Patent classifications
H05H7/20
METHODS AND SYSTEMS FOR TREATMENT OF SUPERCONDUCTING MATERIALS TO IMPROVE LOW FIELD PERFORMANCE
A system and method for treating a cavity comprises preparing a superconducting radio frequency (SRF) cavity for removal of a dielectric layer from on an inner surface of the SRF cavity, subjecting the SRF cavity to a heat treatment in order to remove the dielectric layer from the inner surface of the SRF cavity, and preventing the development of a new dielectric layer on the inner surface of the SRF cavity by preventing an interaction between the inner surface of the SRF cavity and atmospheric gasses.
Acceleration cavity, accelerator, and resonance frequency adjustment method of acceleration cavity
An objective of the invention is to provide an acceleration cavity, an accelerator, and a resonance frequency adjustment method of an acceleration cavity that can change the natural resonance frequency of the acceleration cavity without occupying space between adjacent accelerator cavities. A QWR includes: a body portion whose axial direction is parallel to the vertical direction, and having a cylindrical side face portion; an upper face portion provided in an upper part of the body portion and is a plate-shaped member; and a deformation adjustment portion applying a pressing force on the upper face portion to deform the upper face portion.
AUTOMATIC TUNING OF DRESSED MULTICELL CAVITIES USING PRESSURIZED BALLOONS
A method and system for automatically tuning hollow structures, can include pressurized balloons located in one or more targeted cells of a hollow structure of a device having a hollow structures and respective cells. A pressurized balloon can be inserted into a targeted cell so as to localize plastic deformation to the targeted cell using prescribed values of global force and balloon pressure. A pair of inflate/deflate rods associated with an independent air supply for the pressurized balloon can inflate or deflate the pressurized balloon without affecting other pressurized balloons. The pair of inflate/deflate rods can be automatically insertable or removable from the hollow structure by controlled motorized motions.
AUTOMATIC TUNING OF DRESSED MULTICELL CAVITIES USING PRESSURIZED BALLOONS
A method and system for automatically tuning hollow structures, can include pressurized balloons located in one or more targeted cells of a hollow structure of a device having a hollow structures and respective cells. A pressurized balloon can be inserted into a targeted cell so as to localize plastic deformation to the targeted cell using prescribed values of global force and balloon pressure. A pair of inflate/deflate rods associated with an independent air supply for the pressurized balloon can inflate or deflate the pressurized balloon without affecting other pressurized balloons. The pair of inflate/deflate rods can be automatically insertable or removable from the hollow structure by controlled motorized motions.
IN SITU SRF CAVITY PROCESSING USING OPTICAL IONIZATION OF GASES
A system and method for the in situ processing of internal SRF cavity surfaces to reduce field emission and improve maximum gradient. An electromagnetic radiation source is introduced in the bore of a superconducting cavity to enhance ionization or dissociation of gases which then remove contaminants from the surface of the cavity, either through direct surface bombardment, chemical reaction or through the production of radiation which interacts with the contaminants. An RF or low frequency electromagnetic field may be established in the cavity which further enhances the ionization or dissociation process and may cause the ions to bombard sites with enhanced electric fields. The invention removes the requirement that the RF field be sufficient by itself to ionize gas in the cavity. The in situ processing method could enable exposure of the entire internal surface of multiple cells in an RF structure to ionized or dissociated gas simultaneously rather than on a cell by cell basis.
IN SITU SRF CAVITY PROCESSING USING OPTICAL IONIZATION OF GASES
A system and method for the in situ processing of internal SRF cavity surfaces to reduce field emission and improve maximum gradient. An electromagnetic radiation source is introduced in the bore of a superconducting cavity to enhance ionization or dissociation of gases which then remove contaminants from the surface of the cavity, either through direct surface bombardment, chemical reaction or through the production of radiation which interacts with the contaminants. An RF or low frequency electromagnetic field may be established in the cavity which further enhances the ionization or dissociation process and may cause the ions to bombard sites with enhanced electric fields. The invention removes the requirement that the RF field be sufficient by itself to ionize gas in the cavity. The in situ processing method could enable exposure of the entire internal surface of multiple cells in an RF structure to ionized or dissociated gas simultaneously rather than on a cell by cell basis.
Compact SRF Based Accelerator
An accelerator comprising at least one accelerator cavity, an electron gun, at least one cavity cooler configured to at least partially encircle the accelerator cavity, a cooling connector, an intermediate conduction layer formed between the at least one cavity cooler and the at least one accelerator cavity configured to facilitate thermal conductivity between the cavity cooler and the accelerator cavity, a mechanical support connected to the accelerator cavity via at least one endplate and configured for stabilizing the accelerator cavity, and a refrigeration source for providing refrigerant via the cooling connector to the at least one cavity cooler.
Compact SRF Based Accelerator
An accelerator comprising at least one accelerator cavity, an electron gun, at least one cavity cooler configured to at least partially encircle the accelerator cavity, a cooling connector, an intermediate conduction layer formed between the at least one cavity cooler and the at least one accelerator cavity configured to facilitate thermal conductivity between the cavity cooler and the accelerator cavity, a mechanical support connected to the accelerator cavity via at least one endplate and configured for stabilizing the accelerator cavity, and a refrigeration source for providing refrigerant via the cooling connector to the at least one cavity cooler.
Device for tuning SCRF cavity
The present invention relates to method and device invention made in SS316LN for tuning single-cell or multi-cell SCRF cavity for precise slow and fast tuning with low hysteresis. The tuning mechanism (device) for SCRF cavity consists of two thick square flanges connected to each other through two parallel sets of X-link levers pivoted in between such that the motion of top end of flange and bottom end of flange equalizes; wherein the top end of X-link connects one square flange to the bottom end of the other square flange and vice-versa using thin flat flexure plates; wherein the flexure plates are joined on X-link and square flange by bolts having spring locks; the square flanges have platform on the top that transfer motion and these are connected through power screw mechanism; wherein the power screw for linear actuation is rotated using worm-wheel.
Device for tuning SCRF cavity
The present invention relates to method and device invention made in SS316LN for tuning single-cell or multi-cell SCRF cavity for precise slow and fast tuning with low hysteresis. The tuning mechanism (device) for SCRF cavity consists of two thick square flanges connected to each other through two parallel sets of X-link levers pivoted in between such that the motion of top end of flange and bottom end of flange equalizes; wherein the top end of X-link connects one square flange to the bottom end of the other square flange and vice-versa using thin flat flexure plates; wherein the flexure plates are joined on X-link and square flange by bolts having spring locks; the square flanges have platform on the top that transfer motion and these are connected through power screw mechanism; wherein the power screw for linear actuation is rotated using worm-wheel.