WO1997044804A1 - Canon a electrons a plusieurs sections emettrices generant plusieurs groupements d'electrons - Google Patents

Canon a electrons a plusieurs sections emettrices generant plusieurs groupements d'electrons Download PDF

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Publication number
WO1997044804A1
WO1997044804A1 PCT/US1997/008461 US9708461W WO9744804A1 WO 1997044804 A1 WO1997044804 A1 WO 1997044804A1 US 9708461 W US9708461 W US 9708461W WO 9744804 A1 WO9744804 A1 WO 9744804A1
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Prior art keywords
electrons
electron
cavity
area
gun
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PCT/US1997/008461
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English (en)
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Frederick M. Mako
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Schwartz, Ansel, M.
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Priority to CA002254137A priority Critical patent/CA2254137A1/fr
Priority to EP97925638A priority patent/EP0900446A1/fr
Publication of WO1997044804A1 publication Critical patent/WO1997044804A1/fr

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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J3/00—Details of electron-optical or ion-optical arrangements or of ion traps common to two or more basic types of discharge tubes or lamps
    • H01J3/02—Electron guns
    • H01J3/023—Electron guns using electron multiplication

Definitions

  • the present invention is related to electron guns for producing bunched electrons and subsequently using those electron bunches to generate rf energy. More specifically, the present invention is related to an electron gun that uses an rf cavity subjected to a rotating and oscillating electric field at a given frequency for the production of bunched electrons and uses an output cavity for the production of a higher frequency and higher power oscillating electric field than that power and frequency in the input cavity.
  • High-current pulses are widely used in injector systems for electron accelerators, both for industrial linear accelerators (li ⁇ acs) as well as high-energy accelerators for linear colliders.
  • Short-duration pulses are also used for microwave generation, in klystrons and related devices, for research on advanced methods of particie acceleration, and for injecto ⁇ used for free-electron laser (FEL) drivers.
  • FEL free-electron laser
  • TeV linear colliders for high energy physics will require rf sources capable of 500 MW/m of rf power with a typical pulse length of 50 ns. This requires a 50 MW source with a corresponding pulse width of 1 ⁇ s at a frequency between 10 and 20 GHz before pulse compression [R Ruth, ed., Report of the Linear Collider Working Group, Proceedings ofthe 1990 Summer Study on High Energy Physics, Snowmass, CO, June 25 - July 13, 1990]. Because the cost ofthe resources will be a large fraction of the operating cost ofthe accelerator, there is a need for high-power microwave sources capable of multi-megawatt performance at high efficiency. To ensure that modulator costs do not become excessive, the potential driver should aiso be able to satisfy the above requirements working at a voltage of about 600 kV.
  • the described invention is a high power frequency multiplying device that utilizes a
  • the GMPG produces a number of electron bunches per rf period using a natural bunching process that results from resonant amplification of a current of secondary electrons in an rf input cavity. This natural bunching provides high-current densities
  • the GMPG is an outgrowth of a simpler device, the Micro-Pulse Gun (MPG) [Patent Pending], that operates on the same fundamental principle but with only one bunch per rf period.
  • MPG Micro-Pulse Gun
  • the GMPG secondary emission process does not cause erosion or evaporation and therefore will have a longer lifetime.
  • the natural bunch formation is a resonant process which is not prone to phase instability.
  • a system for producing a high-power high frequency microwave generator using a Gatling Micro-Pulse Gun.
  • the system consists of five distinct components: (1) the GMPG which includes an output grid; (2) a post-acceleration section; (3) a radial magnetic compression section; (4) an output cavity; and (5) a beam collector.
  • the system has been characterized in detail for the transverse normalized emittance ["The Physics of Charged-Particle Beams", ID. Lawson, Clarendon Press, Oxford, (1977), p. 181], energy spread, and bunch expansion throughout the entire system. This is important for determining the output power and system efficiency.
  • the basis of the concept is a novel device to generate multiple, high-current density, micro-pulse electron bunches.
  • the device is named the Gatling Micro-pulse Gun (GMPG). It utilizes the resonant amplification of electron current by secondary emission in an rf cavity, with pre-designated areas on one side of the cavity that are partially transparent to allow the transmission of output bunches. Multiple bunches are produced sequentially during an rf period by exploiting the unique properties of a rotating electromagnetic mode. The mode illustrated is TM n10 . This method allows frequency multiplication in an output cavity.
  • GMPG Gatling Micro-pulse Gun
  • the GMPG is high-power, high-frequency microwave generation.
  • the narrow bunches are required for this application.
  • the final current density in the GMPG increases rapidly with frequency, namely as frequency cubed.
  • the upper frequency will be limited by practical considerations such as required peak power, finite secondary emission time, secondary-emission current density for the input cavity, and breakdown in the output cavity.
  • the GMPG has been thoroughly characterized by finding the saturated current density dependence on the gap spacing, peak cavity voltage, resonant frequency and applied axial magnetic field.
  • the peak particle energy emerging from the GMPG has also been characterized by finding its dependence on gap spacing, peak cavity voltage and frequency. Peak particle energy from the input cavity always corresponds to about. 75% of the peak rf voltage. Beam loading and frequency shift have been evaluated and can easily be tolerated. Setting up the required TM no rotating mode in the input cavity of the GMPG has been established along with means to efficiently couple power into the GMPG without significant mode distortion. Absolute power requirements and the loaded Q of the GMPG have been found and are not restrictive. Breakdown in the input cavity has been examined and is not a problem.
  • the beam emittance has been determined for various conditions of grid wire thickness, grid wire densities, axial magnetic field strengths, and magnetic scale length. While the presence of the output grids causes some emittance growth, the results are not significant for the intended application. Both rf and post acceleration field leakage through the grid region have been evaluated and shown to be insignificant.
  • the GMPG mechanism minimizes emittance growth compared to a DC type gun. Resonant particles are loaded into the wave at near zero rf phase angle; thus, the resonant particles experience a much lower transverse kick from the grid wires. Also, by providing a 45° radial focusing electrode after the second grid, the transverse field at the second grid is reduced significantly, which minimizes emittance growth.
  • the only significant transverse emittance growth comes from the magnetic compression region, which only causes a reduction in the output cavhy efficiency of about 3%.
  • Grid heating has been shown not to be a problem.
  • An input cavity design has been used which includes tapered waveguide for feeding in rf power and provides electric and magnetic beam focusing.
  • various materials have been used for fabrication ofthe input cavity.
  • the transverse emittance growth and bunch expansion do not significantly affect the system performance.
  • a design utilizing pulsed high voltage was used for post acceleration.
  • Magnetic compression is used to bring the bunches near the axis for injection into the output cavity.
  • the most significant increase in transverse emittance occurs in this section- However, the loss of device efficiency is only a few percent.
  • the fourth component of the system is the output cavity.
  • the output cavity For good coupling, low transverse emittance growth (or high beam conversion efficiency) and high power handling, the
  • the TM ⁇ mode was used.
  • the TM M0 mode locks at the output frequency and shows no mode competition.
  • the fifth component is the beam collector which is also used for energy recovery.
  • the resulting system efficiency is 59% without beam energy recovery and 75% with beam energy recovery.
  • the system efficiency includes the input cavity efficiency, input driver efficiency (a 15 MW klystron at 2.85 GHz), output cavity efficiency, and the beam collector conversion efficiency. Breakdown in the output cavity appears to be manageable.
  • One ofthe advantages ofthe GMPG over a klystron is that the bunch length is short compared to the rf period, which gives rise to higher beam to rf conversion efficiency.
  • the first component of the present invention pertains to the electron gun.
  • the electron gun comprises an rf cavity having a first side with emitting surfaces and a second side with transmitting and emitting sections.
  • the gun is also comprised of a mechanism for producing a rotating and oscillating force which encompasses the emitting surfaces and the sections so electrons are directed between the emitting surfaces and the sections to contact the emitting surfaces and generate additional electrons and to contact the sections to generate additional electrons or escape the cavity through the sections.
  • the sections preferably isolate the cavity from external forces outside and adjacent to the cavity.
  • the sections preferably include transmitting and emitting grids.
  • the grids can be of an annular shape, or of a circular shape, or of a rhombohedron shape.
  • the mechanism preferably includes a mechanism for producing a rotating and oscillating electric field that provides the force and which has a radial component that prevents the electrons from straying out ofthe region between the grids and the emitting surfaces. Additionally, the gun includes a mechanism for producing a magnetic field to force the electrons between the grids and the emitting surfaces.
  • the first component of the present invention pertains to a method for producing electrons.
  • the method comprises the steps of moving at least a first electron in a first direction at one location. Next there is the step of striking a first area with the first electron. Then there is the step of producing additional electrons at the first area due to the first electron. Next there is the step of moving electrons from the first area to a second area and transmitting electrons through the second area and creating more electrons due to electrons from the first area striking the second area. These newly created electrons from the second area then strike the first area, creating even more electrons in a recursive, repetitive manner between the first and second areas. This process is also repeated at different locations.
  • the second component of the present invention pertains to the post-acceleration to high energy of the electron bunches from the first component, the electron gun. Outside the transmitting area of the electron gun an accelerating electric field provides the means to accelerate the electron bunches to high energy.
  • the third component of the present invention pertains to the means for decreasing the radial location of electron bunches. After post-acceleration, the electron bunches have to be prepared for the interaction in the fourth component, the output cavity.
  • An external magnetic field which increases in strength along the path of the accelerated electron bunches is used as a means to decrease the radial position ofthe electron bunches so that they can be injected into the output cavity.
  • the radial decrease is performed in such a way that the radial position of the bunches, after reduction, is equal to the radius at which the output cavity electric field is at a peak.
  • the fourth component of the present invention pertains to the means for producing coherent microwave radiation in a cylindrical output cavity.
  • the driving source of energy comes from the electron bunches arriving into the output cavity, one every rf period ofthe output cavity radiation frequency.
  • the intention is to force the bunches to couple near the peak of the axial eiectric field of the design mode.
  • the electron bunches are allowed to pass through holes that are equally-spaced azimuthally in the output cavity walls (both front and back faces).
  • the fifth component of the present invention provides a means to collect the electron bunches and provide energy recover so as to produce a voltage to accelerate the initial electron bunches.
  • the present invention pertains to an electron gun.
  • the electron gun comprises an rf cavity having a first side with multiple non-simultaneous emitting surfaces and a second side with multiple transmitting and emitting sections.
  • the electron gun also comprises a mechanism for producing a rotating and oscillating force which encompasses the multiple emitting surfaces and the multiple sections so electrons are directed between the multiple emitting surfaces and the multiple sections to contact the multiple emitting surfaces and generate additional electrons and to contact the multiple sections to generate additional electrons or escape the cavity through the multiple sections.
  • the present invention pertains to an apparatus for generating rf energy.
  • the apparatus comprises a mechanism focusing non-simultaneous multiple electron bunches.
  • the apparatus also comprises an output cavity which receives non-simultaneous multiple electron bunches and produces rf energy as the non-simultaneous multiple electron bunches pass through it.
  • the present invention pertains to a method for producing electrons. The method comprises the steps of moving at least a first electron in a first direction at a first time. Then there is the step of moving at least a second electron in the first direction at a second time. Next, there is the step of striking a first area with the first electron. Next, there is the step of producing additional electrons at the first area due to the first electron.
  • FIG. 1 Perspective view of Gatling MPG driving an output cavity.
  • the post acceleration structure, magnetic compression system and collector are not shown.
  • FIG. 2 Side view of GMPG input cavity showing double grid and emitting and transmitting surfaces. Electron bunches, concave shaping of the cavity, post acceleration section, magnetic compression for TMr ⁇ mode, the output cavity and collector are also shown. Figure is not to scale.
  • Figure 3 TM 110 rotating mode electric and magnetic field pattern used in the GMPG.
  • Figure 15 Emittance growth due to double-grid extraction with an injection beam energy of 50 kV.
  • the wire thickness is 0.1 mm.
  • Figure 17 Results of the normalized bunch emittance and pulse width after compression for different solenoid radii, a.
  • Figure 18 Plots of the on-axis axial magnetic field are shown as a function of the axial coordinate for different values of solenoid radii.
  • Figure 19 Overall schematic of the GMPG's device with frequency multiplying. After undergoing post-acceleration, the micro-bunches are adiabatically compressed towards the axis for injection into the output cavity. This representative device is for the TM ⁇ o mode in the output cavity.
  • FIG. 20 Spatial distribution of the rf electric field excited inside the output cavity by the micro-pulses is shown as a function of the transverse x coordinate.
  • the profile for the TM ⁇ mode is also shown (solid line).
  • Figure 21 Frequency spectrum of the field shown in Fig. 20. Single mode excitation is achieved at 11.4 GHz.
  • Figure 22 Plots showing the output cavity efficiency as a function of the bunch emittance. In each case, the beam current and beam emittance are adjusted before injection into the output cavity.
  • the beam radius is r b - 5.45 mm.
  • Figure 23 Schematic representation of the robust pierce gun.
  • the electron gun 10 comprises an rf cavity having a first side 14 with multiple non-simultaneous emitting surfaces 16 and a second side 18 with multiple transmitting and emitting sections 20.
  • the electron gun 10 also comprises a mechanism 22 for producing a rotating and oscillating force which encompasses the multiple emitting surfaces 16 and the multiple sections 20 so electrons are directed between the multiple emitting surfaces 16 and the multiple sections 20 to contact the multiple emitting surfaces 16 and generate additional electrons and to contart the multiple sections 20 to generate additional electrons or escape the cavity through the multiple sections 20.
  • each section isolates the cavity from external forces outside and adjacent the cavity.
  • the multiple sections 20 preferably include transmitting and emitting double grids 24.
  • the multiple grids 24 are of an annular shape.
  • the multiple grids 24 are of a circular shape or of a rhombohedron shape.
  • the producing mechanism 22 preferably includes a mechanism 26 for producing a rotating and oscillating eiectric field that provides the force and which has a radial component that confines the electrons to the multiple regions between the emitting grids 24 and the emitting surfaces 16. Additionally, the producing mechanism 22 includes a mechanism 28 for producing multiple bunches of electrons in the multiple regions 30 between the multiple emitting grids 24 and the multiple emitting surfaces 16. Additionally, the gun 10 can include a mechanism 32 for producing a magnetic field to confine the electrons to the multiple regions between the multiple emitting grids 24 and the multiple emitting surfaces 16. Additionally, the gun can include a mechanism for producing an electrostatic electric field 28 to confine and accelerate the electron bunches after exiting the multiple sections 20.
  • the present invention pertains to an apparatus 100 for generating rf energy.
  • the apparatus comprises a mechanism focusing non-simultaneous multiple electron bunches.
  • the apparatus 100 also comprises an output cavity 40 which receives non-simultaneous multiple electron bunches and produces rf energy as the non-simultaneous multiple electron bunches pass through it.
  • the present invention pertains to a method for producing electrons.
  • the method comprises the steps of moving at least a first electron in a first direction at a first time. Then there is the step of moving at least a second electron in the first direction at a second time. Next, there is the step of striking a first area with the first electron. Next, there is the step of producing additional electrons at the first area due to the first electron. Then, there is the step of moving electrons from the first area to a second area. Next, there is the step of transmitting electrons to the second area and creating more electrons due to electrons from the first area striking the second area. Then, there is the step of striking a third area with the second electron.
  • Micro-pulses or bunches are produced by resonantly amplifying a current of secondary electrons in an input rf cavity operating in a TM U0 rotating mode. Bunching occurs rapidly and is followed by saturation of the current density in ten to fifteen rf periods.
  • the "bunching" process is not the conventional method of compressing or chopping a long beam into short beams, but results by selecting particles that are in phase with the rf electric field, i.e., resonant.
  • One wall of the cavity is highly transparent (e.g. a grid) to electrons but opaque to the input rf field.
  • the transparent wall allows for the transmission of the energetic electron bunches and serves as the cathode of a high-voltage injector.
  • the reason for the name "Micro Pulse Gun” is the fact that the pulse is only a few percent of the rf period in contrast to the usual r/guns where the pulse width is equal to half the //period.
  • Figure 1 shows a perspective view of the Gatling micropulse gun emitting four (as an example) equally-spaced azimuthal electron-bunches. Emission is implemented from four emitting "button cathodes" rather than the entire cavity wall by choice of materials.
  • the post-acceleration electrodes and magnetic compression coils are not shown in Fig. 1.
  • radial expansion is controlled by electric and maenetic fields.
  • the four bunches are shown separated in time by ⁇ iN b where ris the //period of the TM ⁇ legally rotating mode and _ ⁇ is the number of bunches equal to 4 in this case.
  • the pulse width is small compared to ⁇ /N b .
  • Axial and radial expansion of the pulse is minimized outside the cavity by using rapid acceleration and a combination of electrostatic and magnetic focusing.
  • the four bunches are compressed and transported into an output cavity.
  • the cavity In order to reduce radial space charge expansion in the input cavity, the cavity should have a concave shape, as shown in Fig. 2 (this is only required when the axial magnetic field is desired to be small in the input cavity).
  • the output cavity may operate in a TMo., 0 mode or a TM ⁇ o non-rotating or rotating mode.
  • This Gatling micro-pulse electron gun provides a high peak power, multi-kiloampere, picosecond-long electron source which is suitable for many applications. Of particular interest are injectors for accelerators, 1.0-40 GHz rf generators for linear colliders and super-power nanosecond radar.
  • the right wall of the input cavity in Fig. 2 is constructed with a transmitting circular shaped double grid which allows for the transmission of high current density electron bunches.
  • the inside surface of the grid facing the interior ofthe cavity provides an emitting surface for electron multiplication.
  • a path for the rf current is maintained by using radial and azimuthal wires.
  • the double grid provides a means to isolate the post-accelerating field (outside the cavity) from the rf field. This prevents the accelerating field from pulling out electrons that are not resonant with the rf field.
  • the second grid (to the right) is electrically isolated from the first grid and can be dc biased (-500 to -1000 volts) to create a barrier for low energy electrons.
  • the resonant particles are loaded into the wave at low phase angles. When they reach the output grid 180° later, they experience a reduced transverse kick from the grid wires. This reduces the emittance growth from the first grid in the Gatling MPG.
  • the post-accelerating field increases the final emittance, but within acceptable levels.
  • a simplified model is presented which excludes space charge, transit time, amplitude and phasing effects but shows the principle behind utilizing multipacting for the GMPG.
  • Fig. 2 is shown an rf input cavity operating in a TM no rotating mode. Assume that at the gridded wall of the cavity there is a single electron at rest and located radially at about half the cavity radius where the axial electric field peaks. Assume also, that this electron can transit the cavity in one-half the rf period and is in proper phase with the field. This electron is accelerated across the cavity and strikes the surface S. A number b. of secondary electrons are emitted off this electrode, where ⁇ is the secondary electron yield of surface S.
  • the seed current density J uttl can be created by several possible sources including thermionic emission, radioactivity, field emission or ultraviolet radiation.
  • thermionic emission radioactivity
  • field emission ultraviolet radiation.
  • a small thoriated tungsten loop of wire is used to create seed electrons.
  • a similar arrangement is used in the GMPG.
  • the secondary emission yield ⁇ is defined to be the average number of secondary electrons emitted for each incident primary electron and is a function of the primary electron energy e.
  • ⁇ for all materials increases at low electron energies, reaches a maximum ⁇ at energy ⁇ ,,,,,, and monotonically decreases at high energies.
  • Table I gives some commonly used materials with high and low values of ⁇ [D. E. Gray (coord. Ed.), Amer. Inst. of Physics Handbook, 3rd Edition, McGraw-Hill; E. L. Garwin, F. K. King, R E. Kirby and 0. Aita, I Appl. Phys. 61, 1145 (1987); A. R Nyaiesh, et al., I Vac. Sci. Tech. A, 4, 2356 (1986); S. Michizono, et al., I Vac. Sci. Tech. A, 10, 1180 (1992)].
  • GaP GaP is not sensitive to oxygen but is sensitive to water. Thus GaP has been rejected for use as a high secondary emitter. MgO is a good candidate for lower particle energy ( ⁇ 60 keV) and would have to be applied in a thin layer in order to avoid charge buildup.
  • Another very robust emitter material that is currently under intensive study is diamond film. Diamond films have been very successfully used. Diamond is the material of choice for the GMPG since it is durable and can be exposed to air (robust) and has a reasonable yield up to about 300 keV.
  • the entire GMPG cavity (except for the specified secondary emission sites) needs to be built with a low secondary emission coefficient.
  • carbon appears to be the most desirable material.
  • vacuum problems may occur.
  • vacuum seals will be difficult.
  • the unloaded cavity Q will be too low.
  • a pure titanium cavity seems to be a good solution since it has a low secondary yield and excellent vacuum properties; however, its high electrical resistivity gives a low unloaded cavity Q
  • Cavity surface coatings can give a fa ⁇ or of two improvement in breakdown field along with several orders of magnitude reduction in dark emission current on an OFHC copper cavity.
  • CaF 2 and TIN are excellent candidates for cavity coatings. These would be the preferred coatings for high average power cavities.
  • 304 stainless steel works well.
  • Input parameters for the GMPG input cavity are: peak //voltage (PQ, frequency (f), cavity gap spacing (d), and magnetic focusing field (B_ ).
  • Output parameters are: current density, particle energy, transverse emittance and pulse width.
  • Current density is evaluated near the exit grid (right side of input cavity, Fig. 2).
  • a positive current density is the current that travels from right to left.
  • a negative current density describes the exiting beam. Current asymmetry occurs because the positive/ negative beam pulses have substantially different charge densities and velocities at the exit grid.
  • the corresponding particle energy at the peak of the distribution is plotted as a function of frequency in Fig. 6.
  • the particle energy scales like the square of the frequency.
  • the resonant voltage also scales like the frequency squared then the particle energy scales linearly with the resonant voltage.
  • Each curve is a spline fit to the data.
  • the saturated current density is the peak current density, after 10 to 15 cycles, from the current density vs time traces like that shown previously.
  • the current density plots also show the "tuning range" for the GMPG. A very tolerant tuning range is a key result. Even if the electric field changed by 30% from, say, beam loading, resonance would still occur but at a lower current density.
  • Figure 8 gives the peak voltage (V 0 ) as a function ofthe normalized drive voltage (q,) for different gap spacings at a frequency of 2.85 GHz. This figure gives the drive voltages used to maintain resonance for the results in Eg 7. These voltages or the corresponding electric fields have been shown to be easily within the limits of breakdown.
  • Figure 10 shows that the particle energy at the peak of the distribution scales linearly with the peak rf voltage. In fact the particle energy reaches the theoretical maximum value for a particle that starts at zero phase angle and zero electric field and ends up at zero electric field with a phase angle of ⁇ .
  • Figure 11 shows the data with a fitted curve of the saturated current density dependence on the gap spacing while maintaining resonance.
  • the current density scales like the gap spacing raised to the 1.75 power.
  • Figure 12 shows the corresponding particle energy at the peak of the distribution as a function of the gap spacing. Essentially the particles reach the maximum possible energy in a sine wave starting near zero phase angle and ending near a phase angle of ⁇ .
  • Figure 13 shows the peak resonant voltage for the cavity as a function of gap spacing.
  • Figure 14 shows a plot of the input cavity power required as a function of frequency for different gap spadngs.
  • J ⁇ - (fd) 2 for fixed ⁇ 0 .
  • the electron bunch energy spread ⁇ E/E comes from the diameter ofthe emission area.
  • the //voltage decreases as the electron emission diameter increases, thus the electrons in a bunch receive an energy spread.
  • the required //power is directly proportional to the electron bunch energy spread.
  • Figure 15 illustrates the beam emittance and transmission (7) for a wire thickness of 0.1 mm.
  • the piots are emittance and transmission versus the number of wires per cm. Note from the plots in Fig. 15 that for a span of 14 wires/cm, a transmission efficiency of ⁇ 75% can be obtained with a final beam emittance of 25 mm-mrad.
  • Post-acceleration of the beam as it emerges from the input cavity of the GMPG is required to allow successful transport ofthe high-current micro bunches and thus to increase the beam energy for conversion to rf power inside the output cavity. Post-acceleration is accomplished using pulsed high voltage.
  • linac injectors accelerate the beam to a few MeV, typically starting from an e-gun voltage of 100 kV. This brings the beam to a relativistic velocity, and reduces the perveance, hence space charge effects, to a manageable level.
  • the bunch particle energy will be accelerated from 50 keV to 650 keV.
  • the average beam power is 72 MW. This power level is sufficient for the production of 50 MW of 11.4 GHz microwave radiation in the output cavity.
  • An appropriately shaped (to minimize field enhancement) post-acceleration geometry is employed in the acceleration process. This geometry is achieved by providing a 45° radial focusing electrode after the second grid.
  • the transverse field at the second grid is reduced significantly which minimizes the emittance growth.
  • a 10.9 mm-radius bunch with a particle energy of 50 keV is injected into the accelerating section.
  • the voltage applied between the accelerating electrode and cavity wall is 600 kV.
  • the accelerating gap spacing, L m is varied from 2-5 cm with insignificant changes in the results.
  • An accelerating gap spacing of 5 cm is selected to prevent breakdown problems.
  • Figure 16 is a plot of the bunch normalized emittance, measured after acceleration, as a function of the applied axial magnetic field, B curat. It can be clearly seen that as the axial magnetic field is increased emittance growth during acceleration is reduced. It should also be noted that the pulse width at injection is 7 ps. For all the cases shown in Fig. 16, the pulse width expansion during acceleration is about 28.6% yielding a pulse width of about 9 ps at the end of the accelerating process, regardless ofthe amount of axial magnetic field.
  • the micro-bunches After post-acceleration, the micro-bunches have to be prepared for the interaction in the output cavity. Magnetically compressing the bunches in radius after acceleration allows injection into the output cavity. The compression is done so that the radial displacement of the bunches, after compression, is equal to the radius at which the cavity electric field peaks in the output cavity. For the TM ⁇ mode operating at 11.4 GHz, the second lobe of the electric field peaks at a radius of 2 cm.
  • the focusing magnetic fields employed were (approximately) the near-axis magnetic fields of a solenoid.
  • the micro-bunches, as they come from the post-acceleration region, are injected at full energy (650 kV) into a drift region solely under the influence of the compressing fields.
  • the current density is fixed to 375 A/cm 2 with a beam cross-section of 3.73 cm 2 and initial pulse width of 9 ps
  • the injection distance for each bunch from the system axis is fixed to 3.2 cm.
  • Figure 17 summarizes the beam transport results obtained.
  • Figure 17 shows the resulting bunch emittance and pulse width after compression as a function of solenoid effective radius, a, for the parameters above.
  • the profile of the axial magnetic field, measured on axis, is shown for different solenoid radii in Fig. 18.
  • This section was directed to the production of coherent microwave radiation in a cylindrical cavity operating in the TM ⁇ , mode.
  • the driving source is a group of high-current short electron bunches arriving in the cavity one every rf period of the output radiation frequency.
  • the bunches are 1.09 cm in diameter and have a duration of 10.5 ps.
  • the intention was to force the bunches to couple with the axial electric field of the second radial lobe of this mode.
  • the electric field of second lobe peaks at a radial distance r p .
  • r p 1.6 cm.
  • Figure 19 illustrates the overall schematic of the GMPG system. After formation of the bunches in the input cavity, they undergo acceleration and adiabatic magnetic compression before entering the output cavity.
  • the cavity is of cylindrical geometry with a radius of 4.94 cm and length L. ⁇ 1 cm.
  • Four openings are inserted along the front and back faces of the cavity to allow the passage of the micro-bunches.
  • the diameter of each beam "tube” is 1.5 cm and its distance from the axis is 1.6 cm.
  • Bunches are injected into the cavity with an energy of 650 kV, pulse width ( ⁇ p ) of 10.5 ps, and a normalized emittance of 225 mm-mrad.
  • the current in each bunch is typically 1400 A and the beam radius (r b ) is 5.45 mm.
  • Each bunch enters the output cavity at a radial position of 1.6 cm from the cavity axis every 88 ps.
  • the bunches arrive into the beam tubes clockwise or counterclockwise, the direction depending on the direction of rotation ofthe rotating mode in the modulating input cavity.
  • 4 bunches arrive into the output cavity, each arriving into a different beam tube.
  • Figure 21 shows the frequency spectrum ofthe wave excited by the bunches inside the cavity. It can be seen that single mode excitation is achieved at 11.4 GHz with no mode competition.
  • the next step is to find how the bunch emittance affected the efficiency of the output interaction.
  • the bunches after acceleration and beam compression undergo emittance growth and pulse width expansion. It was shown, for the parameters of interest, that after magnetic beam compression a micro-pulse with a pulse width of 10.5 ps with a normalized emittance of -225 mm-mrad could be produced. Thus, it was of interest to determine how the efficiency degraded with beam quality.
  • the rf efficiency is defined simply as the ratio of rf power excited by the beam divided by the average beam power.
  • the summary of //efficiency versus emittance is shown in Fig. 22.
  • plots of efficiency as a function of bunch emittance are shown for different values of beam current density.
  • the device performance was set at an rf output power of 50 MW at 11.4 GHz.
  • the resulting system efficiency is 59% without beam energy recovery and 75% with beam energy recovery.
  • the system efficiency includes the input cavity efficiency and input driver efficiency (a 15 MW klystron at 2.85 GHz) and the beam collector conversion efficiency. For energy recovery a depressed collector is used.
  • Table JJ shows the parameters for this device with a factor of four in frequency multiplication. Note that a factor of four in magnetic compression is required for spatially matching the beam bunches from the input cavity operating at 2.85 GHz with the TM U0 rotating mode to the output cavity operating at 11 4 GHz with the TM ⁇ mode. Beam pulses are generated at about half the respective cavity radius which corresponds to the peak of the axial electric field.

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  • Particle Accelerators (AREA)
  • Electron Sources, Ion Sources (AREA)
  • Microwave Tubes (AREA)

Abstract

Canon à électrons générant plusieurs groupements d'électrons pour produire de l'énergie RF. Ce canon à électrons (10) comprend une cavité d'entrée RF présentant un premier côté à surfaces émettrices multiples (14, 16) et un deuxième côté à sections d'émission et de transmission multiples (18, 20). Ce canon à électrons comprend également un mécanisme de génération de force de rotation et d'oscillation (26) entourant les surfaces (16) et les sections (20) émettrices multiples. Ces sections multiples (20) comprennent en outre plusieurs grilles (24) annulaires, circulaires ou rhomboédriques. De plus, un procédé de production de plusieurs groupements d'électrons mis en oeuvre selon la présente invention est également décrit.
PCT/US1997/008461 1996-05-22 1997-05-20 Canon a electrons a plusieurs sections emettrices generant plusieurs groupements d'electrons WO1997044804A1 (fr)

Priority Applications (2)

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CA002254137A CA2254137A1 (fr) 1996-05-22 1997-05-20 Canon a electrons a plusieurs sections emettrices generant plusieurs groupements d'electrons
EP97925638A EP0900446A1 (fr) 1996-05-22 1997-05-20 Canon a electrons a plusieurs sections emettrices generant plusieurs groupements d'electrons

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US65162696A 1996-05-22 1996-05-22
US08/651,626 1996-05-22

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WO1997044804A1 true WO1997044804A1 (fr) 1997-11-27

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9065244B1 (en) 2014-05-01 2015-06-23 The Boeing Company Compact modular free electron laser (FEL) architecture

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111341631B (zh) * 2020-04-07 2021-05-14 电子科技大学 一种利用二次电子倍增的电磁波发生器

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2381320A (en) * 1940-11-28 1945-08-07 Westinghouse Electric Corp Electromagnetic apparatus
US2591322A (en) * 1946-08-30 1952-04-01 Csf Generator of ultra-short electromagnetic waves

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2381320A (en) * 1940-11-28 1945-08-07 Westinghouse Electric Corp Electromagnetic apparatus
US2591322A (en) * 1946-08-30 1952-04-01 Csf Generator of ultra-short electromagnetic waves

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9065244B1 (en) 2014-05-01 2015-06-23 The Boeing Company Compact modular free electron laser (FEL) architecture

Also Published As

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IL120874A0 (en) 1997-09-30
CA2205989A1 (fr) 1997-11-22
CA2254137A1 (fr) 1997-11-27
EP0809271A3 (fr) 2000-03-15
JPH1055763A (ja) 1998-02-24
EP0809271A2 (fr) 1997-11-26
EP0900446A1 (fr) 1999-03-10

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