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M. R. Howells, Advanced Light Source DIFFRACTION GRATING MONOCHROMATORS (PGMs) Malcolm R. Howells Advanced Light Source

DIFFRACTION GRATING MONOCHROMATORS (PGMs) · 2017. 3. 30. · M. R. Howells, Advanced Light Source COLLIMATED LIGHT SX700 (CLSX700) • This is the current and deservedly the most

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  • M. R. Howells, Advanced Light Source

    DIFFRACTION GRATING

    MONOCHROMATORS

    (PGMs)

    Malcolm R. Howells

    Advanced Light Source

  • M. R. Howells, Advanced Light Source

    PLANE GRATING SYSTEMS: GENERAL

    Focus condition for a spherical grating

    cos2

    r− cos

    R

    +

    cos2

    ′ r − cos

    R

    = 0 let R ⇒ ∞ → ′ r = −r

    cos2

    cos2

    Note that if r = ∞ then ′ r = ∞ irrespective of cff i.e . the grating then does no focusing

    Using cff =cos

    cos and recalling that M = −

    ′ r r

    cos

    cos → M = cff

    Eliminating between

    m

    d0= sin + sin and cff =

    cos

    cos

    sin =

    m

    d−

    m

    d

    2 1

    cff2 + 1−

    1

    cff2

    2

    1−1

    cff2

    r

    r'

    B

    A

    Grating

    α β

    Source point

    Virtualimage

    (of the grating alone)

  • M. R. Howells, Advanced Light Source

    COLLIMATED LIGHT SX700 (CLSX700)

    • This is the current and deservedly the most popular of many versions (used in ALS MES project)

    • The original (Petersen) held fixed focus by maintainingand introduced the still-essential mechanism for positioning the plane mirror (next slide)

    • CLSX700 has constant focus position irrespective of the value of cff which therefore becomes a user-controlled variable

    • This can be used to track the efficiency maximum, suppress high orders or maximize resolution

    • Sagittal focusing mirrors reduce sensitivity to manufacturing errors (Jark 1992) see next slide, othertypes were paraboloid (Kunz 1968), ellipsoid (Petersen 1982), elliptical cylinder (Nyholm 1985) orsphere (Padmore 1989)

    cff = cos cos = 2.25

    Kunz 1968Petersen 1982Follath 1997

  • M. R. Howells, Advanced Light Source

    FORGIVENESS FACTOR

    Requirement: ′ s T ≤1

    2′ s T → 2 ′ r T ≤

    1

    2

    ′ r r

    sT

    T ≤1

    4

    sTr

    ′ s S ≤12

    ′ s S → 2 ′ r S ≤12

    ′ r

    r sS

    S ≤14

    sSr

    Reasons for the factor 2's:

    1. Ray deviation is twice that of the mirror

    2. Quadratic sum of and /2 is 1.1 implying a 10% error which we declare acceptable

  • M. R. Howells, Advanced Light Source

    THE ZEISS MIRROR MECHANISM

    • Reimer 1983• Pimpale 1991

    • This mechanism, patented by BESSY and Zeiss, is a major reason for the success of this design

    • The idea is to find a point about which to rotate the mirror such that the central ray always hits thegrating pole - this can be done with only a few microns error

    • The easy and less accurate solution is continue the mirror surfaces at maximum and minimum angle tointersect the y axis and take the average of the two points - this will be near A (0, D/2) for small angles

    • More accurate solutions (Pimpale 1991) are close to B (0, 3D/2) - best solutions are good within 10µmif D ≤ 8 cm and the grazing angle is less than 10° - B itself is a good solution to within 10 µm if D ≤ 3cm and the grazing angle is less than 10°

  • M. R. Howells, Advanced Light Source

    SOME WORKING CURVES FOR PGM’S

  • M. R. Howells, Advanced Light Source

    • 300/mm grating

    • 79°<

  • M. R. Howells, Advanced Light Source

    m

    d= sin + sin so

    = d cosm

    d

    dq=

    d

    d

    d

    dq=

    d cos

    m ′ r

    Fractional bandwidth due to the entrance slit is

    source

    = qr

    cos

    m d≡ s

    r A cff( )

    Angularerror

    Normalizedangulardispersion

    In the small - angle approximation

    A cff( ) ≅ dm

    2

    cff2 −1( )

    NB - the grating changes the angular

    spread by 1cff (cff is the magnification)

    Follath 1997, 2001

    source

    =s

    r A cff( )

    exit

    slit

    = ′ s

    ′ r cff A cff( )

    aberr

    = ′ y ′ r

    cff A cff( )

    preopt

    = po A cff( )

    focopt

    = fo cff A cff( )

    grating

    = gr 1 + cff( ) A cff( )

    total

    =

    i

    2

    i∑ = 1

    R

    CONTRIBUTIONS TO THE SX700 RESOLUTION

  • M. R. Howells, Advanced Light Source

    BESSY U125/1-PGM

    Foc optic 0.05 sec

    Slit 10 µm

    Grating 0.2 sec

    Preoptic 0.25 sec

    Source 50 µm

    Follath 2001

    –ve order +ve order

    BESSY U125/1-PGM

    Preoptic 0.25 sec

    Source 50 µm

    Foc optic 0.05 sec

    Grating 0.2 sec

    Slit 10 µm

    RESOLUTION CONTRIBUTIONS FOR A BESSY PGM

    TOTAL

    TOTAL

  • M. R. Howells, Advanced Light Source

    Petersen 1986

    SGM –veorder

    SGM +veorder

    WORKING CURVES FOR cff=2.25 ETC

  • M. R. Howells, Advanced Light Source

    BESSY CLSX700'S: SUMMARY

  • M. R. Howells, Advanced Light Source

    BESSY U125/1-PGM BEAM LINE

    Follath 2002

    Effective total length = 27 m

  • M. R. Howells, Advanced Light Source

    BESSY PGM RESOLUTION DEMONSTRATION

    • Doppler width 0.4 meV

    • Monochromatorcontribution 0.65 meV

    • Resolving power=1.0x105

    • Rotation increments- grating: 17 nrad- mirror: 9 nrad

    • Measured with 1200/mmgrating at cff =10 to 12

    Picture from R. Follath, BESSY

  • M. R. Howells, Advanced Light Source

    1200mm

    300/mm

    Where we are(925/mm)

    Where they are

    BESSY PGM'S: RESOLUTION SUMMARY

    Where we'd like to be

  • M. R. Howells, Advanced Light Source

    Mono angles

    75eV 2000eV

    Cff = 1

    Cff = 10

    thermaldistortionn

    good higher ordersuppression

    goodefficiencywith deepgrooves

    goodefficiencywithshallowgrooves

    resolutioninsensitive to slopeerrors

    mechanical limits

    largeincludedangle

    smallincludedangle

    mechanical limits

    Parameters for this study:150 lines/mm 25nm groove depth (operating from 75 eV to 800eV)(low dispersion)

    1200 lines/mm 6nm groove depth (operating from 300 eV to 2000eV)(high dispersion)

    Slide from TonyWarwick

  • M. R. Howells, Advanced Light Source

    OPTICAL PATH FUNCTION: VARIED-LINE-SPACING GRATINGS

    d(w) = d0 1 + v1w + v2w2 + ...( ) n w( ) = ni00wi

    i=1

    F = Cijkijk∑ ,r( )wil j zk + Cijk

    ijk∑ , ′ r ( )wil j ′ z k + m

    d0nijk

    n100 =1n200 = −v1 2

    n300 = v12 − v2( ) 3

    n400 = −v13 + 2v1v2 − v3( ) 4

    nijk = 0 if i or k ≠ 0

    Now the groove spacing d(w) and number n(w) are functions of w and are also expressed as power series

    So the optical path function becomes

    Evidently the use of VLS can benefit aberrations of the form i00:

    Defocus, coma, spherical aberration but not ones with j, k ≠0

  • M. R. Howells, Advanced Light Source

    WHY DO VLS GRATINGS WORK?

    The spherical - grating focus condition is now:

    F( )200 =1

    2w2

    cos2

    r−

    cos

    R

    +

    cos2

    ′ r −

    cos

    R

    v1m

    d0

    = 0

    So setting R = ∞, using the grating equation and switching to grazing angles a, b

    1

    ′ r =

    cos a − cos bsin2 b

    − 1

    r

    sin2 a

    sin2 b=

    1

    rv1r

    −2sina + b

    2

    sin

    a − b2

    sin2 b −

    sin2 a

    sin2 b

    Now approximating sin a ≅ a etc

    1

    ′ r =

    1

    r−v1r

    a2 − b2

    2b2 −

    a2

    b2

    Evidently if v1 =−2r

    then ′ r = −r

    IDENTICALLY (for all values of a, b

    and thus . Moreover if, in addition,

    v2 =1

    r2 then coma and sperical aberration

    are corrected as well under the same small -

    angle assumption

    B

    Source point r

    r'

    A

    Grating

    α β

    Virtualimage

    This works equally well in converging or diverginglight (principle of reversibility) although the literaturediscusses only converging.

  • M. R. Howells, Advanced Light Source

    -4.0E-06

    -2.0E-06

    0.0E+00

    2.0E-06

    4.0E-06

    6.0E-06

    8.0E-06

    1.0E-05

    0 20 40 60 80 100 120 140

    Wavelength (Å)

    0.0E+00

    1.0E-03

    2.0E-03

    3.0E-03

    4.0E-03

    5.0E-03

    6.0E-03

    0 500 1000 1500

    Wavelength (Å)

    DOES v1 = –r/2, r' = –r GIVE OPTIMUM FOCUSING?

    • No - the usual procedure is to write the focus equation twice for two wavelengths of exact focus and solve for r' and v1 -(this requires a fixed included angle or at least a fixed focusing principle) - the nominal focal distance then changes by asmall amount (2% in the above case) - this gives locally better focus although not much improvement over a large range

    • Note that all of the design studies in the literature except one (Koike 1995) consider only fixed-included-angle cases andoffer, sometimes very good, although still approximate solutions but they have SGM-like disadvantages.

    • Now that the variable-included angle schemes are available we have exact focus solutions such as CLSX700 or classicalSX700 although the latter does not give control of the included angle to the user.

    • Therefore retrofitting VLS to a standard SX700 makes some sense to give user control of the included angle howevernote that the focal length or the focal distance of the mirror would have to change.

    • Conclusion: VLS role in general-purpose monochromators is becoming minor but it is still strong in spectrographs.

  • M. R. Howells, Advanced Light Source

    0.00001

    0.0001

    0.001

    0.01

    0.1

    1

    1 10 100 1000 10000Wavelength (Å)

    Defocus

    1 µr slope error

    Mirror coma

    Source size

    Total

    • VLS solution with cffchosen for maximumefficiency (between 1.5and 2.5)

    • Wavelengths of exactfocus: 20 Å and 80 Å

    • Source: size 50 µm anddistance 15 m

    • Beam height: 2mm

    • Inside (+ve) order

    • 1200/mm

    VLS RETROFIT TO AN SX700

  • M. R. Howells, Advanced Light Source

    MES PROJECT CALCULATIONS

    First, second and third orderefficiency calculations for alaminar grating 150/mm

  • M. R. Howells, Advanced Light Source

    MES PROJECT CALCULATIONS

    Source-size-limited resolving power fora source of size FWHM = 40 µm atdistance 12 m with a 150/mm grating

  • M. R. Howells, Advanced Light Source

    MES PROJECT CALCULATIONS

    Cylindrical mirror slope errorneeded to get a resolving power of7500 with the 150/mm grating

  • M. R. Howells, Advanced Light Source

    MES PROJECT CALCULATIONS

    Grating slope error needed toget 7500 resolving power with150/mm grating

  • M. R. Howells, Advanced Light Source

    Mirror cooling for high heatload at low energy (75eV)

    slope error for glidcop mirror 75eV

    -2.00E-05

    -1.50E-05

    -1.00E-05

    -5.00E-06

    0.00E+00

    0 100 200 300

    mm

    rad

    Cff=1.25 dT=4.29

    Cff=2.5 dT=1.99Cff=5 dT=1.42

    slope error for glidcop mirror 300eV

    -6.00E-06-5.00E-06-4.00E-06-3.00E-06-2.00E-06-1.00E-060.00E+00

    0 100 200 300

    mm

    rad

    Cff=1.25 dT=1.44

    Cff=2.5 dT=0.40

    Cff=5 dT=0.26

    slope error for silicon mirror 300eV

    -1.20E-06-1.00E-06-8.00E-07-6.00E-07-4.00E-07-2.00E-070.00E+00

    0 100 200 300

    mm

    rad

    Cff=1.25 dT=2.50

    Cff=2.5 dT=0.68Cff=5 dT=0.43

    slope error for silicon mirror 75eV

    -5.00E-06

    -4.00E-06

    -3.00E-06-2.00E-06

    -1.00E-06

    0.00E+00

    0 100 200 300

    mm

    rad

    Cff=1.25 dT=7.80

    Cff=2.5 dT=3.45Cff=5 dT=2.42

    absorbed power density300eV

    0

    0.02

    0.04

    0.06

    0.08

    0.1

    -200 -100 0 100 200

    mm

    W/m

    m2

    Cff=1.25, 2theta=173.9

    Cff=2.5, 2theta=176.9

    Cff=5.0, 2theta=177.5

    absorbed power density75eV

    0

    0.05

    0.1

    0.15

    0.2

    0.25

    0.3

    -200 -100 0 100 200

    mm

    W/m

    m2

    Cff=1.25, 2theta=167.9

    Cff=2.5, 2theta=173.8

    Cff=5.0, 2theta=175.0

    The rms slope error (µrad) of the pre-mirror corresponding to a resolvingpower R=7500 (FWHM) from the150l/mm grating.

    11.5

    5

    1

    500 1000eV

    1

    2

    3

    4

    Cff=1.25Cff=2.5

    Cff=5.0

  • M. R. Howells, Advanced Light Source

    JENOPTIC SX700 MONOCHROMATOR

    Three gratings

    UHV rotary encoder

    Grating drive arm

    Mirror drive arm

    Plane mirror

  • M. R. Howells, Advanced Light Source

    New implementation of SX700monochromator

    Legs filled with epoxy granite

    Heavy pump below bellows onseparate support

    6-strut alignment

    Lightweight rigid honeycombtable

    Aluminum structural vessel

    External sine-bar drives andlinear encoders

    Seal joint below beam heightfor alignment access

    External grating changer

  • M. R. Howells, Advanced Light Source

    Monochromator chamber,vacuum test Oct 2001

  • M. R. Howells, Advanced Light Source

    monochromator scanningmechanism with integral cooling

    Pressure equalized water feed

    Pressure-equalized water feed

    Silicon plane mirror

    Double grating

    Water lines on sine bar

    Water manifold with no flexingparts

    Grating carriage with roll andyaw adjusters for double

    grating

    Invar structural frame