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Chinese SONG progress and its design introduction Guomin Wang gmwang@niaot.ac.cn2011-9-16 Nanjing Institute of Astronomical Optics & Technology Nanjing Institute of Astronomical Optics & Technology SONG 4 th Workshop College of Charleston
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Outline: Progress introduction Telescope design introduction
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PROGRESS INTRODUCTION
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August 13, 2010: Finished the PDR
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December 25, 2010: Finished the CDR
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Now, we are… Structure constructing
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Now, we are… mirror fabrication Mirrors material test report from Russia LZOS Preparing
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Large bearing manufacturing Azimuth bearing φ680 × φ880 × 80 Delivery time: 4 months
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Large bearing manufacturing Altitude bearing φ240 × φ320 × 38 Delivery time: 4 months
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Preparing contract for long-term elements, such as... Torque motors Encoders
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Telescope schedule ItemScheduleStatus Preliminary Design ReviewAug., 2010Closed Critical Design ReviewDec., 2010Closed Factory AcceptanceNov., 2012On going Ready for ShipmentDec.,2012... On site AcceptanceApr., 2013...
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TELESCOPE DESIGN INTRODUCTION
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General requirements Cassegrain system; M1: paraboloid, 1m clear aperture, Zeodur material, active support and close-loop controled through S-H; M2: hyperboloid, fused silica material, active positioned by 5- DOF unit; M3: flat mirror, Zeodur material, 180°turn to direct the light to different Nasmyth platform; System ratio: F/36.7;
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General requirements Image quality: 80% energy encircled in 0.3″ @ lucky imaging focus ; Nasmyth focus: VIS camera (450 - 650nm), RED camera (650 - 1000nm), Focus monitoring camera (< 450nm), auxiliary focus; FOV @ Nasmyth: R32.52″ ; Coudé focus: spectrograph (480 - 680nm); FOV @ Coudé: 10″ ; ADC: doublet prism; Optical derotator: three - mirror
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General requirements Range of azimuth: 0 º ~ ±220º; Range of altitude: 10 º ~ 89º Max. acceleration: 2 º/sec 2 ; Max. pointing speed: 20 º/sec; Blind spot: 2 º (diameter); Tracking accuracy: RMS 0.3″, 90s, no guiding ; Pointing accuracy: RMS 5″, 70 º ≥ ZD ≥1 º; Repeat pointing accuracy: ≤ RMS 1″, 70 º ≥ ZD ≥1 º; First frequency: large than 8 Hz;
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General view
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F/36.7 layout
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F/36.7 parameters ItemParameters M1ф1000 Primary ratioF2.3 System ratioF36.667 Primary focus length2300 System focus length36666.8 ( λ=546.1nm ) FOVR32.52″ M1-M2 distance2100 mm M2–M3 distance1600 mm M3–focus distance1588.3 mm Working wavelength VIS ( λ=450 ~ 650nm ) RED ( λ=650 ~ 1000nm )
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F/36.7 imaging quality after ADC Spot diagram of VIS @ ZD = 5 °
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F/36.7 imaging quality after ADC Spot diagram of VIS @ ZD = 45 °
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F/36.7 imaging quality after ADC Spot diagram of VIS @ ZD = 75 °
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F/36.7 imaging quality after ADC Spot diagram of RED @ ZD = 5 °
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F/36.7 imaging quality after ADC Spot diagram of RED @ ZD = 45 °
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F/36.7 imaging quality after ADC Spot diagram of RED @ ZD = 75 °
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Nasmyth optical design From telescope To Coudé
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Nasmyth structure
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Coudé optical design From telescope
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Coudé structure
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Optical elements list Item Size ( mm ) MaterialCoatingAccuracyQty. M1φ1030x75ZeodurAL λ/50 1 M2φ96x25Fused silicaAL λ/60 1 M3φ76X15 ZeodurAL λ/60 1 M4φ30x5ZeodurAL λ/60 3 M5φ54x8ALZeodurλ/605 Wedge prism φ40x6, ∠ 5° H-LAK10/H- ZF1 450-1000nm antireflection λ/60 2 K mirror 160x44x10ZeodurAL λ/60 2 K mirror 236x30x8ZeodurAL λ/60 1 Dichroic mirror 1 φ30x3Fused silica 450-620nm (R) 680-1000nm (T) λ/30 1 Dichroic mirror 2 φ30x3Fused silica 450-620nm Half-reflection λ/30 1
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ItemSize ( mm ) CoatingMaterialAccuracyQty. Field lens 1φ20x4AntireflectiveH-K9LN=1, ΔN=0.11 Field lens 2φ20x5AntireflectiveH-K9LN=1, ΔN=0.11 Achromatic lense1φ20x7.5AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.21 Achromatic lense2φ20x7.2AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.21 Achromatic lense3φ38x7.5AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.21 Achromatic lense4φ22x7AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.21 Achromatic lense5φ24x9AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.21 Achromatic lense6φ22x7.2AntireflectiveH-K9L/H-ZF2N=1, ΔN=0.22 Protect mirrorφ54x8AntireflectiveFused silicaλ/103 Dichroic prism32x32x3 2 AntireflectiveFused silica λ/10 ± 10″ 1 Dichroic mirror 4φ32x3Half-reflectiveFused silicaλ/101 Tilt mirrorφ32x5Al 480-680nmZeodurλ/201 Filterφ22x3480-680nmFused silicaλ/103
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Basement Structure Constrained the 8 fixed anchor bolts; Applied 3.5 t on the bearing place to simulate the above weight; Apply 1g on the structure; Apply 700N on the place of 1373mm from the bearing to simulate the wind force at 15 m/s; Max. stress: 49.92 MpaMax. deformation: 0.022 mm
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Levelness adjustment Rated load (N) Max. load (N) Unit torque (Nm/10 4 N) Adjustable height of adjusting bolt (mm) Adjustable height (mm) Unit weight (kg) 20000600002.50.2557 Table 2-1 Parameeters of iron pad
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Azimuth bearing Type Crossed roller bearing d680 mm D880 mm H80 mm Axial runout< 0.02 mm Radial runout< 0.02 mm Axial sitffness5000 N/m Radial stiffness10000 N/m Tilt stiffness 450000 Nm/mrad
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Azimuth encoder
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Azimuth motor Friction torque: 67.5N.m ; Inertial torque: 50N.m ; Wind torque: 139N.m ; Swiss Etel Company: TMB0450-100; Rated torque: 561Nm; Rated current: 11.3A;
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Max. deformation: 0.042mm Constrain nodes connecting to bearing; Add 1180N on top surface of center section to simulate the above weight; Add 5390N on the down surface to simulate the down weight; Add 1g to the structure; Apply 400N at the place of 149.5mm above center section to simulate the wind force; Max. stress: 12.64 Mpa
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M1 support ¢ 1010mm, thickness 45mm, center hole 65mm, flat bottom; Axial supporting: Fixed supporting: 3; Pneumatic active supporting: 33 (6+9+18); Lateral supporting: 10 counterweight level; R1 = 151.72mm, F1 = 28.664N ; R2 = 296.5mm, F2=31.183N; R3 = 449.12mm, F3=36.775N;
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Mirror cell calculation Max. stress: 2.9 MPaMax. deformation: 0.58 um
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Force actuator Diaphragm Air Cylinder(Bellofram)
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Electro- pneumatic regulator SMC Regulator
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Force sensor
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M2 positioning unit Δx (ΔY)±7 μm ΔZ±3μm Δθx(Δθx)±20″
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43 M1-M2 offset calculation θ° uy ( um ) uz ( um ) Rotx(″) 00.0011.710.00 101.5211.570.14 202.7911.150.27 303.8010.440.39 404.569.440.50 505.108.130.58 605.466.510.65 705.684.590.70 805.792.410.73 905.830.000.74 Uz-altitute angleUy-altitute angle Rotx-altitute angle
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Frequency calculation ModeFrequency (Hz)Mode shape 124.8Fork lateral 226.8Fork fore-and-aft 346.4Truss lateral 452.2Truss fore-and-aft 554.5Top ring torsion 673.7Center section
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Control architecture
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TCS configuration Master Computer (Advantech Industrial PC) Slave Computer(UMAC)
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M2 control configuration
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Communication
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3-D Of SONG telescope
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THANK YOU !!!
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