Embodiments are generally related to SRF (Superconducting Radio Frequency) cavities utilized in linear accelerator devices and systems. Embodiments additionally relate to SRF linear accelerators that employ multicell cavities. Embodiments further relate to the use of pressurized balloons in multicell cavities in SRF applications.
Linear accelerator devices use intense radio frequency electromagnetic fields to accelerate the speed of particles to create beams used for a variety of applications. These applications include driving industrial processes, security & imaging applications, food and medical sterilization, medical treatments, isotope creation and physics research. SRF (Superconducting Radio Frequency) technology allows for the construction of linear accelerators that are both compact and efficient at using “wall plug” electrical power to create a particle beam.
SRF accelerating cavities are commonly used in linear accelerators or particle accelerators. Due to their very small RF losses, much higher acceleration efficiencies, and higher continuous wave (CW) accelerating fields than normal conducting cavities, SRF cavities are now considered the device of choice for many of today's leading applications in high energy and nuclear physics, including energy recovery linear accelerators (ERLs), linear colliders, neutrino factories, spallation neutron sources, and rare isotope accelerators. These projects place enormous demands not only on advances in beam performance, but also on more reliable and economic methods for fabrication, assembly, and operation.
Some SRF linear accelerators may employ the use of multicell cavities rather than simply a single cavity. Multicell cavities must meet certain requirements to operate properly in a particle accelerator in terms of resonance frequency, field flatness and eccentricity. Cavities are typically tuned to meet these requirements by plastic deformation. Tuning must be accomplished before welding a helium vessel to the bare cavity when there is access to the cavity's cells. Dressed cavities, however, can become detuned during the preparation, testing, and qualification process, which basically render them unusable for cryomodules assembly. Currently, a straightforward process does not exist for tuning dressed cavities other than cutting the helium vessel to access the outer surface of a cavity cell, then tune the bare cavity and dress it back. This typically has a significant impact on the cost and the schedule of large-scale particle accelerator projects, which can include, for example, hundreds of cavities.
The following summary is provided to facilitate an understanding of some of the innovative features unique to the disclosed embodiments and is not intended to be a full description. A full appreciation of the various aspects of the embodiments disclosed herein can be gained by taking the entire specification, claims, drawings, and abstract as a whole.
It is, therefore, one aspect of the disclosed embodiments to provide for an improved SRF linear accelerator method and system.
It is another aspect of the disclosed embodiments to provide for a noninvasive tuning method and system capable of handling dressed cavities in an SRF linear accelerator without removing an associated helium vessel.
It is a further aspect of the disclosed embodiments to provide for an SRF linear accelerator tuning method and system that relies on plasticity deforming of a multicell cavity by introducing customized balloons and then pressurizing such balloons as targeted cells while applying a global force on the cavity flanges.
It is a further aspect of the disclosed embodiments to implement an SRF linear accelerator system in which the aforementioned pressurized balloons localize the plastic deformation to targeted cells using prescribed values of both global force and balloon pressure.
The aforementioned aspects and other objectives and advantages can now be achieved as described herein. Methods and systems are disclosed for non-invasively tuning dressed multicell cavities. In general, a multicell cavity can be plastically deformed as result of introducing a customized balloon to a cavity and then pressurizing the balloon to a targeted cell while applying a global force on the cavity flanges. The pressurized balloons localize the plastic deformation to the targeted cells using prescribed values of both global force and balloon pressure.
The accompanying figures, in which like reference numerals refer to identical or functionally-similar elements throughout the separate views and which are incorporated in and form a part of the specification, further illustrate the present invention and, together with the detailed description of the invention, serve to explain the principles of the present invention.
The particular values and configurations discussed in these non-limiting examples can be varied and are cited merely to illustrate one or more embodiments and are not intended to limit the scope thereof.
Subject matter will now be described more fully herein after with reference to the accompanying drawings, which form a part hereof, and which show, by way of illustration, specific example embodiments. Subject matter may, however, be embodied in a variety of different forms and, therefore, covered or claimed subject matter is intended to be construed as not being limited to any example embodiments set forth herein; example embodiments are provided merely to be illustrative. Likewise, a reasonably broad scope for claimed or covered subject matter is intended. Among other things, for example, subject matter may be embodied as methods, devices, components, or systems/devices. Accordingly, embodiments may, for example, take the form of hardware, software, firmware or any combination thereof (other than software per se). The following detailed description is, therefore, not intended to be interpreted in a limiting sense.
Throughout the specification and claims, terms may have nuanced meanings suggested or implied in context beyond an explicitly stated meaning. Likewise, phrases such as “in one embodiment” or “in an example embodiment” and variations thereof as utilized herein do not necessarily refer to the same embodiment and the phrase “in another embodiment” or “in another example embodiment” and variations thereof as utilized herein may or may not necessarily refer to a different embodiment. It is intended, for example, that claimed subject matter include combinations of example embodiments in whole or in part.
In general, terminology may be understood, at least in part, from usage in context. For example, terms, such as “and”, “or”, or “and/or” as used herein may include a variety of meanings that may depend, at least in part, upon the context in which such terms are used. Typically, “or” if used to associate a list, such as A, B, or C, is intended to mean A, B, and C, here used in the inclusive sense, as well as A, B, or C, here used in the exclusive sense. In addition, the term “one or more” as used herein, depending at least in part upon context, may be used to describe any feature, structure, or characteristic in a singular sense or may be used to describe combinations of features, structures, or characteristics in a plural sense. Similarly, terms such as “a”, “an”, or “the”, again, may be understood to convey a singular usage or to convey a plural usage, depending at least in part upon context. In addition, the term “based on” may be understood as not necessarily intended to convey an exclusive set of factors and may, instead, allow for existence of additional factors not necessarily expressly described, again, depending at least in part on context. Additionally, the term “step” can be utilized interchangeably with “instruction” or “operation”.
Unless defined otherwise, all technical and scientific terms used herein have the same meanings as commonly understood by one of ordinary skill in the art. As used in this document, the term “comprising” means “including, but not limited to.” The term “at least one” conveys “one or more”.
The cylindrically shaped body of the helium vessel 13 further engages with a cooling cylinder 12. Each of the cavities 14 may be composed of a metallic material that is superconducting at a cavity operating temperature. This material may constitute the entire cavity or be a coating on an inner surface of each linear accelerator cavity. In one example embodiment, each cavity of the multicell cavities 14 may comprise pure niobium. In other example embodiments, each cavity may be, but not limited to, for example, a niobium, an aluminum or a copper cavity coated in niobium-tin (Nb3Sn) or other superconducting materials. The cavities are associated with one or more helium vessels. As will be discussed in greater detail herein, the disclosed embodiments allow for the non-invasive tuning of dressed cavities without removing the helium vessel(s) such as the helium vessel 13.
It should be appreciated that although the embodiments discussed herein generally involve the use of a hollow structure such as the aforementioned cavity, the disclosed embodiments are suitable for locally deforming any hollow structure that is not accessible from the outside of the cavity for one reason or another, and which is composed of multiple segments. Such a hollow structure may be a cavity, a filter, and so on.
It should be appreciated that the number of multicell cavities shown in
Note that a non-limiting example of an SRF linear accelerator system in which the disclosed embodiments can be implemented is disclosed in U.S. Patent Application Publication No. 20170094770 entitled “Compact SRF Based Accelerator,” which published on Mar. 30, 2017 to Robert Kephart and is incorporated herein by reference in its entirety. It should be appreciated that the SRF linear accelerator system disclosed in non-limiting U.S. Patent Application Publication No. 20170094770 is but one example of a compact SRF based linear or particle accelerator in which the disclosed methods and systems can be utilized. The disclosed devices, systems and techniques can be implemented in the context of other types and sizes of SRF based linear or particle accelerators.
The graphs shown in
Dressed cavities can become accidentally deformed during the aforementioned qualification and testing process. As discussed previously herein, there currently does not exist a straightforward device and/or a technique that effectively tunes dressed cavities other than cutting the vessel and then tuning the bare cavity and dressing it back. This conventional approach typically has a significant impact on cost and schedule.
The graph 70 shown in
The basic concept behind the disclosed embodiments is thus to use pressurized balloons from cavity's inside surface to apply forces on targeted cells and localize plastic deformation. The target cell thus gets plastically deformed and the other cells remain in the linear elastic region because of lower stresses.
It can be appreciated that the disclosed balloon technique has been implemented to successfully bring an LCLS-II multicell elliptical cavity back to specification after being accidentally detuned during a pressure test. The cavity was also qualified after balloon tuning with no degradation in quality factor and gradient, proving that the used balloon material can be cleaned with residuals on the inner cavity surface.
Based on the foregoing, it can be appreciated that a number of example embodiments (both preferred and alternative embodiments) are disclosed herein. In a preferred embodiment, for example, a system for radio frequency tuning of hollow structures can be configured to include at least one pressurized balloon located in at least one targeted cell of a hollow structure of a device having a plurality of hollow structures and a plurality of respective cells. The at least one pressurized balloon is targeted to the at least one targeted cell so as to localize plastic deformation to the at least one targeted cell using prescribed values of global force and balloon pressure with respect to the at least one pressurized balloon, thereby facilitating a noninvasive tuning of the at least one targeted cell of the hollow structure.
In some example embodiments, the aforementioned device can be implemented as or in the context of an SRF (Superconducting Radio Frequency) cavity for use in a particle accelerator.
In still other example embodiments, the aforementioned pressurized balloon can be configured as a rubberized/nylon balloon. Such a pressurized balloon can be pressurized after being introduced to the targeted cell of the hollow structure. The targeted cell is plastically deformed while other cells remain in an elastic region because of a lower stress. The hollow structure generally comprises a cavity. In some example embodiments, this cavity can be composed of a multicell elliptical cavity among a plurality of adjacent cavities.
In other example embodiments, this cavity may be configured as a dressed multicell cavity among a plurality of adjacent cavities. In still other example embodiments, the hollow structure can be configured as a filter.
In still another example embodiment, a system for radio frequency tuning of hollow structures, can be configured, which includes at least one pressurized balloon located in at least one targeted cell of a hollow structure of a device comprising an SRF cavity for use in a particle accelerator and having a plurality of hollow structures and a plurality of respective cells, wherein the at least one pressurized balloon is targeted to the at least one targeted cell so as to localize plastic deformation to the at least one targeted cell using prescribed values of global force and balloon pressure with respect to the at least one pressurized balloon, thereby facilitating a noninvasive tuning of the at least one targeted cell of the hollow structure.
In yet another example embodiment, a method for radio frequency tuning of hollow structures can be implemented. Such a method can include, for example, steps, operations or instructions, such as locating one or more pressurized balloons in one or more targeted cells of a hollow structure of a device having a group of hollow structures and a group of respective cells; and targeting the one or more pressurized balloons to one or more of the targeted cell so as to localize plastic deformation to the targeted cell(s) using prescribed values of global force and balloon pressure with respect to the one or more pressurized balloons, thereby facilitating a noninvasive tuning of the targeted cell(s) of the hollow structure.
It will be appreciated that variations of the above-disclosed and other features and functions, or alternatives thereof, may be desirably combined into many other different systems or applications. It will also be appreciated that various presently unforeseen or unanticipated alternatives, modifications, variations or improvements therein may be subsequently made by those skilled in the art which are also intended to be encompassed by the following claims.
The invention described in this patent application was made with Government support under the Fermi Research Alliance, LLC, Contract Number DE-AC02-07CH11359 awarded by the U.S. Department of Energy. The Government has certain rights in the invention.
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