Vacuum for Accelerators

Similar documents
UHV - Technology. Oswald Gröbner

Vacuum Pumps. Two general classes exist: Gas transfer physical removal of matter. Mechanical, diffusion, turbomolecular

Experience from the LEP Vacuum System

Vacuum. Residual pressure can thwart the best cryogenic design. Each gas molecule collision carries ~kt from the hot exterior to the cold interior.

ION Pumps for UHV Systems, Synchrotrons & Particle Accelerators. Mauro Audi, Academic, Government & Research Marketing Manager

Lecture 4. Ultrahigh Vacuum Science and Technology

( KS A ) (1) , vapour, vapor (USA) , saturation vapour pressure. , standard reference conditions for gases. , degree of saturation

Vacuum System of Synchrotron radiation sources

Vacuum II. G. Franchetti CAS - Bilbao. 30/5/2011 G. Franchetti 1

Vacuum. Kai Schwarzwälder, Institut für Physik Universität Basel October 6 th 2006

MOLECULAR SURFACE PUMPING: CRYOPUMPING

λ = 5 10 p (i.e. 5 cm at 10 3 Torr, or ( )

Industrial Surfaces Behaviour Related to the Adsorption and Desorption of Hydrogen at Cryogenic Temperature

Non-Evaporable Getters

1. SYNCHROTRON RADIATION-INDUCED DESORPTION

Repetition: Physical Deposition Processes

NEXTorr HV 100 HIGHLIGHTS

Lecture 3 Vacuum Science and Technology

Generation of vacuum (pumps) and measurements

Vacuum techniques (down to 1 K)

Vacuum I. G. Franchetti CAS - Bilbao. 30/5/2011 G. Franchetti 1

Angular Correlation Experiments

The Vacuum Case for KATRIN

Sputter Ion Pump (Ion Pump) By Biswajit

Ultra-High Vacuum Technology. Sputter Ion Pumps l/s

VACUUM PUMPING METHODS

Cold / sticky system. Vincent Baglin. CERN AT-VAC, Geneva

Previous Lecture. Electron beam lithoghraphy e - Electrons are generated in vacuum. Electron beams propagate in vacuum

To move a particle in a (straight) line over a large distance

Physical Vapor Deposition

Rough (low) vacuum : Medium vacuum : High vacuum (HV) : Ultrahigh vacuum (UHV) :

Study of Distributed Ion-Pumps in CESR 1

Vacuum Technology for Particle Accelerators

Vacuum Solutions for Ion Thruster Testing

A Vacuum point of view

Earlier Lecture. In the earlier lecture, we have seen non metallic sensors like Silicon diode, Cernox and Ruthenium Oxide.

Generation of vacuum (pumps): Vacuum (pressure) measurements:

Conductance of an aperture

DEPOSITION OF THIN TiO 2 FILMS BY DC MAGNETRON SPUTTERING METHOD

Monte Carlo Simulations of Synchrotron Radiation and Vacuum Performance of the MAX IV Light Sources

Vacuum Technology and film growth. Diffusion Resistor

Optimized Annular Triode Ion Pump for Experimental Areas in the LHC

Table 1: Residence time (τ) in seconds for adsorbed molecules

6.5 Optical-Coating-Deposition Technologies

CapaciTorr HV Pumps. making innovation happen,together

A SIMULATION STUDY OF THE ELECTRON CLOUD IN THE EXPERIMENTAL REGIONS OF LHC

Results on a-c tubes subjected to synchrotron irradiation

Lecture 10. Vacuum Technology and Plasmas Reading: Chapter 10. ECE Dr. Alan Doolittle

Chemistry Instrumental Analysis Lecture 34. Chem 4631

NEXTorr Z 100 HIGHLIGHTS

THE LARGE HADRON COLLIDER VACUUM SYSTEM

Electron Cloud Studies made at CERN in the SPS

High-Pressure Volumetric Analyzer

Hydrogen in the LCLS2 Beamline Vacuum

Supercritical Helium Cooling of the LHC Beam Screens

Vacuum gas dynamics investigation and experimental results on the TRASCO-ADS Windowless Interface

Conductance of an aperture

Advanced Lab Course. X-Ray Photoelectron Spectroscopy 1 INTRODUCTION 1 2 BASICS 1 3 EXPERIMENT Qualitative analysis Chemical Shifts 7

Secondary Ion Mass Spectrometry (SIMS)

Electron cloud experiments, and cures in RHIC

PHYSICAL VAPOR DEPOSITION OF THIN FILMS

Ma5: Auger- and Electron Energy Loss Spectroscopy

Continued Work toward XHV for the Jefferson Lab Polarized Electron Source

EXPERIMENTAL INVESTIGATIONS OF THE ELECTRON CLOUD KEY PARAMETERS

Vacuum and mechanical design of ILC DR

The Q Machine. 60 cm 198 cm Oven. Plasma. 6 cm 30 cm. 50 cm. Axial. Probe. PUMP End Plate Magnet Coil. Filament Cathode. Radial. Hot Plate.

Vacuum Systems. V. Baglin. CERN TE-VSC, Geneva. Vacuum, Surfaces & Coatings Group Technology Department

Deuterium Gas Analysis by Residual Gas Analyzer

Chapter III: III: Sputtering and secondary electron emission

Chapiter VII: Ionization chamber

Huashun Zhang. Ion Sources. With 187 Figures and 26 Tables Э SCIENCE PRESS. Springer

CapaciTorr HV 200 HIGHLIGHTS

Conductance measurement of a conical tube and calculation of the pressure distribution

Optimization of the SIS100 Lattice and a Dedicated Collimation System for Ionisation Losses

(4) vacuum pressure & gas desorption in the IRs ( A.

Vacuum System in Accelerator

Ionization Detectors

Ion Implanter Cyclotron Apparatus System

Mass Spectrometry in MCAL

Electrical Discharges Characterization of Planar Sputtering System

A 200 kev Electrostatic Accelerator

Metal Deposition. Filament Evaporation E-beam Evaporation Sputter Deposition

VACUUM SYSTEM FOR STANFORD STORAGE R7NG, SPEAR* U. Curmnings, N. Dean, F. Johnson, J. Jurow, J. Voss ERRATA

Chapter 13: Partial Pressure Analysis

Experimental Results of a LHC Type Cryogenic Vacuum System Subjected to an Electron Cloud

Preliminary design of the new HL-LHC beam screen for the low-β triplets

Vacuum in Accelerators

A PHOTON-STOP FOR THE VLHC-2 ENGINEERING DESIGN PART 1

Extrel Application Note

Partial pressure gauges

Fundamentals of Mass Spectrometry. Fundamentals of Mass Spectrometry. Learning Objective. Proteomics

THIN FLEXIBLE POLYMER SUBSTRATES COATED BY THICK FILMS IN ROLL-TO-ROLL VACUUM

Ionization Techniques Part IV

Introduction to Thin Film Processing

LECTURE 5 SUMMARY OF KEY IDEAS

Experimental techniques of Surface Science and how a theorist understands them

- A spark is passed through the Argon in the presence of the RF field of the coil to initiate the plasma

Progress Report on Chamber Dynamics and Clearing

Partial Pressure Analysis for Large Vacuum Systems

Matti Laan Gas Discharge Laboratory University of Tartu ESTONIA

Transcription:

Vacuum for Accelerators Oswald Gröbner Baden, 22 September 2004 1) Introduction and some basics 2) Pumps used in accelerators 3) Desorption phenomena 4) Practical examples Oswald Gröbner, Retired from CERN Vacuum Group. Present Address: Schmiedgasse 5, Innsbruck, AT-6020, Austria e-mail: Oswald.Grobner@cern.ch, Oswald.Groebner@CHELLO.at 1 Oswald Gröbner

Literature Books: The Physical Basis of Ultrahigh Vacuum, P.A. Redhead, J.P. Hobson, E.V. Kornelsen, American Vacuum Society Classics, American Institute of Physics, 1993 Foundations of Vacuum Science and Technology, Ed. J.M. Lafferty, John Wiley & Sons, 1998 Handbook of Accelerator Physics and Engineering, A. W. Chao, M. Tigner, World Scientific, 1998 CAS CERN Accelerator School : Vacuum Technology, Ed. : S. Turner. CERN 99-05, 19 August 1999 Handbuch Vakuumtechnik, M. Wutz et. al, Vieweg, Braunschweig/Wiesbaden, 2000 Journals: VACUUM Journal of Vacuum Science and Technology (A) Nuclear Instruments and Methods (Section A) 2 Oswald Gröbner

Accelerators at CERN Nearly all CERN accelerators require ultrahigh vacuum Total length of vacuum systems over 60 km LEP is replaced by LHC (cryogenic vacuum system) 3 Oswald Gröbner

Pressure and Molecular Density Ideal gas law: P V = N No R T P pressure, V volume, T temperature N number of molecules R gas constant = 8.31 kj kmol -1 K -1, No = 6.02 10 26 molecules kmol -1 Molecular density n = N V Pressure : P = n k T Boltzmann constant k = 1.38 10-23 J/K Note : R = No k Note: In nearly all cases, it is the gas density rather than the pressure, which matters. Units : Pressure : Pa (N/m 2 ), mbar = 100 Pa, Torr = 133 Pa Gas load : Pa m 3 = 7.5 Torr l, mbar l ~ 2.4 10 19 molecules at RT Specific outgassing rate : Gas release from the walls Pa m 3 /s/m 2 ~ 7.5 10-4 Torr l/s/cm 2 Leak rate : Pa m 3 /s or W, mbar l/s or Torr l/s 4 Oswald Gröbner

Wall collisions Frequency of wall collisions n = 1 4 n v Proportional to the number density n and to the average molecular velocity v. Distribution of Molecular Velocities Maxwell-Boltzmann distribution of molecular velocities at the temperature T 3 1 dn N dv = 4 - m v 2 Ê m ˆ 2 Á 2 2 kt v e p Ë 2 kt 8 kt Average velocity is given by (m = M m o ): v =, numerically ~146 T p M m o M (m s-1 ) Molecular velocities for N 2 at 50, 100, 300 and 500K. Mean molecular velocities at 20 C (m/s) H 2 N 2 Air A Kr 1754 470 464 393 272 5 Oswald Gröbner

Mean Kinetic Energy The kinetic energy : E = 1 kin 2 m v 2 = 1 2 M m Ê 8kT ˆ oá = 4 Ë p M m o p kt M molecular weight, m o = 1.66 10-27 kg E kin does not depend on the molecular mass, M, but only on temperature T. In thermal equilibrium heavy molecules move sufficiently slowly and light molecules move sufficiently fast to carry on average the same kinetic energy. Total and Partial Pressures Each gas component n 1, n 2, n 3, contributes to the total pressure : P i = n i kt The total pressure is therefore the sum of the partial pressures: P = Â P = k T Ân i i i i Partial pressures for atmospheric air Gas % Pi (Pa) N 2 78.1 7.9 10 4 O 2 20.5 2.8 10 3 Ar 0.93 1.2 10 2 CO 2 0.0033 4.4 Ne 1.8 10-3 2.4 10-1 He 5.2 10-4 7 10-2 6 Oswald Gröbner

Mean Free Path D molecular diameter (~3 10-8 m) r v D Volume traversed by a molecule per second : p D 2 v Molecule collides with all other molecules contained within the cylinder of radius D. Number of collisions: Z ª p D 2 v n. The mean free path l = v Z = 1 2 p D 2 n It also follows that n l µ P l ª const. Note: 2 accounts for the fact that molecules in the cylinder are not stationary. For air the product n l ª 2.5 10 14 m -2. For N 2 at 20 C and at 1 Pa -> l ~ 9 mm 7 Oswald Gröbner

Molecular Flow Conditions Knudsen relation: gas flow Q µ DP applies if the mean free path >> relevant dimensions of system Molecular flow conductance c = 4 v (m 3 H 3 /s) L Ú A 2 dl 0 L length of the element (L >> transverse dimensions). H perimeter, A cross section of the element. The conductance is proportional to the mean molecular velocity, i.e. to T M. A cylindrical duct with uniform section and radius r : Ê Ë ˆ c= 4 3 v r3 Á L ~ 306 r3 Á L An orifice (pumping orifice, L~0) : c= 1 4 v A ~ 36.5 A T M. Conductance of elements in series or in parallel add the same as for electric circuits Ê Ë ˆ T M. Series : 1 c = 1 c 1 + 1 c 2 and parallel: c = c 1 +c 2 For complicated geometries it is often necessary to use Monte Carlo calculations for the molecular flow. 8 Oswald Gröbner

Vacuum characteristics gas : Nitrogen, N 2, 20 C, M = 28 Summary expressions: n = P kt kt = 4.04 10-21 Joule r = M mo n M mo = 4.65 10-26 kg mo = 1.66 10-27 kg n = 1 T n v and v = 146 4 1 l = 2p D 2 n D (N 2 ) = 3.15 10-10 m M Pressure P Pa n r n l m -3 kg m -3 m -2 s -1 m atm 10 5 2.5 10 25 1.16 2.9 10 27 9 10-8 primary vacuum high vacuum 1 20 2.5 10-5 1.16 10 22 2.9 10 9 10 10-1 2.5 10 19 1.16 10-6 2.9 10 21-3 9 10-2 10-4 16 2.5 10-9 1.16 10 18 2.9 10 9 10 10-7 2.5 10 13 1.16 10-12 2.9 10 15 1 9 10 4 uhv 10-10 2.5 10 10 1.16 10-15 2.9 10 12 9 10 7 xhv <10-11 9 Oswald Gröbner

Thermal Conductivity Thermal conductivity of a gas is independent of the pressure when the pressure is well above the molecular flow regime. In the transition regime, the heat transfer is proportional to the pressure and to the temperature difference. Principle of pressure measurement with a Pirani gauge. 10-3 Torr < P < 10 Torr At very low pressures, the heat transfer by conduction is negligible : vacuum for thermal insulation in cryogenics. LHC Cryodipole is 10 Oswald Gröbner

Basic Vacuum System V volume (m 3 ), F surface (m 2 ) P pressure (Pa), S pumping speed (m 3 /s) q specific outgassing rate (Pa m 3 /s/ m 2 ) P q F Stationary conditions (P is independent of volume) P = q F S Dynamic pressure V P = q F - S P t S V Solution (constant K depends on initial conditions) P(t)= K e - S V t + q F S The time constant of the pump down: V S To obtain a low pressure : Low outgassing rate of the surface, No leaks! Large pumping speed 11 Oswald Gröbner

Linear Vacuum System (Accelerators) x x+dx x Q(x) q 2S 2L 2S Gas flow: Q(x) [Pa m 3 s -1 ], specific outgassing rate: q(x) ) [Pa m s -1 ] Specific surface area per unit length: A[m], molecular conductance per unit length: c [m 4 s -1 ] dq dx = Aq and Q(x) = - c dp dx c d 2 P dx 2 = - A q 12 Oswald Gröbner

Boundary conditions for this configuration: È dp By symmetry = 0 and the pressure at x = 0 Î dx x =± L P(x = 0) = Q(0) = 2 A q L Q (x = 0) 2 S Ê One obtains a parabolic pressure distribution: P(x) = A qá Ë 2L x - x2 2 c + L ˆ S The average pressure, relevant for the beam: P av = 1 2L 2L Ú P( x)dx 0 Ê = A q L2 3c + L ˆ Á Ë S Note: the pressure is limited by the molecular conductance of the system. In spite of an increase of the pumping speed S, the average pressure is limited to the value : P av min = A q L2 3c Two important requirements : Large diameter of the vacuum chamber Close spacing of pumps 13 Oswald Gröbner

Beam Lifetime due to Vacuum Beam loss by Bremsstrahlung : - de dx = E X o Lifetime 1 t = - 1 N dn dt = cbr X o W X o radiation length, cb speed of the particles and the gas density r = m 0M kt P W is the probability per radiation length to emit a photon with an energy larger than the energy acceptance of the machine so that the particle will be lost. The lifetime t = X o cbrw µ X o P For nitrogen or CO one finds typically tp = 3.410-8 (Torr hours) Consequence : UHV is required for storage rings. Heavy molecules with short radiation length must be avoided. 14 Oswald Gröbner

Turbomolecular Pump Molecules collide with the surface and gain a velocity component in the direction of the movement. Pumping speed of a turbomolecular pump S µ v A S independent of pressure v rotational speed, typically at least >40000 rpm A: pump geometry, large entrance flange Compression ratio of the pump is defined as K = P outlet P inlet Rotor v P outlet = 10-3 mbar P inlet = P outlet /K K is an exponential function of the molecular weight and of the rotational speed (10 3 for H 2 to 10 9 for N 2 ) Hence the compression ratio is large for heavy molecules -> 'clean vacuum' without heavy hydrocarbon molecules. Oil contamination from primary pump can be avoided. 15 Oswald Gröbner

Sputter-Ion-Pump Configuration of a parallel electric and magnetic field produces a self-maintained discharge plasma. -> Penning configuration Ionised residual gas molecules are accelerated towards the Ti cathode and trapped i.e. removed from the gas phase. In a particle accelerator, the magnetic field is provided by bending magnets. --> integrated, linear ion-pumps. To increase the pumping speed, arrays of many cells are used 16 Oswald Gröbner

Pumping mechanisms Gettering -> chemisorption of active species on sputtered Ti film: H 2, CO, N 2, O 2, CO 2 Diffusion -> of H 2 into the Ti- cathode (re-diffusion!) Cracking -> of inert hydrocarbons into C, H, O which can be pumped, chemisorbed Nobel gases: energetic ions of He, Ne, A by implantation into the cathode: ion burial of energetic ions. -> Argon instability due to pumping of large quantities of air. To increase the discharge intensity and thus the pumping speed it is desirable to increase the sputtering rate of the titanium cathode Ë Triode Sputter-Ion pump with grazing incidence of ions on a grid cathode Note: Molecules are not removed from the vacuum system. Therefore, important memory effect of previously pumped gas (Argon). Discharge current is proportional to pressure -> useful pressure measurement. 17 Oswald Gröbner

Surface Pumping Surface pumping speed -> S µ 1 4 v nf Getters (chemisorption E~eV) Evaporable getter pumps (Ti sublimators, Ba getters used in vacuum tubes) Non Evaporable Getters (NEG) Ti, Zr, V Gettering surface achieved by sublimation from a Ti-filament. Surface activation (heating -> reduction of surface oxide layer and diffusion of O into the bulk) Sputter deposited getter film has been a new development for LHC, ESRF and other machines Cryo-pumps (physisorption E~ mev) requires cold pumping surface Sorption (capacity ~ monolayer) Condensation (vapour pressure) 18 Oswald Gröbner

Configuration : Titanium sublimation pump Deposition of a thin film of fresh Ti on the inner surface of the vacuum chamber Filament temperature ~ 1300 deg C To increase the lifetime pumps have several filaments (3 6) Depending on the amount of gas pumped, the film has to be regenerated (e.g. typically at 10-6 Pa after one hour) The pumping speed increases with the surface of the pump and can be very substantial. Note : only chemically active molecules can be pumped. 19 Oswald Gröbner

Non-Evaporable Getters or Bulk getters (NEG) : Getter material ( e.g. Ti, Zr, V) produced in the form of an alloy e.g. with Al and used as a bulk material. For LEP : metal ribbon coated with a thin layer of getter powder has been used. Clean, active, gettering surface is produced by heating under vacuum. Gas adsorbed on the surface diffuses into the bulk and a clean surface can be obtained. Activation requires heating from 350 C up to 700 C for one hour depending on the specific getter. A new development consisting of a combination of evaporable getters and of bulk getters has been developed at CERN -> sputter deposited getter film few mm coated directly onto the inner surface of vacuum chambers. Double advantage : large pumping speed without conductance limitation low outgassing rate. Note: Getters have a limited total pumping capacity and a memory effect of the gas previously pumped. Getters pump only chemically active gas i.e. nobel gases and hydrocarbons (methane, ) are NOT pumped. Combination with ion pumps is required. 20 Oswald Gröbner

Pumping speed of a St101 getter Reduction of the pumping speed due to the gradual saturation of the surface by adsorbed molecules. During re-activation, molecules diffuse into the bulk. A fresh surface is obtained for the next pumping cycle. 10 4 Linear pumping speed (l s -1 m -1 ) 10 3 10 2 activated NEG CO saturated NEG requires reconditioning H 2 10 1 10-4 10-3 10-2 10-1 10 0 Gas load CO (Torr l s -1 m -1 ) 21 Oswald Gröbner

Preparation of LEP vacuum system with NEG pumps Typical bakeout cycle with NEG 180 160 degas activate 1x10-3 1x10-4 recondition 140 1x10-5 Temperature ( C) 120 100 80 60 1x10-6 1x10-7 1x10-8 1x10-9 Pressure (Torr) 40 1x10-10 20 1x10-11 0 0 5 10 15 20 25 30 35 40 45 50 1x10-12 Time (hours) Within less than 12 hours after the bakeout uhv conditions can be achieved. 22 Oswald Gröbner

Cryo-Pumpimg Adsorption of molecules at low temperature -> e.g. at liquid helium temperature A) Sorption Adsorption of gas molecules with low surface coverage, to avoid the effect of the vapour pressure of the condensate. Increasing the effective surface area by a coating with a large specific surface area e.g. charcoal. -> Adsorption isotherms. B) Condensation adsorption in multi-layers -> limitation due to the vapour pressure of the condensed gas. C) Cryo-trapping Cryo-sorption of a gas e.g. H 2 or He with a high vapour pressure in the presence of an easily condensable carrier gas e.g. Ar. 23 Oswald Gröbner

Characteristics of cryo-pumping : Large pumping speed and low limit pressure limitation occurs due to vapour pressure of the condensed gas Large capacity -> Attention!! hazardous over-pressure may build-up during warming up of a cryo-pumped system.! -> a safety valve required! -> clean vacuum -> absence of heavy hydro-carbon molecules. -> in combination with superconducting magnets or accelerating cavities, very effective integrated cryo-pumping can be obtained -> e.g. in LHC -> the walls of the vacuum system act as pumps (LHC). The saturated vapour pressure limits the total quantity of gas, which can be cryosorbed at low pressure. Increase of the specific surface area of a cryo pump by using special cryosorbing materials with a large specific surface -> e.g. activated charcoal. Commercial cryp-pump with a cryo-pannel : Baffel is needed to intercept thermal radiation. Risk of overpressure during warm-up if a too large amount of gas has been condensed. 24 Oswald Gröbner

Cryopumps in accelerator vacuum systems In combination with superconducting magnets or accelerating cavities, at little (or no) extra cost very effective integrated cryo-pumps can be obtained in an otherwise conductance limited vacuum systems. Large freedom in the design of cryopumps: since the cold walls of the vacuum system act as pumps (LHC). The limitations of cryopumps due to the exposure to environmental room temperature radiation and to the bombardment by beam induced energetic particles (photons, electrons, ions) must be taken into account. Imposes -> LN 2 cooled baffles and the LHC beam screen. This requirement arises not only for heat load reasons but mainly to avoid re-desorption of molecules. 25 Oswald Gröbner

Vapour pressure of common gases and of Hydrogen Pressure (Torr) 10-6 10-7 10-8 10-9 10-10 P 4.17k P 3.6K P 3.37K P 3.07K P 2.79K P 2.3K 4.71 K 3.6 K 3.37 K 3.07 K 2.79 K 10-11 2.3 K 10-12 0 1 2 3 4 5 6 7 Coverage (H 2 molecules cm -2 10 15 ) 26 Oswald Gröbner

Thermal Desorption - E Specific desorption rate : q [Pa m 3 s -1 m -2 ] q = Const e kt Molecular residence time t = 1 E ekt Log[q] n o E activation energy for desorption, log[ q] = A - B 1 T n o ~ 10 13 s -1 vibration frequency in the surface potential Physisorbed molecules E < 40 kj/mole (0.4 ev) Chemisorbed molecules E > 80 kj/mole (0.8 ev) 1/T Bakeout between 150 300 C : reduced residence time. Reduction for H 2 O, CO, CO 2 (by factors of 10-2 to 10-4 ) At higher temperature > 400-500 C -> cracking of hydrocarbon molecules (C-H) Note: Strongly reduced thermal desorption at cryogenic temperatures 27 Oswald Gröbner

Thermal outgassing rates of some materials Comparison of organic materials and of metals Unbaked samples (usually H 2 O dominates) Baked samples (24 hours at 150 C to 300 C) Typical values after 50 hours of pumping : (units : Torr l s -1 cm -2 ) Gas Al, Stainless steel H 2 5 10-13 CH 4 5 10-15 CO 1 10-14 CO 2 1 10-14 28 Oswald Gröbner

Synchrotron Radiation Induced Desorption Gas desorption occurs in two steps : 1 -> photons -> produce photo-electrons 2-> photo-electrons -> excite molecules which subsequently can desorb thermally Gas flow : Q = h G, here G is the linear photon flux (photons/s/m) Q µ h I E r +Q o Q o, thermal desorption rate, h, molecular desorption yield (molecules per photon), r, bending radius 10-6 Vacuum conditioning in LEP Dynamic pressure : P dyn = Q S increases proportionally with the beam intensity : DP (Pa/mA). I Beam cleaning (scrubbing) of the vacuum system is an essential procedure in many machines.. Dynamic pressure (Torr/mA) 10-7 10-8 10-9 10-10 10-11 10-1 10 0 10 1 10 2 10 3 10 4 10 5 Beam dose (ma h) NEG reconditioning 29 Oswald Gröbner

Hot Filament ionization Gauge Operating principle : Residual gas molecules are ionized by the electrons emitted from a hot filament. Ions are collected by a "collector electrode". This ion current is proportional to the gas density, n, and hence to the total pressure, P. The ionization probability Pi (number of ion electron pairs produced per m and per Pa) depends on the type of molecule and on the kinetic energy of the electrons. Ion collector current : I + = Ie Pi L P Where : Ie emission current of the filament, L, path length of the electrons, P total pressure Product Pi L i.e., the gauge sensitivity is obtained by calibration. 30 Oswald Gröbner

Partial Pressure Measurement Combination of an ion source with a mass spectrometer: 1) Ion source 2) Quadrupole mass filter 3) Ion collector, Faraday-cup or secondary electron multiplier Ions with different mass to charge ratio are injected into the quadrupole structure. As they traverse the structure, ions are subjected to a periodically varying transverse electric field, which excites transverse oscillations. Ions with an incorrect charge to mass ratio have unstable orbits, are lost and do not reach the collector. Qualitative analysis is relatively straightforward, e.g. identification of: H 2, H 2 O, CO/N 2, O 2, CO 2 Quantitative analysis requires a perfectly calibrated system and knowledge of cracking pattern for each residual gas component. 1,40E-10 1,20E-10 1,00E-10 8,00E-11 6,00E-11 4,00E-11 2,00E-11 0,00E+00 0-2,00E-11 10 20 30 40 50 60 Série1 31 Oswald Gröbner

Criteria influencing the Choice of Materials Low outgassing rate Low vapour pressure Temperature resistant -> bakeout Thermal and electrical conductivity -> beam interaction Corrosion resistance -> leaks Low induced radioactivity -> handling High mechanical strength -> 1dN/cm 2 external atmospheric pressure! Machining, welding Low cost Common choices: Stainless steel Aluminium Copper Ceramics for electric insulation Low porosity -> leaks Brazing to metal -> leaks For particular applications: Be for detectors for high transparency Organic materials (e.g. as composite materials (carbon-fibre & epoxy), polymers to be used in small quantities 32 Oswald Gröbner