Integrated fluidjet system for stripping, prepping and coating a part
10272468 ยท 2019-04-30
Assignee
Inventors
- Mohan M. Vijay (Ottawa, CA)
- Meisheng M. Xu (Ottawa, CA)
- Emilio Panarella (Ottawa, CA)
- Wenzhuo Yan (Ottawa, CA)
- Andrew Hung Tieu (Ottawa, CA)
- Bruce R. Daniels (Ottawa, CA)
Cpc classification
B05B17/0607
PERFORMING OPERATIONS; TRANSPORTING
B25J21/00
PERFORMING OPERATIONS; TRANSPORTING
B05C15/00
PERFORMING OPERATIONS; TRANSPORTING
B05B16/40
PERFORMING OPERATIONS; TRANSPORTING
C25D5/34
CHEMISTRY; METALLURGY
B05B5/032
PERFORMING OPERATIONS; TRANSPORTING
B05B5/08
PERFORMING OPERATIONS; TRANSPORTING
B05B16/20
PERFORMING OPERATIONS; TRANSPORTING
C25D13/22
CHEMISTRY; METALLURGY
B05B1/08
PERFORMING OPERATIONS; TRANSPORTING
C25D5/08
CHEMISTRY; METALLURGY
B05B5/006
PERFORMING OPERATIONS; TRANSPORTING
B05B1/083
PERFORMING OPERATIONS; TRANSPORTING
B05B5/10
PERFORMING OPERATIONS; TRANSPORTING
B05C19/00
PERFORMING OPERATIONS; TRANSPORTING
B05B12/08
PERFORMING OPERATIONS; TRANSPORTING
B08B3/024
PERFORMING OPERATIONS; TRANSPORTING
B05B13/0431
PERFORMING OPERATIONS; TRANSPORTING
B05B5/001
PERFORMING OPERATIONS; TRANSPORTING
B24C5/005
PERFORMING OPERATIONS; TRANSPORTING
C25D15/00
CHEMISTRY; METALLURGY
B05B5/035
PERFORMING OPERATIONS; TRANSPORTING
B25J11/0075
PERFORMING OPERATIONS; TRANSPORTING
B05B17/06
PERFORMING OPERATIONS; TRANSPORTING
C23C18/1806
CHEMISTRY; METALLURGY
C25D5/007
CHEMISTRY; METALLURGY
B05B5/082
PERFORMING OPERATIONS; TRANSPORTING
B24C7/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B05C19/00
PERFORMING OPERATIONS; TRANSPORTING
B05C15/00
PERFORMING OPERATIONS; TRANSPORTING
B05B5/00
PERFORMING OPERATIONS; TRANSPORTING
B05B5/10
PERFORMING OPERATIONS; TRANSPORTING
B05B17/06
PERFORMING OPERATIONS; TRANSPORTING
C25D5/00
CHEMISTRY; METALLURGY
C25D5/34
CHEMISTRY; METALLURGY
C25D15/00
CHEMISTRY; METALLURGY
C25D5/08
CHEMISTRY; METALLURGY
B05B16/40
PERFORMING OPERATIONS; TRANSPORTING
B05B12/08
PERFORMING OPERATIONS; TRANSPORTING
B05B5/16
PERFORMING OPERATIONS; TRANSPORTING
B24C5/00
PERFORMING OPERATIONS; TRANSPORTING
B25J21/00
PERFORMING OPERATIONS; TRANSPORTING
B25J11/00
PERFORMING OPERATIONS; TRANSPORTING
B08B3/02
PERFORMING OPERATIONS; TRANSPORTING
B05B13/04
PERFORMING OPERATIONS; TRANSPORTING
B05B5/08
PERFORMING OPERATIONS; TRANSPORTING
B05B5/035
PERFORMING OPERATIONS; TRANSPORTING
B05B5/03
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An integrated liquidjet system capable of stripping, prepping and coating a part includes a cell defining an enclosure, a jig for holding the part inside the cell, an ultrasonic nozzle having an ultrasonic transducer for generating a pulsed liquidjet, a coating particle source for supplying coating particles to the nozzle, a pressurized liquid source for supplying the nozzle with a pressurized liquid to enable the nozzle to generate the pulsed liquidjet to sequentially strip, prep and coat the part, a high-voltage electrode and a ground electrode inside the nozzle for charging the coating particles, and a human-machine interface external to the cell for receiving user commands and for controlling the pulsed liquidjet exiting from the nozzle in response to the user commands.
Claims
1. A method of stripping, prepping and coating a part, the method comprising: holding the part inside a cell that defines an electrically shielded enclosure, the cell having a door to fully enclose the cell; generating a pulsed liquidjet using an ultrasonic nozzle disposed inside the cell; supplying coating particles to the nozzle; supplying the nozzle with a pressurized liquid to enable the nozzle to generate the pulsed liquidjet to sequentially strip, prep and coat the part; charging the coating particles using a high-voltage electrode and a ground electrode inside the nozzle; stripping the part by controlling the pulsed liquidjet; prepping the part by controlling the pulsed liquidjet; and coating the part by controlling the pulsed liquidjet.
2. The method as claimed in claim 1 further comprising optically inspecting the part to determine when stripping is complete and then automatically switching to prepping.
3. The method as claimed in claim 2 further comprising detecting when prepping is complete and then automatically switching to coating.
4. The method as claimed in claim 3 further comprising detecting when coating is complete.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(33) The present invention provides an integrated system and method for both prepping and coating a part or, alternatively for stripping, prepping and re-coating a part.
(34) In general, and by way of overview, prepping of the surface is first performed using coating particles as disclosed by the applicant in U.S. Pat. No. 8,389,066 B2 issued Mar. 5, 2013) which is hereby incorporated by reference. U.S. Pat. No. 8,389,066 B2 discloses a novel method and system for prepping a surface that uses the same type of particles that are used for coating as blasting particles for first prepping the surface. This technique eliminates many of the disadvantages associated with conventional grit blasting. In the present invention, once the surface has been prepped using coating particles as abrasive particles, the same type of coating particles (which are generally of a smaller mesh size) are used for coating the surface.
(35) Coating is then performed by entraining the coating particles in a high-speed (e.g. supersonic) continuous or pulsed liquidjet or gasjet and by electrostatically charging the surface to be coated as well as the particles for high-speed electro-coating of the surface. In other words, in some embodiments of the invention, the surface is charged to a polarity opposite to that of the particles. The charged particles are made to impact at high velocity on the oppositely charged surface. This creates both mechanical and electronic bonds between the particles and the surface.
(36) The integrated stripping, prepping and coating system enables a novel three-stage method for stripping, prepping and coating a surface of a part or object.
(37) First, if the part to be coated is new, it needs to be prepped before applying the coating. The prepping of the part can be done either with the fluidjet only or by entraining coating particles as the blasting particles (i.e. as the abrasive particles) in the fluidjet to thereby prep the surface to a desired (prescribed or predetermined surface roughness). Second, once the surface has been prepped, the surface is then coated by applying to the surface the same type of particles that were used to prep the surface, i.e. the particles for prepping and coating have the same chemical composition.
(38) Alternatively, if the part is old, that is, has been in service, the residual deteriorated coating needs to be stripped before prepping it to the required specifications. In this case, the three-stage process involves stripping, prepping followed by re-coating of the part. A very important aspect of this novel invention is that all three stages are carried out in one cell. In one embodiment, the coating particles have a diameter greater than 1 micron. The coating particles can be carried by a pulsed waterjet, a continuous waterjet, a pulsed airjet, a continuous airjet or any other pulsed or continuous fluid stream. Because the coating particle is used as the blasting particle, the problems associated with grit-blasting or prepping using a different particle than what is used to coat the surface are eliminated. The prepping stage not only saves time and cost as there is no need to clean or rinse the grit-blasted surface, but also reduces waste and cleanup time (because a different abrasive is not used). Furthermore, this prepping stage enhances the bonding or adhesion of the coating particle to the prepped surface since no foreign abrasive particles are embedded into the surface to be coated. Once prepped, the same type (composition) of coating particles is used to coat the surface. However, the coating particles are electrically charged while the surface is optionally oppositely charged. The electrically charged coating particles are then accelerated to high speeds to strike the surface to be coated.
(39) The coating stage thus combines electrostatic and cold spray techniques. In the electrostatic spraying technique, the particles (powder) which are used as a coating material, are charged positively and are sprayed on the object to be coated, which is charged negatively. However, in the conventional electrostatic powder coating technique, the object is then heated to a very high temperature, so that the particles melt, flow and react chemically to form a coating. In the present invention, the heating process is eliminated by using the cold spray technique. In the cold spray technique, as described above, the particles are accelerated to very high speeds, and when they impact the object to be coated, they impregnate the surface and form purely mechanical bonds. Cold spray is also known in the industry as supersonic particle deposition. Regardless of its name, it is a process of coating a surface in which particles are accelerated to supersonic speeds while entrained in nozzle gas flow and are subsequently deposited by impact onto a surface. In some embodiments, the particles are accelerated in supersonic gasjets, e.g. to velocities up to 500-1000 m/s. As such, the technique may be used for coating soft substrates, for example, coating aluminum alloy parts with tungsten carbide particles. In at least some embodiments of the present invention, the charged particles are propelled to the same magnitudes of speeds as in the cold spray technique. Furthermore, if the fluid jet carrying the charged particles is a pulsed water jet, the impact pressure is the waterhammer pressure which enhances the impregnation of the particles deeper into the substrate (i.e. each subsequent pulse hammers the particles carried by the previous pulses into the surface). However, when the charged particles impregnate the negatively charged object, they form both mechanical and electronic bonds. Therefore, the adhesion of the coating to the substrate will be much stronger than achieved in either the cold spray technique or the electrostatic spray technique. By controlling the voltage difference between the particles and the object and by controlling the speed of the particles, the technique will achieve the same coatings as obtained in any of the thermal spray coating techniques, for example HVOF, without requiring a high-temperature flame.
(40) In one embodiment, for particularly soft surfaces such as aluminum alloys, prepping can be achieved with a pulsed fluidjet without entraining abrasive particles (as disclosed in U.S. Pat. No. 8,550,873, which is hereby incorporated by reference).
(41) In the various embodiments of this invention, which will be described below in greater detail, a pulsed or continuous waterjet or airjet apparatus is used to entrain a coating particle such as, for example, a thermal spray coating particle or other coating particle, that is to be applied to the surface after the surface prepping is complete. By entraining the coating particle into the fluid stream, the coating particle is thus used as an abrasive or blasting particle. In other words, the coating particle and the abrasive particle are the same, or at least highly similar in composition, hardness, granularity, etc. Conventionally, a surface is prepped using an abrasive to produce a desired surface finish or surface roughness. According to SSPC (The Society for Protective Coatings) Pocket Guide to Coating Information (SSPC 01-09), depending on the coating technique and the surface to be coated, various materials such as aluminum oxide (1680-44 microns in size), coal slag (1680-297 microns), copper slag (1680-149 microns), garnet (841-149 microns), glass beads (595-37 microns), silicon carbide (500-63 microns) are employed for prepping the surfaces. This surface finish or surface roughness is typically determined ahead of time by the type of coating particle that is to be applied. Thus, empirically, it is known that optimal particle retention (coating-surface adhesion) is achieved by prepping the surface to within a certain range of surface roughness. In the prior art, the surface is then typically prepped to within that desired range of surface roughness using a standard abrasive particle (blasting particle) such as, for example, grit, garnet or Zeolite. Remnants of foreign blasting particles (abrasive particles) can remain embedded in the atomic matrix of the surface being prepped. These embedded particles can reduce the adhesion of the subsequent coating and/or create local points of weakness leading to unpredictable failure. This problem is obviated by using the coating particle as the blasting particle (abrasive particle), which ensures that no foreign particles remain after prepping. If coating particles are embedded into the atomic matrix of the surface being prepped, then this has no deleterious effect since this particle would have been applied to the surface eventually in the subsequent coating operation. Particles that do not adhere to the surface can be reused or recycled for the subsequent coating stage.
(42) In one embodiment, coating particles of a different granularity (mesh size) can be used to prep the surface prior to application of the coating. For example, the coating particles used for prepping may be larger in mesh size than the coating particles used for coating. Using a larger particle to prep the surface is advantageous as these larger particles more closely resemble the larger grit-blast particles that are traditionally used for surface prepping. Despite their larger mesh size, these larger coating particles tend to become smaller in mesh size as they impinge on the surface and are themselves blasted by subsequently impinging particles. A large proportion of the particles that fail to adhere to the surface tend to be these particles of a reduced size. These reduced-size (non-adhered) particles, however, are ideal for coating operations because coating particles used for actually coating should have a smaller mesh size than those used for blasting/abrasion. Accordingly, these reduced-size particles can be recycled and reused, with optional filtering, for subsequent coating of the prepped surface.
(43) Various embodiments of the present invention will now be described below, by way of example, with reference to the attached drawings.
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(45) In the embodiment shown by way of example in
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(49) As further depicted by way of example in
(50) Particles are directed at a part 22 (or component or substrate) having an exterior or exposed surface. This part 22 may be supported by a workpiece support, holder, clamp or jig 23. A rotating device 24 may be provided to rotate the part 22. The angular velocity (rate of rotation) of the rotating device may be microprocessor-controlled to achieve variable particle deposition rates. The microprocessor may control both the angular velocity of the rotating device and also the metering valve to regulate the rate of particles striking a given unit area of the part.
(51) As further depicted by way of example in
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(53) In one embodiment, the waterjet nozzle 31 may be an ultrasonic waterjet nozzle. A pulsed waterjet nozzle may be used to entrain the coating particles into a pulsed (modulated) waterjet. Pulsed waterjet technology has been developed by Applicant and has been disclosed in U.S. Pat. No. 7,594,614 (Vijay et al.) entitled ULTRASONIC WATERJET APPARATUS and in U.S. Pat. No. 5,154,347 entitled ULTRASONICALLY GENERATED CAVITATING OR INTERRUPTED JET which are hereby incorporated by reference. The fundamentals of the technique are explained using
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(57) Several phenomena accompany the flow of liquid (e.g. water) in insulated tubes. As is known, a triboelectric effect may occur in the flowing liquid (Ravalo, B. et al. Demonstration of the triboelectricity effect by the flow of liquid water in the insulated pipe, Journal of Electrostatics, Vol. 69, 2011). This is simply is the transfer of electric charges from the inside surface of the insulated tube to the flowing liquid. This phenomenon may enhance charging of the coating particles in the liquidjet.
(58) Another phenomenon which may enhance the coating process disclosed in this invention is the so-called electrical double layer formation. This is illustrated in H.sub.3O.sup.++OH.sup.
(59) Once a metallic particle gets into the water, it will be surrounded by some water ions (both positive and negative). Due to the electronic structure of the metallic atoms and the water ions and electro-chemical properties, the water ions of only one electrical polarity (negative or positive ions) is absorbed onto the metallic particle and formed the first layer of surface charge on the surface of the metallic particle or the interface between the water and the particle. This layer is tightly bounded to the surface. Because of the first layer of charge, some counter-ions will be drawn to this layer of ions and form the second electrical layer of the counterpart of the first. The second layer is very loosely connected to the first layer.
(60) The copper particle has 29 electrons outside the nucleus, one electron at the outmost orbit, as shown in
(61) When an electrical field is applied to the metallic particle with electrical double layer, it will behave like a single charged particle and move along the electric field line to the electrode. This phenomenon is called electrophoresis. Under the action of the applied electric field, the ions in the second layer will separate from the particle charged with the opposite electric charges (ions) in the first layer. The ions in the first layer are still tightly bound with the particle and move with it as one. This process is shown in
(62) Based on the observations made in the previous two sections, several embodiments of the nozzle configurations, particle injection systems and charging system are disclosed in the following sections.
(63) In some embodiments of the system, the nozzle is a rotating pulsed fluidjet nozzle comprising an ultrasonic transducer for modulating the fluid stream, the nozzle comprising a rotating head having one or more angled outlets. Rotating head nozzles are useful for prepping and coating internal surfaces such as the inside surface of a tubular structure.
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(65) The operating principle is as follows. The coating particles, accelerated by high-frequency pulses of water, will impact the substrate. In order to generate a uniform mixture of particles in the pulses, air can also be used to inject the particles in the mixing chamber. As disclosed in U.S. Pat. Nos. 8,691,014 and 8,389,066, at a certain speed, which is determined by the pressure, the particles will just prep the surface. When the electrical field is applied, they will enter the material matrix of the substrate and bond electronically with the atoms of the substrate, resulting in a coating with high bond strength.
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(80) The nozzle may be an ultrasonic nozzle having a piezoelectric or magnetostrictive transducer connected to a microtip for modulating the fluidjet. The nozzle is designed for ultrasonically modulating a waterjet or other liquid jet to produce a high-pressure forced pulsed waterjet. Pressurized water is brought into the nozzle at the water inlet. Coating particles are injected or suctioned into the nozzle via two angled particle inlets (suction ports). In this particular configuration, the particle inlets (suction ports) are part of a cylindrical body threaded onto the nozzle as an outer annular component surrounding the portion of the nozzle housing the microtip. A central passageway in the cylindrical body defines a mixing chamber. The mixing chamber is placed downstream of the angled particle inlets (suction ports) to mix the particles with the modulated/pulsed waterjet to create a pulsed slurry (i.e., the slurry consists of water and the particles). The nozzle also includes an outlet (or outlet tube) extending downstream from the mixing chamber inside the cylindrical body.
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(83) This novel integrated system enables stripping, prepping and coating of parts to be refurbished (or, alternatively, prepping and coating of new parts that do not require stripping off of old or worn coatings). Stripping and prepping the surface can be achieved with a pulsed or continuous fluidjet, with or without the abrasives (which may be coating particles). Coating may be accomplished using the novel electro-coating technique. In that instance, coating can be accomplished by a flick of the electrical switch that turns on the electric field to charge the coating particles. In other words, all the operations can be carried out in a single booth or cell such as the one shown by way of example in
(84) From the foregoing, it is apparent that the fluid jet can be a continuous gas jet (e.g. airjet), a pulsed gas jet (e.g. pulsed airjet), a continuous liquid jet (e.g. continuous waterjet) or a pulsed liquid jet (e.g. pulsed waterjet). Regardless of the nature of the fluid jet, the same type of coating particles that are to be subsequently used for coating the surface are first used as the blasting particles (abrasive particles) for prepping the surface. The coating particles are then entrained into the fluid stream, be it liquid or gas, continuous or pulsed, and electrically charged before being accelerated to supersonic speeds for impingement upon the surface to be coated. The particles may be electrically charged prior to entrainment into the fluid jet or after entrainment into the fluid jet.
(85) In the embodiment described above, the part is charged to a polarity opposite to that of the particles. However, in other embodiments, it is possible to charge only the particles. The excess electrons carried by the charged particles will be drawn to the part because the part is grounded, and therefore the part provides a conduit to ground for the electrons to flow.
(86) In some embodiments, the integrated stripping (if required), prepping and coating system includes a computer, microprocessor or microcontroller to control stripping (if required), prepping and coating operations for the system. For example, the microprocessor may initiate stripping and prepping by disabling (switching off) the ionizing electric field, if it is active from a previous cycle of stripping and prepping and coating, and switching the valve(s) of the particle delivery subsystem to the desired particle hopper (where two different mesh sizes of coating particles are used, if required, one for stripping and prepping, the other for coating). The microprocessor may also, for example, control the operation of the pump and/or ultrasonic generator (where a pulsed fluid jet is used). The microprocessor may also, for example, control the valve for regulating the delivery/entrainment of particles into the nozzle.
(87) Determining when stripping, if required, and prepping of the part is complete may be done by the microprocessor (or alternatively by a technician or other user). The microprocessor may determine that stripping and prepping of the part is complete based on a pre-programmed or predetermined surface finish, which is determined by the magnitude of values Ra and/or Rz.
(88) The microprocessor may then automatically switch the system from stripping/prepping mode to coating mode although, in other embodiments, this may be done manually by a technician or other user. For coating, the electric field is activated by switching on the DC power supply. This may be done by the microprocessor. For example, the microprocessor may transmit an activation signal to the switch that turns on the DC power. When coating is complete, the microprocessor sends a deactivation signal to the switch to turn off the electric field. The voltage output of the DC power supply may also be controlled by the microprocessor to provide a variable strength of electric field.
(89) For coating mode, the microprocessor may also be used to switch the particle hopper to entrain a different mesh size of the same type of coating particles. The microprocessor may control the valve to regulate the flow of coating particles into the nozzle. The microprocessor may also control the pump and/or the ultrasonic generator as it may, in certain cases, be desirable to operate the nozzle at a different pressure and/or ultrasonic frequency for stripping, prepping and coating, although the same pressure and ultrasonic frequency may be employed in most cases for stripping, prepping and coating.
(90) The microcontroller (along with the rest of the stripping/prepping/coating system) may be integrated within a fully automated or robotic part refurbishment system capable of receiving a part, stripping the part, prepping the part and then coating the part. In other words, the novel prepping and coating system may be integrated within a comprehensive part refurbishment system that strips an existing coating, preps the surface to a desired surface roughness, and applies a new coating. The coating removal stage may be performed using pulsed or continuous fluid jets, and with or without an abrasive entrained into the fluid jet. The microprocessor can control the fluid jet and any (optional) abrasive entrainment so that the nozzle operates at different sets of operating parameters for stripping, prepping and coating. For example, a first set of operating parameters may be used for coating removal, a second set of operating parameters may be used for surface prepping, and a third set of operating parameters may be used for coating. One single integrated system can thus perform all refurbishment operations needed to completely refurbish a part.
(91) Further aspects of this invention are now described below.
(92) As disclosed in U.S. Pat. No. 7,594,614 (Vijay et al.), almost all parts used in industries require some type of coating to protect against corrosion, wear, etc. An example is the landing gear of an airplane. Generally, the coating of a part is a multi-step process consisting of cleaning it, removing any existing coating, and prepping the surface to required specifications before applying the new coating. Note that cleaning means to removing any dirt, grime or dust without removing the coating. Stripping means removing the coating. Prepping means roughening the surface of the part to a desired Ra and/or Rz value although the surface profile may be characterized using other parameters such as Rmax (largest peak to valley measurement), Rt (maximum peak to lowest valley measurement and Pc (peak count). Coating means applying a particle or powder coating to the part (the main difference between a conventional liquid paint and a powder coating being that the powder coating does not require a solvent to keep the binder and filler parts in a liquid suspension form). Traditionally, prepping the surface is conducted by blasting with abrasive media, which are generally sand particles or other media, which are foreign particles, which may cause damage to the atomic structure of the substrate. As disclosed by Vijay (in U.S. Pat. No. 8,389,066), this problem can be overcome by using the same particles which are used for coating the part. For example, if titanium particles are used for coating the part, then the same particles can be used for prepping the surface. It is also possible to prep the surface with high-frequency pulsed waterjet (US Patent Application Publication 2011/0250361 which is hereby incorporated by reference) or a cavitating waterjet (U.S. Pat. No. 8,297,540 which is hereby incorporated by reference) with or without abrasives in the jet. Furthermore, the operations are normally conducted at different locations. The part may be stripped at one plant, sent to another for prepping and yet another factory for re-coating. This entails increase in the turnaround time (TAT) with considerable amount of money spent on shipping, warehousing and other costs. The purpose of the invention disclosed in this application is to carry out all these processes at a single location resulting in considerable savings in time and cost. Yet another advantage is that the entire technique is environmentally friendly since no waste products are generated.
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(94) Accordingly,
(95) The novel system and method is believed to be a significant improvement over known techniques, specifically overcoming the following deficiencies with prior-art technologies:
(96) (1) Chrome Plating: this technique will not be allowed for coating parts in aerospace industry because the coating process is carcinogenic.
(97) (2) Plasma Spray: Although it is used extensively, this technique has some drawbackshigh temperatures, low bond strength and high porosity. This technique is used for TBC coatings (i.e. ceramic coatings).
(98) (3) Cold Spray: This technique involves propelling the particles at high velocities for impacting the surface to be coated. This is a purely mechanical bonding by impregnation. This is used mainly for coating soft substrates such as aluminum and titanium alloys and is not suitable for high-strength steels.
(99) (4) HVOF (High-Velocity-Oxy-Fuel): Particles are injected basically in a flamejet. The particles melt and form droplets, forming the coating after impacting the surface. The technique will replace chrome plating in all industries. The main drawback is high-temperatures and low deposition efficiency along with very large size.
(100) The novel system and method disclosed herein provides at least two broad inventive concepts: (1) a single integrated system (e.g. single cell, booth, station, etc.) for stripping, prepping and re-coating a part; and (2) coating the part using a novel coating technique that is believed to be significantly better than the cold spray technique and may achieve the same coating characteristics as HVOF without the above-mentioned drawbacks.
(101) Some of the factors used in testing the new technique were:
(102) 1. Bond Strength (Adhesion to the substrate, ): Good bond strength is considered to be 69-MN/m2.
(103) The variables that can be controlled in the method are:
(104) Speed of particles (Vp): Vp is related to the speed of the fluidjet (Vj). If water is used as the medium, since pump pressures up to 100-kpsi (690-MPa) can be used, Vj can be varied quite readily (Note: Vp will always be <Vj, due to frictional effects in the mixing chamber; therefore it is quite important to design a highly effective mixing chamber). The magnitude of Vp will also depend on the type of particle used for coating (say WC as opposed to Cr) because of the variation in density, c (function of size of particles). The jet carrying the particles could be solid core liquid jet, pulsed or continuous, or could be droplet jets. As shown in the design of the nozzles, by proper design of the mixing chamber into which particles are injected, it is possible generate both solid core liquid or droplet jets.
(105) Voltage of the charged particles (Vc): This can also be varied from 5 to Vcmax (e.g. 5-500 kV). However, from the standpoint of safety, the magnitude of Vc must be as low as possible, which can be accomplished by increasing Vj. Also, since the bonding of the particles to the substrate is both electronic and mechanical, the bond strength would be significantly better than cold spray.
(106) Standoff Distance (Sd): This is another important variable to control the bond strength, thickness and area of coating and deposition efficiency. For any given combination of the type of coating particles and the part to be coated, it is possible to achieve desired uniform thickness of the coating, area of coating and the bond strength by a proper set of Vj, Vc and Sd and frequency (f), if pulsed fluidjets are employed.
(107) 2. Surface Profile (Prepping): Bond strength is known to be a function of surface profile. Since we are using particles for coating, the same particles can be used for prepping (AFPWJ), if it is not possible to prep with the fluidjet only, pulsed or continuous. Although the values of Ra (rms value of the surface roughness) and Rz (peak to valley of the surface roughness; ASME B46.1-2002), are used to measure the quality of the prepped surface, Rz appears to be the determining factor for strength of the bond. Therefore, , the bond strength of the coating is a function of Vj which propels the particles at a speed of Vp, Vc, Sd, Rz, and c. The coating thickness on the other hand, depends on the number of passes of the fluidjet nozzle over the surface to be quoted. For example, in the HVOF technique the magnitude of the thickness of coating per pass of the flame jet over the surface is of the order of 0.0005-in. In the novel coating technique proposed in this application, it is possible to achieve twice or three times the coating thickness per pass as the technique has, in addition to the fluidjet properties, the voltage.
(108) Nozzle embodiments for coating the part are shown by way of example in
(109) To summarize, the present invention provides two broad inventive aspects: (1) a single integrated stripping, prepping and coating system and its related method and (2) an electrostatic (electric field) coating technique that harnesses the benefits of high-speed continuous or pulsed fluidjets. The novel high-speed fluidjet electrostatic (electric field) coating technique may be used in the integrated stripping, prepping and coating system and method or it may be used alone (i.e. outside the context of the integrated booth). Likewise, in another embodiment, the single integrated stripping, prepping and coating system may use a cold-spray coating technique instead of the electrostatic technique. The novel integrated coating system provides a one-stop apparatus enabling a part to be stripped, prepped and then coated using the same system (e.g. the same booth, cell or station) without having to transport or move the part to another location or, in some cases, without even having to re-remount or re-jig the part on the turntable or jig within the cell, booth or station. The single integrated system, in the illustrated embodiment, is a single booth or station having preferably a full sound-proofed enclosure inside which the part remains for the entire process of stripping, prepping and coating, a robotically mounted nozzle that performs all stripping, prepping and coating processes, and a single electrical power supply for the station. The cell includes a door to access the turn table or jig for installing and removing the part. The cell may have a window to observe operations from the exterior of the cell. The cell is preferably a water-proof enclosure formed as a Faraday cage and preferably includes an exhaust system for exhausting air or moisture from the cell. The exhaust system or a separate cooling system may be used to cool the Faraday cage, the high-voltage generator or other equipment that generates heat. In other words, the single integrated station performs all stripping, prepping and coating operations using a fluidjet from a robotically controlled nozzle. In a best mode of implementing the technology, the system strips the part using a forced pulsed waterjet and preps the part with the forced pulsed waterjet entraining coating particles as abrasive particles. Coating is then performed by activating the electric field so that the forced pulsed waterjet carries electrically charged coating particles to the part. In this implementation, the pressure, standoff distance, ultrasonic frequency remain the same for all three steps; however, in other implementations, the system may vary these operating parameters to optimize each of the stripping, prepping and coating steps. Although the operating parameters in most embodiments remains constant during a particular step, the system in another embodiment may vary the operating parameters within a particular step, e.g. it may be desirable to augment the electric field as coating progresses.
(110) In one embodiment, the same type (i.e. same chemical composition) of coating particles that are used for coating the surface are also used for prepping the surface. In the prepping stage, uncharged coating particles are entrained into the high-speed continuous or pulsed fluid jet to prep the surface to the prescribed surface roughness. Subsequently, in the coating stage, the same type of coating particles are electrically charged and driven at high speed at the prepped surface of the part to thereby coat the part.
(111) The stripping, prepping and coating methods and processes may be performed in response to user commands (user input) received from an operator, e.g. via the HMI. Alternatively, a series of sequential commands may be programmed by user input. In a further implementation, an automated system may automatically detect when stripping of the part is complete using a machine vision subsystem that performs optical inspection of the part and then automatically switches to prepping mode. Detecting that stripping (coating removal) is done may be based on sensing the color of the part and/or the surface roughness by measuring Ra and/or Rz and comparing to a predetermined range of acceptable Ra/Rz values. Likewise, the automated system may automatically detect when prepping is complete. For detecting that prepping is done, the system uses the machine vision subsystem. by measuring Ra/Rz and comparing to a predetermined range of target Ra/Rz values. If the measured Ra/Rz is within the predetermined range, then the system considers prepping complete and then automatically switches to coating mode. The automated system may automatically detect when coating is complete using the machine vision subsystem. The system may then notify the user that the process is has been completed. The machine vision subsystem may include a CCD or CMOS sensor (or a group of sensors) coupled to a microscope that provides data to a microprocessor running a machine vision algorithm to evaluate surface texture. Another optical inspection technique involves directing a laser at the surface and capturing the reflected light to evaluate the surface roughness (e.g. U.S. Pat. Nos. 4,334,780, 5,585,921, 5,436,645, and 7,184,138, which are hereby incorporated by reference). The automated system may have a processor or central processing unit (CPU) coupled to a memory for executing control software that receives user input and/or machine vision (optical inspection) data and sets and/or dynamically adjusts operating parameters (e.g. electric field voltage, fluid pressure, coating particle metering rate, standoff distance, applied magnetic field, applied heat) to provide a user-specified surface finish or roughness, e.g. a specified Ra or Rz value. The memory may store a database of desired Ra or Rz values for different materials, applications and coatings. Therefore, the user may enter the material type, application or type of part (e.g. landing gear) and the desired coating. The automated system may compute the target Ra or Rz value and then perform the stripping, prepping and coating to achieve the target Ra or Rz value.
(112) It is to be understood that the singular forms a, an and the include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to a device includes reference to one or more of such devices, i.e. that there is at least one device. The terms comprising, having, including, involving, entailing and containing are to be construed as open-ended terms (i.e., meaning including, but not limited to,) unless otherwise noted. All methods described herein can be performed in any suitable order unless otherwise indicated herein or otherwise clearly contradicted by context. The use of examples or exemplary language (e.g., such as) is intended merely to better illustrate or describe embodiments of the invention and is not intended to limit the scope of the invention unless otherwise claimed.
(113) While several embodiments have been provided in the present disclosure, it should be understood that the disclosed systems and methods might be embodied in many other specific forms without departing from the spirit or scope of the present disclosure. The present examples are to be considered as illustrative and not restrictive, and the intention is not to be limited to the details given herein. For example, the various elements or components may be combined or integrated in another system or certain features may be omitted, or not implemented.
(114) In addition, techniques, systems, subsystems, and methods described and illustrated in the various embodiments as discrete or separate may be combined or integrated with other systems, modules, techniques, or methods without departing from the scope of the present disclosure. Other items shown or discussed as coupled or directly coupled or communicating with each other may be indirectly coupled or communicating through some interface, device, or intermediate component whether electrically, mechanically, or otherwise. Other examples of changes, substitutions, and alterations are ascertainable by one skilled in the art and could be made without departing from the spirit and scope disclosed herein.
(115) Accordingly, the embodiments of the present invention described above are intended to be exemplary only. As will be appreciated by those of ordinary skill in the art, to whom this specification is addressed, many variations, modifications, and refinements can be made to the embodiments by using the inventive concepts presented herein. The scope of the exclusive right sought by the applicant is therefore intended to be defined solely by the appended claims.