Film formation method

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a U.S. national stage application of International Application No. PCT/JP2019/014149, filed on Mar. 29, 2019.

BACKGROUND
Technical Field

The present invention relates to a method of forming a film by cold spraying.

Background Information

There is a known method for manufacturing a sliding member in which a valve seat having exceptional abrasion resistance at high temperature can be formed by blowing a powder of metal or another raw material by cold spraying onto a seating portion of an engine valve (WO 2017/022505 A1—Patent Document 1).

SUMMARY

When enabled for multi-valve capability, automobile engines are provided with a plurality of intake and exhaust valves. Therefore, when valve seats are formed by cold spraying in the seating portions of a plurality of valves, it is necessary for a cylinder head and a nozzle of a cold spray device to be moved relative to each other, the nozzle and the plurality of seating portions to be faced sequentially toward each other, and a raw material powder to be ejected from the nozzle and blown onto the seating portions faced toward the nozzle.

When the spraying of raw material powder is interrupted, the cold spray device requires a standby time of several minutes until the raw material powder will again be stably blown. Therefore, it is preferable that raw material powder be continuously sprayed for as long as possible without interruption. However, when one valve seat film is formed, the nozzle and the cylinder head are moved relative to each other in a 360° circle, but overlapping portions are created at the film formation starting point and film formation finishing point of the circular trajectory, or a turnback point appears where the nozzle movement speed reaches zero at the film formation starting point or the film formation finishing point.

In a trajectory where a turnback point arises in the first layer of an overlapping portion, the incline in the end part of the first film formation starting point becomes steep, and when a second layer is sprayed at this location, the flattening of the raw material powder is hindered and an insufficient coating film is formed.

A problem to be solved by the present invention is to provide a cold-spraying film formation method with which the forming of an insufficient coating film can be minimized.

The present invention overcomes the problem described above by providing a film formation method in which a coating film is formed on parts where a film is formed while a nozzle of a cold spraying device is relatively moved along a film formation trajectory in which film formation starting points and film formation finishing points of the parts where a film is formed overlap to form overlapping portions, and a raw material powder is continuously sprayed from the nozzle, wherein a film is formed such that at the film formation starting points of the overlapping portions, an angle of inclination in end parts of the coating film relative to the surfaces of the parts where a film is formed is 45° or less.

According to the present invention, the angle of inclination in the end parts of the coating film at the film formation starting points of the overlapping portions is 45° or less, and the angle of inclination in the end parts of the first layer is prevented from being steep; therefore, the forming of an insufficient coating film can be minimized.

BRIEF DESCRIPTION OF THE DRAWINGS

Referring now to the attached drawings which form a part of this original disclosure.

FIG. 1 is a cross-sectional view of a cylinder head on which a valve seat film is formed using a cold spray device according to the present invention;

FIG. 2 is an enlarged cross-sectional view of a periphery of the valve of FIG. 2;

FIG. 3 is a configuration diagram of one embodiment of the cold spray device according to the present invention;

FIG. 4 is a front view of a spray gun of one embodiment of the cold spray device according to the present invention;

FIG. 5 is a cross-sectional view alone line along line V-V in FIG. 4;

FIG. 6 is a front view of a state in which the spray gun in FIG. 4 has been offset;

FIG. 7 is a front view of a film formation factory including the cold spray device according to present invention;

FIG. 8 is a plan view of FIG. 7;

FIG. 9 is a flowchart of a procedure for manufacturing a cylinder head using the cold spray device according to the present invention.

FIG. 10 is a perspective view of a cylinder head rough material on which a valve seat film is formed using the cold spray device according to the present invention.

FIG. 11 is a cross-sectional view of an intake port along line XI-XI of FIG. 10.

FIG. 12 is a cross-sectional view of a state in which an annular valve seat part has been formed by a cutting step in the intake port of FIG. 11.

FIG. 13 is a cross-sectional view of a state in which a valve seat film is formed in the intake port of FIG. 12.

FIG. 14 is a cross-sectional view of an intake port in which a valve seat film has been formed.

FIG. 15 is a cross-sectional view of an intake port after the finishing step of FIG. 9.

FIG. 16 is a plan view of a cylinder head rough material, depicting an example of movement trajectories when a nozzle of the cold spray device moves over opening parts of intake ports and exhaust ports in the film formation method according to the present invention.

FIG. 17 is a plan view of a movement trajectory relative to one intake port of FIG. 16.

FIG. 18A shows a cross-section of a coating film in which a film has been formed using a movement trajectory of a comparative example, in which a turnback point is set in an overlapping portion of a film formation starting point and a film formation finishing point.

FIG. 18B shows a cross-section of a coating film when a film has been formed on the movement trajectory of the film formation method according to the present invention.

FIG. 19 is a graph of the relationship between the nozzle movement speed and the film formation trajectory in one embodiment of the film formation method according to the present invention.

FIG. 20 is a graph of the relationship between the amount of raw material powder sprayed from the nozzle and the film formation trajectory in another embodiment of the film formation method according to the present invention.

FIG. 21 is a cross-sectional view of a raw material powder supply section of FIG. 3.

FIG. 22 is a perspective view of a weighing section of FIG. 21.

FIG. 23 is a cross-sectional view along line XXIII-XXIII of FIG. 22.

FIG. 24 is a plan view of a shape of the weighing section (disc) corresponding to the movement trajectory of FIG. 17.

FIG. 25 is an expanded cross-sectional view along line XXV-XXV of FIG. 24.

FIG. 26 is a graph of the relationship between a gun distance and the film formation trajectory in yet another embodiment of the film formation method according to the present invention.

FIG. 27 is a plan view of an intake port of yet another embodiment of the film formation method according to the present invention.

FIG. 28A is a cross-sectional view along line XXVIII-XXVIII of FIG. 27.

FIG. 28B is a cross-sectional view along line XXVIII-XXVIII of FIG. 27, showing another example of FIG. 28A.

DETAILED DESCRIPTION OF EMBODIMENTS

An embodiment of the present invention is described below on the basis of the drawings. There shall first be described an internal combustion engine 1 provided with a valve seat film, in which a film formation method and a cold spray device of the embodiment are preferably applied. FIG. 1 is a cross-sectional view of the internal combustion engine 1, showing mainly the configuration around the cylinder head.

The internal combustion engine 1 comprises a cylinder block 11 and a cylinder head 12 assembled on an upper part of the cylinder block 11. The internal combustion engine 1 is, for example, an in-line four-cylinder gasoline engine, and the cylinder block 11 has four cylinders 11a arranged in the depth direction of the drawing. The cylinders 11a accommodate pistons 13 that move in a reciprocating manner vertically in the drawing, and the pistons 13 link via connecting rods 13a to crankshafts 14 extending in the depth direction of the drawing.

In a surface 12a of the cylinder head 12 that attaches to the cylinder block 11, in positions corresponding to the cylinders 11a, four recesses 12b constituting combustion chambers 15 of the cylinders are formed. The combustion chambers 15 are spaces for combusting an air-fuel mixture of fuel and intake air, and are configured from the recesses 12b of the cylinder head 12, top surfaces 13b of the pistons 13, and inner peripheral surfaces of the cylinders 11a.

The cylinder head 12 is provided with intake ports 16 via which the combustion chambers 15 and one side surface 12c of the cylinder head 12 communicate. The intake ports 16 assume a substantially cylindrical form that is curved, and guide intake air into the combustion chambers 15 from an intake manifold (not shown) connected to the side surface 12c. The cylinder head 12 is also provided with exhaust ports 17 that communicate the combustion chambers 15 and another side surface 12d of the cylinder head 12. The exhaust ports 17 have roughly cylindrical shapes curved in the same manner as the intake ports 16, and discharge exhaust air produced in the combustion chambers 15 to an exhaust manifold (not shown) connected to the side surface 12d. The internal combustion engine 1 of the present embodiment has two intake ports 16 and exhaust ports 17 each for one cylinder 11a.

The cylinder head 12 is provided with intake valves 18 that open and close the intake ports 16 in relation to the combustion chambers 15, and exhaust valves 19 that open and close the exhaust ports 17 in relation to the combustion chambers 15. The intake valves 18 and the exhaust valves 19 are each provided with a valve stem 18a or 19a in the form of a round rod and a valve head 18b or 19b in the form of a disc provided at a distal end of the valve stem 18a or 19a. The valve stems 18a and 19a are slidably inserted through roughly cylindrical valve guides 18c and 19c assembled in the cylinder head 12. The intake valves 18 and the exhaust valves 19 are thereby free to move along axial directions of the valve stems 18a and 19a in relation to the combustion chambers 15.

FIG. 2 is an enlarged view of a communicating portion between a combustion chamber 15, an intake port 16, and an exhaust port 17. The intake port 16 has a roughly cylindrical opening portion 16a provided in the portion communicating with the combustion chamber 15. Formed in an annular edge part of the opening portion 16a is an annular valve seat film 16b that comes into contact with the valve head 18b of the intake valve 18. When the intake valve 18 moves upward along the axial direction of the valve stem 18a, an upper surface of the valve head 18b comes into contact with the valve seat film 16b and closes up the intake port 16. Conversely, when the intake valve 18 moves downward along the axial direction of the valve stem 18a, a gap is formed between the upper surface of the valve head 18b and the valve seat film 16b and the intake port 16 is opened.

The exhaust port 17 is provided with a roughly circular opening portion 17a in the communicating portion between the intake port 16 and the combustion chamber 15, and formed in an annular edge part of the opening portion 17a is an annular valve seat film 17b that comes into contact with the valve head 19b of the exhaust valve 19. When the exhaust valve 19 moves upward along the axial direction of the valve stem 19a, an upper surface of the valve head 19b comes into contact with the valve seat film 17b and closes up the exhaust port 17. Conversely, 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 film 17b and the exhaust port 17 is opened. A diameter of the opening portion 16a of the intake port 16 is set larger than a diameter of the opening portion 17a of the exhaust port 17.

In the four-cycle internal combustion engine 1, only the intake valve 18 is opened when the piston 13 descends, whereby the air-fuel mixture is introduced into the cylinder 11a from the intake port 16 (intake stroke). The intake valve 18 and the exhaust valve 19 are then closed, and the piston 13 is raised to roughly top dead center to compress the air-fuel mixture inside the cylinder 11a (compression stroke). When the piston 13 has reaches roughly top dead center, the compressed air-fuel mixture is ignited by a sparkplug and the air-fuel mixture thereby explodes. This explosion causes the piston 13 to descend to bottom dead center, and the explosion is converted to rotational force via a linked crankshaft 14 (combustion/expansion stroke). Lastly, when the piston 13 reaches bottom dead center and begins to ascend again, only the exhaust valve 19 is opened and exhaust inside the cylinder 11a is discharged to the exhaust port 17 (exhaust stroke). The internal combustion engine 1 generates output by repeating the cycle described above.

The valve seat films 16b and 17b are formed by cold spraying directly on the annular edge parts of the openings 16a and 17a of the cylinder head 12. Cold spraying is a method in which a working gas at a temperature lower than the melting point or softening point of a raw material powder is brought to a supersonic flow, the working gas is charged with raw material powder carried by a carrier gas, the gas with the powder is sprayed from a nozzle tip to collide with a base material while in a solid-phase state, and a coating film is formed by plastic deformation of the raw material powder. In comparison to thermal spraying, in which a material is melted and deposited on a base material, the characteristics of cold spraying are that a dense coating film that does not oxidize can be obtained in the atmosphere, thermal alteration is minimized because the effect of heat on the material particles is small, the film is formed at a fast rate, the film can be made thicker, and adhesion efficiency is high. Because of the fast film-forming rate and the thick film in particular, cold spraying is suitable when the present invention is applied with structural materials such as the valve seat films 16b and 17b of the internal combustion engine 1.

FIG. 3 is a schematic diagram of a cold spray device 2 of the present embodiment, which is used to form the valve seat films 16b and 17b described above. The cold spray device 2 of the present embodiment is provided with a gas supply section 21 that supplies the working gas and the carrier gas, a raw material powder supply section 22 that supplies the raw material powder for the valve seat films 16b and 17b, a spray gun 23 that sprays the raw material powder as a supersonic flow using working gas of which the temperature is not higher than the melting point of the powder, and a refrigerant circulation circuit 27 that cools a nozzle 23d.

The gas supply section 21 is provided with a compressed gas vessel 21a, a working gas line 21b, and a carrier gas line 21c. The working gas line 21b and the carrier gas line 21c are each provided with a pressure adjuster 21d, a flow rate adjustment valve 21e, a flow rate gauge 21f, and a pressure gauge 21g. The pressure adjusters 21d, the flow rate adjustment valves 21e, the flow rate gauges 21f, and the pressure gauges 21g are supplied to adjust the respective pressures and flow rates of the working gas and carrier gas from the compressed gas vessel 21a.

A tape heater or another heater 21i is installed in the working gas line 21b, and the heater 21i heats the working gas line 21b by being supplied with electric power from an electric power source 21h via electric power supply wires 21j and 21j. The working gas is introduced into a chamber 23a of the spray gun 23 after being heated by the heater 21i to a temperature lower than the melting point or softening point of the raw material powder. A pressure gauge 23b and a thermometer 23c are installed on the chamber 23a, a pressure value and a temperature value detected via respective signal lines 23g and 23g are outputted to a controller (not shown), and these values are supplied for feedback control of the pressure and temperature.

The raw material powder supply section 22 is provided with a raw material powder supply device 22a, and a weighing section 22b and a raw material powder supply line 22c added to the raw material powder supply device 22a. The carrier gas from the compressed gas vessel 21a passes through the carrier gas line 21c and is introduced into the raw material powder supply device 22a. A predetermined amount of raw material powder weighed by the weighing section 22b is carried into the chamber 23a via the raw material powder supply line 22c.

The spray gun 23 sprays the raw material powder P, which has been carried into the chamber 23a by the carrier gas, from the tip of the nozzle 23d at a supersonic flow with the aid of the working gas, and causes the raw material powder P to collide in a solid-phase state or in a solid-liquid coexistent state with a base material 24 to form a coating film 24a. In the present embodiment, the cylinder head 12 is applied as the base material 24, and the valve seat films 16b and 17b are formed by spraying the raw material powder P by cold spraying onto the annular edge parts of the openings 16a and 17a of the cylinder head 12.

The nozzle 23d is internally provided with a flow channel (not shown) through which water or another refrigerant flows. The tip end of the nozzle 23d is provided with a refrigerant introduction part 23e through which the refrigerant is introduced into the flow channel, and a base end of the nozzle 23d is provided with a refrigerant discharge part 23f through which the refrigerant in the flow channel is discharged. The refrigerant is introduced into the flow channel of the nozzle 23d through the refrigerant introduction part 23e, the refrigerant flows through the flow channel, and the refrigerant is discharged from the refrigerant discharge part 23f, whereby the nozzle 23d is cooled.

The refrigerant circulation circuit 27, via which the refrigerant is circulated through the flow channel of the nozzle 23d, is provided with a tank 271 that stores the refrigerant, an introduction pipe 274 connected to the above-described refrigerant introduction part 23e, a pump 272 that is connected to the introduction pipe 274 and that causes the refrigerant to flow between the tank 271 and the nozzle 23d, a cooler 273 that cools the refrigerant, and a discharge pipe 275 connected to the refrigerant discharge part 23f. The cooler 273 is composed of, for example, a heat exchanger, etc., and the cooler causes the refrigerant that has cooled the nozzle 23d and risen in temperature to exchange heat with air, water, gas, or another refrigerant, thus cooling the refrigerant.

Refrigerant stored in the tank 271 is drawn into the refrigerant circulation circuit 27 by the pump 272, and the refrigerant is supplied to the refrigerant introduction part 23e via the cooler 273. The refrigerant supplied to the refrigerant introduction part 23e flows through the flow channel in the nozzle 23d from the tip-end side toward the rear-end side, during which time the refrigerant exchanges heat with the nozzle 23d and the nozzle 23d is cooled. Having flowed to the rear-end side of the flow channel, the refrigerant is discharged from the refrigerant discharge part 23f to the discharge pipe 275, and returns to the tank 271. Thus, the refrigerant is circulated in the refrigerant circulation circuit 27 while being cooled, so that the nozzle 23d is cooled, and therefore, the raw material powder P can be kept from adhering to the spray passage of the nozzle 23d.

The valve seats of the cylinder head 12 require heat resistance and abrasion resistance high enough to withstand striking input from the valves in the combustion chambers 15, as well as thermal conductivity high enough to cool the combustion chambers 15. To comply with these requirements, the valve seat films 16b and 17b, which are formed from, for example, a powder of a precipitation-hardening copper alloy, make it possible to obtain valve seats that are harder than the cylinder head 12, which is formed from an aluminum alloy for casting, and that have exceptional heat resistance and abrasion resistance.

Because the valve seat films 16b and 17b are formed directly on the cylinder head 12, it is possible to achieve higher thermal conductivity than in prior-art valve seats in which separate seat rings are pressed-fitted and formed in port openings. Furthermore, compared to cases of using separate seat rings, not only is it possible to bring the valve seat films closer to a water jacket for cooling, but it is also possible to achieve secondary effects such as increasing throat diameters of the intake ports 16 and the exhaust ports 17 and promoting tumble flow by optimizing port shape.

The raw material powder P used to form the valve seat films 16b and 17b is preferably a metal that is harder than aluminum alloys for casting and that yields the heat resistance, abrasion resistance, and thermal conductivity needed for the valve seats; for example, it is preferable to use the precipitation-hardening copper alloy mentioned above. A Corson alloy containing nickel and silicon, chromium copper containing chromium, zirconium copper containing zirconium, etc., can be used as the precipitation-hardening copper alloy. Furthermore, for example: a precipitation-hardening copper alloy containing nickel, silicon, and chromium; a precipitation-hardening copper alloy containing nickel, silicon, and zirconium; a precipitation-hardening alloy containing nickel, silicon, chromium, and zirconium; a precipitation-hardening copper alloy containing chromium and zirconium; etc., can be applied.

Additionally, multiple types of raw material powders, e.g., a first raw material powder and a second raw material powder can be mixed to form the valve seat films 16b and 17b. In this case, for the first raw material powder it is preferable to use a metal that is harder than aluminum alloys for casting and that yields the heat resistance, abrasion resistance, and thermal conductivity needed for the valve seats; for example, it is preferable to use a precipitation-hardening copper alloy mentioned above. Additionally, a metal harder than the first raw material powder is preferably used as the second raw material powder. For example, an iron-based alloy, a cobalt-based alloy, a chromium-based alloy, a nickel-based alloy, a molybdenum-based alloy, or another alloy, or a ceramic, etc., can be applied as the second raw material powder. Additionally, one of these metals can be used alone, or a combination of two or more can be used as appropriate.

Valve seat films formed by mixing a first raw material powder and a second raw material powder harder than the first raw material powder can have better heat resistance and abrasion resistance than valve seat films formed from only a precipitation-hardening copper alloy. Such effects are achieved presumably because the second raw material powder causes an oxide coating film present on the surface of the cylinder head 12 to be removed and a new interface to be formed by exposure, and adhesiveness between the cylinder head 12 and the metal coating film improves. Such effects are also presumably because adhesiveness between the cylinder head 12 and the metal coating film are improved by an anchor effect brought about by the second raw material powder being embedded in the cylinder head 12. Furthermore, such effects are presumably because when the first raw material powder collides with the second raw material powder, some of the kinetic energy thus produced is converted to heat energy or some of the first raw material powder plastically deforms, and the heat produced by this process further promotes precipitation hardening in some of the precipitation-hardening copper alloy used as the first raw material powder.

In the cold spray device 2 of the present embodiment, the cylinder head 12 in which the valve seat films 16b and 17b are formed is secured to a pedestal 45, and the tip end of the nozzle 23d of the spray gun 23 is rotated along the annular edge parts of the openings 16a and 17a of the cylinder head 12, whereby raw material powder is sprayed. The cylinder head 12 is not caused to rotate and therefore does not need to occupy a large space, and the spray gun 23 has a smaller moment of inertia than the cylinder head 12 and therefore has exceptional rotational transient characteristics and responsiveness. However, because a high-pressure pipe (high-pressure hose) constituting the working gas line 21b is connected to the spray gun 23 as shown in FIG. 3, there is a possibility that the rotational transient characteristics and responsiveness will be impeded by deformation rigidity due to twisting of the hose of the working gas line 21b when the spray gun 23 is caused to rotate. In view of this, the rotational transient characteristics and responsiveness are improved by configuring the cold spray device 2 of the present embodiment as shown in FIGS. 4 to 8.

FIG. 4 is a front view of the spray gun 23 of one embodiment of the cold spray device 2 according to the present invention, FIG. 5 is a cross-sectional view along line V-V in FIG. 4, FIG. 6 is a front view of a state in which the spray gun 23 in FIG. 4 is offset, FIG. 7 is a front view of a film formation factory including the cold spray device 2 according to the present invention, and FIG. 8 is a plan view of FIG. 7.

The cylinder head 12, which is a workpiece, is placed in a predetermined orientation on the pedestal 45 of a film formation booth 42 of a film formation factory 4 shown in FIGS. 7 and 8. For example, as shown in FIG. 10, the cylinder head 12 is secured to the pedestal 45 so that the recesses 12b of the cylinder head 12 are at the upper surface, and the pedestal 45 is tilted so that center lines of the openings 16a of the intake ports 16 or center lines of the openings 17a of the exhaust ports 17 are oriented in a vertical direction.

The film formation factory 4 is provided with the film formation booth 42, in which a film formation process is carried out, and a carrier booth 41. A pedestal 45 on which the cylinder head 12 is placed and an industrial robot 25 that holds the spray gun 23 are installed in the film formation booth 42. The carrier booth 41 is provided at the front portion of the film formation booth 42, cylinder heads 12 are carried in and out between the exterior and the carrier booth 41 through a door 43, and cylinder heads 12 are carried in and out between the carrier booth 41 and the film formation booth 42 through a door 44. For example, when the film formation process for one cylinder head 12 is being performed in the film formation booth 42, a cylinder head 12 that has ended the preceding process is carried out to the exterior from the carrier booth 41. Because the film formation process performed by the cold spray device 2 involves noise produced by supersonic shock waves, scattering of raw material powder, etc., the carrier booth 41 is installed and the film formation process is performed with the door 44 closed, whereby other operations can be performed simultaneously with the film formation process, such as carrying out a processed cylinder head 12 and carrying in a to-be-processed cylinder head 12.

The spray gun 23 is rotatably mounted on a base plate 26 secured to a hand 251 of the industrial robot 25 installed in the film formation booth 42 of the film formation factory 4 shown in FIGS. 7 and 8. A configuration of the spray gun 23 of the present embodiment is described below with reference to FIGS. 4 to 6. First, as shown in FIG. 4, a bracket 252 is secured to the hand 251 of the industrial robot 25, the base plate 26 is rotatably attached to the bracket 252, and the spray gun 23 is secured to the base plate 26.

More specifically, as shown in FIGS. 4 and 5, the bracket 252 is secured to the hand 251 of the industrial robot 25, a body of a motor 29 is secured to the bracket 252, a drive shaft 291 of the motor 29 is connected to a first base plate 261 via a pulley and a belt (not shown), and the first base plate 261 is caused to rotate relative to the bracket. The motor 29 rotates in two directions over a range of, for example, 360° at maximum. For example, if the drive shaft 291 is caused to rotate 360° clockwise so that the raw material powder is sprayed at the opening portion 16a of one intake port 16, the drive shaft 291 is caused to rotate 360° counterclockwise back to the original position, the drive shaft 291 is again caused to rotate 360° clockwise so that the raw material powder is sprayed at the opening portion 16a of the next intake port 16, and thereafter the same action is repeated.

The base plate 26 is composed of the first base plate 261 and a second base plate 262, and the first base plate 261 and the second base plate 262 are provided so as to be capable of sliding in a direction (the left-right direction in FIG. 4) orthogonal to a rotational axis C via a linear guide 281. An amount by which the second base plate 262 is offset relative to the first base plate 261 is adjusted and a spray diameter D of a film-forming material is set by driving a hydraulic cylinder 282.

A cover 263 is mounted on the second base plate 262 and the spray gun 23 is secured to a lower end part of the cover. The spray gun 23 is secured to the second base plate 262 via the cover 263 so that the spraying direction of the nozzle 23d is directed toward the rotational axis C. Because the second base plate 262 can be offset in relation to the first base plate 261 by the linear guide 281 and the hydraulic cylinder 282 mentioned above, the position of the tip end of the nozzle 23d of the spray gun 23 can be adjusted to be horizontal in relation to the rotational axis C.

Thus, when the position of the tip end of the nozzle 23d is set from being on the line of the rotational axis C shown in FIG. 4 to a position away from the rotational axis C as shown in FIG. 6, the spray diameter D will be smaller should the gun distance be the same. Because the openings 16a of the intake ports 16 are larger in diameter than the openings 17a of the exhaust ports 17, the tip end is in the position on the rotational axis C shown in FIG. 4 when the valve seat films 16b are formed in the openings 16a of the intake ports 16, and the tip end is in the position separated from the rotational axis C shown in FIG. 6 when the valve seat films 17b are formed in the openings 17a of the exhaust ports 17.

The working gas line 21b shown in FIG. 3, which guides high-pressure gas at 3-10 MPa supplied from the compressed gas vessel 21a to the spray gun 23, forms one pipe bundle 20 with other pipes described hereinafter, and hangs down to reach the spray gun 23 from an upper part of the base plate 26 mounted to the hand 251 of the industrial robot 25 as shown in FIG. 7. Near the base plate 26 in this configuration, the working gas line is separably connected via a swivel joint or another rotating coupling 21k, and the heater 21i is provided below the coupling, as shown in FIG. 4. The working gas line 21b shown in FIG. 4, extending from the rotating coupling 21k to the chamber 23a, is configured from a high-pressure hose that can withstand high pressures of 3-10 MPa, and is arranged along the rotational axis C so as to encircle the axis, as shown in FIG. 4. The working gas line 21b can be shaped into, for example, a helix in advance so as to encircle the rotational axis C, but a high-pressure hose that can withstand high pressures of 3-10 MPa is hard and retains shape; therefore, a shape-retaining mold can be provided on the outer periphery so that the high-pressure hose conforms to the helical shape.

The raw material powder supply line 22c, which is shown in FIG. 3 and which guides the raw material powder supplied from the raw material powder supply device 22a to the spray gun 23, is arranged in the periphery of the industrial robot 25 as the pipe bundle 20 shown in FIG. 7, is hung down to the spray gun 23 from the upper part of the base plate 26. Below the base plate 26 in this configuration, the raw material powder supply line 22c is configured in the pipe arrangement including metal pipes and metal couplings and is connected to the chamber 23a of the spray gun 23 as shown in FIG. 4.

The electric power supply wires 21j and 21j, which are shown in FIG. 3 and which guide electric power supplied from the electric power source 21h to the heater 21i, are arranged in the periphery of the industrial robot 25 as the pipe bundle 20 shown in FIG. 7, hung down from the upper part of the base plate 26, and connected to the heater 21i. Additionally, a signal wire 23g that outputs a detection signal from the pressure gauge 23b to a controller (not shown) and a signal wire 23h that outputs a detection signal from the thermometer 23c to a controller (not shown), these signal wires being shown in FIG. 3, are inserted through piping including metal pipes and metal couplings from the chamber 23a of the spray gun 23, and in this state the signal wires are guided from the chamber 23a of the spray gun 23 to the second base plate 262, and along with other components such as the working gas line 21b, the raw material powder supply line 22c, and the electric power supply wires 21j, are arranged in the periphery of the industrial robot 25 from the upper part of the base plate 26.

The introduction pipe 274 and the discharge pipe 275, which are shown in FIG. 3 and which guide the refrigerant supplied from the refrigerant circulation circuit 27 to the nozzle 23d of the spray gun 23, are arranged in the periphery of the industrial robot 25 as the pipe bundle 20 shown in FIG. 7, hung from the upper part of the base plate 26, and connected to the refrigerant introduction part 23e at the tip end of the nozzle 23d and the refrigerant discharge part 23f at the base end of the nozzle 23d. Below the base plate 26 in this configuration, the introduction pipe 274 and the discharge pipe 275 are configured in the piping including the metal pipes and metal couplings and are connected to the nozzle 23d of the spray gun 23, as shown in FIG. 4.

As described above, the working gas line 21b, which is configured from a high-pressure hose that is hard and very stiff against deformation, is arranged such that the rotating coupling 21k thereof is disposed on the line of the rotational axis C as shown in FIG. 4, and below the rotating coupling 21k, the working gas line extends along and encircles the rotational axis C. Other than the working gas line 21b, the electric power supply wires 21j and 21j, the raw material powder supply line 22c, the introduction pipe 274, the discharge pipe 275, and the signal wires 23g and 23h are disposed around the rotational axis C in positions encircling the working gas line 21b, as shown in FIG. 5.

Next, the method for manufacturing the cylinder head 12 provided with the valve seat films 16b and 17b shall be described. FIG. 9 is a flowchart of steps for processing the valve portion in the method for manufacturing the cylinder head 12 of the present embodiment. The method for manufacturing the cylinder head 12 of the present embodiment includes a casting step S1, a cutting step S2, a coating step S3, and a finishing step S4, as shown in FIG. 9. The steps for processing portions other than the valve are omitted for the sake of simplifying the description.

In the casting step S1, an aluminum alloy for casting is poured into a mold in which a sand core has been set, and cylinder head rough material, having intake ports 16, exhaust ports 17, etc., formed in a body section, is shaped by casting. The intake ports 16 and the exhaust ports 17 are formed in the sand core, and recesses 12b are formed in the die. FIG. 10 is a perspective view of a cylinder head rough material 3 shaped by casting in the casting step S1, as seen from a side of an attachment surface 12a for the cylinder block 11. The cylinder head rough material 3 is provided with four recesses 12b, and the recesses 12b each have two intake ports 16 and two exhaust ports 17. The two intake ports 16 and the two exhaust ports 17 of an individual recess 12b merge together in the cylinder head rough material 3, and all communicate with openings provided in both side surfaces of the cylinder head rough material 3.

FIG. 11 is a cross-sectional view of the cylinder head rough material 3 along line XI-XI of FIG. 10, showing an intake port 16. The intake port 16 is provided with a circular opening portion 16a exposed in a recess 12b of the cylinder head rough material 3.

In the next cutting step S2, the cylinder head rough material 3 is subjected to milling by an end mill, a ball end mill, etc., and an annular valve seat portion 16c is formed in the opening portion 16a of the intake port 16 as shown in FIG. 12. The annular valve seat portion 16c is an annular groove constituting a base shape of a valve seat film 16b, and is formed in an outer periphery of the opening portion 16a. In the method for manufacturing the cylinder head 12 of the present embodiment, the raw material powder P is sprayed by cold spraying to form a coating film on the annular valve seat portion 16c, and the valve seat film 16b is formed on the coating film as a foundation. Therefore, the annular valve seat portion 16c is formed to be one size larger than the valve seat film 16b.

In the coating step S3, the raw material powder P is sprayed onto the annular valve seat portion 16c of the cylinder head rough material 3 using the cold spray device 2 of the present embodiment, and the valve seat film 16b is formed. More specifically, in the coating step S3, the cylinder head rough material 3 is secured in place and the spray gun 23 is rotated at a constant speed so that the raw material powder P is blown onto the entire periphery of the annular valve seat portion 16c while the annular valve seat portion 16c and the nozzle 23d of the spray gun 23 are kept at a constant distance in the same orientation (except for the embodiment shown in FIG. 26), as shown in FIG. 13.

The tip end of the nozzle 23d of the spray gun 23 is held in the hand 251 of the industrial robot 25, above the cylinder head 12 secured to the pedestal 45. The pedestal 45 or the industrial robot 25 sets the position of the cylinder head 12 or the spray gun 23 so that a center axis Z of the intake port 16 in which the valve seat film 16b is formed is vertical and is the same as the rotational axis C, as shown in FIG. 4. In this state, a coating film is formed on the entire periphery of the annular valve seat portion 16c due to the spray gun 23 being rotated about the C axis by the motor 29 while the raw material powder P is blown onto the annular valve seat portion 16c from the nozzle 23d.

While the coating step S3 is being carried out, the nozzle 23d introduces the refrigerant supplied from the refrigerant circulation circuit 27 into the flow channel from the refrigerant introduction part 23e. The refrigerant cools the nozzle 23d while flowing from the tip-end side toward the rear-end side of the flow channel formed inside the nozzle 23d. Having flowed to the rear-end side of the flow channel, the refrigerant is discharged from the flow channel by the refrigerant discharge part 23f and recovered.

When the spray gun 23 rotates once about the C axis and the formation of the valve seat film 16b ends, the rotation of the spray gun 23 is temporarily stopped. During this rotation stoppage, the industrial robot 25 moves the spray gun 23 so that the center axis Z of the intake port 16 in which the valve seat film 16b will next be formed coincides with a reference axis of the industrial robot 25. After the spray gun 23 has finished being moved by the industrial robot 25, the motor 29 restarts the rotation of the spray gun 23 and a valve seat film 16b is formed on the next intake port 16. The valve seat films 16b and 17b are hereinafter formed on all of the intake ports 16 and exhaust ports 17 of the cylinder head rough material 3 by repeating this operation. When the spray gun 23 switches between forming a valve seat film on the intake ports 16 and forming a valve seat film on the exhaust ports 17, the tilt of the cylinder head rough material 3 is changed by the pedestal 45.

FIG. 16 is a plan view of the cylinder head rough material 3, depicting an example of movement trajectories MT when the nozzle 23d of the cold spray device 2 moves over the openings of the intake ports 16 and the exhaust ports 17 in the film formation method according to the present invention. The nozzle 23d is moved along the movement trajectories MT shown by the arrows, relative to the openings 16a of the eight intake ports 16 and the openings 17a of the eight exhaust ports 17 of the cylinder head rough material 3 shown in FIG. 16. The following is a description of the movement trajectory MT relative to the intake ports 16, but the movement trajectory relative to the exhaust ports 17 is set in the same manner.

As described above, when the nozzle 23d rotates 360° clockwise in relation to one intake port 16, the nozzle rotates 360° counterclockwise and returns to the original position until moving to the next intake port 16, and rotates 360° clockwise in relation to the next intake port 16 as well. The nozzle 23d sprays raw material powder while rotating 360° clockwise in relation to each of the eight intake ports 16. The trajectory of this circle is referred to as a film formation trajectory T. The film formation trajectory T depicted is a 360° clockwise trajectory, but may be a 360° counterclockwise trajectory.

The movement trajectory MT relative to the eight intake ports 16 is configured from circular film formation trajectories T for each of the annular valve seat portions 16c of the intake ports 16 and connecting trajectories CT by which adjacent circular film formation trajectories T are connected, and the movement trajectory MT is thus a series of continuous trajectories. The nozzle 23d is thus moved along the movement trajectory MT while raw material powder is continuously sprayed without interruption from the nozzle 23d. The circular film formation trajectory for one annular valve seat portion 16c begins from a film formation starting point, moves clockwise or counterclockwise, and then laps at the film formation starting point, this overlapping portion being a film formation finishing point. Specifically, a film formation trajectory T is a trajectory in which a film formation starting point and a film formation finishing point of an annular valve seat portion 16c, which is a film-deposited portion, overlap to form an overlapping portion.

FIG. 17 is an enlarged plan view of a movement trajectory MT for the openings 16a₁to 16a₈of one intake port 16 of FIG. 16, using an arrow to show the trajectory of the relative movement of the nozzle in order from the top, to the middle, and to the bottom. Because the nozzle 23d is caused to rotate clockwise in relation to the annular valve seat portion 16c of the opening portion 16a of this intake port 16, in the movement trajectory MT shown in FIG. 17, from left to right in the top drawing, the nozzle 23d is moved linearly to the annular valve seat portion 16c (P₁→P₂, connecting trajectory CT), and taking this point to be a film formation starting point P₂, the nozzle 23d is caused to rotate clockwise in the circular film formation trajectory T as shown in the middle drawing (P₂→P₃→P₄→P₅). The direction at the film formation finishing point P5, which overlaps the film formation starting point P₂, is changed, and the nozzle 23d is moved rightward in FIG. 17 (P₅→P₆, connecting trajectory CT). In such a movement trajectory MT, there is a first turnback point where the movement speed of the nozzle 23d reaches zero at the film formation starting point P2 of the annular valve seat portion 16c, and there is a second turnback point where the movement speed of the nozzle 23d reaches zero at the film formation finishing point P5. The term “turnback point” refers to a point on the movement trajectory MT where the movement speed of the nozzle 23d reaches zero, and refers to a point where the movement trajectory changes to a right angle or an acute angle (≤90°).

FIG. 18A is a cross-section of a coating film in an overlapping portion when a film has been formed along the movement trajectory MT of a comparative example. At the first turnback point located at the film formation starting point P2, the speed of the nozzle 23d temporarily reaches zero but the raw material powder continues to be sprayed; therefore, the valve seat film 16b1 constituting the first layer will have a steep end part slant S. The symbol θ shall be used to denote the inclination angle of the end part of the coating film relative to the surface of the annular valve seat portion 16c, which is a film-deposited portion, and describing the end part slant S as steep is to say that the inclination angle θ of the end part is in a range near 90°. Cold spraying causes the raw material powder in a solid-phase state to collide with the base material at supersonic speed and plastically deform; therefore, when the second layer is sprayed on the surface of the first layer having a steep end part slant S, the raw material powder of the second layer will not adequately flatten and the internal pore diameter in the valve seat film 16b₂of the second layer will increase. The undesirable increase in porosity due to such inadequate flattening is caused by the steep end part slant S in the valve seat film 16b₁constituting the first layer. In other words, when the circular trajectory T of the annular valve seat portion 16c, which is the film-deposited portion, includes a turnback point in the first layer within the range from the film formation starting point P₂to the film formation finishing point P5 (including the end point), the end part slant S will be steep at the turnback point. However, even if a turnback point is included in the second layer of the overlapping portion, the problem of inadequate flattening does not occur as long as the end part slant S of the valve seat film 16b₁of the first layer is not steep.

In the film formation method of the present embodiment, when a turnback point is included in the first layer of the circular film formation trajectory T, or in other words, when the film formation trajectory T of the parts where a film is formed is a trajectory in which the film formation starting point P₂and the film formation finishing point P5 overlap to form an overlapping portion, the film is formed such that at the film formation starting point P2 of the overlapping portion, the inclination angle θ of the end part of the coating film relative to the surface of the annular valve seat portion 16c, which is a film-deposited portion, is 45° or less as shown in FIG. 18B, and more preferably 20° or less (and at least 0°). FIG. 18B is a cross-section of a coating film in an overlapping portion when a film has been formed along the movement trajectory MT of the present embodiment presented below. Observing the overlapping portion of this annular valve seat portion 16c, the surface of the valve seat film 16b₁of the first layer is flat because the inclination angle θ of the end part is 45° or less. Accordingly, even though the valve seat film 16b₂of the second layer, which is a film formation finishing point, overlaps the valve seat film 16b₁, the raw material powder of the second layer is adequately flattened and the collision direction is substantially perpendicular to the surface of the valve seat film 16b₁of the first layer; therefore, the raw material powder of the second layer is adequately flattened and the internal pore diameter of the valve seat film 16b₂is adequately small.

In order for the film to be formed such that the inclination angle θ of the end part of the coating film of the first layer at the film formation starting point P2 of the overlapping portion is 45° or less as shown in FIG. 18B, and more preferably 20° or less (and at least 0°), examples of means for accomplishing this include: (1) setting the average movement speed of the nozzle 23d in a predetermined range including the film formation starting point P₂lower than the average movement speed of the nozzle 23d in another range; (2) setting the amount of raw material powder sprayed from the nozzle 23d in a predetermined range including the film formation starting point P2 less than the amount sprayed from the nozzle 23d in another range; (3) setting the gun distance of the nozzle 23d in a predetermined range including the film formation starting point P2 greater than the gun distance of the nozzle 23d in another range; and (4) forming a recess in a predetermined range including the film formation starting point P₂in the annular valve seat portion 16c, which is a film-deposited portion. Any one of these means can be used, and any two or more can be used together.

(1) Average Movement Speed of Nozzle

FIG. 19 is a graph of a relationship between the film formation trajectory (nozzle position) and the movement speed of the nozzle 23d, and a relationship between the film formation trajectory (nozzle position) and the average movement speed of the nozzle 23d, in one embodiment of the film formation method according to the present invention. In the single unit of the movement trajectory MT of the nozzle 23d shown in FIG. 17, the connecting trajectory CT from a position P₁to the film formation starting point P₂and a connecting trajectory CT from the film formation finishing point P₅to a position P₆are taught to the industrial robot 25. The film formation trajectory T from the film formation starting point P₂to the film formation finishing point P₅depends on the rotational driving of the spray gun 23 by the motor 29. In the present example, the average movement speed of the nozzle 23d in a predetermined range including the film formation starting point P₂, e.g., from the position P₁to a position P₃is set lower than the average movement speed of the nozzle 23d in another range, e.g., from the position P₃to a position P₄. The average movement speed of the nozzle 23d from the position P₃to the position P₆can be set lower than the average movement speed of the nozzle 23d in another range, e.g., from the position P₃to the position P₄.

In the present example, in a range including the position P₁, the nozzle 23d is moved at a greatest speed v1, decelerated at a high deceleration rate so that the speed reaches zero at the film formation starting point P2, and then accelerated at a great acceleration rate so as to reach a speed v2 lower than v1 just before the position P3, as shown in FIG. 19. The deceleration rate just before the film formation starting point P2 and the acceleration rate immediately after are set to large values so that the time during which the nozzle 23d passes through the range from the position P₁to the position P₃is short. The average speed from the position P₁to the position P₃is thereby greater than the average speed v2 from the position P₃to the position P₄as shown n FIG. 19, and therefore a film can be formed with the inclination angle θ of the end part of the coating film of the first layer at 45° or less in the film formation starting point P₂of the overlapping portion.

(2) Amount of Raw Material Powder Sprayed from Nozzle

FIG. 20 is a graph of a relationship between the amount of raw material powder sprayed from the nozzle 23d and the film formation trajectory (nozzle position) in another embodiment of the film formation method according to the present invention. In the present example, the amount of raw material powder sprayed from the nozzle 23d in a predetermined range including the film formation starting point P₂, e.g., from the position P₁to the position P₃is set less than the amount of raw material powder sprayed from the nozzle 23d in another range, e.g., from the position P₃to the position P₄. The amount of raw material powder sprayed from the nozzle 23d from the position P₄to the position P₆can be set less than the amount of raw material powder sprayed from the nozzle 23d in another range, e.g., from the position P₃to the position P₄.

FIGS. 21-25 are drawings of the specific configuration of the raw material powder supply section 22 for controlling the amount of raw material powder supplied as described above, FIG. 21 being a cross-sectional view of the raw material powder supply section 22, FIG. 22 being a perspective view of the weighing section 22b, and FIG. 23 being cross-sectional view along line XXIII-XXIII of FIG. 22.

The raw material powder supply section 22, as shown in FIG. 21, is provided with a hopper 221 into which raw material powder is loaded, and the weighing section 22b, which weighs the raw material powder from the hopper 221 into different volumes over time. The weighing section 22b is provided with a disc 222, a drive unit 226 that causes the disc 222 to rotate at a constant rotational speed when raw material powder is being supplied, and an annular groove part 223 that is formed in an upper surface of the disc 222 and that receives the raw material powder from the hopper 221. The raw material powder is loaded into the hopper 221 from above, and the raw material powder due to its own weight is received into the annular groove part 223 of the disc 222 of the weighing section 22b.

At the position where the supply of raw material powder falls from the hopper 221 under gravity, there is provided a first scraping member 224 that scrapes away surplus raw material powder by horizontally leveling an open upper edge of the annular groove part 223 when the disc 222 rotates, as shown in FIGS. 22 and 23. Additionally, at the position where the raw material powder received in the annular groove part 223 of the disc 222 is sucked into the raw material powder supply line 22c, there is provided a second scraping member 225 that scrapes away surplus raw material powder by horizontally leveling the open upper edge of the annular groove part 223 when the disc 222 rotates. Due to the first scraping member 224 and the second scraping member 225, the supplied amount of raw material powder weighed by the annular groove part 223 is more accurately weighed and supplied to the spray gun 23 via the raw material powder supply line 22c.

The rotating action of the disc 222 and the relative movement action of the nozzle 23d are synchronized by a controller (not shown) of the cold spray device 2. For example, one unit of the movement trajectory MT of the nozzle 23d corresponds to one rotation of the disc 222, and the disc 222 rotates at a constant speed in synchronization with the movement of the nozzle 23d along one unit of the movement locus MT. In this embodiment, one unit of the movement trajectory MT of the nozzle 23d is a repeating unit in which the film formation process performed on the eight intake ports 16 shown in FIG. 16 is completed by repeating said unit. The disc 222 rotates once in synchronization with the movement of the nozzle 23d along one unit of the movement trajectory MT, whereby the amount of raw material powder supplied with respect to the position of the nozzle 23d is determined by the volume of the annular groove part 223 of the disc 222.

Specifically, the annular groove part 223 of the disc 222 has the same width throughout the entire periphery as shown in FIG. 22, but a depth of a bottom surface of the annular groove part 223 corresponds to one unit of the film formation trajectory T of the annular valve seat portion 16c. For example, assuming that a connecting trajectory CT and a film formation trajectory T for one annular valve seat portion 16c corresponds to one rotation of the disc 222, the depth of the bottom surface once around the annular groove part 223 is formed as shown in FIG. 25. FIG. 24 is a plan view of the shape of the weighing section 22b (disc) corresponding to the movement trajectory MT of FIG. 17, and FIG. 25 is an expanded cross-sectional view along line XXV-XXV of FIG. 24.

The positions in the annular groove part 223 of the disc 222 indicated by the symbols P1 and P6 in FIG. 24 correspond to the positions P1 and P6 of the movement trajectory MT in FIG. 17, the positions in the annular groove part 223 of the disc 222 indicated by the symbols P2 and P5 in FIG. 24 correspond to the film formation starting point P2 and the film formation finishing point P5 of the movement trajectory MT in FIG. 17, and the positions in the annular groove part 223 shown by the symbols P3 and P4, which are clockwise from P2, correspond to the positions P3 and P4 of the movement trajectory MT in FIG. 17. When the nozzle 23d from P1 of the connecting trajectory CT toward the film formation starting point P2, the movement speed of the nozzle 23d approaches 0 as the nozzle approaches the film formation starting point P2 and reaches 0 at the film formation starting point P2. The nozzle 23d then gradually increases in speed, reaches a predetermined speed at the position P3, and from there moves while maintaining a predetermined speed until the position P4. Lastly, the movement speed of the nozzle 23d approaches 0 as the nozzle approaches the film formation finishing point P5 and reaches 0 at the film formation finishing point P5, after which the speed is gradually increased toward the next adjacent annular valve seat portion 16c, up to the position P6.

Thus, when the nozzle 23d is moved along the movement trajectory MT, the movement speed differs depending on the position, and the thickness of the coating film increases in relative fashion in a range where the movement speed is low. Specifically, in the range from the film formation starting point P2 to the position P3 and the range from the position P4 to the film formation finishing point P5 shown in FIG. 24, the thickness of the coating film increases in relative fashion because the movement speed of the nozzle 23d is relatively low. Inasmuch, as shown in the expanded cross-sectional view of FIG. 25, in the range from the position P3 clockwise to the position P4, the depth D1 of the bottom surface of the annular groove part 223 is a constant depth, whereas at the film formation starting point P2 and the film formation finishing point P5, the depth D2 of the bottom surface of the annular groove part 223 is a lesser value than the depth D1.

Preferably, the sum of the supplied amount of raw material powder determined by the volume of the annular groove part 223 in the range from the film formation starting point P2 to the position P3 and the supplied amount of raw material powder determined by the volume of the annular groove part 223 in the range from the position P4 to the film formation finishing point P5, i.e., the supplied amount of raw material powder supplied to an overlapping portion of the coating film, is equal to the supplied amount of raw material powder in the range from the position P3 to the position P4, which is equivalent to the same distance. The thickness of the coating film in an overlapping portion and the thickness of the coating film in other parts are thereby made the same, and it is easy to remove surplus coating film.

[3] Gun Distance of Nozzle

FIG. 26 is a graph of a relationship between gun distance and film formation trajectory (nozzle position) in yet another embodiment of the film formation method according to the present invention. In the present example, the gun distance of the nozzle 23d in a predetermined range including the film formation starting point P2, e.g., from the position P1 to the position P3 is set greater than the gun distance of the nozzle 23d in another range, e.g., from the position P3 to the position P4, as shown in FIG. 26. In addition, the gun distance of the nozzle 23d from the position P4 to the position P6 can be greater than the gun distance of the nozzle 23d in another range, e.g., from the position P3 to the position P4.

The term “gun distance of the nozzle 23d” refers to a linear distance from the tip end of the nozzle 23d to a film-deposited portion, but when raw material powder is sprayed from the nozzle 23d by cold spraying, a coating film is formed in a conical pattern. Accordingly, the amount of raw material powder per unit area decreases commensurately as the gun distance of the nozzle 23d increases, and the thickness of the coating film can therefore be reduced.

[4] Recess in Part where Film is Formed

FIG. 27 is a plan view of an intake port of yet another embodiment of the film formation method according to the present invention, and FIG. 28A is a cross-sectional view along line XXVIII-XXVIII of FIG. 27. In the present example, a recess 16d is formed in a predetermined range including the film formation starting point P2 of the annular valve seat portion 16c, which is a film-deposited portion. A shape of the recess 16d can be a recess curved along the circumferential direction of the annular valve seat portion 16c as shown in FIG. 28A, or can be a recess in which depth increases after the film formation starting point P2 toward the position P3 as shown in FIG. 28B. FIG. 28B is a cross-sectional view along line XXVIII-XXVIII of FIG. 27, showing another example of FIG. 28A.

By forming the recess 16d in a predetermined range including the film formation starting point P2 of the annular valve seat portion 16c, which is a film-deposited portion, the surplus coating film when the valve seat film 16b1 of the first layer is formed is absorbed by the recess 16d as shown in FIG. 28A, and the end part slant S therefore decreases. Additionally, in a recess 16d that is deeper just before the film formation starting point P2 as shown in FIG. 28B, the surplus coating film when the valve seat film 16b1 of the first layer is formed is further absorbed by the recess 16d, and the end part slant S therefore further decreases.

Returning to FIG. 9, in the finishing step S4, finishing is performed on the valve seat films 16b and 17b, and on the intake ports 16 and the exhaust ports 17. In the finishing of the valve seat films 16b and 17b, the surfaces of the valve seat films 16b and 17b are milled using a ball end mill, and the valve seat films 16b are adjusted to a predetermined shape. In the finishing of the intake ports 16, a ball end mill is inserted into the intake ports 16 from the openings 16a, and the inner peripheral surfaces of the intake ports 16 at the sides having the openings 16a are each cut along a processing line PL shown in FIG. 14. The processing line PL is a range in which a surplus coating film SF, which results from the raw material powder P scattering and adhering to the inside of the intake port 16, is formed comparatively thick; i.e., a range in which the surplus coating film SF is formed thick enough to affect the intake performance of the intake port 16.

Thus, through the finishing step S4, surface roughness in the intake ports 16 due to cast-shaping is eliminated, and the surplus coating film SF formed in the coating step S3 can be removed. FIG. 15 shows an intake port 16 after the finishing step S4. As with the intake port 16, a valve seat film 17b is formed in the exhaust port 17 via formation of a small-diameter part in the exhaust port 17 by cast-shaping, formation of an annular valve seat part by cutting, cold spraying on the annular valve seat part, and finishing. Therefore, a detailed description shall not be given for the procedure of forming the valve seat films 17b in the exhaust ports 17.

As described above, in the film formation method using the cold spray device 2 of the present embodiment, the cylinder head rough material 3 having the annular valve seat portions 16c and the nozzle 23d of the cold spray device 2 are moved relative to each other along the film formation trajectory T in which the film formation starting points P₂and the film formation finishing points P₅overlap to form the overlapping portions, and the coating film is formed on the annular valve seat portions 16c while the raw material powder supplied from the raw material powder supply section 22 is sprayed from the nozzle 23d. In this film formation method, the film is formed such that at each of the film formation starting points P₂of the overlapping portions, the inclination angle θ of the end part of the coating film relative to the surface of the annular valve seat portion 16c, which is the film-deposited portion, is 45° or less as shown in FIG. 18B, and preferably 20° or less (and at least 0°). Due to this configuration, even though the valve seat films 16b are overlapped by the valve seat films 16b of the second layers, which are the film formation finishing points, the collision direction is 45° or less relative to the surfaces of the valve seat films 16b of the first layers; therefore, the raw material powder of the second layers is adequately flattened and the internal pore diameters of the valve seat films 16b are adequately small.

In the film formation method using the cold spray device 2 of the present embodiment, the film can be formed such that the inclination angle θ of the end part of the coating film of the first layer at the film formation starting points P₂of the overlapping portions is 45° or less because the average movement speed of the nozzle 23d in predetermined ranges including the film formation starting points P2, e.g., from the positions P₁to the positions P₃, is set lower than the average movement speed of the nozzle 23d in other ranges, e.g., from the positions P3 to the positions P4.

In the film formation method using the cold spray device 2 of the present embodiment, the film can be formed such that the inclination angle θ of the end part of the coating film of the first layer at the film formation starting points P2 of the overlapping portions is 45° or less because the amount of the raw material powder sprayed from the nozzle 23d in predetermined ranges including the film formation starting points P2, e.g., from the positions P1 to the positions P3, is set less than the amount sprayed from the nozzle 23d in other ranges, e.g., from the positions P3 to the positions P4.

In the film formation method using the cold spray device 2 of the present embodiment, the film can be formed such that the inclination angle θ of the end part of the coating film of the first layer at the film formation starting points P₂of the overlapping portions is 45° or less because the gun distance of the nozzle 23d in predetermined ranges including the film formation starting points P₂, e.g., from the positions P₁to the positions P₃, is set greater than the gun distance of the nozzle 23d in other ranges, e.g., from the positions P₃to the positions P₄.

In the film formation method using the cold spray device 2 of the present embodiment, the film can be formed such that the inclination angle θ of the end part of the coating film of the first layer at the film formation starting points P2 of the overlapping portions is 45° or less because the recesses 16d are formed in predetermined ranges including the film formation starting points P2 of the annular valve seat portions 16c, which are the parts where a film is formed.

The annular valve seat portions 16c described above are equivalent to the parts where a film is formed according to the present invention.

Number	Name	Date	Kind
20170057023	Sharp	Mar 2017	A1
20220042177	Shibayama	Feb 2022	A1

Number	Date	Country
3 854 908	Jul 2021	EP
2007-16737	Jan 2007	JP
2015-139725	Aug 2015	JP
2016-171281	Sep 2016	JP
2017022505	Feb 2017	WO

Film formation method

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