HIGH-CURRENT CONDUCTION COOLED SUPERCONDUCTING RADIO-FREQUENCY CRYOMODULE
20190098741 ยท 2019-03-28
Inventors
- Gianluigi Ciovati (Yorktown, VA, US)
- Thomas J. Schultheiss (Commack, NY, US)
- John Rathke (Centerport, NY, US)
- Robert Rimmer (Yorktown, VA, US)
- Frank Marhauser (Yorktown, VA, US)
- Fay Hannon (Poquoson, VA, US)
- Jiquan Guo (Yorktown, VA, US)
Cpc classification
F17C3/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A high-current, compact, conduction cooled superconducting radio-frequency cryomodule for particle accelerators. The cryomodule will accelerate an electron beam of average current up to 1 ampere in continuous wave (CW) mode or at high duty factor. The cryomodule consists of a single-cell superconducting radio-frequency cavity made of high-purity niobium, with an inner coating of Nb.sub.3Sn and an outer coating of pure copper. Conduction cooling is achieved by using multiple closed-cycle refrigerators. Power is fed into the cavity by two coaxial couplers. Damping of the high-order modes is achieved by a warm beam-pipe ferrite damper.
Claims
1. A superconducting radio-frequency (SRF) cryomodule for accelerating an electron beam, comprising: a vacuum vessel; an SRF cavity within said vacuum vessel; a coaxial input power coupler extending through said vacuum vessel and connected to said SRF cavity; a cryocooler having a cold head, said cold head connected to the SRF cavity; a water-cooled beam pipe higher-order mode absorber for damping of high-order modes; a thermal shield; a magnetic shield; and an entrance beam tube and an exit beam tube.
2. The SRF cryomodule of claim 1 wherein said (SRF) cryomodule includes an electron beam current of at least of 1 ampere an energy of 1 to 10 MeV.
3. The SRF cryomodule of claim 1 further comprising: said entrance beam tube having a diameter and said exit beam tube having a diameter; and said diameter of said exit beam tube is larger than the diameter of said entrance beam tube.
4. The SRF cryomodule of claim 1 further comprising: an entrance beamline ultra-high vacuum valve on said entrance beam tube; and an exit beamline ultra-high vacuum valve on said exit beam tube.
5. The SRF cryomodule of claim 1 further comprising: said SRF cavity is selected from the group consisting of niobium (Nb) and metal with thermal conductivity greater than 500 W/(m K) at 4 degrees K; said RF cavity includes an inner surface; said inner surface of said SRF cavity is includes a thin film coating for reducing RF losses; and said thin film coating is a superconductor having a critical temperature greater than 15 K.
6. The SRF cryomodule of claim 5 further comprising: said thin film coating is 1 to 1.5 m thick; and said thin film coating is selected from the group consisting of Nb.sub.3Sn, Nb.sub.3Ge, NbN, and NbTiN; and said cryocooler maintaining said SRF cavity at 4.3 K.
7. The SRF cryomodule of claim 1 further comprising: said SRF cavity includes an outer surface; said outer surface of said SRF cavity includes a coating; and said coating on said outer surface of said SRF cavity is selected from the group consisting of copper and tungsten.
8. The SRF cryomodule of claim 7 wherein said coating on said outer surface of said SRF cavity is deposited on said SRF cavity by vacuum plasma-spraying, electroplating, or by a combination of vacuum plasma-spraying and electroplating.
9. The SRF cryomodule of claim 1 further comprising: said coaxial input power coupler including an outer conductor having an inner surface; said inner surface of said outer conductor of said power coupler includes a section with a layer of high-temperature superconductor; and said high-temperature superconductor having a critical temperature greater than 90 K.
10. The SRF cryomodule of claim 9 further comprising said layer of high-temperature superconductor is applied to said inner surface of said outer conductor by methods selected from the group consisting of physical-chemical vapor deposition, pulsed laser deposition, and a combination of physical-chemical vapor deposition and pulsed laser deposition.
11. The SRF cryomodule of claim 1 wherein said coaxial input power coupler is capable of sustaining a minimum of 500 kilowatt of power.
12. The SRF cryomodule of claim 1 further comprising: said cryocooler includes a first stage cold head and a second stage cold head; said first stage cold head of said cryocooler is at a temperature of 50-80 K; and said second stage cold head of said cryocooler is at a temperature of 4.3-9 K.
13. The SRF cryomodule of claim 1 further comprising: said magnetic shield including an inner and an outer magnetic shield; and said inner and outer magnetic shields are constructed of a high permeability metal having high magnetic shielding properties; and said thermal shield is constructed of oxygen free electronic copper.
14. The SRF cryomodule of claim 1 further comprising: a high thermal conductivity strain relief section between said second stage cold head and said SRF cavity; and said high thermal conductivity strain relief section is selected from the group consisting of copper and tungsten.
15. The SRF cryomodule of claim 1 wherein said water-cooled beam pipe higher-order mode absorber is a ferrite damper.
16. A superconducting radio-frequency (SRF) cryomodule for accelerating an electron beam, comprising: a vacuum vessel; an elliptical SRF cavity within said vacuum vessel; two coaxial input power couplers extending through said vacuum vessel and connected to said SRF cavity; one or more cryocoolers each having a first stage cold head and a second stage cold head with said second stage cold head of said cryocoolers maintaining a temperature of 4.3-9 K; a water-cooled beam pipe higher-order mode absorber for damping of high-order modes; a thermal shield; a magnetic shield; and an entrance beam tube and an exit beam tube.
17. The SRF cryomodule of claim 16 further comprising said first stage cold head of said cryocoolers is at a temperature of 50-80 K.
18. The SRF cryomodule of claim 16 further comprising: a thermal link between said second stage cold head and said SRF cavity; and said thermal link is selected from the group consisting of copper and tungsten.
19. The SRF cryomodule of claim 1 wherein said cryocoolers each provide a cooling power greater than or equal to 1.5 watt at 4.2 K.
20. A method for accelerating an electron beam to an electron beam current of at least 1 ampere at an energy of 1 to 10 MeV, comprising: providing a superconducting radio-frequency (SRF) cryomodule including a vacuum vessel, an SRF cavity within said vacuum vessel, an coaxial input power coupler extending through said vacuum vessel and connected to said SRF cavity, a cryocooler, an entrance beam tube and an exit beam tube, a thermal shield, a magnetic shield, and a water-cooled beam pipe higher-order mode absorber on said exit beam tube; cooling said SRF cavity to between 4.3 K and 9 K with said cryocooler; providing said exit beam tube with a greater diameter than said entrance beam tube to damp high-order modes in said SRF cavity; further damping high-order modes in said SRF cavity with said water-cooled beam pipe higher-order mode absorber; removing infrared heat generated by the SRF cavity with said thermal shield; and removing magnetic flux lines of interfering magnetic fields with said magnetic shield.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
[0017] Reference is made herein to the accompanying drawings, which are not necessarily drawn to scale and wherein:
[0018]
[0019]
[0020]
[0021]
[0022]
DETAILED DESCRIPTION OF THE INVENTION
[0023] With reference to
[0024] The SRF cavity 12 is preferably of elliptical shape and geometric tailored to the energy of the incoming beam. The SRF cavity 12 is preferably fabricated from high-purity niobium (Nb) having a residual resistivity ratio of greater than 300 and includes a thickness of 3-5 millimeters. Alternatively, metals with thermal conductivity greater than 500 W/(m K) at 4 K, such as tungsten or copper, could also be used.
[0025] As shown in
[0026] The SRF cavity 12 outer surface 20 is coated with a layer 22 preferably of copper or tungsten, and most preferably of pure copper having a purity of greater than 99.98%. The method of applying the outer layer 22 is preferably by electroplating, vacuum plasma spraying, or by a combination of vacuum plasma-spraying and electroplating. The outer coating is not required if the cavity is fabricated from a metal other than Nb.
[0027] Referring to
[0028] With reference to
[0029] With reference to
[0030] Magnetic fields are preferably minimized in the SRF cavity 12 through the use of an inner magnetic shield 42 and an outer magnetic shield 44. With reference to
[0031] With reference to
[0032] The volume within the cavity is isolated from the outside environment by means of two vacuum valves 52 outside the vacuum vessel, which are preferably all-metal gate valves. A vacuum valve 52 is included on the entrance 46 and on the exit beam tube 48.
[0033] The description of the present invention has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the invention. The embodiments herein were chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.