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Spatial Characterization Of Two-Photon States - GAP-Optique

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4. OAM transfer in noncollinear configurations<br />

4.1 Ellipticity in noncollinear configurations<br />

In the experimental implementation of spdc, the detection system selects the<br />

photons that are emitted in a certain spatial direction. In a collinear configuration,<br />

the selection is not a problem since all the photons are emitted in the<br />

same direction. But, in a noncollinear configuration, the photons are emitted in<br />

different azimuthal directions described by the angle α, therefore the detection<br />

system selects only a section of the full cone. As the symmetry is broken when<br />

only a portion of the cone is considered, the oam transfer mechanism can not<br />

be described by the selection rule in 3.18. This section studies this mechanism<br />

in a simple spdc configuration by calculating the spatial distribution of the<br />

signal photon after fixing the oam content of the pump and idler photons.<br />

As a first example, consider a Gaussian pump beam lp = 0 and an idler<br />

photon projected into a Gaussian mode li = 0, given by<br />

<br />

u(qi) = Ni exp − w2 i<br />

4 (qx2 i + q y2<br />

i )<br />

<br />

, (4.1)<br />

the spatial distribution of the signal photon is given by the normalized mode<br />

function<br />

<br />

Φs(qs) = Ns dqiΦq(qs, qi)u(qi). (4.2)<br />

This integral has an analytical solution for simple spdc configurations. Consider<br />

a degenerate spdc process with negligible Poynting vector walk-off. After<br />

suppressing the correlations between space and frequency the spatial part of<br />

the two-photon state is given by<br />

<br />

<br />

with<br />

Φq(qs, qi) = exp<br />

− w2 p<br />

4 ∆2 0 − w2 p<br />

4 ∆2 1<br />

∆0 =q x s + q x i<br />

∆1 =q y s cos ϕs + q y<br />

i cos ϕi<br />

∆k = − q y s sin ϕs + q y<br />

i<br />

sin ϕi.<br />

<br />

L<br />

sinc<br />

2 ∆k<br />

<br />

(4.3)<br />

(4.4)<br />

Therefore, using the sinc to exponential approximation, the signal mode function<br />

defined by equation 4.2 is given by<br />

<br />

<br />

Φs(qs) =Ns exp<br />

× exp<br />

<br />

−<br />

w2 pw2 i<br />

4(w2 p + w2 qx2 s<br />

i )2<br />

− 4w2 pγ 2 L 2 cos ϕs 2 sin ϕs 2 + (w 2 p cos ϕs 2 + γ 2 L 2 sin ϕs)w 2 i<br />

4(w 2 p cos ϕs 2 + γ 2 L 2 sin ϕs 2 + w 2 i )<br />

q y2<br />

s<br />

<br />

(4.5)<br />

When the coefficients of the variables q x s and q y s are equal, the signal mode<br />

function reduces to a Gaussian and the selection rule is fulfilled. These coefficients<br />

are equal in collinear configurations, or in noncollinear configurations in<br />

38<br />

.

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