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The principal structural feature of the title compound, C20H9F5, is the dihedral angle of 51.22 (5)° between the substituent phenyl ring and the fluorene fragment of the mol­ecule. This results in the close approach of an F atom to the plane of the fluorene fragment, compromising the planarity of the latter. The conformation also permits virtually complete overlap and π–π interaction of the phenyl ring of one mol­ecule with the five-membered ring of the fluorene of another, in infinite chains of head-to-tail mol­ecules.

Supporting information

cif

Crystallographic Information File (CIF) https://doi.org/10.1107/S1600536802023280/cf6231sup1.cif
Contains datablocks global, I

hkl

Structure factor file (CIF format) https://doi.org/10.1107/S1600536802023280/cf6231Isup2.hkl
Contains datablock I

CCDC reference: 203016

Key indicators

  • Single-crystal X-ray study
  • T = 298 K
  • Mean [sigma](C-C) = 0.004 Å
  • R factor = 0.045
  • wR factor = 0.113
  • Data-to-parameter ratio = 11.7

checkCIF results

No syntax errors found

ADDSYM reports no extra symmetry








Computing details top

Data collection: P3 Software (Nicolet, 1980); cell refinement: P3 Software; data reduction: RDNIC (Howie, 1980); program(s) used to solve structure: SHELXS97 (Sheldrick, 1997); program(s) used to refine structure: SHELXL97 (Sheldrick, 1997); molecular graphics: ORTEP-3 (Farrugia, 1997); software used to prepare material for publication: SHELXL97 and PLATON (Spek, 1990).

9-Pentafluorophenylmethylene-9H-fluorene top
Crystal data top
C20H9F5F(000) = 696
Mr = 344.27Dx = 1.524 Mg m3
Monoclinic, P21/nMo Kα radiation, λ = 0.71073 Å
a = 12.931 (6) ÅCell parameters from 14 reflections
b = 7.448 (3) Åθ = 8.2–12.3°
c = 15.647 (6) ŵ = 0.13 mm1
β = 95.29 (3)°T = 298 K
V = 1500.5 (11) Å3Block, green-yellow
Z = 40.50 × 0.30 × 0.30 mm
Data collection top
Nicolet P3
diffractometer
Rint = 0.031
Radiation source: normal-focus sealed tubeθmax = 25.1°, θmin = 2.1°
Graphite monochromatorh = 015
θ–2θ scansk = 08
2772 measured reflectionsl = 1818
2656 independent reflections2 standard reflections every 50 reflections
1580 reflections with I > 2σ(I) intensity decay: none
Refinement top
Refinement on F2Secondary atom site location: difference Fourier map
Least-squares matrix: fullHydrogen site location: inferred from neighbouring sites
R[F2 > 2σ(F2)] = 0.045H-atom parameters constrained
wR(F2) = 0.113 w = 1/[σ2(Fo2) + (0.0485P)2]
where P = (Fo2 + 2Fc2)/3
S = 1.01(Δ/σ)max < 0.001
2656 reflectionsΔρmax = 0.19 e Å3
227 parametersΔρmin = 0.18 e Å3
0 restraintsExtinction correction: SHELXL97, Fc*=kFc[1+0.001xFc2λ3/sin(2θ)]-1/4
Primary atom site location: structure-invariant direct methodsExtinction coefficient: 0.036 (2)
Special details top

Experimental. Scan rates, dependent on prescan intensity (Ip), were in the range 58.6 (Ip>2500) to 5.33 (Ip<150) ° 2θ min-1. Scan widths, dependent on 2θ, were in the range 2.4 to 2.7 ° 2θ. Stationary crystal, stationary counter background counts were taken on either side of the peak each for 25% of the total (peak plus background) count time.

Geometry. All e.s.d.'s (except the e.s.d. in the dihedral angle between two l.s. planes) are estimated using the full covariance matrix. The cell e.s.d.'s are taken into account individually in the estimation of e.s.d.'s in distances, angles and torsion angles; correlations between e.s.d.'s in cell parameters are only used when they are defined by crystal symmetry. An approximate (isotropic) treatment of cell e.s.d.'s is used for estimating e.s.d.'s involving l.s. planes.

Least-squares planes (x,y,z in crystal coordinates) and deviations from them (* indicates atom used to define plane)

- 1.6060 (0.0083) x - 6.7213 (0.0039) y + 6.6070 (0.0072) z = 1.5455 (0.0022)

* 0.0081 (0.0022) C1 * -0.0473 (0.0022) C2 * -0.0580 (0.0025) C3 * -0.0052 (0.0024) C4 * 0.0346 (0.0025) C5 * 0.0387 (0.0023) C6 * 0.0455 (0.0024) C7 * 0.0043 (0.0025) C8 * -0.0404 (0.0026) C9 * -0.0532 (0.0027) C10 * -0.0113 (0.0023) C11 * 0.0434 (0.0022) C12 * 0.0409 (0.0020) C13 0.0296 (0.0032) C14 0.0972 (0.0037) C15 1.0583 (0.0039) C16 1.1003 (0.0047) C17 0.1904 (0.0053) C18 - 0.7410 (0.0050) C19 - 0.7708 (0.0044) C20 2.0138 (0.0031) F1 2.0311 (0.0043) F2 0.2086 (0.0054) F3 - 1.6265 (0.0053) F4 - 1.7048 (0.0039) F5

Rms deviation of fitted atoms = 0.0379

- 1.8028 (0.0132) x + 6.7109 (0.0048) y + 6.6005 (0.0148) z = 0.9296 (0.0073)

Angle to previous plane (with approximate e.s.d.) = 51.22 (0.05)

* 0.0213 (0.0017) C15 * -0.0172 (0.0018) C16 * -0.0010 (0.0019) C17 * 0.0150 (0.0019) C18 * -0.0100 (0.0019) C19 * -0.0081 (0.0018) C20 - 0.0969 (0.0033) F1 - 0.0133 (0.0035) F2 0.0504 (0.0035) F3 - 0.0083 (0.0034) F4 - 0.0186 (0.0033) F5

Rms deviation of fitted atoms = 0.0138

- 1.6476 (0.0067) x - 6.7140 (0.0038) y + 6.6294 (0.0067) z = 1.5535 (0.0020)

Angle to previous plane (with approximate e.s.d.) = 51.35 (0.05)

* 0.0035 (0.0022) C1 * -0.0529 (0.0023) C2 * -0.0599 (0.0025) C3 * -0.0025 (0.0024) C4 * 0.0385 (0.0025) C5 * 0.0389 (0.0023) C6 * 0.0457 (0.0024) C7 * 0.0082 (0.0025) C8 * -0.0374 (0.0027) C9 * -0.0548 (0.0027) C10 * -0.0167 (0.0024) C11 * 0.0388 (0.0023) C12 * 0.0332 (0.0021) C13 * 0.0172 (0.0019) C14 0.0810 (0.0032) C15 1.0419 (0.0035) C16 1.0804 (0.0041) C17 0.1669 (0.0046) C18 - 0.7646 (0.0043) C19 - 0.7907 (0.0038) C20 2.0008 (0.0027) F1 2.0112 (0.0036) F2 0.1816 (0.0046) F3 - 1.6536 (0.0043) F4 - 1.7248 (0.0032) F5

Rms deviation of fitted atoms = 0.0370

- 1.5233 (0.0140) x - 6.8362 (0.0049) y + 6.0754 (0.0165) z = 1.4282 (0.0037)

Angle to previous plane (with approximate e.s.d.) = 2.27 (0.10)

* 0.0059 (0.0018) C1 * -0.0012 (0.0019) C2 * -0.0051 (0.0021) C3 * 0.0066 (0.0021) C4 * -0.0017 (0.0020) C5 * -0.0045 (0.0019) C6

Rms deviation of fitted atoms = 0.0047

- 1.6265 (0.0158) x - 6.7580 (0.0052) y + 6.4308 (0.0176) z = 1.5238 (0.0056)

Angle to previous plane (with approximate e.s.d.) = 1.47 (0.13)

* -0.0118 (0.0015) C1 * 0.0088 (0.0016) C6 * -0.0021 (0.0016) C7 * -0.0050 (0.0015) C12 * 0.0100 (0.0015) C13 - 0.0499 (0.0043) C2 - 0.0533 (0.0052) C3 - 0.0106 (0.0052) C4 0.0120 (0.0045) C5 - 0.0577 (0.0045) C8 - 0.1178 (0.0055) C9 - 0.1315 (0.0055) C10 - 0.0752 (0.0043) C11 0.0635 (0.0053) C15 1.0127 (0.0059) C16 1.0472 (0.0074) C17 0.1418 (0.0084) C18 - 0.7773 (0.0080) C19 - 0.7999 (0.0065) C20 1.9639 (0.0047) F1 1.9663 (0.0077) F2 0.1526 (0.0097) F3 - 1.6581 (0.0087) F4 - 1.7220 (0.0061) F5

Rms deviation of fitted atoms = 0.0083

- 1.4974 (0.0141) x - 6.6061 (0.0053) y + 7.1327 (0.0169) z = 1.8010 (0.0078)

Angle to previous plane (with approximate e.s.d.) = 2.94 (0.14)

* -0.0019 (0.0018) C7 * -0.0014 (0.0020) C8 * 0.0033 (0.0023) C9 * -0.0018 (0.0022) C10 * -0.0015 (0.0020) C11 * 0.0033 (0.0018) C12

Rms deviation of fitted atoms = 0.0023

Refinement. Refinement of F2 against ALL reflections. The weighted R-factor wR and goodness of fit S are based on F2, conventional R-factors R are based on F, with F set to zero for negative F2. The threshold expression of F2 > σ(F2) is used only for calculating R-factors(gt) etc. and is not relevant to the choice of reflections for refinement. R-factors based on F2 are statistically about twice as large as those based on F, and R- factors based on ALL data will be even larger.

Anisotropic displacement parameters refined for all non-H atoms. H atoms placed in calculated positions and refined with a riding model.

Fractional atomic coordinates and isotropic or equivalent isotropic displacement parameters (Å2) top
xyzUiso*/Ueq
F10.30765 (12)0.1983 (2)0.41178 (9)0.0625 (5)
F20.50868 (13)0.1904 (2)0.47131 (9)0.0698 (5)
F30.65148 (11)0.0479 (3)0.37512 (11)0.0786 (6)
F40.59190 (12)0.0834 (2)0.21646 (11)0.0726 (5)
F50.39028 (11)0.0855 (2)0.15771 (9)0.0566 (5)
C10.04055 (18)0.0113 (3)0.23347 (15)0.0402 (6)
C20.01064 (19)0.0760 (4)0.15201 (17)0.0509 (7)
H20.05990.11770.11710.061*
C30.0944 (2)0.0776 (4)0.1233 (2)0.0625 (8)
H30.11580.11990.06860.075*
C40.1673 (2)0.0162 (4)0.1759 (2)0.0659 (9)
H40.23740.02010.15620.079*
C50.1385 (2)0.0503 (4)0.2567 (2)0.0611 (8)
H50.18810.09250.29110.073*
C60.03374 (19)0.0529 (3)0.28539 (16)0.0455 (7)
C70.0205 (2)0.1180 (3)0.36578 (16)0.0464 (7)
C80.0183 (2)0.2013 (4)0.43491 (18)0.0640 (8)
H80.08930.21900.43600.077*
C90.0503 (3)0.2578 (4)0.50226 (19)0.0744 (10)
H90.02510.31340.54940.089*
C100.1562 (3)0.2327 (4)0.50053 (18)0.0679 (9)
H100.20130.27240.54630.081*
C110.1955 (2)0.1493 (4)0.43159 (16)0.0532 (7)
H110.26680.13290.43090.064*
C120.12806 (19)0.0904 (3)0.36354 (15)0.0428 (6)
C130.14509 (18)0.0049 (3)0.28036 (14)0.0379 (6)
C140.23204 (18)0.0475 (3)0.24647 (16)0.0424 (6)
H140.22210.09120.19060.051*
C150.34053 (18)0.0464 (3)0.28422 (15)0.0388 (6)
C160.37518 (19)0.1202 (3)0.36296 (16)0.0446 (6)
C170.4783 (2)0.1206 (4)0.39399 (16)0.0485 (7)
C180.55114 (19)0.0507 (4)0.34516 (18)0.0506 (7)
C190.52104 (19)0.0163 (4)0.26503 (17)0.0475 (7)
C200.41770 (19)0.0172 (3)0.23625 (15)0.0422 (6)
Atomic displacement parameters (Å2) top
U11U22U33U12U13U23
F10.0609 (10)0.0719 (11)0.0558 (9)0.0026 (8)0.0119 (8)0.0146 (9)
F20.0768 (11)0.0778 (12)0.0513 (10)0.0100 (9)0.0127 (8)0.0093 (9)
F30.0440 (10)0.0941 (14)0.0937 (13)0.0022 (9)0.0153 (9)0.0025 (11)
F40.0443 (9)0.0943 (13)0.0819 (12)0.0020 (9)0.0208 (8)0.0096 (10)
F50.0532 (9)0.0736 (11)0.0438 (9)0.0072 (8)0.0093 (7)0.0080 (8)
C10.0401 (14)0.0378 (15)0.0431 (15)0.0002 (12)0.0064 (11)0.0029 (12)
C20.0437 (16)0.0548 (18)0.0537 (17)0.0019 (14)0.0020 (13)0.0011 (14)
C30.0547 (18)0.063 (2)0.067 (2)0.0006 (16)0.0093 (15)0.0042 (16)
C40.0404 (17)0.070 (2)0.085 (2)0.0016 (15)0.0019 (16)0.0063 (19)
C50.0419 (17)0.065 (2)0.077 (2)0.0031 (15)0.0131 (15)0.0032 (17)
C60.0422 (16)0.0414 (16)0.0542 (17)0.0019 (12)0.0122 (13)0.0082 (13)
C70.0525 (16)0.0424 (16)0.0463 (15)0.0042 (13)0.0163 (13)0.0063 (13)
C80.067 (2)0.073 (2)0.0548 (18)0.0154 (17)0.0218 (16)0.0055 (17)
C90.098 (3)0.074 (2)0.0537 (19)0.025 (2)0.0229 (19)0.0038 (17)
C100.089 (2)0.069 (2)0.0437 (17)0.0103 (18)0.0012 (16)0.0109 (15)
C110.0599 (18)0.0549 (18)0.0444 (16)0.0073 (14)0.0031 (13)0.0059 (14)
C120.0491 (16)0.0388 (15)0.0415 (15)0.0031 (12)0.0094 (12)0.0016 (12)
C130.0370 (13)0.0379 (14)0.0390 (14)0.0015 (11)0.0050 (11)0.0026 (11)
C140.0405 (15)0.0488 (16)0.0374 (13)0.0005 (12)0.0010 (11)0.0015 (12)
C150.0392 (14)0.0396 (15)0.0379 (14)0.0033 (12)0.0052 (11)0.0040 (12)
C160.0443 (16)0.0448 (16)0.0455 (15)0.0022 (13)0.0083 (12)0.0019 (13)
C170.0521 (17)0.0504 (17)0.0417 (15)0.0083 (14)0.0024 (13)0.0015 (13)
C180.0360 (15)0.0533 (18)0.0606 (18)0.0037 (13)0.0061 (13)0.0078 (15)
C190.0382 (15)0.0487 (17)0.0571 (17)0.0017 (13)0.0127 (13)0.0024 (14)
C200.0456 (15)0.0444 (16)0.0372 (14)0.0040 (13)0.0063 (12)0.0001 (12)
Geometric parameters (Å, º) top
F1—C161.344 (3)C8—C91.379 (4)
F2—C171.342 (3)C8—H80.930
F3—C181.338 (3)C9—C101.384 (4)
F4—C191.340 (3)C9—H90.930
F5—C201.347 (3)C10—C111.382 (4)
C1—C21.384 (3)C10—H100.930
C1—C61.399 (3)C11—C121.384 (3)
C1—C131.482 (3)C11—H110.930
C2—C31.391 (4)C12—C131.483 (3)
C2—H20.930C13—C141.345 (3)
C3—C41.385 (4)C14—C151.471 (3)
C3—H30.930C14—H140.930
C4—C51.376 (4)C15—C161.385 (3)
C4—H40.930C15—C201.386 (3)
C5—C61.388 (4)C16—C171.376 (4)
C5—H50.930C17—C181.369 (4)
C6—C71.465 (4)C18—C191.372 (4)
C7—C81.381 (3)C19—C201.370 (3)
C7—C121.409 (3)
C2—C1—C6120.4 (2)C10—C11—C12119.4 (3)
C2—C1—C13130.5 (2)C10—C11—H11120.3
C6—C1—C13109.2 (2)C12—C11—H11120.3
C1—C2—C3118.8 (3)C11—C12—C7119.2 (2)
C1—C2—H2120.6C11—C12—C13132.6 (2)
C3—C2—H2120.6C7—C12—C13108.1 (2)
C4—C3—C2120.2 (3)C14—C13—C1122.6 (2)
C4—C3—H3119.9C14—C13—C12131.9 (2)
C2—C3—H3119.9C1—C13—C12105.48 (19)
C5—C4—C3121.6 (3)C13—C14—C15129.9 (2)
C5—C4—H4119.2C13—C14—H14115.1
C3—C4—H4119.2C15—C14—H14115.1
C4—C5—C6118.4 (3)C16—C15—C20115.3 (2)
C4—C5—H5120.8C16—C15—C14125.0 (2)
C6—C5—H5120.8C20—C15—C14119.5 (2)
C5—C6—C1120.6 (3)F1—C16—C17117.2 (2)
C5—C6—C7131.2 (3)F1—C16—C15120.2 (2)
C1—C6—C7108.2 (2)C17—C16—C15122.5 (2)
C8—C7—C12121.0 (3)F2—C17—C18119.4 (2)
C8—C7—C6129.9 (3)F2—C17—C16120.8 (2)
C12—C7—C6109.0 (2)C18—C17—C16119.7 (2)
C9—C8—C7118.8 (3)F3—C18—C17120.3 (2)
C9—C8—H8120.6F3—C18—C19119.9 (2)
C7—C8—H8120.6C17—C18—C19119.8 (2)
C8—C9—C10120.7 (3)F4—C19—C20120.6 (2)
C8—C9—H9119.6F4—C19—C18120.2 (2)
C10—C9—H9119.6C20—C19—C18119.2 (2)
C11—C10—C9120.8 (3)F5—C20—C19117.9 (2)
C11—C10—H10119.6F5—C20—C15118.7 (2)
C9—C10—H10119.6C19—C20—C15123.3 (2)
C6—C1—C2—C30.6 (4)C7—C12—C13—C14179.5 (3)
C13—C1—C2—C3179.5 (3)C11—C12—C13—C1175.5 (3)
C1—C2—C3—C40.4 (4)C7—C12—C13—C11.4 (3)
C2—C3—C4—C51.2 (5)C1—C13—C14—C15178.0 (2)
C3—C4—C5—C60.8 (4)C12—C13—C14—C154.1 (5)
C4—C5—C6—C10.2 (4)C13—C14—C15—C1651.8 (4)
C4—C5—C6—C7178.4 (3)C13—C14—C15—C20134.6 (3)
C2—C1—C6—C51.0 (4)C20—C15—C16—F1174.9 (2)
C13—C1—C6—C5179.2 (2)C14—C15—C16—F11.0 (4)
C2—C1—C6—C7177.9 (2)C20—C15—C16—C173.9 (4)
C13—C1—C6—C71.9 (3)C14—C15—C16—C17177.8 (2)
C5—C6—C7—C82.5 (5)F1—C16—C17—F22.5 (4)
C1—C6—C7—C8176.3 (3)C15—C16—C17—F2178.7 (2)
C5—C6—C7—C12179.8 (3)F1—C16—C17—C18176.9 (2)
C1—C6—C7—C121.1 (3)C15—C16—C17—C181.9 (4)
C12—C7—C8—C90.1 (4)F2—C17—C18—F31.6 (4)
C6—C7—C8—C9177.0 (3)C16—C17—C18—F3179.0 (2)
C7—C8—C9—C100.4 (5)F2—C17—C18—C19178.2 (2)
C8—C9—C10—C110.5 (5)C16—C17—C18—C191.2 (4)
C9—C10—C11—C120.0 (5)F3—C18—C19—F40.5 (4)
C10—C11—C12—C70.4 (4)C17—C18—C19—F4179.3 (2)
C10—C11—C12—C13177.1 (3)F3—C18—C19—C20178.2 (2)
C8—C7—C12—C110.5 (4)C17—C18—C19—C202.0 (4)
C6—C7—C12—C11177.1 (2)F4—C19—C20—F50.7 (4)
C8—C7—C12—C13177.9 (2)C18—C19—C20—F5179.3 (2)
C6—C7—C12—C130.2 (3)F4—C19—C20—C15178.5 (2)
C2—C1—C13—C140.5 (4)C18—C19—C20—C150.2 (4)
C6—C1—C13—C14179.6 (2)C16—C15—C20—F5177.8 (2)
C2—C1—C13—C12177.8 (3)C14—C15—C20—F53.6 (3)
C6—C1—C13—C122.0 (3)C16—C15—C20—C193.0 (4)
C11—C12—C13—C142.6 (5)C14—C15—C20—C19177.3 (2)
 

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