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Focus shaping using cylindrical vector beams

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Abstract

We report a focus shaping technique using generalized cylindrical vector beams. A generalized cylindrical vector beam can be decomposed into radially polarized and azimuthally polarized components. Such a generalized cylindrical beam can be generated from a radially polarized or an azimuthally polarized light using a two-half-wave-plate polarization rotator. The intensity pattern at the focus can be tailored by appropriately adjusting the rotation angle. Peak-centered, donut and flattop focal shapes can be obtained using this technique.

©2002 Optical Society of America

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Figures (9)

Fig. 1
Fig. 1 Generalized cylindrical vector beam with ϕ0 rotation from the purely radially polarization.
Fig. 2.
Fig. 2. A polarization rotator consisting of two half-wave plates. ∆ϕ is the angle between the fast axes of the two half-wave plates.
Fig. 3
Fig. 3 Focusing of a cylindrical vector beam. In the diagram, f is the focal length of the objective lens. Q(r, φ) is an observation point in the focal plane.
Fig.4
Fig.4 Intensity distribution at focal plane for radially polarized beam.
Fig.5
Fig.5 Intensity distribution in the vicinity of focus for radially polarized beam.
Fig.6
Fig.6 Intensity distribution at the focal plane for an azimuthally polarized beam. The focal field only has an azimuthal component. The radial and longitudinal components are zero.
Fig. 7
Fig. 7 Total intensity distributions in the vicinity of focus for azimuthally polarized beam.
Fig.8
Fig.8 Intensity distribution at focal plane for ϕ0=24°. Flattop focus is obtained.
Fig. 9
Fig. 9 Total intensity distribution in the vicinity of focus for ϕ0=24°.

Equations (8)

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E ( r , φ ) = P [ cos ϕ 0 e r + sin ϕ 0 e φ ]
T = ( cos ( 2 Δ ϕ ) sin ( 2 Δ ϕ ) sin ( 2 Δ ϕ ) cos ( 2 Δ ϕ ) ) = R ( 2 Δ ϕ )
E ( r , φ , z ) = E r e r + E z e z + E φ e φ
E r ( r , φ , z ) = A cos ϕ 0 0 θ max cos 1 / 2 ( θ ) P ( θ ) sin θ cos θ J 1 ( k r sin θ ) e i k z cos θ d θ
E z ( r , φ , z ) = i A cos ϕ 0 0 θ max cos 1 / 2 ( θ ) P ( θ ) sin 2 θ J 0 ( k r sin θ ) e i k z cos θ d θ
E φ ( r , φ , z ) = A sin ϕ 0 0 θ max cos 1 / 2 ( θ ) P ( θ ) J 1 ( k r sin θ ) e i k z cos θ d θ
P ( θ ) = { 1 if sin 1 ( 0.1 ) θ sin 1 ( NA ) 0 otherwise
F = 2 π R 3 ε 1 c ( ε 2 ε 1 ε 2 + 2 ε 1 ) I
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