Airfoils and other components in a turbine section of a gas turbine engine are typically formed of a superalloy and may include thermal barrier coatings to extend temperature capability and lifetime. Ceramic materials, such as monolithic ceramics, ceramic matrix composites, and combinations of these, are under consideration to replace superalloys. Among other attractive properties, ceramic materials have high temperature resistance. Ceramic materials, however, typically cannot be directly substituted for a superalloy. Rather, there are manufacturing and design factors that are unique to ceramics and which challenge practical implementation.
A method for machining a ceramic workpiece according to an example of the present disclosure includes providing a sonotrode that has a transducer and a horn arranged along an axis. The horn has helical slots and terminates at a tip. The tip is brought into proximity of the ceramic workpiece and an abrasive media is provided to a work zone around the tip. The transducer produces ultrasonic vibration that axially propagates down the horn and causes axial vibration at the tip. The helical slots convert a portion of the axial vibration to torsional vibration at the tip. The axial vibration and the torsional vibration cause the abrasive media to abrade the ceramic workpiece in the work zone and thereby remove a localized portion of the ceramic workpiece.
In a further embodiment of any of the foregoing embodiments, the horn includes a first section that tapers and a second section that has a uniform cross-section, and the helical slots are on the second section.
In a further embodiment of any of the foregoing embodiments, the second section is cylindrical and has a solid core.
In a further embodiment of any of the foregoing embodiments, the second section has a diameter and each of the helical slots has a constant depth, and a ratio of the diameter to the constant slot depth is 5:1 to 10:1.
In a further embodiment of any of the foregoing embodiments, the second section has a diameter and each of the helical slots has a slot length, and a ratio of the diameter to the slot length is 1:1 to 1:4.
In a further embodiment of any of the foregoing embodiments, each of the helical slots has a constant depth and a slot length, and a ratio of the slot length to the constant slot depth is 5:1 to 20:1.
In a further embodiment of any of the foregoing embodiments, the second section has a diameter and each of the helical slots has a slot length and a constant slot depth, and a ratio of the slot length to the constant slot depth divided by the diameter is 1:1 to 1:2.
In a further embodiment of any of the foregoing embodiments, each of the helical slots defines a first slot end that is distal from the tip and a second slot end that is proximal to the tip, the first slot ends are located at a first common axial position, and the second slot ends are located at a second common axial position.
In a further embodiment of any of the foregoing embodiments, the second common axial position is no more than 12.7 millimeters from the tip.
In a further embodiment of any of the foregoing embodiments, the first slot end and the second slot end are circumferentially offset by 45° to 135°.
In a further embodiment of any of the foregoing embodiments, the horn includes a first section that tapers and a second section that has a uniform cross-section, and the helical slots are on the first section.
In a further embodiment of any of the foregoing embodiments, each of the helical slots defines an angle of 30° to 60° with the axis.
In a further embodiment of any of the foregoing embodiments, the horn is a step horn.
In a further embodiment of any of the foregoing embodiments, the ceramic workpiece is a ceramic matrix composite.
An ultrasonic machining system according to an example of the present disclosure includes a sonotrode that has a transducer and a horn arranged along an axis. The horn has helical slots and terminates at a tip. Upon operation, with the tip in proximity of a ceramic workpiece, the transducer produces ultrasonic vibration that axially propagates down the horn and causes axial vibration at the tip. The helical slots convert a portion of the axial vibration to torsional vibration at the tip, and the axial vibration and the torsional vibration cause an abrasive media in a work zone around the tip to abrade the ceramic workpiece and thereby remove a localized portion of the ceramic workpiece.
In a further embodiment of any of the foregoing embodiments, the horn includes a first section that tapers and a second section that has a uniform cross-section, and the helical slots are on either the first section or the second section.
In a further embodiment of any of the foregoing embodiments, the helical slots are on the second section, the second section has a diameter, each of the helical slots has a constant depth, each of the helical slots has a slot length, a ratio of the diameter to the constant slot depth is 5:1 to 10:1, and a ratio of the diameter to the slot length is 1:1 to 1:4.
In a further embodiment of any of the foregoing embodiments, a ratio of the slot length to the constant slot depth is 5:1 to 20:1.
In a further embodiment of any of the foregoing embodiments, each of the helical slots defines a first slot end that is distal from the tip and a second slot end that is proximal to the tip, the first slot ends are located at a first common axial position, and the second slot ends are located at a second common axial position.
In a further embodiment of any of the foregoing embodiments, the second common axial position is no more than 12.7 millimeters from the tip, the first slot end and the second slot end are circumferentially offset by 45° to 135°, and each of the helical slots defines an angle of 30° to 60° with the axis.
The present disclosure may include any one or more of the individual features disclosed above and/or below alone or in any combination thereof.
The various features and advantages of the present disclosure 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.
One challenge to implementing ceramic materials in place of superalloys is that ceramic materials must be processed differently than superalloys. The processes used to form ceramic materials into the desired geometry of a functional component have unique limitations. For instance, for a superalloy, cooling holes, slots, and the like can be formed during casting or, for relatively small dimensions, by precision machining after casting. Ceramic materials, however, are hard and brittle in comparison to superalloys. As a result, there is considerable difficulty in efficiently machining holes, slots, or other small features, and doing so with a desired degree of accuracy. Ultrasonic machining (“USM”) is one technique that is under consideration for forming these features. USM generally involves mechanical vibration at approximately 20 kHz or more in the presence of an abrasive media to cause removal of material. When used on ceramics, however, USM yields low material removal rates that are insufficient for practical implementation on ceramics. In this regard, as will be discussed herein, the present disclosure provides a method and system for USM that facilitates increased material removal rates on ceramic materials.
The horn 24 is mechanically coupled to the transducer 22 and includes several sections. As shown, the horn 24 is a step horn, although it is to be understood that the type of horn is not necessarily limited to step horns. The horn 24 includes a first section 26 and a second section 28. A least a portion of the first section 26 tapers in cross-section, to focus the vibration. In the illustrated example, the initial portion of the first section 26 adjacent to the transducer 22 is cylindrical but then transitions to conical. The second section 28 has a uniform cross-section and terminates at a tip 30. In this example, the second section 28 is cylindrical. Both the first section 26 and the second section 28 are solid and may be formed from an alloy or steel, such as but not limited to an aluminum alloy or steel.
The horn 24 further includes helical slots 32. In this example, the helical slots 32 are on the second section 28. The helical slots 32 serve to convert a portion of the axial vibration (V1) to torsional vibration V2, while limiting excitation of undesirable bending modes. The degree and manner to which the helical slots 32 do this can be controlled via the slot geometry.
As shown in representative
As also shown in
In one example, a ratio of the diameter D to the constant slot depth d is 5:1 to 10:1. In a further example, a ratio of the diameter D to the slot length L is 1:1 to 1:4. In a further example, a ratio of the slot length L to the constant slot depth d is 5:1 to 20:1. In a further example, a ratio of the slot length L to the constant slot depth d divided by the diameter D is 1:1 to 1:2. In a further example, each of the slots 32 has an angle G with respect to the axis A that is from 30° to 60°. In a further example of any of the above examples, the first slot end 32a and the second slot end 32b are circumferentially offset by 45° to 135°. In a further example of any of the above examples, the second common axial position A2 is also no more than 12.7 millimeters from the tip.
The sonotrode 20 with the above features, or combinations thereof, facilitates adaptation of USM for the machining of ceramic material. For instance, most of the material removal is due to the axial vibration V1. Therefore, the portion of the axial vibration V1 that is converted into the torsional vibration V2 can be limited via the above prescribed ranges. Moreover, the cycles of vibration should be in sync such that the peak amplitude of the axial vibration V1 coincides with the peak amplitude of torsional vibration V2. Also, the torsional vibration V2 can be primarily induced at or near the tip 30 by placing the slots 32 near the tip 30 per the above range. In one alternative shown in
With the tip 30 in proximity of the ceramic workpiece 40, the transducer 22 (
The tip 30 of the sonotrode 20 can be advanced into the ceramic workpiece 40 as material is removed in order to form a deeper hole and/or translated along the surface of the ceramic workpiece 40 to produce a slot. Additionally, a mass element 25 (
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 this disclosure. The scope of legal protection given to this disclosure can only be determined by studying the following claims.
The present disclosure claims priority to U.S. Provisional Application No. 63/281,156 filed Nov. 19, 2021.
Number | Date | Country | |
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63281156 | Nov 2021 | US |