Injection nozzle

Abstract: An injection nozzle for use in delivering fuel to a combustion space, the injection nozzle comprising a nozzle body (10), at least a part of which is provided with a first coating (14; 14 a ) arranged so as to reduce the temperature of at least a part of the nozzle body (10), in use. The coating (14; 14 a ) may have either a higher or lower thermal conductivity than the thermal conductivity of the nozzle body (10).

Description: This invention relates to an injection nozzle suitable for use in a fuel injector for use in the delivery of fuel under high pressure to a combustion space of a compression ignition internal combustion engine. An injection nozzle is exposed, in use, to the temperature within the engine cylinder or other combustion space. As a result, the parts of the injection nozzle which are exposed to such temperatures, for example the seating surface, must be able to withstand such temperatures without significant degradation which would otherwise result in an undesirable reduction in the service life of the injection nozzle. Further, the deposition of fuel lacquer within the injection nozzle, which can undesirably effect, for example, the fuel flow rate through the injector, is accelerated where the nozzle is exposed to high operating temperatures. In a known arrangement, in order to protect an injection nozzle from degradation resulting from the temperature within the cylinder or combustion space, a heat shield in the form of a tubular member is provided, the heat shield surrounding a part of the injection nozzle, shielding that part of the nozzle from combustion flames, in use, and conducting heat away from the injection nozzle. Although such an arrangement may result in the service life of the injection nozzle being increased, the provision of the additional heat shield results in the arrangement being relatively complex. Further, in some arrangements, insufficient space may be available to permit the use of such a heat shield. It is an object of the invention to provide an injection nozzle in which the disadvantageous effects described hereinbefore are reduced. Patent application no. DE 3623221 A provides a fuel injection nozzle in which a nozzle neck of a nozzle body guiding a nozzle needle has a cylindrical casing composed of a thermally conductive metal, which is drawn to the nozzle tip and completely covers this, the covering material being electrically or electrochemically applied in thin layers. Patent application no. WO 99/31382A concerns an injector comprising a nozzle pierced with at least one fuel outlet orifice towards an engine combustion chamber. A ceramic coating is deposited on the nozzle outer orifice, preferably in a break definine a recess in said outer surface, at least around and immediately downstream of the outlet orifice, relative to the fuel passage direction. Patent application no. JP 62020672 is directed to a fuel valve with improved durability by applying a surface treatment to impart corrosion resistance. According to the present invention there is provided an injection nozzle for use in delivering fuel to a combustion space, the injection nozzle comprising a nozzle body, the nozzle body comprising a tip region which projects from an engine cylinder head within which the injection nozzle is received, in use, into the combustion space, the tip region being provided with one or more outlet opening and wherein at least a part of the nozzle body is provided with a first coating formed from a material having a higher thermal conductivity than the thermal conductivity of the nozzle body, which first coating is provided over at least the part of the exterior of the nozzle body which is exposed to the temperature within the combustion space, in use, characterised in that the nozzle body is also coated, at least in part, with a second coating formed from a material having a lower thermal conductivity than the thermal conductivity of the nozzle body, and that said first and second coatings are arranged so as to reduce the temperature of at least a part of the nozzle body, in use. The provision of such coatings, thus, reduces the risk of degradation and of deposition of fuel lacquer, and increases the service life of the injection nozzle. Typically the first coating has a thickness of up to 1 mm. Conveniently, the thermally insulating coating (i.e. the second coating) may be a ceramic material. The provision of a coating having a higher thermal conductivity than the thermal conductivity of the nozzle boy increases the rate of heat transfer from the nozzle body to the cylinder head within which the nozzle body is received. Thus, heat is transferred away from the one or more outlet openings provided in the nozzle body at a higher rate compared with arrangements in which the nozzle body is uncoated or in which the nozzle body is coated entirely with a material having a lower thermal conductivity than the nozzle body. Conveniently, the nozzle body may be formed from steel. The first coating is preferably formed from any one of aluminium nitride, aluminium, copper, silver or gold. At least a part of the tip region of the nozzle body may be uncoated. This has the effect of further improving the heat transfer away from the or each outlet opening. As stated above, at least a part of the tip region is coated with a second coating formed from a material having a lower thermal conductivity than the thermal conductivity of the nozzle body. This has the effect of reducing heat transfer to the tip region, whilst the coating of higher thermal conductivity increases heat transfer away from the tip region. Thus, the or each outlet opening reaches a lower operating temperature for given operating conditions. Typically, the second coating has a thickness of up to lmm. Preferably, the first or second coatings may be bonded to the nozzle body by means of an additional substrate material. The invention will further be described, by way of example, with reference to the accompanying drawings in which; Figure 1 is a diagrammatic sectional view of an injection nozzle; and Figures 2 and 3 are diagrammatic sectional views of alternative injection nozzles. The injection nozzle illustrated in the accompanying drawings comprises a nozzle body 10 having a blind bore 11 formed therein, the blind bore 11 being supplied with fuel under pressure from a suitable source, for example the common rail of a common rail fuel system. The blind bore 11 is shaped to define, adjacent the blind end thereof, a seating surface 12. In use, a valve needle 17 is slidable within the bore 11. The valve needle 17 is shaped for engagement with the seating surface 12 to control communication between a delivery chamber defined between the bore 11 and the valve needle 17 upstream of the line of engagement between the valve needle 17 and the seating surface 12, and at least one outlet opening 13 which communicates with the bore I 1 downstream of the seating surface 12. It will be appreciated that when the valve needle 17 engages the seating surface 12, then fuel is unable to flow from the delivery chamber to the outlet opening(s) 13, thus fuel injection does not take place. Upon movement of the valve needle 17 away from the seating surface 12, fuel is able to flow from the delivery chamber past the seating surface to the outlet opening(s) 13 and injection of fuel takes place. The position occupied by the valve needle 17 is controlled by any suitable technique, for example by controlling the fuel pressure within a control chamber defined, in part, by a surface associated with the valve needle, to control the magnitude of a force applied to the valve needle urging the valve needle towards its seating. Although the description hereinbefore is of a fuel injector intended for use in a common rail type fuel system, it will be appreciated that the invention is not restricted to injectors of this type, and that the invention is applicable to all types of fuel injector, no matter how they are controlled. As illustrated in Figure 1, the exterior of the nozzle body 10 is provided with a coating 14 of a ceramic material, the coating 14 being heat resistant and being relatively thermally insulating. Although in Figure 1, the ceramic coating 14 is applied over a large part of the exterior of the nozzle body 10, this need not be the case, and the coating 14 could, if desired, be applied only to the part of the nozzle body 10 to the right of the broken line 15, this being the part of the nozzle body 10 which, in use, projects into the cylinder or other combustion space of an engine, and being the part containing the seating surface 12, and so being the part of the nozzle body where there is the greatest risk of degradation, and also the region where the deposition of fuel lacquer is most problematic. It is thought that in order to achieve the desired level of thermal protection for the injection nozzle, it may be desirable to provide a coating of thickness up to 1 mm, although it will be appreciated that the invention is not limited to this particular thickness of material, and that the thickness of the coating will, in practise, be dependent, to some extent, upon the thermal properties of the coating material and the ability of the material of the nozzle body to withstand degradation resulting from exposure to high temperatures. It will be appreciated that alternative materials having similar heat-shielding properties to a ceramic material may be used for the coating 14. As it is thought that the formation of a ceramic coating of thickness up to 1 mm including openings which align with the outlet openings 13 may be difficult to achieve, it is envisaged to provide the coating on the nozzle body 10 before the outlet opening(s) 13 are drilled, and that the outlet opening(s) 13 may be drilled through the ceramic material coating and the nozzle body 10 in the same operation. Alternatively, the nozzle body 10 may be shielded in the regions of the outlet opening(s) during the coating process to prevent outlet openings being coated. The coating may additionally or alternatively, if desired, be provided in suitable places on the nozzle body 10, prior to heat treatment of the nozzle body 10, thereby sheilding the nozzle body 10 and thus avoiding the formation of a carbon rich layer in places where it is not desired. Figure 2 shows a fuel injector in which similar parts to those shown in Figure 1 are denoted with like reference numerals. In Figure 2, the nozzle body 10 is arranged within an engine cylinder head 20 in a conventional manner, the nozzle body 10 being received within a cap nut 22 which is received within a further bore provided in the cylinder head 20. The nozzle body 10 is provided with an annular sealing member 24 which is arranged to provide a seal between the associated engine cylinder into which fuel is delivered and the upper parts of the injection nozzle and the cylinder head 20. A part of the length of the nozzle body 10 is received within the further bore provided by the cylinder head 20, the nozzle body being provided with a tip region 26 which projects through the open end of the further bore into the associated engine cylinder or other combustion space. The tip region 26 of the nozzle body 10 is that part of the nozzle body 10 which contains the seating surface 12 and the outlet openings 13, and is therefore that part of the nozzle body 10 where there is the greatest risk of degradation and the region where the deposition of fuel lacquer is most problematic. In Figure 2, the exterior of the nozzle body 10 is provided with the coating 14a formed from a material which has a higher thermal conductivity than the material from which the nozzle body 10 is formed, rather than being formed from a material having a lower thermal conductivity. Usually, the nozzle body 10 is formed from a steel alloy having a thermal conductivity in the region of 50 W/mK. Thus, suitable materials from which the coating 14 a may be formed include aluminium nitride (having a thermal conductivity of 200 W/mK), aluminium (having a thermal conductivity of 204 W/mK), copper (having a thermal conductivity of 384 W/mK), silver (having a thermal conductivity of 407 W/mK) or gold (having a thermal conductivity of 310 W/mK). It will be appreciated, however, that alternative materials having similar thermal properties to the aforementioned materials may also be used for the coating 14 a . As the coating 14a applied to the nozzle body 10 has a higher thermal conductivity than the nozzle body itself, the rate of heat transfer to the nozzle body 10 will be slightly higher than for the case where no coating is applied or where a coating 14 of lower thermal conductivity than that of the nozzle body 10 is applied, as described previously. In Figure 2, heat is transferred from the tip region 26, including the region in which the outlet openings 13 are formed, to the cylinder head 20 and the sealing member 24 at a higher rate. The net effect of providing the coating 14 a of relatively higher thermal conductivity is therefore to increase the rate of heat transfer away from the region of the nozzle body 10 where the deposition of fuel lacquer is most problematic. Thus, the operating temperature of that part of the tip region 26 containing the outlet openings 13 is reduced. As shown in Figure 2, the coating 14 a is applied to the part of the nozzle body 10 which projects from the cap nut 22, and an enlarged diameter region of the nozzle body 10 which is received within the cap nut 22. By applying the coating to the enlarged diameter region of the nozzle body, heat is conducted more effectively to the cap nut 22. In Figure 3 corresponding reference numerals are used to denote similar parts to those shown in Figures 1 and 2. In this Figure, the coating 14 a , having a higher thermal conductivity than the thermal conductivity of the nozzle body 10, is only applied along a part of the exterior of the nozzle body 10, including the part of the exterior of the nozzle body 10 received within the cylinder head 20, such that at least a part of the tip region 26 remains uncoated. This further increases that rate of transfer of heat away from the region of the nozzle body 10 provided with the outlet openings 13 to the sealing member 24 and the cylinder head 20, thereby further reducing the operating temperature of this region of the nozzle body 10. It will be appreciated that more or less of the exterior of the nozzle body 10 may be coated, such that more or less of the tip region 26 to that shown in Figure 3 remains uncoated. In accordance with the present invention, the part of the tip region 26 which is uncoated in Figure 3 is coated with a material having a lower thermal conductivity than the thermal conductivity of the nozzle body 10. For example, at least a part of the tip region 26 may be coated with a ceramic material. This provides the further advantage that the rate of heat transfer to the ceramic coated part of the tip region 26 is reduced, whilst the coating 14a of higher thermal conductivity increases the rate of heat transfer away from the tip region 26. Thus, the operating temperature of the part of the tip region 26 provided with the outlet openings 13 is further reduced. In order to achieve the desired level of heat transfer away from the nozzle body 10, it may be desirable to provide a coating 14 a having a thickness of up to 1 mm. The nozzle body 10 may be provided with a multi-layer coating, whereby a first coating having a lower thermal conductivity than the thermal conductivity of the nozzle body 10 is applied to the nozzle body 10 (as shown in Figure 1) and a further coating having a higher thermal conductivity than the thermal conductivity of the nozzle body 10 is applied to the first coating. Typically, the further coating may be formed from a material having properties similar to that of the coating 14 a , as described previously with reference to Figures 2 and 3. As described previously, the first coating serves to insulate the nozzle body 10, whilst the further coating will aid the conduction of heat away from the nozzle body 10. Alternatively, the order in which the coatings are layered may be reversed such that a first coating having a relatively high thermal conductivity is applied to the nozzle body 10 and an additional coating having a relatively low thermal conductivity is applied to the first coating. Typically, the additional coating may be formed from a material having properties similar to the coating 14, as described previously with reference to Figure 1. This is particularly advantageous if the additional coating (i.e. the outermost layer) having a relatively low thermal conductivity is only applied to a lower region of the nozzle body 10, preferably only that region which projects from the cylinder head 20 and is exposed to temperatures within the combustion space. In any of the embodiments of the invention, and for either a ceramic or other material, an additional substrate material may be applied to the nozzle body 10 to which a coating 14, 14 a is to be applied to ensure satisfactory bonding of the coating(s) to the nozzle body. Additionally, in any of the embodiments of the invention, the nozzle body 10 preferably forms an interference fit within the cylinder head 20, as this improves the effectiveness of the coating 14, 14 a . The effect of the coating(s) is also improved if the nozzle body 10 forms an interference fit within the cap nut 22. As mentioned hereinbefore, the invention is not restricted to the particular type of injector described hereinbefore, or to injectors suitable for use with common rail type fuel systems. By way of example, the invention is also applicable to fuel pressure actuable injectors suitable for use with rotary distributor pumps, to injectors of the outwardly opening type and to injectors having more than one set of outlet openings and having a valve needle operable between first and second stages of lift.

Claims: An injection nozzle for use in delivering fuel to a combustion space, the injection nozzle comprising a nozzle body (10), the nozzle body (10) comprising a tip region which projects from an engine cylinder head within which the injection nozzle is received, in use, into the combustion space, the tip region being provided with one or more outlet opening (13) and wherein at least a part of the nozzle body (10) is provided with a first coating (14; 14 a ) formed from a material having a higher thermal conductivity than the thermal conductivity of the nozzle body (10), which first coating (14; 14 a ) is provided over at least the part of the exterior of the nozzle body (10) which is exposed to the temperature within the combustion space, in use, characterised in that the nozzle body (10) is also coated, at least in part, with a second coating formed from a material having a lower thermal conductivity than the thermal conductivity of the nozzle body (10), and that said first and second coatings are arranged so as to reduce the temperature of at least a part of the nozzle body (10), in use. The injection nozzle as claimed in Claim 1, wherein the second coating is formed from a ceramic material. The injection nozzle as claimed in Claims 1 or 2, comprising an additional substrate material applied to the nozzle body (10), whereby the first coating is bonded to the nozzle body (10) by means of the additional substrate material.

Inventors: GREEN ALAN CONWAY, LAMBERT MALCOLM DAVID DICK, NANDY MODHU, GREEN, ALAN CONWAY, LAMBERT, MALCOLM DAVID DICK, NANDY, MODHU
Applicants: DELPHI TECH INC, DELPHI TECHNOLOGIES, INC.
Application year: 2000
Main classification: F02M61
IPC codes: F02M61