270219 A NZ 270219A
Authority
NZ
New Zealand
Prior art keywords
electrode
ruthenium
nickel
spark plug
intermetallic compound
Prior art date
Application number
NZ270219A
Inventor
Hermanus De Villiers Steyn
Ira Mervyn Wolff
Rudolph Coetzee
Michael Bernard Cortie
Original Assignee
Mintek
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 Mintek filed Critical Mintek
Publication of NZ270219A publication Critical patent/NZ270219A/en

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T13/00Sparking plugs
    • H01T13/20Sparking plugs characterised by features of the electrodes or insulation
    • H01T13/39Selection of materials for electrodes

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  • Spark Plugs (AREA)

Description

<div class="application article clearfix" id="description"> <p class="printTableText" lang="en">2702 1 <br><br> Priority Date(s): Jl3.|!.r*.l3.3 <br><br> Complete Specification FiM: <br><br> Claw: (6) <br><br> Publication Dst*: ...2..4.MAR..M <br><br> P.O. Journal No: IHrJ.tf: <br><br> SPARK PLUG OR IGNITER ELECTRODES AND SPARK PLUGS OR IGNITERS EMBODYING SAME <br><br> We, MINTEK, a legal body organised and existing under the laws of Sbuth Africa, of 200 Hans Strijdom Drive, Randburg, Transvaal Province, Republic of South Africa do hereby decisis the invention for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement. <br><br> PATENTS FORM 5 PATENTS ACT 1953 COMPLETE SPECIFICATION <br><br> Number Dated <br><br> - 1 - <br><br> 2702 <br><br> - 2 - <br><br> FIELD OF THE INVENTION <br><br> THIS INVENTION relates to spark plug or igniter electrodes, including both positive and negative electrodes, tips or inserts for such electrodes, and spark plugs and igniters embodying same. The spark plugs may be of the general nature employed 5 in internal combustion engines for effecting ignition thereof. An igniter may be of the general type for use in turbine engines. <br><br> 2702 <br><br> - 3 - <br><br> BACKGROUND TO THE INVENTION <br><br> Trends in modern high performance engines have resulted in more exact performance requirements. <br><br> There is a trend towards long-life spark plugs. Furthermore, the introduction of unleaded fuels is 5 enabling spark plug manufacturers to use different and new materials. <br><br> Accordingly, the longevity of spark plugs, in particular the electrodes thereof, is of increasing importance in view of the increased demands thereon. <br><br> 10 It is the object of this invention to provide inserts or tips for spark plug electrodes, spark plug electrodes and spark plugs embodying same, in which the electrodes are able to stand up to the rigorous use made of them. <br><br> SUMMARY OF THE INVENTION <br><br> 15 <br><br> In accordance with this invention there is provided a spark plug or igniter electrode characterised in <br><br> 270 <br><br> - 4 - <br><br> that the electrode, or a tip or insert mounted onto or into the electrode, is made at least predominantly of one or more intermetallic compounds having a melting point above 1400°C and <br><br> 5 wherein the intermetallic compound or compounds is or are chosen to exhibit adequate toughness, resistance to thermal shock, and electrical conductivity. <br><br> It is to be understood that in this specification <br><br> 10 the term "tip" is to be interpreted as including a pad, layer, or any other separate element secured to an electrode. Such a tip is preferably bonded, such as to a nickel or nickel alloy electrode part, by diffusion welding or the like. <br><br> 15 Further features of the invention provide for the intermetallic compound or compounds to be selected from the groups comprising ruthenium and aluminium (herein referred to as ruthenium aiuminide); ruthenium, aluminium and nickel; . platinum and <br><br> 2702 <br><br> - 5 - <br><br> aluminium; ruthenium and titanium; nickel and aluminium; titanium and aluminium; ruthenium and zirconium; ruthenium and tantalum; iron and aluminium; niobium (columbium) and aluminium; 5 molybdenum and silicon; iridium and niobium; <br><br> iridium and hafnium; iridium and titanium; iridium and tantalum; and for the intermetallic material optionally to be dispersed in one or more other phases thereby forming a dual- or multi-phase 10 material. <br><br> The intermetallic compounds are solid-state intermediate phases in alloy systems, generally formed between chemically dissimilar metals. They often have relatively simple stoichiometric 15 proportions and often have narrow composition ranges of homogeneity (or even a fixed composition). The nature of atomic bonding may vary from metallic to ionic. They are often believed to have essentially nonmetallic properties 20 such as poor electrical conductivity (S.H. Avner, <br><br> Introduction to Physical Metallurgy, McGraw-Hill Second Edition, p. 149). They have long been known to have high melting points and good oxidation resistance. <br><br> 2702 <br><br> - 6 - <br><br> However, the perception that they show poor ductility and other "non-metallic" properties has prevented intermetallic compounds from being widely used as general engineering materials. Some 5 intermetallic compounds are well researched materials today, and have found a number of applications - however, they have not yet been implemented on the scale envisaged, particularly in high-temperature gas turbines. Care should <br><br> 10 accordingly be exercised in selecting the intermetallic compound or compounds to be used in implementing the invention. <br><br> The particular advantage of ruthenium aluminide (the presently preferred intermetallic compound) 15 and some other intermetallic compounds is that they exhibit significant toughness at room temperature; have a high melting point; good oxidation resistance; and, outstanding corrosion resistance. The thermo-dynamic stability that these materials 20 exhibit at elevated temperatures and in an aggressive medium is therefore paramount. It has also been demonstrated that these compounds exhibit <br><br> 2702 <br><br> - 7 - <br><br> adequate electrical and thermal conductivity as well as adequate resistance to thermal fatigue. <br><br> Of particular interest are dual or multi phase materials comprising ruthenium aluminide, in an 5 excess of ruthenium; preferably containing between <br><br> 80 and 99 mass percent Ru; and most preferably about 90 mass percent Ru. <br><br> Some intermetallic compounds such as ruthenium aluminide are, however, difficult to manufacture by 10 conventional techniques such as melting and casting, in view of their very high melting points (approximately 2050°C for ruthenium aluminide); the aggressive attack of ruthenium aluminide and other intermetallics on refractories in the molten state; 15 and, the volatilisation of aluminium consequent on the high temperature. <br><br> However, applicant has devised a number of processes for the manufacture of such intermetallic compounds and one such process forms the subject 20 matter of applicant's South African Patent No. <br><br> 2702 <br><br> - 8 - <br><br> 94/3636 entitled "The Manufacture of Ordered Intermetallic Compounds". <br><br> In that patent we describe a process for the production of intermetallic. precious metal 5 aluminide compounds wherein the required metal, in powdered form, is intimately mixed with powdered aluminium in the required relative quantities, generally based, at least to a Ian:;- extent, on the stoichiometric atomic ratios of the. precious metal 10 and aluminium in the intermetallic product. The intimately mixed powders are formed into a shaped body using any necessary optional steps such as de-gassing, and in particular, encapsulating such as in tantalum or molybdenum foil and a titanium 15 can, followed by heating under pressure to effect reactive hot isostatic pressing followed by any required homogenisation at elevated temperature. <br><br> In the case of ruthenium aluminide, which is the material chosen for further testing, the aluminium 20 powder particle size range was between 22 and 72 fj.m and that of the precious metal was from 13 to 58 |im on average. The preferred powder size was about 22 <br><br> 2702 <br><br> - 9 - <br><br> txm in the case of aluminium and about 13/Ltm in the case of the precious metal. The compaction pressure is preferably chosen from the range between 415 and 750 MPa and preheating at a 5 temperature of about 500°C is preferably carried out preparatory to sintering at a temperature of about 1600°C for a period of about 12 hours. <br><br> A number of other manufacturing processes can be used without deviating from the scope of this 10 invention. These include, but are not limited to, <br><br> a variety of melting processes, forming processes, and a variety of powder metallurgy processes such as sintering and metal spraying processes. Material may also be produced by any combination of 15 the above . processes without deviating from the scope hereof. <br><br> The invention also provides a spark plug or other igniter embodying onh or more electrodes as defined above. Whilst usually both or all of. the 20 electrodes will be made according to the invention, <br><br> it may be that only one, for example the central electrode, employs an intermetallic compound. The <br><br> 2702 <br><br> - 10 - <br><br> spark plugs may be utilised in engines operating on leaded or unleaded fuels. Although ruthenium aluminide, with compositions close to 50 atomic per cent Ru, is attacked by leaded fuels, 5 ruthenium-rich ruthenium aluminide may be utilised in engines operating on leaded fuels. <br><br> In order that the invention may be more fully understood a detailed description thereof is given below. In this description reference is made to 10 the accompanying drawings. <br><br> BRIEF DESCRIPTION OF THE DRAWINGS <br><br> In the drawings <br><br> Figure 1 is an elevation of an experimental spark plug to which the invention is applied; <br><br> 15 <br><br> Figure 2 <br><br> is an enlarged elevation of the electrode end of the experimental spark plug with a modified central electrode <br><br> 2702 <br><br> - 11 - <br><br> fitted with an insert of intermetallic material; and, <br><br> Figure 3 is a view similar to Figure 2 but showing the standard shape of central 5 electrode. <br><br> DETAILED DESCRIPTION OF THE INVENTION WITH REFERENCE TO THE DRAWINGS <br><br> It has been found that certain intermetallic compounds exhibit relatively high electrical and thermal conductivity. For example, as indicated in <br><br> Table 1 the electrical resistivity of ruthenium <br><br> 10 aluminide compares favourably with those of previous metals used commercially in spark plug electrodes viz. platinum and gold-50-mass%-palladium. Electrical resistivity of three ruthenium aluminide materials, viz. 52 atomic <br><br> 15 per cent Ru and 48 atomic per cent A1 (80,23 mass % <br><br> Ru) (Ru52Al48); 48 atomic per cent Ru and 52 atomic per cent A1 (77,57 mass % Ru) (Ru48A152) ; and, 70 <br><br> atomic per cent Ru and 30 atomic per cent A1 (90 <br><br> mass % Ru) (Ru A1 ) was measured as well as those 70 30 <br><br> 20 of Pt and of Au-Pd alloy. Values for the resistivity of Pt from the literature are also given. <br><br> 270 <br><br> - 12 - <br><br> TABLE 1 <br><br> Electrical resistivity of previous metals and ruthenium aluminide compounds as a function of temperature. <br><br> (Resistivity given in ohm-cm) <br><br> 5 <br><br> TEMPERATURE (C) <br><br> Pt(exp) Experimental alloy <br><br> Values from literature <br><br> Au-Pd(exp) Experimental alloy (note 1) <br><br> RU48A152 <br><br> RU52A148 <br><br> RU70AI30 <br><br> 10 <br><br> 20 <br><br> 10,6 <br><br> 27,7 <br><br> 20 <br><br> 11,1 <br><br> 23,2 <br><br> 21 <br><br> 11, 6 <br><br> 24 <br><br> 15, 1 <br><br> 23,8 <br><br> 35 <br><br> 15, 7 <br><br> 15 <br><br> 90 <br><br> 13,4 <br><br> 24, 1 <br><br> 98 <br><br> 13,9 <br><br> 26,2 <br><br> 100 <br><br> 14, 0 <br><br> 102 <br><br> 13,6 <br><br> 28, 6 <br><br> 17, 3 <br><br> 26, 1 <br><br> 109 <br><br> 14, 1 <br><br> 17, 6 <br><br> 20 <br><br> 125 <br><br> 27,4 <br><br> 184 <br><br> 17,6 <br><br> 193 <br><br> 17,7 <br><br> 200 <br><br> 18, 0 <br><br> 21,1 <br><br> 204 <br><br> 29,7 <br><br> 25 <br><br> 211 <br><br> 30,3 <br><br> 281 <br><br> 21,3 <br><br> 29,8 <br><br> 29,8 <br><br> 294 <br><br> 21,5 <br><br> 300 <br><br> 21, 5 <br><br> 30,4 <br><br> 25,0 <br><br> 33,5 <br><br> 302 <br><br> 21,7 <br><br> 25, 1 <br><br> 30 <br><br> 306 <br><br> 33,5 <br><br> 386 <br><br> 24,7 <br><br> 390 <br><br> 35,8 <br><br> 398 <br><br> 36,3 <br><br> 400 <br><br> 25,5 <br><br> 31,9 <br><br> 28,8 <br><br> 37,0 <br><br> 35 <br><br> 401 <br><br> 29, 3 <br><br> 500 <br><br> 28,9 <br><br> 27,9 <br><br> 32, 6 <br><br> 40,4 <br><br> 502 <br><br> 29,0 <br><br> 33 , 0 <br><br> 39,9 <br><br> 531 <br><br> 41,5 <br><br> 600 <br><br> 31,6 <br><br> 33,4 <br><br> 40 <br><br> 601 <br><br> 42,9 <br><br> 700 <br><br> 34, 5 <br><br> 46,0 <br><br> 706 <br><br> 47,3 <br><br> 710 <br><br> 35,4 <br><br> 798 <br><br> 49,3 <br><br> 45 <br><br> 800 <br><br> 37, 3 <br><br> 895 <br><br> 52,7 <br><br> 900 <br><br> 40, 3 <br><br> 1000 <br><br> 43,1 <br><br> 43,1 <br><br> 1013 <br><br> 57, 3 <br><br> 50 <br><br> - 13 - <br><br> 270 <br><br> Also the thermal conductivity of NiAl has been reported to be higher than that of some nickel-based superalloys. It is known that a correlation exists between thermal conductivities 5 and electrical conductivities of metallic materials. <br><br> It should therefore be clear that both electrical conductivity and thermal conductivity of certain intermetallic compounds, and specifically those of ruthenium aluminide, are sufficient to allow these 10 materials to be used as spark plug or igniter electrodes, provided that the melting point of such intermetallic compound exceeds 1400°C. <br><br> - 14 - <br><br> EXPERIMENTAL TRIALS <br><br> The functionality of intermetallic compounds for use in spark-plug electrodes was tested as follows <br><br> Experimental material was prepared by one of two routes, namely: <br><br> (i) by arc melting, and <br><br> (ii) by reactive hot isostatic pressing of the constituent elements as described above and in our said South African Patent No. 94/3636 and outlined above. <br><br> A number of different compositions of experimental ruthenium aluminide materials were manufactured and tested in a number of experiments. <br><br> In each case an experimental electrode insert 1 of 1mm in diameter for centre (negative) electrode 2 of a spark plug 3 was machined from the respective experimental material to the required geometry. The electrode inserts were incorporated into standard spark plug configurations as centre electrodes only, whereby each experimental electrode insert was held within a nickel socket, <br><br> 270219 <br><br> - 15 - <br><br> and was contacted to the nickel by cold deforming. <br><br> Experimental trials comprised the following: <br><br> (i) Evaluation of spark intensity <br><br> Mounting of the spark plugs in an ignition 5 system test-bed, whereupon sparking was induced by the application of voltage, as with conventional ignition systems utilised in spark ignited engines. The sparking behaviour was observed, and compared with 10 that of standard spark plugs. <br><br> Relative to standard spark plugs, the spark intensity of the experimental spark plugs was similar. Transfer of the spark took place from the experimental electrode 15 material and not from the surrounding nickel jacket, confirming sufficient electrical conductivity of the ruthenium aluminide. <br><br> 2702 <br><br> - 16 - <br><br> (ii) Evaluation of performance utilising leaded fuel <br><br> The following experimental ruthenium aluminide alloys were manufactured by arc 5 melting:- <br><br> 1. slightly rich in aluminium <br><br> 2. stoichiometric in ruthenium and aluminium, based on an atomic ratio of 50:50, and <br><br> 10 slightly rich in ruthenium. <br><br> The lengths of the ruthenium aluminide electrode inserts were varied slightly for comparative purposes. <br><br> The spark plugs were mounted in a standard 15 six-cylinder internal combustion engine, connected to a dynamometer capable of maintaining the engine at a constant speed, with parameters such as torque, power, engine coolant temperature, and fuel consumption being directly measurable. The <br><br> 20 performance was subsequently determined under full- <br><br> and partial axle loading at .speeds up to 5000 revolutions per minute. Testing vas carried out <br><br> 27 <br><br> 17 - <br><br> using leaded fuel consistent with an octane rating of 93. <br><br> The performance of the electrodes was further evaluated by microstructural analysis of the working tip. Wear characteristics were monitored by means of computerised profile scanning on a Mitutoyo Scanpak-3 V2.10. <br><br> These experiments yielded the following observations in respect of ruthenium aluminide <br><br> 10 <br><br> having a 50:50 atomic ratio: <br><br> 1. The experimental materials yielded comparable fuel consumption, torque, <br><br> 15 <br><br> and power to the standard spark plugs under identical operating conditions. The results showed a variation in performance between the experimental and standard commercial spark plugs (reference nickel electrodes) of less than 2%. <br><br> 27 <br><br> - 18 - <br><br> 2. No ignition difficulties were encountered during hot or cold start-ups of the experimental spark plugs. <br><br> 5 3. The experimental spark plugs were not associated with any uneven or irregular running or knocking of the engine. <br><br> 4. The experimental spark plugs were not associated with "run-on" after the <br><br> 10 engine had been switched off while running at high speeds, caused by self-ignition due to an excessively hot electrode. <br><br> 5. The experimental-electrodes proved to <br><br> 15 have a high resistance to the thermal shock and mechanical vibration encountered, and that none of the electrodes failed during testing. <br><br> 20 <br><br> 6. <br><br> The wear-performance of the experimental electrodes can be modified <br><br> 270 <br><br> - 19 - <br><br> by changing, amongst other things, the electrode length, and the design of the spark plug configuration. <br><br> 7. Solid-state welding had taken place 5 between the experimental electrode inserts and the nickel sheath, demonstrating that the experimental material can be successfully bonded to nickel. <br><br> 10 8. Ruthenium aluminide of this particular composition is subject to chemical attack by the tetraethyl lead component in leaded fuels. <br><br> (iii) Evaluation of electrode erosion utilising 15 leaded fuel and Ru-rich ruthenium aluminide material that had been manufactured by arc melting <br><br> 20 <br><br> As in prior art it is known that ruthenium is resistant to attack by the tetra-ethyl lead component in fuels, centre electrode <br><br> 27 <br><br> - 20 - <br><br> inserts were manufactured from the following ruthenium-rich dual-phase ruthenium-aluminide alloys: <br><br> 1. 60.2 atomic per cent Ru and 39.8 atomic 5 percent A1, <br><br> 2. 7 0.61 atomic per cent Ru and 29.39 atomic per cent Alf <br><br> 3. 85.53 atomic per cent Ru and 16.47 atomic per cent Al. <br><br> 10 Spark plugs containing these electrode inserts were tested in a dynamometer-mounted engine that was run on leaded fuel at engine speeds up to 5 000 r/min at full open throttle and full load. <br><br> 15 This experiment yielded the following results: <br><br> 1. Performance of the spark plugs and the resulting engine performance was in all <br><br> - 21 - <br><br> respects similar to results obtained by using standard commercial spark plugs (reference nickel electrodes). <br><br> Erosion rates of the centre electrodes were less than the erosion rates that could be expected of commercia?. nickel electrodes. This indicates that <br><br> Ru-rich ruthenium aluminide may be utilised as a spark plug electrode material for use in fuels with a high lead content. <br><br> There exists an optimum composition for erosion resistance in the hypo-eutectic region between 80 and 95 mass per cent ruthenium for leaded fuels. <br><br> Solid-state welding had taken place between the experimental electrode inserts and the nickel sheath, demonstrating that the experimental material can be successfully bonded to nickel. <br><br> 2702 <br><br> - 22 - <br><br> (iv) Evaluation of electrode erosion relative to the erosion of a commercial gold-palladium electrode. utilising unleaded fuel and material manufactured bv hot isostatic 5 pressing <br><br> Centre electrode inserts as described above were manufactured from the following ruthenium aluminide materials that had been manufactured by hot isostatic pressing: <br><br> 1n TABLE 2 <br><br> 15 <br><br> RU PER CENT <br><br> Al PER CENT <br><br> PER CENT <br><br> BORON <br><br> ATOMIC <br><br> MASS <br><br> ATOMIC <br><br> MASS <br><br> ATOMIC <br><br> MASS <br><br> 50 <br><br> (78,93) <br><br> 50 <br><br> (21,07) <br><br> 0 <br><br> 0 <br><br> 53 <br><br> (80,86) <br><br> 47 <br><br> (19,14) <br><br> 0 <br><br> 0 <br><br> 52,735 <br><br> (80,79) <br><br> 46,765 <br><br> (19,13) <br><br> 0,5 <br><br> (0,08) <br><br> The electrode configuration was similar to that of a standard commercial spark plug which has a gold-palladium electrode tip. <br><br> 20 <br><br> Spark plugs containing the experimental ruthenium aluminide centre electrodes were <br><br> - 23 - <br><br> 270? <br><br> tested in two experiments (40 and 48 hours respectively) to compare erosion rates. The tests were conducted at full load and at engine speeds between 3500 and 5500 r/min. <br><br> 5 These experiments indicated that:- <br><br> 1. Erosion rates of the ruthenium aluminide materials was similar to and in some cases better than that of the gold-palladium material in unleaded 10 fuels. <br><br> 2. The alloy with 53 atomic per cent ruthenium exhibited lower erosion rates that the alloy with 50 atomic per cent ruthenium. <br><br> 15 3. The addition of boron did not improve the resistance to erosion of the experimental spark plugs. <br><br> 4. The performance of the spark plugs and the resulting engine performance was in <br><br> 20 <br><br> 1 <br><br> - 24 - <br><br> all respects similar to results obtained by using standard commercial spark plugs. <br><br> 5. Solid-state welding had taken place <br><br> 5 between the experimental electrode inserts and the nickel sheath, demonstrating that the experimental material can be successfully bonded to nickel. <br><br> 10 6. Voltage demand and spark-over time for the experimental spark plugs compared favourably with those of commercial spark plugs containing nickel or gold-palladium centre electrodes. <br><br> 15 (v) Evaluation of electrode erosion utilising <br><br> Ru-rich ruthenium aluminide (manufactured bv arc melting) and unleaded fuel <br><br> 20 <br><br> Centre electrode inserts of arc-melted alloys containing 85, 90 and 95 mass per cent ruthenium were subjected to a limited <br><br> 2702 1 <br><br> - 25 - <br><br> (8-hour) test in an engine, running on unleaded fuel at 35000r/min and full load. A standard commercial spark plug with a gold-palladium centre electrode was used as reference in this experiment to compare erosion results. <br><br> The following results were obtained: <br><br> 1. Less erosion occurred on the ruthenium aluminide insert than on the gold-palladium insert. (2,3 /xm for the alloy containing 85 mass % Ru versus 30,1 /urn for the gold-palladium insert). <br><br> 2. An optimum composition for erosion resistance of ruthenium and aluminium exists between 80 and 95 mass per cent ruthenium for unleaded fuels. <br><br> - 26 - <br><br> 270219 <br><br> (vi) Evaluation of electrode erosion utilising Ru-ricto ruthenium aluminide (manufactured bv hot isostatic pressing) in unleaded fuel <br><br> Centre electrode inserts of 1,0 mm diameter were manufactured from the following ruthenium aluminide materials: <br><br> TABLE 3 <br><br> 10 <br><br> 15 <br><br> RU PER <br><br> CENT <br><br> kl PER <br><br> CENT <br><br> BORON PER CENT <br><br> SAMPLE <br><br> ATOMIC <br><br> MASS <br><br> ATOMIC <br><br> MASS <br><br> ATOMIC <br><br> MASS <br><br> NO. <br><br> R 95 <br><br> 53 <br><br> (80,86) <br><br> 47 <br><br> (19,14) <br><br> 0 <br><br> 0 <br><br> R104 <br><br> 58 <br><br> (83,80) <br><br> 42 <br><br> (16,20) <br><br> 0 <br><br> 0 <br><br> R 98 <br><br> 63 <br><br> (86,45) <br><br> 37 <br><br> (13,55) <br><br> 0 <br><br> 0 <br><br> R101 <br><br> 68 <br><br> (88,84) <br><br> 32 <br><br> (11,16) <br><br> 0 <br><br> 0 <br><br> R100 <br><br> 52,735 <br><br> (80,79) <br><br> 46,765 <br><br> (19,13) <br><br> 0,5 <br><br> 0,08 <br><br> 20 <br><br> 25 <br><br> Spark plugs containing these inserts were tested in an engine that was run on unleaded fuel at full load at the engine speed where peak torque is delivered. A standard spark plug with a nickel-base centre electrode of diameter 2,52 mm was fitted as a reference. The face of the RuAl electrodes was therefore 0,79 mm2 compared to that of 4,99 <br><br> 2 <br><br> mm of the reference nickel electrode. The sparking surface of the reference nickel <br><br> 2702 1 <br><br> - 27 - <br><br> electrode was therefore more than six times larger than that of the ruthenium aluminide electrode inserts. <br><br> After 72 hours, electrode wear was measured. The addition of boron did not improve the resistance to erosion. <br><br> The average erosion rate over the face of the reference nickel electrode was 0,8 fjLm per hour, and at the centre it was 0,35/xm per hour. <br><br> The results indicate that an optimum Ru-content exists at or close to the eutectic composition of 70,61 atomic per cent Ru. <br><br> The test was continued for another 144 hours at the engine speed where peak torque is delivered and with a wide open throttle. Two spark plugs with electrodes of each of the following compositions were fitted for this test:- <br><br> - 28 - <br><br> 2702J <br><br> 1. 63 atomic per cent Ru and 3 7 atomic per cent A1 [86,45 mass % Ru]: One spark plug not used before and one previously used in the 72-hour test described <br><br> 5 above. <br><br> 2. 68 atomic per cent Ru and 32 atomic per cent A1 [88,84 mass % Ru]: One spark plug not used before and one previously used in the 72-hour test described <br><br> 1 q above. <br><br> 3. Standard nickel-base: One spark plug not used before and one previously used in the 72-hour test described above. <br><br> Electrode erosion was again measured after <br><br> 15 144 and 216 cumulative test hours. Erosion measured over the face of the reference electrode was misleading, because sparking alsp occurred from the side of the centre electrode facing the positive electrode. <br><br> 20 This led to low erosion rates measured at <br><br> 27 <br><br> - 29 - <br><br> the electrode centre and over the electrode face of the reference spark plug. <br><br> The average erosion rate over the face of the reference nickel-alloy electrode was 5 similar after 72, 144 and 216 hours. It was evident that a limited amount of sparking occurred from the nickel base supporting the insert, while sever erosion was measured at the corresponding edge of the reference 10 electrode. Table 4 shows the results obtained. <br><br> - 30 - <br><br> 27 <br><br> TABLE 4 <br><br> Erosion rates after an additional 144 hours endurance testing <br><br> AREAS WHERE EROSION WAS MEASURED <br><br> REFERENCE POINT ON FIGURE 5 <br><br> EROSION RATE lum/h) <br><br> 72 hours 144 hours 216 hours <br><br> Ni BASED REFERENCE ELECTRODE <br><br> Spark Face <br><br> A <br><br> 0,80 <br><br> 0,70 <br><br> 0,77 <br><br> Electrode Centre <br><br> B <br><br> 0,35 <br><br> 0,40 <br><br> 0,41 <br><br> Side Facing Pos. Electrode <br><br> C <br><br> 0,71 <br><br> 0,78 <br><br> 0,93 <br><br> AVERAGE <br><br> — <br><br> 0,62 <br><br> 0, 63 <br><br> 0,70 <br><br> EXPERIMENTAL PLUG - (68 ATOMIC % Ru) <br><br> Spark Face <br><br> D <br><br> 0,47 <br><br> 0,83 <br><br> 0,99 <br><br> Electrode Centre <br><br> E <br><br> 0, 11 <br><br> 0,53 <br><br> 0,60 <br><br> Side Facing Pos. Electrode <br><br> F <br><br> 0,20 <br><br> 0,18 <br><br> 0,12 <br><br> AVERAGE <br><br> — <br><br> 0,26 <br><br> 0, 67 <br><br> 0,57 <br><br> EXPERIMENTAL PLUG - (63 ATOMIC % Ru) <br><br> Spark Face <br><br> D <br><br> 0, 58 <br><br> 0,76 <br><br> 2,47 <br><br> Electrode Centre <br><br> E <br><br> 0,14 <br><br> 0,85 <br><br> 2,16 <br><br> Side Facing Pos. Electrode <br><br> F <br><br> 0, 10 <br><br> 0, 26 <br><br> 0,22 <br><br> AVERAGE <br><br> — <br><br> 0,27 <br><br> 0,62 <br><br> 1,62 <br><br> 2702 <br><br> - 31 - <br><br> The erosion resistance of the ruthenium aluminide alloys were comparable to that of the reference nickel-alloy electrodes irrespective of the fact that the reference nickel electrode had a sparking surface more than 6 times larger than that of the experimental ruthenium aluminide electrodes. <br><br> After 144 and 216 test hours, the reference nickel-alloy electrodes showed very stable erosion on the sparking surface of the centre electrode end. The 63 atomic per cent Ru alloy apparently showed a sharp increase in erosion after 72 hours testing. This observation is based on one sample <br><br> 27 <br><br> - 32 - <br><br> only. The 68 atomic per cent ruthenium alloy compared exceptionally well with the reference nickel-alloy electrodes of some 6 times the size (effective area). <br><br> ^ In order to obtain erosion results for nickel-alloy electrodes and ruthenium aluminide electrodes of the same diameter, ruthenium aluminide inserts containing 68 atomic % Ru, and of l mm in diameter and commercial nickel-alloy electrodes machined to <br><br> 10 1 mm diameter were tested simultaneously for 60 <br><br> hours in the same six-cylinder engine described previously on unleaded fuel at full load at the engine speed where peak torque is delivered. Erosion results were as follows: <br><br> 15 TABLE 5 <br><br> 20 <br><br> EROSION MEASURED AT: <br><br> EROSION RATE (Um/h)* <br><br> Ni <br><br> RU—Al <br><br> The Electrode Centre <br><br> 0,63 <br><br> 0, 12 <br><br> Over.the Electrode Face <br><br> 1,00 <br><br> 0,40 <br><br> The side of the <br><br> 0,28 <br><br> 0, 23 <br><br> Electrode facing the <br><br> oositive electrode <br><br> Average <br><br> 0,64 <br><br> 0,25 <br><br> This also proved that results previously obtained with ruthenium aluminide inserts were reproducible. <br><br> (vii) Alloys containing nickel, ruthenium and aluminium <br><br> In addition to additions of ruthenium to the RuAl-base materials, it is envisaged that nickel can be added to the RuAl phase in such a way that part of the ruthenium is substituted with the cheaper nickel, without deleteriously affecting the desirable properties of the RuAl-base phase. This type of substitution is considered possible because both Ru and Ni form B2 (body centred cubic) aluminide compounds with aluminium, and the atomic radii and electronegativities of Ru and Ni are sufficiently close to allow the substitution of one for the other in the crystal lattice of RuAl. (The metallic atomic radius of Ru is 0,13 3 nm while that of Ni is 0,124 nm, and the electronegativities are 2,2 and 1,8 respectively). <br><br> 2702 <br><br> - 34 - <br><br> This was tested by preparing a series of alloys, the compositions of which are given in Table 6, by arc melting. The alloys were perceived to have a structure Ni Ru Al. <br><br> X 1-x <br><br> TABLE 6 <br><br> Composition of test samples, atomic % <br><br> 10 <br><br> Sample <br><br> X <br><br> RU <br><br> Ni <br><br> Al <br><br> NH-0 <br><br> 0 <br><br> 50, 0 <br><br> 0,0 <br><br> 50, 0 <br><br> NH-1 <br><br> 0,25 <br><br> 37,5 <br><br> 12 , 5 <br><br> 50, 0 <br><br> NH-5 <br><br> 0,51 <br><br> 25, 0 <br><br> 25,0 <br><br> 50,0 <br><br> NH-2 <br><br> 0,75 <br><br> 12, 5 <br><br> 37,5 <br><br> 50,0 <br><br> NH-4 <br><br> 1, 00 <br><br> 0 <br><br> 50,0 <br><br> 50,0 <br><br> The alloys were then examined using metallography, X-ray diffraction and hardness testing. It was found that the addition of Ni to RuAl, or Ru to NiAl, raised the hardness of the material considerably. <br><br> The tests indicated that in the Ni-Al-Ru ternary system, compounds with the general formula Ni Ru Al have the same B2 structure and Ni can <br><br> 270 <br><br> - 35 - <br><br> substitute at least partially for Ru. Ni can also substitute for Ru in other parts of the Ru-Al phase system e.g. in the Ru-rich sections where high durability of electrode inserts has been proven 5 experimentally. Ni-Al-Ru alloys with a combined <br><br> Ru+Ni content of 42 or more atomic per cent, are suitable to be used in spark plug electrodes. <br><br> The fact that Ni atoms can substitute for Ru atoms explains the diffusion bonding that was observed to 10 have taken place during engine operation. <br><br> Diffusion bonding as well as other welding techniques such as (but not limited to) electrical resistance welding can be harnessed as a production technique, in particular to bond tips, of or 15 containing, intermetallic compounds to a nickel or nickel alloy electrode. <br><br> OTHER METALLIC COMPOUNDS. DESIGNS AND PROCESS ROUTES <br><br> It will be understood that numerous different 20 binary and ternary intermetallic compounds with melting points above 1400°C and materials <br><br> 270 <br><br> - 36 - <br><br> containing such compounds may be used to form spark plug electrodes or tips or inserts for electrodes without departing from the scope hereof. A few examples of many other binary intermetallic 5 compounds that may be sued for form electrodes are materials comprising essentially of nickel and aluminium, <br><br> - platinum and aluminium (compositions as described in our U.S.A. patent <br><br> 10 17/0/127), <br><br> titanium and aluminium, <br><br> - ruthenium and tantalum, <br><br> iron and aluminium, <br><br> - niobium (columbium) and aluminium, 15 - molybdenum and silicon, <br><br> iridium and niobium (columbium), and ruthenium and titanium, <br><br> hafnium and iridium, <br><br> ruthenium and zirconium, 20 ~ iridium and titanium, <br><br> iridium and tantalum. <br><br> 2702 <br><br> - 37 - <br><br> It will be further understood that compositions may deviate from stoichiometric intermetallic compositions and may therefore include multi-phase structures without departing from the scope hereof. <br><br> 5 Intermetallic compounds with melting points above <br><br> 1400°C in a matrix of other metals may according to this invention be produced in any ratio by means of any suitable process. For example, powdered or sub-divided intermetallic material may be embodied 10 in a ductile metallic phase thus yielding a composite material embodying good arc erosion resistance and good workability. A dispersion of intermetallic phases with melting points above 1400°C may also be used to restrict grain growth of 15 a ductile metallic phase of a multi-phase or composite material at elevated temperatures. The ductile metallic phase could include metals such as Ni, Pt, Au, Pd, Ag, or any other suitable metal or any combination of such metals. <br><br> 20 It will also be understood that, numerous different geometric configurations of positive and negative spark plug electrodes containing intermetallic <br><br> - 38 - <br><br> 270 <br><br> compounds may be designed without, departing from the scope hereof. For example, the intermetallic material may be sintered into the ceramic insulator body to form a centre electrode. <br><br> 5 Apart from arc melting and reactive hot isostatic pressing, the intermetallic material may be manufactured by a number of different processes without departing from the scope hereof. These include a variety of powder metallurgical <br><br> 10 processes, a variety of metal-spraying processes and a number of melting techniques. <br><br> Spark plugs and igniters typically also contain ceramic components such as alumina insulators. Ceramic materials are also increasingly considered for the manufacture automotive components. The intermetallic compounds according to this invention lend themselves to sintering processes compatible with ceramic materials. It is possible to sinter ceramic components and intermetallic compounds according to this invention in one production step. Should a specific shrinkage during sintering be required, this could be achieved by mixing specific <br><br> - 39 - <br><br> 27 <br><br> amounts of pre-reacted intermetallic powders with elemental metal powders. <br><br></p> </div>

Claims (9)

<div class="application article clearfix printTableText" id="claims"> <p lang="en"> .40- 27 0 2 1 9<br><br> CLAMS<br><br>
1. A spark plug or Igniter electrode characterised in that the electrode, or a tip or insert mounted onto or into the electrode, is made at least predominantly or one or more intermetallic compounds having a melting point above 1400°C at least one of which is an intermetallic compound of ruthenium and aluminium and wherein the intermetallic compound or compounds is or are chosen to exhibit adequate toughness, resistance to thermal shock, and electrical conductivity.<br><br>
2. An electrode as claimed in claim 1 in which the intermetallic compound is present as one phase in a dual or multi-phase material.<br><br>
3. An electrode as claimed in claim 2 in which the other phase is a nickel or nickel alloy material of substantially conventional composition.<br><br>
4. An electrode as claimed in claim 2 in which the intermetallic compound is ruthenium aluminide in an excess of ruthenium.<br><br>
5. An electrode as claimed in claim 4 in which the ruthenium content of the dual phase material is from 80 to 99 mass per cent.<br><br>
6. An electrode as claimed in any one of the preceding claims in which the electrode has a tip bonded thereto and wherein the tip is made of, or contains, the intermetallic compound or compounds.<br><br>
7. An electrode as claimed in claim 6 in which the tip is bonded to a nickel or nickel alloy electrode part. N &gt;<br><br> - 41 -<br><br> 27 0 2 19<br><br>
8. A spark plug or other igniter embodying an electrode as claimed in any one of claims 1 to 7.<br><br>
9. A spark plug as claimed in claim 8 in which more than one electrode thereof are as claimed in any one of claims 1 to 7.<br><br> RUSSELL MgVEAQH WEST WALKER<br><br> p« v I<br><br> ATTORNEYS FOR THE APPLICANT<br><br> </p> </div>
NZ270219A 1993-12-23 1994-12-20 Spark plug electrode of intermetallic compound NZ270219A (en)

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DE19939319B4 (en) * 1999-07-29 2004-05-06 Robert Bosch Gmbh Spark plug for an internal combustion engine
DE102004018933B4 (en) * 2004-04-20 2014-10-09 Robert Bosch Gmbh Method for producing a center electrode of a spark plug
DE102006015167B3 (en) * 2006-03-30 2007-07-19 W.C. Heraeus Gmbh Production of a wire or strip used e.g. as an electrode in spark plugs comprises producing an intermetallic compound, grinding, mixing with metal powder, feeding the mixture into a tube and deforming the filled tube
JP4927955B2 (en) * 2007-01-31 2012-05-09 ユラ・テック・カンパニー・リミテッド Spark plug
US7969078B2 (en) * 2008-05-19 2011-06-28 Federal Mogul Ignition Company Spark ignition device for an internal combustion engine and sparking tip therefor
US8274204B2 (en) * 2009-11-24 2012-09-25 Federal-Mogul Ignition Company Spark plug with platinum-based electrode material
US8334642B2 (en) * 2010-05-11 2012-12-18 Caterpillar Inc. Spark plug
WO2012016072A2 (en) * 2010-07-29 2012-02-02 Federal-Mogul Ignition Company Electrode material for use with a spark plug
JP5641453B2 (en) * 2010-09-09 2014-12-17 独立行政法人物質・材料研究機構 High temperature alloy material with excellent oxidation resistance and method for producing the same
JP6035177B2 (en) 2012-08-20 2016-11-30 株式会社デンソー Spark plug for internal combustion engine
JP6038698B2 (en) * 2013-03-22 2016-12-07 日本碍子株式会社 Ceramic member and member for semiconductor manufacturing equipment
US10815896B2 (en) 2017-12-05 2020-10-27 General Electric Company Igniter with protective alumina coating for turbine engines

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JPS5581477A (en) * 1978-12-15 1980-06-19 Nippon Soken Ignition plug
JPS61135082A (en) * 1984-12-06 1986-06-23 日本特殊陶業株式会社 Spark plug
JPH0828312B2 (en) * 1987-11-09 1996-03-21 ニチコン株式会社 Aluminum alloy electrode for electrolytic capacitors
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JP2858910B2 (en) * 1990-09-14 1999-02-17 昭和アルミニウム株式会社 Aluminum foil for electrolytic capacitor electrodes
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