Patent Grant
11535942
The present invention relates to a coating method using a cold spray method.
A method of manufacturing a sliding member is known, which includes spraying a raw material powder such as metal powder onto the seating portion of an engine valve using a cold spray method thereby to be able to form a valve seat having excellent high-temperature wear resistance (Patent Document 1).
Engines such as those of automobiles include a plurality of intake and exhaust engine valves because of the multi-valve system. Accordingly, when valve seats are formed on the seating portions of a plurality of engine valves using a cold spray method, it is necessary to relatively move the cylinder head and the nozzle of a cold spray apparatus, cause each of the plurality of seating portions and the nozzle to sequentially face each other, and inject a raw material powder from the nozzle to spray the powder onto the seating portion facing the nozzle.
However, when suspending the injection of the raw material powder, the cold spray apparatus requires a waiting time of several minutes until the raw material powder can be stably sprayed again. Thus, in the case of forming coats on a plurality of coating portions such as seating portions using the cold spray method, if the spraying of the raw material powder and its stopping are repeated for each coating portion, the cycle time will increase due to the waiting time of the cold spray apparatus.
A problem to be solved by the present invention is to provide a coating method in which the cycle time when forming coats on a plurality of coating portions using the cold spray method can be shorter than that when forming coats on the plurality of coating portions by repeating the spraying of the raw material powder and its stopping.
The present invention solves the above problem through, when relatively moving the nozzle of a cold spray apparatus, continuing the injection of a raw material powder from the nozzle and setting an angle of the nozzle with respect to the coating target component larger or smaller than that when the nozzle forms coats on the coating portions in a nozzle movement path from a coating portion having been formed with the coat to another coating portion to be subsequently formed with the coat.
According to the present invention, the coats are sequentially formed on the plurality of coating portions without stopping the injection of the raw material powder, and the cycle time can therefore be shorter than that when forming coats on the plurality of coating portions by repeating the spraying of the raw material powder and its stopping.
Hereinafter, one or more embodiments of the present invention will be described with reference to the drawings. First, an engine 1 will be described, which includes valve seat coats formed using the coating method according to one or more embodiments of the present invention.
The engine 1 includes a cylinder block 11 and a cylinder head 12 that is mounted on the upper portion of the cylinder block 11. The engine 1 is, for example, a four-cylinder gasoline engine, and the cylinder block 11 has four cylinders 11a arranged in the depth direction of the drawing sheet. The cylinders 11a house respective pistons 13 that reciprocate in the vertical direction in the figure. Each piston 13 is connected to a crankshaft 14, which extends in the depth direction of the drawing sheet, via a connecting rod 13a.
The cylinder head 12 has a cylinder block mounting surface 12a that is a surface for being mounted on the cylinder block 11. The cylinder block mounting surface 12a is provided with four combustion chamber upper wall portions 12b at positions corresponding to respective cylinders 11a. The combustion chamber upper wall portions 12b define combustion chambers 15 of the cylinders. Each combustion chamber 15 is a space for combusting a mixture gas of fuel and intake air and is defined by a combustion chamber upper wall portion 12b of the cylinder head 12, a top surface 13b of the piston 13, and an inner surface of the cylinder 11a.
The cylinder head 12 includes ports for air intake (referred to as intake ports, hereinafter) 16 that connect between the combustion chambers 15 and one side surface 12c of the cylinder head 12. The intake ports 16 have a curved, approximately cylindrical shape and supply intake air from an intake manifold (not illustrated) connected to the side surface 12c into respective combustion chambers 15. The air supplied into each combustion chamber 15 is mixed with gasoline supplied from an injector, which is not illustrated, to generate a mixture gas.
The cylinder head 12 further includes ports for air exhaust (referred to as exhaust ports, hereinafter) 17 that connect between the combustion chambers 15 and the other side surface 12d of the cylinder head 12. The exhaust ports 17 have a curved, approximately cylindrical shape like the intake ports 16 and exhaust the exhaust gas generated by the combustion of the mixture gas in respective combustion chambers 15 to an exhaust manifold (not illustrated) connected to the side surface 12d. The engine 1 according to one or more embodiments of the present invention is a multi-valve-type engine, and one cylinder 11a is provided with two intake ports 16 and two exhaust ports 17.
The cylinder head 12 is provided with intake valves 18 that open and close the intake ports 16 with respect to the combustion chambers 15 and exhaust valves 19 that open and close the exhaust ports 17 with respect to the combustion chambers 15. Each intake valve 18 includes a round rod-shaped valve stem 18a and a disk-shaped valve head 18b that is provided at the tip of the valve stem 18a. Likewise, each exhaust valve 19 includes a round rod-shaped valve stem 19a and a disk-shaped valve head 19b that is provided at the tip of the valve stem 19a. The valve stems 18a and 19a are slidably inserted into approximately cylindrical valve guides 18c and 19c, respectively. This allows the intake valves 18 and the exhaust valves 19 to be movable with respect to the combustion chambers 15 along the axial directions of the valve stems 18a and 19a.
Like the intake port 16, the exhaust port 17 includes an approximately circular opening portion 17a at the portion communicating with the combustion chamber 15, and the opening portion 17a has an annular edge portion provided with an annular valve seat coat 17b that abuts against the valve head 19b of an exhaust valve 19. When the exhaust valve 19 moves upward along the axial direction of the valve stem 19a, the upper surface of the valve head 19b comes into contact with the valve seat coat 17b to close the exhaust port 17. When the exhaust valve 19 moves downward along the axial direction of the valve stem 19a, a gap is formed between the upper surface of the valve head 19b and the valve seat coat 17b to open the exhaust port 17.
In the four-cycle engine 1, for example, only the intake valve 18 opens when the corresponding piston 13 moves down, and the mixture gas is introduced from the intake port 16 into the cylinder 11a. In an in-cylinder injection-type engine, or a so-called direct injection-type engine, gasoline is injected into the cylinder 11a from the injector, and air is introduced into the cylinder 11a from the intake port 16 to generate a mixture gas. Subsequently, in a state in which the intake valve 18 and the exhaust valve 19 are closed, the piston 13 moves up to compress the mixture gas in the cylinder 11a, and when the piston 13 approximately reaches the top dead center, the mixture gas is ignited to explode by a spark plug, which is not illustrated. This explosion makes the piston 13 move down to the bottom dead center and is converted into the rotational force via the connected crankshaft 14. When the piston 13 reaches the bottom dead center and starts moving up again, only the exhaust valve 19 is opened to exhaust the exhaust gas in the cylinder 11a to the exhaust port 17. The engine 1 repeats the above cycle to generate the output.
The opening portions 16a and 17a of the cylinder head 12 have respective annular edge portions, and the valve seat coats 16b and 17b are formed directly on the annular edge portions using a cold spray method. The cold spray method refers to a method that includes making a supersonic flow of an operation gas having a temperature lower than the melting point or softening point of a raw material powder, injecting the raw material powder carried by a carrier gas into the operation gas to spray the raw material powder from a nozzle tip, and causing the raw material powder in the solid phase state to collide with a base material to form a coat by plastic deformation of the raw material powder. Compared with a thermal spray method in which the material is melted and deposited on a base material, the cold spray method has features that a dense coat can be obtained without oxidation in the air, thermal alteration is suppressed because of less thermal effect on the material particles, the coating speed is high, the coat can be made thick, and the deposition efficiency is high. In particular, the cold spray method is suitable for the use for structural materials such as the valve seat coats 16b and 17b of the engine 1 because the coating speed is high and the coats can be made thick.
The gas supply unit 21 includes a compressed gas cylinder 21a, an operation gas line 21b, and a carrier gas line 21c. Each of the operation gas line 21b and the carrier gas line 21c includes a pressure regulator 21d, a flow rate control valve 21e, a flow meter 21f, and a pressure gauge 21g. The pressure regulators 21d, the flow rate control valves 21e, the flow meters 21f, and the pressure gauges 21g are used for adjusting the pressure and flow rate of the operation gas and carrier gas from the compressed gas cylinder 21a.
The operation gas line 21b is installed with a heater 21i heated by a power source 21h. The operation gas is heated by the heater 21i to a temperature lower than the melting point or softening point of the raw material and then introduced into a chamber 23a in the cold spray gun 23. The chamber 23a is installed with a pressure gauge 23b and a thermometer 23c, which are used for feedback control of the pressure and temperature.
On the other hand, the raw material powder supply unit 22 includes a raw material powder supply device 22a, which is provided with a weighing machine 22b and a raw material powder supply line 22c. The carrier gas from the compressed gas cylinder 21a is introduced into the raw material powder supply device 22a through the carrier gas line 21c. A predetermined amount of the raw material powder weighed by the weighing machine 22b is carried into the chamber 23a via the raw material powder supply line 22c.
The cold spray gun 23 sprays the raw material powder P, which is carried into the chamber 23a by the carrier gas, together with the operation gas as the supersonic flow from the tip of a nozzle 23d and causes the raw material powder P in the solid phase state or solid-liquid coexisting state to collide with a base material 24 to form a coat 24a. In one or more embodiments of the present invention, the cylinder head 12 is applied as the base material 24, and the raw material powder P is sprayed onto the annular edge portions of the opening portions 16a and 17a of the cylinder head 12 using the cold spray method to form the valve seat coats 16b and 17b.
The valve seats of the cylinder head 12 are required to have high heat resistance and wear resistance to withstand the impact input from the valves in the combustion chambers 15 and high heat conductivity for cooling the combustion chambers 15. In response to these requirements, according to the valve seat coats 16b and 17b formed of the powder of precipitation-hardened copper alloy, for example, the valve seats can be obtained which are excellent in the heat resistance and wear resistance and harder than the cylinder head 12 formed of an aluminum alloy for casting.
Moreover, the valve seat coats 16b and 17b are formed directly on the cylinder head 12, and higher heat conductivity can therefore be obtained as compared with conventional valve seats formed by press-fitting seat rings as separate components into the port opening portions. Furthermore, as compared with the case in which the seat rings as separate components are used, subsidiary effects can be obtained such as that the valve seats can be made close to a water jacket for cooling and the tumble flow can be promoted due to expansion of the throat diameter of the intake ports 16 and exhaust ports 17 and optimization of the port shape.
The raw material powder used for forming the valve seat coats 16b and 17b is preferably a powder of metal that is harder than an aluminum alloy for casting and with which the heat resistance, wear resistance, and heat conductivity required for the valve seats can be obtained. For example, it is preferred to use the above-described precipitation-hardened copper alloy. The precipitation-hardened copper alloy for use may be a Corson alloy that contains nickel and silicon, chromium copper that contains chromium, zirconium copper that contains zirconium, or the like. It is also possible to apply, for example, a precipitation-hardened copper alloy that contains nickel, silicon, and chromium, a precipitation-hardened copper alloy that contains nickel, silicon, and zirconium, a precipitation-hardened copper alloy that contains nickel, silicon, chromium, and zirconium, a precipitation-hardened copper alloy that contains chromium and zirconium, or the like.
The valve seat coats 16b and 17b may also be formed by mixing a plurality of types of raw material powders; for example, a first raw material powder and a second raw material powder. In this case, it is preferred to use, as the first raw material powder, a powder of metal that is harder than an aluminum alloy for casting and with which the heat resistance, wear resistance, and heat conductivity required for valve seats can be obtained. For example, it is preferred to use the above-described precipitation-hardened copper alloy. On the other hand, it is preferred to use, as the second raw material powder, a powder of metal that is harder than the first raw material powder. The second raw material powder for application may be an alloy such as an iron-based alloy, a cobalt-based alloy, a chromium-based alloy, a nickel-based alloy, or a molybdenum-based alloy, ceramics, or the like. One type of these metals may be used alone, or two or more types may also be used in combination.
With the valve seat coats formed of a mixture of the first raw material powder and the second raw material powder which is harder than the first raw material powder, more excellent heat resistance and wear resistance can be obtained than those of valve seat coats formed only of a precipitation-hardened copper alloy. The reason that such an effect is obtained appears to be because the second raw material powder allows the oxide film existing on the surface of the cylinder head 12 to be removed so that a new interface is exposed and formed to improve the interfacial adhesion between the cylinder head 12 and the metal coats. Additionally or alternatively, it appears that the anchor effect due to the second raw material powder sinking into the cylinder head 12 improves the interfacial adhesion between the cylinder head 12 and the raw material coats. Additionally or alternatively, it appears that when the first raw material powder collides with the second raw material powder, a part of the kinetic energy is converted into heat energy, or heat is generated in the process in which a part of the first raw material powder is plastically deformed, and such heat promotes the precipitation hardening in a part of the precipitation-hardened copper alloy used as the first raw material powder.
A method of manufacturing the cylinder head 12 according to one or more embodiments of the present invention will then be described.
In the casting step S1, an aluminum alloy for casting is poured into a mold in which sand cores are set, and casting is performed to mold a semimanufactured cylinder head 3 (see
The combustion chamber upper wall portions 12b1 to 12b4 have an approximately circular shape and are recessed with respect to the cylinder block mounting surface 12a. The combustion chamber upper wall portion 12b1 is provided with two opening portions 16a1 and 16a2 of the intake port 16, two opening portions 17a1 and 17a2 of the exhaust port 17, a plug hole 12f1, and an injector hole 12g1. Likewise, the combustion chamber upper wall portion 12b2 is provided with two opening portions 16a3 and 16a4 of the intake port 16, two opening portions 17a3 and 17a4 of the exhaust port 17, a plug hole 12f2, and an injector hole 12g2. The combustion chamber upper wall portion 12b3 is provided with two opening portions 16a5 and 16a6 of the intake port 16, two opening portions 17a5 and 17a6 of the exhaust port 17, a plug hole 12f3, and an injector hole 12g3. The combustion chamber upper wall portion 12b4 is provided with two opening portions 16a7 and 16a8 of the intake port 16, two opening portions 17a7 and 17a8 of the exhaust port 17, a plug hole 12f4, and an injector hole 12g4.
The plug holes 12f1 to 12f4 are holes for attaching spark plugs and are disposed approximately in the centers of the combustion chamber upper wall portions 12b1 to 12b4. The four plug holes 12f1 to 12f4 provided in the semimanufactured cylinder head 3 are therefore arranged along the longitudinal direction of the semimanufactured cylinder head 3.
The two opening portions 16a1 and 16a2 of the intake port 16 are arranged along the longitudinal direction of the semimanufactured cylinder head 3 at positions in contact with the edge portion of the combustion chamber upper wall portion 12b1. Likewise, the opening portions 16a3 to 16a8 are also arranged along the longitudinal direction of the semimanufactured cylinder head 3 at positions in contact with the edge portions of the combustion chamber upper wall portions 12b2 to 12b4. Thus, the eight intake opening portions 16a1 to 16a8 provided in the semimanufactured cylinder head 3 are arranged along the longitudinal direction of the semimanufactured cylinder head 3. The two intake ports 16 provided at each of the combustion chamber upper wall portions 12b1 to 12b4 are merged into one in the semimanufactured cylinder head 3, which communicates with a side surface of the semimanufactured cylinder head 3.
The two opening portions 17a1 and 17a2 of the exhaust port 17 are arranged along the longitudinal direction of the semimanufactured cylinder head 3 at positions in contact with the edge portion of the combustion chamber upper wall portion 12b1 opposite to the opening portions 16a1 and 16a2 with respect to the plug hole 12f1. Likewise, the opening portions 17a3 to 17a8 are also arranged along the longitudinal direction of the semimanufactured cylinder head 3 at positions in contact with the edge portions of the combustion chamber upper wall portions 12b2 to 12b4. Thus, the eight exhaust opening portions 17a1 to 17a8 provided in the semimanufactured cylinder head 3 are arranged along the longitudinal direction of the semimanufactured cylinder head 3. The two exhaust ports 17 provided at each of the combustion chamber upper wall portions 12b1 to 12b4 are merged into one in the semimanufactured cylinder head 3, which communicates with a side surface of the semimanufactured cylinder head 3.
The injector holes 12g1 to 12g4 are holes for attaching injector devices for fuel injection. The injector hole 12g1 is disposed between the two opening portions 16a1 and 16a2 and in contact with the edge portion of the combustion chamber upper wall portion 12b1. Like the injector hole 12g1, the injector holes 12g2 to 12g4 are also arranged at the combustion chamber upper wall portions 12b2 to 12b4. Thus, the four injector holes 12g1 to 12g4 provided in the semimanufactured cylinder head 3 are arranged along the longitudinal direction of the semimanufactured cylinder head 3.
The cutting step S2 will then be described.
The cylinder head 12 according to one or more embodiments of the present invention is processed through spraying the raw material powder P onto the annular valve seat portion 16c using the cold spray method to form a coat and forming the valve seat coat 16b (see
In the coating step S3, the raw material powder P is sprayed onto the opening portions 16a1 to 16a8 of the semimanufactured cylinder head 3 using the cold spray apparatus 2 according to one or more embodiments of the present invention to form the valve seat coats 16b. The semimanufactured cylinder head 3 corresponds to the coating target component of the present invention, and the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 correspond to the coating portions of the present invention. In the coating step S3, the semimanufactured cylinder head 3 and the nozzle 23d of the cold spray gun 23 are relatively moved at a constant speed so that the raw material powder P is sprayed onto the entire circumference of the annular valve seat portion 16c while keeping constant the posture of the annular valve seat portion 16c and nozzle 23d and the distance between the annular valve seat portion 16c and the nozzle 23d.
In one or more embodiments of the present invention, for example, the semimanufactured cylinder head 3 is moved with respect to the nozzle 23d of the cold spray gun 23, which is fixedly arranged, using a work rotating apparatus 4 illustrated in
The tilt stage unit 42 is a stage that supports the work table 41 and rotates the work table 41 around an A-axis arranged in the horizontal direction to tilt the semimanufactured cylinder head 3. The XY stage unit 43 includes a Y-axis stage 43a that supports the tilt stage unit 42 and an X-axis stage 43b that supports the Y-axis stage 43a. The Y-axis stage 43a moves the tilt stage unit 42 along the Y-axis arranged in the horizontal direction. The X-axis stage 43b moves the Y-axis stage 43a along the X-axis orthogonal to the Y-axis on the horizontal plane. This allows the XY stage unit 43 to move the semimanufactured cylinder head 3 to an arbitrary position along the X-axis and the Y-axis. The rotation stage unit 44 has a rotation table 44a that supports the XY stage unit 43 on the upper surface, and rotates the rotation table 44a thereby to rotate the semimanufactured cylinder head 3 around the Z-axis in an approximately vertical direction.
The controller 45 is a control device that controls the movements of the tilt stage unit 42, XY stage unit 43, and rotation stage unit 44. The controller 45 is installed with a teaching program that causes the semimanufactured cylinder head 3 to move with respect to the nozzle 23d of the cold spray apparatus 2.
The tip of the nozzle 23d of the cold spray gun 23 is fixedly arranged above the tilt stage unit 42 and in the vicinity of the Z-axis of the rotation stage unit 44. The controller 45 uses the tilt stage unit 42 to tilt the work table 41 so that, as illustrated in
The controller 45 temporarily stops the rotation of the rotation stage unit 44 when the semimanufactured cylinder head 3 makes one rotation around the Z-axis to complete the formation of the valve seat coat 16b for the opening portion 16a1. While the rotation is stopped, the XY stage unit 43 moves the semimanufactured cylinder head 3 so that the central axis C of the opening portion 16a2 to be subsequently formed with the valve seat coat 16b coincides with the Z-axis of the rotation stage unit 44. After the XY stage unit 43 completes the movement of the semimanufactured cylinder head 3, the controller 45 restarts the rotation of the rotation stage unit 44 to form the valve seat coat 16b on the annular valve seat portion 16c of the next opening portion 16a2. This operation is then repeated thereby to form the valve seat coats 16b and 17b for all the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 of the semimanufactured cylinder head 3. When the valve seat coating target is switched between an intake port 16 and an exhaust port 17, the tilt stage unit 42 changes the tilt of the semimanufactured cylinder head 3 so that the central axis of the exhaust port 17 becomes vertical.
In the finishing step S4, finishing work is performed on the valve seat coats 16b and 17b, the intake ports 16, and the exhaust ports 17. In the finishing work performed on the valve seat coats 16b and 17b, the surfaces of the valve seat coats 16b and 17b are cut by milling work using a ball end mill to adjust the valve seat coats 16b into a predetermined shape.
In the finishing work performed on an intake port 16, a ball end mill is inserted from the opening portion 16a1 into the intake port 16 to cut the inner surface of the intake port 16 on the opening port 16a1 side along a working line PL illustrated in
Thus, according to the finishing step S4, the surface roughness of the intake port 16 due to the cast molding is eliminated, and the excessive coat SF formed in the coating step S3 can be removed.
Like the intake ports 16, each exhaust port 17 is processed through the formation of the exhaust port 17 by the cast molding, the formation of an annular valve seat portion 17c (see
The coating step S3 described above has two problems: (1) the cycle time of the coating step is long; and (2) excessive coats are formed. The problem (1) is due to the characteristics of the cold spray apparatus 2. That is, once the spraying of the raw material powder P is stopped, the cold spray apparatus 2 requires a waiting time of several minutes until the raw material powder P can be stably sprayed again. Thus, in the case of forming the valve seat coats 16b and 17b at the plurality of opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8, if the spraying of the raw material powder P and its stopping are repeated for each opening portion, the cycle time of the coating step S3 will increase.
The problem (2) is a problem caused by applying the present invention to solve the problem (1). That is, in one or more embodiments of the present invention, to solve the problem (1) regarding the cycle time of the coating step S3, the nozzle 23d is moved between any two of the opening portions 16a1 to 16a8 and between any two of the opening portions 17a1 to 17a8 while continuing to inject the raw material powder P. Through this operation, the nozzle 23d does not stop injecting the raw material powder P; therefore, the waiting time is unnecessary and the cycle time of the coating step S3 is shortened, but the problem (2) occurs that the raw material powder P adheres to portions other than the opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 of the semimanufactured cylinder head 3 to form excessive coats. In particular, if the excessive coats are formed beyond the working lines PL for the intake ports 16 and exhaust ports 17, the excessive coats cannot be removed by post-processing, which may affect the engine performance.
The nozzle 23d sequentially forms the valve seat coats 16b for the opening portions 16a1 to 16a8 of the intake ports 16 while moving along the nozzle movement path for air intake Inp. When moving from an opening portion (e.g., the opening portion 16a1) having been formed with the valve seat coat 16b to another opening portion (e.g., the opening portion 16a2) to be subsequently formed with the valve seat coat 16b, the nozzle 23d moves above the opening portion (e.g., the opening portion 16a1) having been formed with the valve seat coat 16b. Likewise, the nozzle 23d sequentially forms the valve seat coats 17b for the opening portions 17a1 to 17a8 of the exhaust ports 17 while moving along the nozzle movement path for air exhaust Enp. When moving from an opening portion (e.g., the opening portion 17a1) having been formed with the valve seat coat 17b to another opening portion (e.g., the opening portion 17a2) to be subsequently formed with the valve seat coat 17b, the nozzle 23d moves above the opening portion (e.g., the opening portion 17a1) having been formed with the valve seat coat 17b.
The coating step S3 according to the present embodiment is an embodiment for carrying out the coating method according to the present invention. To solve the above-described problems (1) and (2), as illustrated in
The nozzle movement path for air intake Inp1 is linearly set along the arrangement direction of the opening portions 16a1 to 16a8 so as to be in contact with the opening portions 16a1 to 16a8 between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17. The nozzle 23d moves on the nozzle movement path for air intake Inp1 from the left side to the right side in the figure. This nozzle movement path for air intake Inp1 allows the nozzle 23d to move above the cylinder block mounting surface 12a and above the combustion chamber upper wall portions 12b1 to 12b4 rather than to move above the opening portions 16a1 to 16a8 of the intake ports 16 or above the opening portions 17a1 to 17a8 of the exhaust ports 17.
For the nozzle movement path for air intake Inp1 thus set, annular coating paths for air intake Idp1 are set on the annular valve seat portions 16c of the respective opening portions 16a1 to 16a8 so as to be in contact with the nozzle movement path for air intake Inp1. In addition, positions at which the nozzle movement path for air intake Inp1 is in contact with the coating paths for air intake Idp1 are set with coating start positions Is1 at which the nozzle 23d starts spraying the raw material powder P onto the annular valve seat portions 16c of the opening portions 16a1 to 16a8 and coating end positions Ie1 at which the nozzle 23d finishes spraying the raw material powder P onto the annular valve seat portions 16c.
The nozzle movement path for air exhaust Enp1 is linearly set along the arrangement direction of the opening portions 17a1 to 17a8 so as to be in contact with the opening portions 17a1 to 17a8 between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17. The nozzle 23d moves on the nozzle movement path for air exhaust Enp1 from the left side to the right side in the figure. This nozzle movement path for air exhaust Enp1 allows the nozzle 23d to move above the cylinder block mounting surface 12a and above the combustion chamber upper wall portions 12b1 to 12b4 rather than to move above the opening portions 16a1 to 16a8 of the intake ports 16 or above the opening portions 17a1 to 17a8 of the exhaust ports 17.
For the nozzle movement path for air exhaust Enp1 thus set, annular coating paths for air exhaust Edp1 are set on the annular valve seat portions 17c of the respective opening portions 17a1 to 17a8 so as to be in contact with the nozzle movement path for air exhaust Enp 1. In addition, positions at which the nozzle movement path for air exhaust Enp1 is in contact with the coating paths for air exhaust Edp1 are set with coating start positions Es1 at which the nozzle 23d starts spraying the raw material powder P onto the annular valve seat portions 17c of the opening portions 17a1 to 17a8 and coating end positions Ee1 at which the nozzle 23d finishes spraying the raw material powder P onto the annular valve seat portions 17c.
In
The nozzle 23d moves seemingly along the nozzle movement path for air intake Inp1 and the coating paths for air intake Idp1 as follows. In the present embodiment, the nozzle 23d is practically fixed and the semimanufactured cylinder head 3 is moved, but for the purpose of clarifying the movement of the nozzle 23d along the nozzle movement path for air intake Inp1 and the coating paths for air intake Idp1, the following description will be made on the assumption that the nozzle 23d moves.
The nozzle 23d linearly moves on the nozzle movement path for air intake Inp1 along the arrangement direction of the opening portions 16a1 to 16a8, that is, the longitudinal direction of the semimanufactured cylinder head 3, while spraying the raw material powder P. After moving from the outside of the semimanufactured cylinder head 3 to above the cylinder block mounting surface 12a, the nozzle 23d passes above the cylinder block mounting surface 12a and moves to above the first opening portion 16a1. When reaching the first coating start position Is1, the nozzle 23d switches the direction of travel so as to fold back in the opposite direction and moves in the counterclockwise direction so as to trace over the annular valve seat portion 16c along the coating path for air intake Idp1, thus forming the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a1.
After moving to the first coating end position Tel, the nozzle 23d switches the direction of travel so as to fold back in the opposite direction, moves again above the combustion chamber upper wall portion 12b1 along the nozzle movement path for air intake Inp1, and moves to the coating start position Is1 for the next opening portion 16a2. When reaching the coating start position Is1 for the opening portion 16a2, the nozzle 23d moves above the second opening portion 16a2 in the counterclockwise direction in the figure so as to trace over the opening portion 16a2 and forms the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a2.
After moving to the coating end position Ie1 of the opening portion 16a2, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 and above the cylinder block mounting surface 12a again along the nozzle movement path for air intake Inp1 and moves to the coating start position Is1 for the opening portion 16a3 of the next combustion chamber upper wall portion 12b2. After that, the valve seat coats 16b are formed on the opening portions 16a3 to 16a8 of the combustion chamber upper wall portions 12b2 to 12b4 in the same manner as for the opening portions 16a1 and 16a2. After finishing the formation of the valve seat coat 16b for the final opening portion 16a8, the nozzle 23d moves above the combustion chamber upper wall portion 12b4 and above the cylinder block mounting surface 12a along the nozzle movement path for air intake Inp1 and is moved to the outside of the semimanufactured cylinder head 3.
When the formation of the valve seat coats 16b for the opening portions 16a1 to 16a8 of the intake ports 16 is completed, the formation of the valve seat coats 17b for the opening portions 17a1 to 17a8 of the exhaust ports 17 is started. The nozzle 23d linearly moves on the nozzle movement path for air exhaust Enp 1 along the arrangement direction of the opening portions 17a1 to 17a8, that is, the longitudinal direction of the semimanufactured cylinder head 3, while spraying the raw material powder P. After moving from the outside of the semimanufactured cylinder head 3 to above the cylinder block mounting surface 12a, the nozzle 23d passes above the cylinder block mounting surface 12a and moves to above the first opening portion 17a1. When reaching the first coating start position Es1, the nozzle 23d switches the direction of travel so as to fold back in the opposite direction and moves in the clockwise direction so as to trace over the annular valve seat portion along the coating path for air exhaust Edp1, thus forming the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a1.
After moving to the coating end position Ee1 of the opening portion 17a1, the nozzle 23d moves again above the combustion chamber upper wall portion 12b1 along the nozzle movement path for air exhaust Enp1 and moves to the coating start position Es1 for the next opening portion 17a2. When reaching the coating start position Es1 for the next opening portion 17a2, the nozzle 23d moves above the second opening portion 17a2 in the clockwise direction in the figure so as to trace over the opening portion 17a2 and forms the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a2.
After moving to the coating end position Ee1 of the opening portion 17a2, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 and above the cylinder block mounting surface 12a again along the nozzle movement path for air exhaust Enp1 and moves to the coating start position Es1 for the opening portion 17a3 of the next combustion chamber upper wall portion 12b2. After that, the valve seat coats 17b are formed on the opening portions 17a3 to 17a8 of the combustion chamber upper wall portions 12b2 to 12b4 in the same manner as for the opening portions 17a1 and 17a2. After finishing the formation of the valve seat coat 17b for the final opening portion 17a8, the nozzle 23d moves above the combustion chamber upper wall portion 12b4 and above the cylinder block mounting surface 12a along the nozzle movement path for air exhaust Enp1 and is moved to the outside of the semimanufactured cylinder head 3.
Thus, the nozzle 23d is moved between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 while continuing to spray the raw material powder P, and the cycle time of the coating step S3 can therefore be shortened as compared with the case in which the spraying of the raw material powder P and its stopping are repeated to form the valve seat coats 16b and 17b at the plurality of opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8.
Moreover, the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp1 are set to allow the nozzle 23d to move above the cylinder block mounting surface 12a and above the combustion chamber upper wall portions 12b1 to 12b4 rather than to move above the opening portions 16a1 to 16a8 of the intake ports 16 or above the opening portions 17a1 to 17a8 of the exhaust ports 17, and it is therefore possible to prevent the excessive coats Sf from being formed at positions in the intake ports 16 or the exhaust ports 17 from which the excessive coats Sf cannot be removed.
The excessive coats Sf are formed on the cylinder block mounting surface 12a, but the cylinder block mounting surface 12a has been conventionally post-processed using a milling machine or the like to improve the flatness, and the excessive coats Sf formed on the cylinder block mounting surface 12a can therefore be removed without providing any new step. Furthermore, the excessive coats Sf are also formed on the combustion chamber upper wall portions 12b1 to 12b4, but the excessive coats Sf on the combustion chamber upper wall portions 12b1 to 12b4 can be removed relatively easily because the combustion chamber upper wall portions 12b1 to 12b4 are exposed to the outside. The excessive coats Sf formed on the combustion chamber upper wall portions 12b1 to 12b4 may be left unremoved if they do not affect the combustion performance of the engine 1.
The nozzle movement path for air intake Inp1 is set linearly along the arrangement direction of the opening portions 16a1 to 16a8 so as to be in contact with the opening portions 16a1 to 16a8, and the coating start positions Is1 and the coating end positions Ie1 are set on the nozzle movement path for air intake Inp1. Likewise, the nozzle movement path for air exhaust Enp1 is linearly set along the arrangement direction of the opening portions 17a1 to 17a8 so as to be in contact with the opening portions 17a1 to 17a8, and the coating start positions Es1 and the coating end positions Ee1 are set on the nozzle movement path for air exhaust Enp1. It is therefore possible to shorten the distance along which the nozzle 23d uselessly injects the raw material powder P, that is, the distance along which the excessive coats Sf are formed. This can suppress the waste of the raw material powder P and reduce the number of steps for removing the excessive coats Sf.
Furthermore, the strength between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 can be increased through setting the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp1 between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17 and spraying the raw material powder P to form the excessive coats Sf thereby applying the compressive residual stress between the intake ports 16 and the exhaust ports 17.
The cylinder head 12 undergoes repetitive heating at a high temperature in a restrained state of being mounted on the cylinder block 11, so that the thermal fatigue phenomenon may possibly cause cracks between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17. That is, the cylinder block mounting surface 12a of the cylinder head 12 tends to expand by receiving heat from the combustion chambers 15 and being heated, but the cylinder head 12 is restrained by the cylinder block 11 and therefore receives the compressive load to yield, thus generating the compressive stress. If, in such a state, the engine 1 is stopped and the cylinder head 12 is cooled, the cylinder block mounting surface 12a of the cylinder head 12 tends to shrink, so that the tensile stress is generated on the yielding surface of the cylinder block mounting surface 12a. Due to repetition of the compressive stress and the tensile stress, cracks may occur between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 which are exposed to the thermally severest condition.
To overcome such a problem, in the present embodiment, the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp 1 are set between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 to form the excessive coats Sf thereby to apply the compressive residual stress as in the case of performing the shot peening process.
Moreover, the excessive coats Sf are not formed in any of the injector holes 12g1 to 12g4 because the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp1 are set between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17. When using the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp1, the excessive coats Sf are formed in the plug holes 12f1 to 12f4, but the plug holes 12f1 to 12f4 are necessarily post-processed to form threaded bores for the spark plugs, and the excessive coats Sf can be removed by that post-processing.
A second embodiment regarding the nozzle movement paths will then be described.
The nozzle movement path for air intake Inp2 is linearly set along the arrangement direction of the opening portions 16a1 to 16a8 so as to be in contact with the opening portions 16a1 to 16a8 between edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 16a1 to 16a8. The nozzle 23d moves on the nozzle movement path for air intake Inp2 from the left side to the right side in the figure. This nozzle movement path for air intake Inp2 allows the nozzle 23d to move above the cylinder block mounting surface 12a and above the combustion chamber upper wall portions 12b1 to 12b4 rather than to move above the opening portions 16a1 to 16a8 of the intake ports 16 or above the opening portions 17a1 to 17a8 of the exhaust ports 17.
For the nozzle movement path for air intake Inp2 thus set, annular coating paths for air intake Idp2 are set on the annular valve seat portions 16c of the respective opening portions 16a1 to 16a8 so as to be in contact with the nozzle movement path for air intake Inp2. In addition, positions at which the nozzle movement path for air intake Inp2 is in contact with the coating paths for air intake Idp2 are set with coating start positions Is2 at which the nozzle 23d starts spraying the raw material powder P onto the annular valve seat portions 16c of the opening portions 16a1 to 16a8 and coating end positions Ie2 at which the nozzle 23d finishes spraying the raw material powder P onto the annular valve seat portions 16c.
The nozzle movement path for air exhaust Enp2 is linearly set along the arrangement direction of the opening portions 17a1 to 17a8 so as to be in contact with the opening portions 17a1 to 17a8 between edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 17a1 to 17a8. The nozzle 23d moves on the nozzle movement path for air exhaust Enp2 from the left side to the right side in the figure. This nozzle movement path for air exhaust Enp2 allows the nozzle 23d to move above the cylinder block mounting surface 12a and above the combustion chamber upper wall portions 12b1 to 12b4 rather than to move above the opening portions 16a1 to 16a8 of the intake ports 16 or above the opening portions 17a1 to 17a8 of the exhaust ports 17.
For the nozzle movement path for air exhaust Enp2 thus set, annular coating paths for air exhaust Edp2 are set on the annular valve seat portions 17c of the respective opening portions 17a1 to 17a8 so as to be in contact with the nozzle movement path for air exhaust Enp2. In addition, positions at which the nozzle movement path for air exhaust Enp2 is in contact with the coating paths for air exhaust Edp2 are set with coating start positions Es2 at which the nozzle 23d starts spraying the raw material powder P onto the annular valve seat portions 17c of the opening portions 17a1 to 17a8 and coating end positions Ee2 at which the nozzle 23d finishes spraying the raw material powder P onto the annular valve seat portions 17c.
The coating start positions Is2 and coating end positions Ie2 of the nozzle movement path for air intake Inp2 are set so that the coats overlap as in the coating start positions Is1 and coating end positions Ie1 of the first embodiment. The valve seat coats 16b are therefore formed without any gap over the entire circumferences of the opening portions 16a1 to 16a8. Likewise, the coating start positions Es2 and coating end positions Ee2 of the nozzle movement path for air exhaust Enp2 are set so that the coats overlap as in the coating start positions Es1 and coating end positions Ee1 of the first embodiment. The valve seat coats 17b are therefore formed without any gap over the entire circumferences of the opening portions 17a1 to 17a8.
The nozzle 23d moves along the nozzle movement path for air intake Inp2 and the coating paths for air intake Idp2 as follows. The nozzle 23d linearly moves on the nozzle movement path for air intake Inp2 along the arrangement direction of the opening portions 16a1 to 16a8, that is, the longitudinal direction of the semimanufactured cylinder head 3, while spraying the raw material powder P. After moving from the outside of the semimanufactured cylinder head 3 to above the cylinder block mounting surface 12a, the nozzle 23d passes above the cylinder block mounting surface 12a and moves to above the first opening portion 16a1. When reaching the first coating start position Is2, the nozzle 23d switches the direction of travel so as to fold back in the opposite direction and moves in the clockwise direction so as to trace over the annular valve seat portion 16c along the coating path for air intake Idp2, thus forming the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a1.
After moving to the first coating end position Ie2, the nozzle 23d moves again above the combustion chamber upper wall portion 12b1 along the nozzle movement path for air intake Inp2 and moves to the coating start position Is2 for the next opening portion 16a2. When reaching the coating start position Is2 for the next opening portion 16a2, the nozzle 23d moves above the second opening portion 16a2 in the clockwise direction in the figure so as to trace over the second opening portion 16a2 and forms the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a2.
After moving to the coating end position Ie2 of the opening portion 16a2, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 and above the cylinder block mounting surface 12a again along the nozzle movement path for air intake Inp2 and moves to the coating start position Is2 for the opening portion 16a3 of the next combustion chamber upper wall portion 12b2. After that, the valve seat coats 16b are formed on the opening portions 16a3 to 16a8 of the combustion chamber upper wall portions 12b2 to 12b4 in the same manner as for the opening portions 16a1 and 16a2. After finishing the formation of the valve seat coat 16b for the final opening portion 16a8, the nozzle 23d moves above the combustion chamber upper wall portion 12b4 and above the cylinder block mounting surface 12a along the nozzle movement path for air intake Inp2 and is moved to the outside of the semimanufactured cylinder head 3.
When the formation of the valve seat coats 16b for the opening portions 16a1 to 16a8 of the intake ports 16 is completed, the formation of the valve seat coats 17b for the opening portions 17a1 to 17a8 of the exhaust ports 17 is started. The nozzle 23d linearly moves on the nozzle movement path for air exhaust Enp2 along the arrangement direction of the opening portions 17a1 to 17a8, that is, the longitudinal direction of the semimanufactured cylinder head 3, while spraying the raw material powder P. After moving from the outside of the semimanufactured cylinder head 3 to above the cylinder block mounting surface 12a, the nozzle 23d passes above the cylinder block mounting surface 12a and moves to above the first opening portion 17a1. When reaching the first coating start position Es2, the nozzle 23d switches the direction of travel so as to fold back in the opposite direction and moves in the counterclockwise direction so as to trace over the annular valve seat portion 17c along the coating path for air exhaust Edp2, thus forming the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a1.
After moving to the coating end position Ee2 of the opening portion 17a1, the nozzle 23d moves again above the combustion chamber upper wall portion 12b1 along the nozzle movement path for air exhaust Enp2 and moves to the coating start position Es2 for the next opening portion 17a2. When reaching the coating start position Es2 for the next opening portion 17a2, the nozzle 23d moves above the second opening portion 17a2 in the counterclockwise direction in the figure so as to trace over the second opening portion 17a2 and forms the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a2.
After moving to the coating end position Ee2 of the opening portion 17a2, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 and above the cylinder block mounting surface 12a again along the nozzle movement path for air exhaust Enp2 and moves to the coating start position Es2 for the opening portion 17a3 of the next combustion chamber upper wall portion 12b2. After that, the valve seat coats 17b are formed on the opening portions 17a3 to 17a8 of the combustion chamber upper wall portions 12b2 to 12b4 in the same manner as for the opening portions 17a1 and 17a2. After finishing the formation of the valve seat coat 17b for the final opening portion 17a8, the nozzle 23d moves above the combustion chamber upper wall portion 12b4 and above the cylinder block mounting surface 12a along the nozzle movement path for air exhaust Enp2 and is moved to the outside of the semimanufactured cylinder head 3.
Thus, in the present embodiment, the nozzle 23d is moved between any two of the opening portions 16a1 to 16a8 and between any two of the opening portions 17a1 to 17a8 while continuing to spray the raw material powder P, and the nozzle 23d is made so as not to move above the opening portions 16a1 to 16a8 or the opening portions 17a1 to 17a8; therefore, the problems (1) and (2) can be overcome as in the first embodiment.
In the present embodiment, the improvement of the strength by the compressive residual stress may not be achieved because the excessive coats Sf are not formed between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8. However, fortunately, the nozzle movement path for air intake Inp2 and the nozzle movement path for air exhaust Enp2 are set at positions separated from each other via the combustion chamber upper wall portions 12b1 to 12b4; therefore, the heat generated during the cold spray is dissipated and the valve seat coats 16b and 17b can be formed in which the residual stress is less likely to accumulate.
Moreover, in the present embodiment, the coating start positions Is2 and Es2 and the coating end positions Ie2 and Ee2 are not disposed on the central portions of the combustion chamber upper wall portions 12b1 to 12b4 at which the temperature during operation of the engine 1 is high and the heat load is large. Rather, the coating start positions Is2 and Es2 and the coating end positions Ie2 and Ee2 are set on the edge portion sides of the combustion chamber upper wall portions 12b1 to 12b4 at which the temperature is lower than that in the central portions and the heat load is smaller than that in the central portions. The performance of the valve seat coats 16b and 17b is therefore not affected even when the strength of the coating start positions Is2 and coating end positions Ie2 of the valve seat coats 16b and the strength of the coating start positions Es2 and coating end positions Ee2 of the valve seat coats 17b become lower than predetermined strength that is preliminarily set.
Furthermore, in the present embodiment, the nozzle movement path for air intake Inp2 is set between the edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 16a1 to 16a8, and the nozzle movement path for air exhaust Enp2 is set between the edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 17a1 to 17a8; therefore, the excessive coats Sf are not formed in any of the plug holes 12f1 to 12f4.
In-cylinder injection-type engines include spray guide-type (center injection-type) engines in which injectors are arranged so as to inject the fuel downward into the fuel chambers from approximately above the centers of the combustion chambers. As illustrated in
A third embodiment regarding the nozzle movement paths will then be described. This embodiment represents a combination of the nozzle movement path for air intake Inp1 or the nozzle movement path for air exhaust Enp1 as described in the first embodiment and the nozzle movement path for air intake Inp2 or the nozzle movement path for air exhaust Enp2 as described in the second embodiment. For example, in the semimanufactured cylinder head 3 illustrated in
According to this embodiment, the nozzle 23d is moved between any two of the opening portions 16a1 to 16a8 and between any two of the opening portions 17a1 to 17a8 while continuing to spray the raw material powder P, and the nozzle 23d is made so as not to move above the opening portions 16a1 to 16a8 or the opening portions 17a1 to 17a8; therefore, the problems (1) and (2) can be overcome as in the first embodiment and the second embodiment.
In the embodiment illustrated in
Also in the embodiment illustrated in
A fourth embodiment regarding the nozzle movement path will then be described.
When the semimanufactured cylinder head 3 has a plurality of combustion chamber upper wall portions 12b1 to 12b4 and the combustion chamber upper wall portions 12b1 to 12b4 include respective opening portions 16a1 to 16a8 and respective opening portions 17a1 to 17a8, the nozzle movement path Np is used to form the valve seat coats 16b and 17b for each of the combustion chamber upper wall portions 12b1 to 12b4. The nozzle movement path Np is connected to coating paths for air intake Idp4 for forming the valve seat coats 16b at the opening portions 16a1 to 16a8 and coating paths for air exhaust Edp4 for forming the valve seat coats 17b at the opening portions 17a1 to 17a8.
Specifically, the nozzle 23d moves along the nozzle movement path Np as follows. The nozzle 23d linearly moves on the nozzle movement path Np along the arrangement direction of the opening portions 16a1 to 16a8, that is, the longitudinal direction of the semimanufactured cylinder head 3, while spraying the raw material powder P. After moving from the outside of the semimanufactured cylinder head 3 to above the cylinder block mounting surface 12a, the nozzle 23d passes above the cylinder block mounting surface 12a and moves to above the first opening portion 16a1. When reaching the first coating start position Is4 at which the nozzle movement path Np is in contact with the coating path for air intake Idp4, the nozzle 23d moves above the opening portion 16a1 in the counterclockwise direction so as to trace over the opening portion 16a1 along the coating path for air intake Idp4 and forms the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a1.
After moving to the coating end position Ie4 of the opening portion 16a1, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 along the width direction of the semimanufactured cylinder head 3 and moves to the coating start position Es4 for the next opening portion 17a1. When reaching the coating start position Es4 for the opening portion 17a1, the nozzle 23d moves above the opening portion 17a1 in the clockwise direction in the figure so as to trace over the opening portion 17a1 and forms the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a1.
After moving to the coating end position Ee4 of the opening portion 17a1, the nozzle 23d moves again above the combustion chamber upper wall portion 12b1 along the longitudinal direction of the semimanufactured cylinder head 3 and moves to the coating start position Es4 for the next opening portion 17a2. When reaching the coating start position Es4 for the opening portion 17a2, the nozzle 23d moves above the opening portion 17a2 in the clockwise direction in the figure so as to trace over the opening portion 17a2 and forms the valve seat coat 17b on the annular valve seat portion 17c of the opening portion 17a2.
After moving to the coating end position Ee4 of the opening portion 17a2, the nozzle 23d moves again above the combustion chamber upper wall portion 12b1 along the width direction of the semimanufactured cylinder head 3 and moves to the coating start position Is4 for the next opening portion 16a2. When reaching the coating start position Is4 for the opening portion 16a2, the nozzle 23d moves above the opening portion 16a2 in the counterclockwise direction in the figure so as to trace over the opening portion 16a2 and forms the valve seat coat 16b on the annular valve seat portion 16c of the opening portion 16a2.
After moving to the coating end position Ie4 of the opening portion 16a2, the nozzle 23d moves above the combustion chamber upper wall portion 12b1 and above the cylinder block mounting surface 12a again along the longitudinal direction of the semimanufactured cylinder head 3 and moves to the coating start position Is4 for the opening portion 16a3 of the next combustion chamber upper wall portion 12b2. After that, the nozzle 23d forms the valve seat coats 16b and 17b at the opening portions 16a3 to 16a8 and opening portions 17a3 to 17a8 of the combustion chamber upper wall portions 12b2 to 12b4 in the same manner as for the opening portions 16a1, 16a2, 17a1, and 17a2. After finishing the formation of the valve seat coat 16b for the final opening portion 16a8, the nozzle 23d moves above the combustion chamber upper wall portion 12b4 and above the cylinder block mounting surface 12a along the nozzle movement path Np and is moved to the outside of the semimanufactured cylinder head 3.
According to this embodiment, the nozzle 23d is moved between any two of the opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 while continuing to spray the raw material powder P, and the nozzle 23d is made so as not to move above the opening portions 16a1 to 16a8 or the opening portions 17a1 to 17a8; therefore, the problems (1) and (2) can be overcome as in the first embodiment and the second embodiment. Moreover, it is possible to suppress the formation of the excessive coats Sf not only in the intake ports 16 and the exhaust ports 17 but also in the plug holes 12f1 to 12f4 and the injector holes 12g1 to 12g4.
Furthermore, in the cold spray method, the higher the temperature of the coating portions to be formed with coats, the easier the coating portions and the raw material powder P can be plastically deformed; therefore, the higher the temperature of the coating portions to be formed with coats, the stronger the raw material powder P can adhere to the coating portions. According to the present embodiment, the valve seat coats 16b and 17b are formed for each of the combustion chamber upper wall portions 12b1 to 12b4 thereby to allow the temperature of the combustion chamber upper wall portions 12b1 to 12b4 formed with the valve seat coats 16b and 17b to be maintained at a high temperature, and the raw material powder P can therefore adhere strongly to the combustion chamber upper wall portions 12b1 to 12b4 to form the valve seat coats 16b and 17b having excellent high-temperature abrasion resistance.
Furthermore, in the present embodiment, the valve seat coats 16b and 17b are formed for each of the combustion chamber upper wall portions 12b1 to 12b4, and the valve seat coats 16b and 17b can therefore be repaired for each of the combustion chamber upper wall portions 12b1 to 12b4.
A fifth embodiment regarding the nozzle movement path or paths will then be described. In this embodiment, when the nozzle 23d moves along the nozzle movement path, the injection angle of the raw material powder P with respect to the injection surface onto which the raw material powder P is injected, that is, the injection angle of the raw material powder P with respect to the cylinder block mounting surface 12a or the combustion chamber upper wall portions 12b1 to 12b4, is made different from an injection angle θ1 of the raw material powder P with respect to the opening portions 16a1 to 16a8 or the opening portions 17a1 to 17a8, which are the coating portions, thereby to change the width and thickness of the excessive coats formed on the cylinder block mounting surface 12a or the combustion chamber upper wall portions 12b1 to 12b4. The following description will be made for a pattern (1) in which the injection angle of the raw material powder P with respect to the cylinder block mounting surface 12a or the combustion chamber upper wall portions 12b1 to 12b4 is made approximately horizontal along the nozzle movement path and a pattern (2) in which the injection angle of the raw material powder P with respect to the cylinder block mounting surface 12a or the combustion chamber upper wall portions 12b1 to 12b4 is made approximately vertical along the nozzle movement path.
First, the injection angle of the raw material powder P in the first embodiment will be described. In the first embodiment, as illustrated in
On the other hand, in the pattern (1) of the present embodiment, when the nozzle 23d is moved along the coating path for air intake Idp1 on the opening portion 16a1 to form the valve seat coat 16b on the annular valve seat portion 16c, as illustrated in
In the pattern (2) of the present embodiment, when the nozzle 23d is moved along the coating path for air intake Idp1 on the opening portion 16a1 to form the valve seat coat 16b on the annular valve seat portion 16c, as illustrated in
According to the pattern (1) of the present embodiment, the post-processing area applied to the semimanufactured cylinder head 3 to remove the excessive coat Sf2 is wider than that in the first embodiment because the width W2 of the excessive coat Sf2 is wider than the width W1 of the excessive coat Sf1. However, the depth of post-processing is shallower than that in the first embodiment because the thickness T2 of the excessive coat Sf2 is thinner than the thickness T1 of the excessive coat Sf1. The post-processing is therefore easier than that in the first embodiment if the excessive coat Sf2 is formed on the cylinder block mounting surface 12a on which the entire surface is cut in the finishing step S4.
According to the pattern (2) of the present embodiment, the depth of post-processing applied to the semimanufactured cylinder head 3 to remove the excessive coat Sf3 is deeper than that in the first embodiment because the thickness T3 of the excessive coat Sf3 is thicker than the thickness T1 of the excessive coat Sf1. However, the post-processing area is narrower than that in the first embodiment because the width W3 of the excessive coat Sf3 is narrower than the width W1 of the excessive coat Sf1. The post-processing is therefore easier than that in the first embodiment if the excessive coat Sf3 is formed on any of the combustion chamber upper wall portions 12b1 to 12b4 which have a narrower area than that of the cylinder block mounting surface 12a and also have curved surfaces or tilted surfaces.
Although not illustrated in detail, the present embodiment is also applied when the valve seat coats 17b are formed at the opening portions 17a1 to 17a8 of the exhaust ports 17. The present embodiment can also be applied when moving the nozzle 23d in the second to fourth embodiments. In the present embodiment, the pattern (1) may be applied to both the cylinder block mounting surface 12a and the combustion chamber upper wall portions 12b1 to 12b4, or the pattern (2) may also be applied to both the cylinder block mounting surface 12a and the combustion chamber upper wall portions 12b1 to 12b4. Alternatively, the pattern (1) may be applied to the cylinder block mounting surface 12a while the pattern (2) may be applied to the combustion chamber upper wall portions 12b1 to 12b4.
In the above fifth embodiment, when the nozzle 23d moves along the nozzle movement path, the injection angle of the raw material powder P from the nozzle 23d is changed. Additionally or alternatively, for example, when the nozzle 23d moves along the nozzle movement path, the moving speed of the nozzle 23d may be set faster than the moving speed for forming the valve seat coats 16b and 17b. This can reduce the thickness of the excessive coats formed on the cylinder block mounting surface 12a and the combustion chamber upper wall portions 12b1 to 12b4.
In the above first to fifth embodiments, as illustrated in
The above first to fifth embodiments have been described by exemplifying the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust port 17 of the semimanufactured cylinder head 3 as the plurality of coating portions of the coating target component, but the present invention can also be applied to other coating target components.
For example, in the cylinder block 11 illustrated in
Additionally or alternatively, in the crankshaft 14 illustrated in
As described above, the coating method according to one or more embodiments of the present invention is a method used for forming a coat on each of a plurality of coating portions that are not continuous with one another. The coating portions are provided on a coating target component such as the semimanufactured cylinder head 3, the cylinder block 11, or the crank shaft 14. This method includes relatively moving the coating target component and the nozzle 23d of the cold spray apparatus 2 to cause each of the plurality of coating portions and the nozzle 23d to sequentially face each other and spraying the raw material powder P from the nozzle 23d onto the coating portions facing the nozzle 23d. When the nozzle 23d is located on a nozzle movement path from a coating portion having been formed with the coat to another coating portion to be subsequently formed with the coat, injection of the raw material powder P from the nozzle 23d is continued. This allows the cycle time to be shorter than that when forming coats on the plurality of coating portions by repeating the spraying of the raw material powder P and its stopping.
According to the coating methods of the first to fifth embodiments of the present invention, in the semimanufactured cylinder head 3 which is the coating target component, when the valve seat coats 16b and 17b are formed on the annular edge portions of the opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 which are the plurality of coating portions, the semimanufactured cylinder head 3 and the nozzle 23d of the cold spray apparatus 2 are relatively moved to cause each of the annular edge portions of the plurality of opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 and the nozzle 23d to face each other, and the nozzle 23d sprays the raw material powder P onto each of the annular edge portions of the opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 facing the nozzle 23d. Then, when the nozzle 23d is located on the nozzle movement path for air intake Inp1 or Inp 2, the nozzle movement path for air exhaust Enp1 or Enp 2, or the nozzle movement path Np along which the nozzle 23d is moved from an opening portion having been formed with the valve seat coat to another opening portion to be subsequently formed with the valve seat coat, injection of the raw material powder P from the nozzle 23d is continued. This allows the cycle time of the coating step S3 to be shorter than that when forming the valve seat coats 16b and 17b at the plurality of opening portions 16a1 to 16a8 and opening portions 17a1 to 17a8 by repeating the spraying of the raw material powder P and its stopping.
According to the coating methods of the first to fifth embodiments, the nozzle movement paths for air intake Inp1 and Inp 2, the nozzle movement paths for air exhaust Enp1 and Enp 2, and the nozzle movement path Np are set so that the nozzle 23d does not move above the opening portions 16a1 to 16a8 of the intake ports 16 or the opening portions 17a1 to 17a8 of the exhaust ports 1, and it is therefore possible to prevent the excessive coats Sf from being formed at positions in the intake ports 16 or the exhaust ports 17 from which the excessive coats Sf cannot be removed.
According to the coating methods of the first to fifth, the nozzle movement paths for air intake Inp1 and Inp 2, the nozzle movement paths for air exhaust Enp1 and Enp 2, and the nozzle movement path Np are set so that the nozzle 23d moves above the cylinder block mounting surface 12a, and the excessive coats Sf are therefore formed on the cylinder block mounting surface 12a. However, fortunately, the cylinder block mounting surface 12a has been conventionally post-processed using a milling machine or the like to improve the flatness, and the excessive coats Sf formed on the cylinder block mounting surface 12a can therefore be removed without providing any new step.
According to the coating methods of the first to fifth embodiments, the nozzle movement paths for air intake Inp1 and Inp 2, the nozzle movement paths for air exhaust Enp1 and Enp 2, and the nozzle movement path Np are set so that the nozzle 23d moves above the combustion chamber upper wall portions 12b1 to 12b4, and the excessive coats Sf are therefore formed on the combustion chamber upper wall portions 12b1 to 12b4. However, fortunately, the excessive coats Sf on the combustion chamber upper wall portions 12b1 to 12b4 can be removed relatively easily because the combustion chamber upper wall portions 12b1 to 12b4 are exposed to the outside. The excessive coats Sf otherwise may not have to be removed if they do not affect the combustion performance of the engine 1, so the cycle time for the semimanufactured cylinder head 3 is not affected.
According to the coating methods of the first to fifth embodiments, the nozzle movement paths for air intake Inp1 and Inp2 are set linearly along the arrangement direction of the opening portions 16a1 to 16a8, and the coating start positions Is1 and Is2 and the coating end positions Ie1 and Ie2 are set on the nozzle movement paths for air intake Inp1 and Inp2. Likewise, the nozzle movement paths for air exhaust Enp1 and Enp2 are set linearly along the arrangement direction of the opening portions 17a1 to 17a8, and the coating start positions Es1 and Es2 and the coating end positions Ee1 and Ee2 are set on the nozzle movement paths for air exhaust Enp 1 and Enp2. The nozzle movement path Np is set linearly along the arrangement direction of the opening portions 16a1 to 16a8, and the coating start positions Is4 and the coating end positions Ie4 are set on the nozzle movement path Np. It is therefore possible to shorten the distance along which the nozzle 23d uselessly injects the raw material powder P, that is, the distance along which the excessive coats Sf are formed. This can suppress the waste of the raw material powder P and reduce the number of steps for removing the excessive coats Sf.
According to the coating method of the first embodiment, the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp 1 are set between the opening portions 16a1 to 16a8 of the intake ports 16 and the opening portions 17a1 to 17a8 of the exhaust ports 17, and the raw material powder can therefore be sprayed between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 to form the excessive coats Sf for applying the compressive residual stress. This can further enhance the strength between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8.
According to the coating method of the first embodiment, the excessive coats Sf are not formed in any of the injector holes 12g1 to 12g4 because the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp1 are set between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8. When using the nozzle movement path for air intake Inp1 and the nozzle movement path for air exhaust Enp 1, the excessive coats Sf are formed in the plug holes 12f1 to 12f4, but the plug holes 12f1 to 12f4 are necessarily post-processed to form threaded bores for the spark plugs, and the excessive coats Sf can be removed by that post-processing.
According to the coating method of the second embodiment, the nozzle movement path for air intake Inp2 is set between the edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 16a1 to 16a8. Likewise, the nozzle movement path for air exhaust Enp2 is set between the edge portions of the combustion chamber upper wall portions 12b1 to 12b4 and the opening portions 17a1 to 17a8. The heat generated during the cold spray is therefore dissipated and the valve seat coats 16b and 17b can be formed in which the residual stress is less likely to accumulate.
According to the coating method of the third embodiment, the nozzle movement path for air intake Inp1 or nozzle movement path for air exhaust Enp1 of the first embodiment and the nozzle movement path for air intake Inp2 or nozzle movement path for air exhaust Enp2 of the second embodiment can be combined as appropriate thereby to exhibit effects resulting from the effect obtained by the first embodiment and the effect obtained by the second embodiment. That is, the raw material powder is sprayed between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8 to form the excessive coats Sf thereby to apply the compressive residual stress, thus further improve the strength between the opening portions 16a1 to 16a8 and the opening portions 17a1 to 17a8, and the heat generated during the cold spray can be dissipated, so that the valve seat coats 16b or the valve seat coats 17b can be formed in which the residual stress is less likely to accumulate.
According to the coating method of the fourth embodiment, the valve seat coats 16b and 17b are formed for each of the combustion chamber upper wall portions 12b1 to 12b4 thereby to allow the temperature of the combustion chamber upper wall portions 12b1 to 12b4 formed with the valve seat coats 16b and 17b to be maintained at a high temperature, and the raw material powder P can therefore adhere strongly to the combustion chamber upper wall portions 12b1 to 12b4 to form the valve seat coats 16b and 17b having excellent high-temperature abrasion resistance. Moreover, the valve seat coats 16b and 17b can be repaired for each of the combustion chamber upper wall portions 12b1 to 12b4.
According to the coating method of the fifth embodiment, in the nozzle movement path for air intake Inp1 or Inp 2, the nozzle movement path for air exhaust Enp1 or Enp 2, or the nozzle movement path Np, the injection angle θ2 or θ3 of the raw material powder P from the nozzle 23d can be made different from the injection angle θ1 of the raw material powder P with respect to the opening portions 16a1 to 16a8 or the opening portions 17a1 to 17a8, which are the coating portions, thereby to change the width and thickness of the excessive coats formed on the cylinder block mounting surface 12a or the combustion chamber upper wall portions 12b1 to 12b4. Thus, the width and thickness of the excessive coats can be changed in accordance with the shapes of surfaces to be formed with the excessive coats, the presence or absence of post-processing, and the like, and the removal of the excessive coats therefore becomes easy by appropriately selecting the width and thickness of the excessive coats.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2018/034350 | 9/18/2018 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2020/059003 | 3/26/2020 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 20140291885 | Etchegoyen | Oct 2014 | A1 |
| 20150197858 | Corbeil et al. | Jul 2015 | A1 |
| 20170250122 | Hamweendo et al. | Aug 2017 | A1 |
| 20180223902 | Izawa | Aug 2018 | A1 |
| Number | Date | Country |
|---|---|---|
| 106367750 | Feb 2017 | CN |
| 10 2006 029 070 | Aug 2007 | DE |
| 102006029070 | Aug 2007 | DE |
| 2016-200043 | Dec 2016 | JP |
| 2016200043 | Dec 2016 | JP |
| WO 2017022505 | Feb 2017 | WO |
| Entry |
|---|
| Blochet et al.; Influence of Spray Angle on Cold Spray with AI for the Repair of Aircraft Components; XP055826836, pp. 1-7; May 31, 2014. |
| Blochet Quentin et al., “Influence of Spray Angle on Cold Spray with A1 for the Repair of Aircraft Components”, May 31, 2014, pp. 1-7, retrieved from the Internet: URL: https://www.researchgate.net/publication/281330261_Influence_of_spray_angle_on_cold_spray_with_A1_for_the_repair_of_aircraft_components, retrieved on Jul. 22, 2021. |
| Number | Date | Country | |
|---|---|---|---|
| 20220042177 A1 | Feb 2022 | US |
