PANAREA IMAT F. Aliotta IPCF-CNR, Messina, ITALY With the ISIS is actually project TS2, the in world’s July 2003 leading began pulsed the neutron and muon construction of a second source.target station at ISIS. -2·s -1). It is 3a August On high flux 2008, pulsed thesource first neutrons (~1012 n∙cm from the The time new targetwidth station of the havemoderated been measured. neutron pulse The secondoftarget station project was at theISIS beginning its path toward the sample completed in the 2009. seven rate Phase One is ~20 ms and pulseAll repetition is 60Hz. neutron are operational. The timeinstruments width of the pulse on the sample depends on the length of the path to the sample area (after tenths of meters the pulse width becomes several hundreds ms). Since 1985, CNR has been supporting the access of italian researchers to the neutron spectroscopy techniques here available. CNR-CCLRC International Agreement for the utilization of the ISIS spallation neutron source in the Rutherford Appleton Laboratory. (CCLRC=Council for the Central Laboratory of the Research Council) Harwell Science & Innovation Campus Diamond ISIS TS-I 20 instruments 50 Hz Target: W, clad in Ta 150 kW 160 μA (240 μA) Proton energy 800 MeV TS-II: 7 instruments 10 Hz Target: W, clad in Ta ( 6.6, 27 cm) 48 kW 40 μA (60 μA) With the project TS2, in July 2003 began the construction of a second target station at ISIS. On 3 August 2008, the first neutrons from the new target station have been measured. The ISIS second target station project was completed in 2009. All seven Phase One neutron instruments are operational. In 2008 a new agreement for collaboration between CNR and STCF Since 1985, CNR has been supporting access of italian researchers to hasthe been performed. the neutron spectroscopy techniques Within here available. this agreement a new project, PANAREA, will be developed, that will be co-financed by CNR and STCF CNR-CCLRC International Agreement for the utilization of the ISIS (2008-2016). Appleton Laboratory. spallation neutron source in the Rutherford (STFC=Science and Technology Facilities (CCLRC=Council for the Central Laboratory of the Research Council) Council) CHIPIR IMAT Progetto per l'CHIP Applicazione dei Neutroni Alla IRradiation IMage and MATerials Ricerca in Elettronica e Archeometria science and engineering Agreement concerning collaboration in scientific research at the spallation neutron source ISIS [...] CNR shall collaborate with CCLRC in the exploitation of ISIS by making contributions as follows: [...] Aiming to collaborate with CCLRC in the development of mutually beneficial instrumentation and techniques associated with the utilisation of ISIS Target Station 1 and especially its new Target Station 2. IMAT A thermal-cold imaging / materials science beamline for TS-II CHIPIR IMAT CHIP IRradiation IMage and MATerials science and engineering The possibility of non-destructive testing and the penetration power of neutrons is the basis of a materials science instrument for engineering, geology, and archaeological sciences. Imat will allow the study of novel alloys and composite materials, phase transformations, creeps and fatigue, corrosion, and ancient fabrication techniques. Available Techniques: Applications: Imaging mode diffraction mode •Neutron radiography and tomography •Aerospace and transportation •Diffraction-enhanced imaging •Fuel and fluid cell technology •Neutron strain •Cultural heritage IMAT will bescanning a world-leading pulsed-source cold neutron radiography •Rapide •Earth sciences stationtexture and analysis facility for materials science, materials processing and •Engineerig and reverse engineering engineering. IMAT diffraction mode Texture capabilities are already IMAT will analysis be significantly complementary to available at thewhich GEM is and POLARIS designed instruments ENGIN-X (TS1) specifically for on ISIS TS1. lattice spacings in engineering evaluating IMAT willmaterials have a in highly flexible and spacious relevant minimum times. sample area to accommodate a diverse range of IMAT will employ a relaxed resolution to bias engineering-specific and user-supplied sample towards higher intensity, and will provide environment and processing cells andinallow greater solid angle detector coverage orderfor to GEM motorised spatial scanning. evaluate texture, phase volume fractions, and strain orientation distributions POLARIS in short data acquisition The instrument will be ideally suited totimes. in-situ The simultaneous processing studies, in which materials areanalysis of internal stress and will be a unique and key capability of the typically peak-broadened sotexture that instrumental beamline. resolution is not a critical parameter. Bragg edge analysis allows to obtain information about the stress and deformation distribution in mechanical components. Energy resolved imaging would allow to clearly distinguish among different materials. To tune the neutron energy around the Bragg edge of the material of interest results in the increasing of the phase contrast. The otained image can be used to select the sample volume which must be investigated by diffraction technique. The fine selection of the neutron energy allows to evidenciate any small local deformation of the crystaline lattice. IMAT: instrument parameters diffraction Common features ofimaging IMAT for the two operating modes are a Bragg edge target/moderator TS-II /broad-face, decoupled solidTS-II /broad-face, decoupled solid-CH4. detector, the sample positioning systems and the sample environment. CH4. (Alternative: /coupled LH2 Switching IMAT from imaging to TS-II diffraction mode must not require sample for high intensity imaging). removing. This will allow a complete survey of a sample by 2D or 3D imaging, wavelength range 1 - 7 Å (dmax at 180°: 3.5 Å l-Ni(100)); 1 - 7 Å (dmax at 180°: 3.5 Å l-Ni(100)); followed by a detailed diffraction analysis of the interesting regions guided by the tomography data.adjustable apertures D=10-100 mm incident motorised jaws, 0.1-20mm; ellipsoidal collimation/focussing beam size/field of view for varying L/D >300 mirror for focussing simulated intensity distribution maximum 20x20 cm2 variable (max horizontal/vertical: 8/20mm) flight path moderatorpinhole 10 m 10 m flight path pinhole sample ~25 m ~25 m spatial resolution image mode better than 0.2x0.2 mm diffraction mode operating mode: 5x5x5 mm3, standard variable from 1-10mm An ellipsoidal mirror will allow switching between image mode and diffraction n/a Δd/d: 0.3 % at 2θ=90° mode with a collimated neutron beam. The neutron focusing device is curved in outgoing beam n/aa length of about 10 m and a standard mode 5 mm, radial two dimensions, with height of about 10removable cm. d-spacing resolution collimation divergence 90° collimators for variable resolution L/D: > 300 (< 0.2° vertical and horizontal) 0.35° horizontally; vertically larger; tunable IMAT drawings Polref Inter Offspec Wish Nimrod Let IMAT TS-II phase 2 IMAT moderator Material LH2, 22K IMAT LAMOR Solid-methane, 26 K De-coupler none Poison none W5 size 110 mm high CHIPIR IMAT on W5 ZOOM Aperture selector D = 10 , 20 , 40 , 75 mm + open L/D = 1000, 500, 250, 133 Incident beamline LET IMAT Disc chopper 1: 10 Hz Position: 12.8 m Source repetition 10 Hz Moderator Liquid H2 /T0-chopper: solid CH4 coupled20 Primary neutron guide Position: 21.1mm m m=3 straight, square, 95x95 Single frame bandwidth 0.5 - 6.5 ǺDisc Flight path to sample 56 m Hz chopper 2: 10 Hz Position: 21.5 m IMAT blockhouse Pinhole selector Day-1 90-degree detectors sample Imaging cameras Diffraction instrument • Large detector coverage for rapid phase and texture analysis • Scintillation detectors; fibre-coded or wavelength shifting fibres • Highly pixellated; each pixel <5deg • Medium spectral resolution for strain analysis Primary flight path 56 m L: pinhole-detector 10 m D: pinhole sizes 10, 20, 40, 75 mm L/D 1000, 500, 250, 133 Spatial resolution Standard: 200 micron Minimum: 100 micron Wavelength resolution 0.7 % at 3Å Neutron flux (L/D=250) 2 ·107 neutrons·cm-2·s-1 Max. field of view 200 x 200 cm2 Strain analysis performance IMAT 400000 intensity E8: de-coupled CH4 W5: coupled H2 200000 ENGIN-X diffraction resolution (3Å/90º) 0.69 % 0.33 % strain resolution [microstrain] 70 50 Bragg intensity 3 Å [a.u.] 8.5 1.0 0 1.8 1.9 2.0 2.1 2.2 2.3 d-spacing (Angstrom) Neutron Flux Gain over ENGIN-X Imaging instrument • High flux moderator • Energy resolution better than 0.8% • Two imaging positions • Gated CCD + Bragg edge transmission detectors Primary flight path 56 m L: pinhole-detector 10 m D: pinhole sizes 10, 20, 40, 75 mm L/D 1000, 500, 250, 133 Spatial resolution Standard: 200 micron Minimum: 100 micron Wavelength resolution 0.7 % at 3Å Neutron flux (L/D=250) 2 ·107 neutrons·cm-2·s-1 Max. field of view 200 x 200 cm2 Imaging instrument: tests (1st prototype) First questions: are we able to get conventional tomography images from the beam flux available at the ISIS pulsed source? are we able to obtain the required spatial resolution performances? First prototype (installed at INES) •Flight Path L = 23.84 m •Source Dimension D ~ 8.5 cm => L / D ~ 280 •Sample-scintillator distance l ~ 10 cm (Mean) •Spatial Resolution: 0.26 < d < 0.42 [mm] •Camera CCD not cooled 640x480 - 8 bit •Optics 8 mm, f: 1.4 •Scintillator ZnS / 6LiF on Al substrate The Imaging Source: DMK 21BF04 Imaging instrument: tests (1st prototype) Imaging instrument: tests (2nd prototype) Further questions: which kind of imaging device is more appropriate to obtain high spatial resolution images on the large field (20x20cm2) that will be available at IMAT? is it possible to obtain the required time resolution by any commercial imaging device? are there practical perspectives to reach an enough high efficiency of energy selective image acquisition? which kind of scintillator plate can ensure us a bright image together with the required space and time resolution performances? which is the better geometry to minimize radiation damages effects of the CCD (or any other imaging device)? Second prototype (portable test chamber) •Flight Path L = variable •Source Dimension D variable •Sample-scintillator distance 8 cm l 30 cm •Spatial Resolution: variable •Camera CCD inter-changeable •Optics 35÷135 mm, f: 4.5÷5.6 •Scintillator variable Scintillator plate Mirror Rotating platform X-Z translator CCD Imaging instrument: tests (2nd prototype) Test at ROTAX sample: nail from a medieval wreck found in the Palermo Gulf. CCD: Andor iStar DH712 scintillator plate: ZnS(Ag)6Li Imaging instrument: tests (2nd prototype) Tests at ROTAX CCD: Andor iStar DH712 scintillator plate: ZnS(Ag)6Li Sample 1: fibula Sample 2: snail Imaging instrument: day 1 CCD Andor iStar 734 Specification Summary Effective active area of CCD Fibre optic taper magnification Effective CCD pixel size Active pixels Read noise 13.3x13.3 mm2 1:1 13x13 mm (100% fill factor) 1024X1024 As low as 2.9e Frame rate (image/sec max,) 0.9 Useful photocatode spectral range 120 – 1090 nm Photocatode QE Minimum optical gate width Up to 50% 1.2 ns Imaging instrument: overall scintillator spatial spatial resolution resolution test tests Slanted Edge Method Line Spread Function 450 Experimental Linear Fit of B Point Spread Function Resolution [mm] 400 350 300 Equation y=a+ Adj. R-Sq 0.9243 250 Value 200 200 300 Standard B Interce 169.89 15.9944 B Slope 0.3241 0.04112 400 500 600 Thickness [mm] 700 800 Imaging instrument: time resolution requirements At TS2 the distance between pulses is 20 ms. The acquisition of energy resolved images with enough energy resolution to distinguish the Bragg edge shift originated by local deformation of a material implies a time resolution of 10 ms. 20 ms 20000 images are required to cover the 20ms interval between pulses with 10 ms aquisitions. Imaging instrument: time resolution requirements At IMAT: the neutron beam section will be 20x20cm2; the estimated neutron flux is about 2∙107 neutron/s. With a 1024x1024 pixel detector, the average counting rate on each pixel will be of 0.95 over 10ms. 20 ms On day 1, recording an image at a single energy value will require an acquisition time of about 30s. Imaging instrument: scintillator time resolution tests type thickness N1 6LiF/ZnS:Ag 225 mm N2 6LiF/ZnS:Cu 225 mm N3 6LiF/ZnS:Ag 450 mm Cu Fe 15.5ms – 0.5ms Cu Fe G.Salvato, F. Aliotta, V. Finocchiaro, D. Tresoldi, C.S.Vasi, R.C. Ponterio – 2010. Nuclear Instruments and methods in physics research, A14.3ms 621, 489, 0.5ms Imaging instrument: drawings of the camera available room: 400x660x900 mm3 requirements: 2048x2048 CCD ready, user friendly OPTICS lens: NIKON 85mm f/1.4 Newport mirrors: silicon wafer (Al coated) Edmund Optics NEUTRON TOMOGRAPHY IN EUROPE Reactors 1. 2. 3. 4. 5. 6. FRM-II BENSC (CONRAD) CASACCIA CEA ATOMINSTITUT KFKI Garching, GERMANY (fast neutrons, 8∙1014 n·cm-2∙s-1) Berlin, GERMANY (cold neutrons, 109 n·cm-2∙s-1) Rome, ITALY (thermal neutrons, 2∙106 n·cm-2∙s-1) Saclay, FRANCE (thermal neutrons, 3.4∙106 n·cm-2∙s-1) Wien, AUSTRIA (thermal neutrons, 1.3∙105 n·cm-2∙s-1) Budapest, HUNGARY (thermal neutrons, 108 n·cm-2∙s-1) Neutron Spallation Sources 1. SINQ (NEUTRA, PGA) Villigen, Switzerland (thermal and cold neutrons, 1014 n·cm-2∙s-1, continuous) 2. LPI Moscow, Russia (thermal and fast neutrons, 109 n·cm-2∙s-1, pulsed)