This disclosure relates to coating equipment and, more particularly, to a deposition apparatus that facilitates deposition of a coating material onto surfaces of a work piece that are difficult to coat.
Physical vapor deposition (“PVD”) is one common method for coating a work piece, such as a gas turbine engine airfoil. For instance, the coating may be a protective coating or a bond coat for adhesion of an over-coating. One type of PVD process utilizes an electron beam to melt and vaporize a source coating material in a crucible. The vaporized source material deposits onto the substrate. Generally, electron beam PVD and variations of this process, such as electron beam directed vapor deposition (“EB-DVD”), coat surfaces that are in a line-of-sight from the crucible. Surfaces that are not in the line-of-sight of the crucible may not receive as much of the coating material.
An example coating deposition apparatus includes a plurality of mounts that are adapted to mount work pieces at respective work piece locations. A crucible is located adjacent the plurality of mounts for emitting a source coating material. A plurality of gas nozzles are respectively directed at the work piece locations to scatter the emitted source coating material at surfaces of the work pieces that are otherwise difficult to coat.
In another aspect, a coating deposition apparatus includes a fixture having a plurality of mounts that are adapted to mount work pieces at respective work piece locations. A gas supply passage runs within the fixture. A crucible is located adjacent the plurality of mounts for presenting a source coating material. A plurality of gas nozzles is connected with the gas supply passage and respectively directed at the work piece locations.
An example method for use with a coating deposition apparatus includes mounting work pieces on a plurality of mounts at respective work piece locations, emitting a source coating material from a crucible that is adjacent to the plurality of mounts, and emitting gas streams from a plurality of gas nozzles that re respectively directed at the work piece locations to direct the emitted source coating material at the work pieces.
The various features and advantages of the disclosed examples will become apparent to those skilled in the art from the following detailed description. The drawings that accompany the detailed description can be briefly described as follows.
The work pieces 22 may be gas turbine engine components, such as airfoils (e.g., blades or vanes), or other components. As will be described in further detail below, the apparatus 20 may be used to deposit a coating material onto surfaces of the work pieces 22 that are not in a line-of-sight of the emitted source coating material or surfaces that are oriented at a steep angle with regard to the line-of-sight.
The type of coating may be any desired coating that is suitable for vapor deposition, such as a metallic coating or a ceramic coating. For instance, the coating is a metallic bond coat or a ceramic thermal barrier coating that includes gadolinia, zirconia, yttria or combinations thereof.
The coating deposition apparatus 20 generally includes a coating chamber 24 for containing the work pieces 22. The coating chamber 24 may be a vacuum chamber and may include various ports for evacuating the interior or for selectively introducing gases that are to be used in the coating process. One or more gas sources (not shown) may be used to provide a desired flow of oxygen or other gas into the coating chamber 24. A pump (not shown) may also be provided to circulate a coolant, such as water, through walls of the coating chamber 24 to control wall temperature.
The work pieces 22 are mounted on a fixture 26 within a coating zone 28. For instance, the coating zone 28 is the spatial volume where the work pieces 22 will be coated. A crucible 30 is located adjacent the coating zone 28, below the fixture 26 in the illustrated example, to present a source coating material for deposition onto the work pieces 22. In this example, the coating deposition apparatus 20 includes at least one electron beam source 34, such as an electron beam gun, mounted relative to the coating chamber 24. One or more electron beam sources 34 may be used to emit electron beams onto a heat source 36 that contains a media 38 to preheat the work pieces 22 to a desired temperature. The electron beam source 34 may also be used to emit electron beams onto the source coating material 32 to vaporize the coating material 32 to coat the work pieces 22.
The coating deposition apparatus 20 may also include a thermal hood 40 for controlling the temperature within the coating zone 28. A screen 42 is located between the crucible 30 and the thermal hood 40 for limiting deposition of the coating material onto the interior surface of the thermal hood 40.
A pair of opposed laterally extending arms 54a and 54b extend from the sting shaft 52. Each of the laterally extending arms 54a and 54b includes a respective support arm 56a, 56b extending therefrom. The support arms 56a and 56b generally extend along a direction that is parallel to the long axis of the sting shaft.
Each of the support arms 56a and 56b includes mounts 58 that are adapted to hold a work piece 22 in a work piece location 60. In this example, the mounts 58 are located on the interior of the structure formed by the fixture 26. That is, the mounts 58 are interior of the U-shape formed by the laterally extending arms 54a and 54b and support arms 56a and 56b.
The coating deposition apparatus 20 further includes a gas supply passage 62 that runs within the fixture 26. The gas supply passage 62 is connected with a gas source 64, which may be located outside of the coating chamber 24. The gas supply passage 62 runs through the sting shaft 52, laterally extending arms 54a and 54b, and the support arms 56a and 56b. A plurality of nozzles 66 are connected to the gas supply passage 62 and are respectively directed at the work piece locations 60. As an example, the nozzles 66 may be incorporated within the mounts 58 or otherwise located near the work piece locations 60. In the example configuration, the nozzles 66 on the support arm 56a are directed in an opposite direction from the nozzles 66 on the other support arm 56b, which further facilitates scattering the vaporized source material.
Referring to
The nozzles 66 serve to emit a gas stream 74 that is directed at the respective work piece 22 in the work piece location 60. The emitted gas stream 74 changes the path of travel 72 of the vaporized coating material 70 such that the vaporized coating material 70 is redirected along an alternate path, such as paths 72a or 72b and deposits onto surface 76 or surface 78 of the work piece 22. For instance, the surface 76 is a non-line-of-sight surface with regard to line-of-sight to the crucible 30. Surface 78 is an angled surface with regard to the line-of-sight to the crucible 30. The nozzles 66 and the emitted gas stream 74 thereby facilitate the deposition of the coating material onto difficult to coat surfaces and thereby extend the coating capability of a physical vapor deposition process or other similar line-of-sight process.
Although a combination of features is shown in the illustrated examples, not all of them need to be combined to realize the benefits of various embodiments of this disclosure. In other words, a system designed according to an embodiment of this disclosure will not necessarily include all of the features shown in any one of the Figures or all of the portions schematically shown in the Figures. Moreover, selected features of one example embodiment may be combined with selected features of other example embodiments.
The preceding description is exemplary rather than limiting in nature. Variations and modifications to the disclosed examples may become apparent to those skilled in the art that do not necessarily depart from the essence of this disclosure. The scope of legal protection given to this disclosure can only be determined by studying the following claims.
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