Sagnac effect is a phase shift induced in a wave propagating in a loop by rotation of the loop. Two waves propagating in opposite directions along a rotating closed loop may interfere in a point of exit, wherein the rotation may cause a phase shift between them. An optical Sagnac Interferometer apparatus may include, for example, a loop trajectory enclosing an area. The interferometer may operate by splitting a beam of light at an entrance of the loop, to two beams which may be made to propagate in opposite directions along the loop trajectory. An interference pattern may be obtained at a point of exit from the loop. When the apparatus rotates, the path length of one of the beams may be effectively shortened, while the path length of the other beam may be effectively lengthened. Therefore, a phase shift may be created between the two beams, dependent on the rotation velocity of the apparatus.
Therefore, a Sagnac interferometer may measure changes in the rotation frequency of the frame that it is fixed to, relative to a global (inertial) frame of reference. The Sagnac effect in a wave propagating through a closed rotating ring induces a phase shift proportional to the rotation frequency Ω of this rotation and the area A of the ring. For light waves with frequency ω this phase shift may be represented by φlight=(2ωA/c2)Ω, where c is the speed of light and w is the light frequency. For matter waves of massive particles with mass m, the induced phase shift may be represented by φmatter=(2mA/)Ω, which is larger than the phase shift in an optical SI having the same area A by mc2/ω, wherein is planck's constant. Therefore, the Sagnac phase is much more sensitive to rotations in a matter-wave SI compared to light wave SI, for example, by 10 orders of magnitude. However, state-of-the-art matter-wave Sagnac interferometers, which are based on beams of atoms traveling in free space, are limited by their area number of atoms and the allowed momentum bandwidth of the atoms.
The subject matter regarded as the invention is particularly pointed out and distinctly claimed in the concluding portion of the specification. The invention, however, both as to organization and method of operation, together with objects, features, and advantages thereof, may best be understood by reference to the following detailed description when read with the accompanying drawings in which:
It will be appreciated that for simplicity and clarity of illustration, elements shown in the figures have not necessarily been drawn to scale. For example, the dimensions of some of the elements may be exaggerated relative to other elements for clarity. Further, where considered appropriate, reference numerals may be repeated among the figures to indicate corresponding or analogous elements.
In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the invention. However, it will be understood by those skilled in the art that the present invention may be practiced without these specific details. In other instances, well-known methods, procedures, and components have not been described in detail so as not to obscure the present invention.
The present invention may provide a Sagnac interferometer employing guided matter wave. The interferometer according to embodiments of the present invention may operate with high flux of particles with wide bandwidth, thus providing a clear and evident signal over transient noise. The interferometer according to embodiments of the present invention may provide better rotation sensitivity than prior interferometers by using matter-waves instead of light waves. The interferometer according to embodiments of the present invention may further provide better rotation sensitivity relative to for example, previous matter-wave SIs (Sagnac interferometers) by providing larger effective area of the SI loop, for example, without enlargement of the real area occupied by the loop.
Reference is now made to
SI 100 may receive input flux of particles through input port i, for example, with momentum bandwidth Δk. If Lα≠Lβ and Δk is relatively wide, e.g., ΔkδL>>1 (δL=Lα−Lβ), the interfering counter-propagating fluxes of wide range of longitudinal momentums from ports α and β may cancel each other at port o, so that, for example, the dependency of the output at port o on the rotational phase shift φmatter and/or the rotation frequency Ω may be substantially weakened. In this case, the rotational sensitivity of SI 100 may be damaged. Only counter-propagating waves which follow trajectories with substantially the same length may contribute visible dependency in the rotational phase shift in the output. In some embodiments of the present invention, in the case of Lα≠Lβ, internal reflections may enable existence of opposite paths with same length.
In case most of the particles follow trajectories with substantially the same length, e.g., the path lengths Lα and Lβ are equal, Δk may be relatively wide without damaging the rotational sensitivity of SI 100. Thus, for example, high flux of particles with wide bandwidth is enabled, thus providing a clear signal which may be evident over transient noise. This may facilitate very sensitive detection of small changes in rotation frequency Ω.
The area A is the effective area enclosed by the trajectory of the particles. As mentioned above, particles may exit loop 110 through splitter 120 in a certain probability (1−R) or may stay in the loop trajectory in a complimentary probability R. As the probability R is larger, the particles may do more passes through loop 110 before leaving loop 110 through output port o. As the particles do more passes, the effective area A is larger, thus, for example, the rotational sensitivity of SI 100 may be greater.
Reference is now made to
Loop 210 may rotate at a rotation frequency Ω relative to inertial frame 240. As described above with reference to
According to some embodiments of the present invention, a particle, for example, an atom, incident from port i may exit at port o through one of four kinds of trajectories: (a) transmission through BS 230, reflection at BS 220 and then transmission through BS 230 again. The total excess phase which may be gained by this path is approximately π; (b) reflection at BS 230, reflection at BS 220 and then reflection at BS 230 again, with substantially no excess phase; (c) transmission at BS 230, transmission at BS 220, propagation in the counterclockwise direction through loop 210 for a certain number of times and then transmission again through BS 220 and then through BS 230, with a total excess phase of approximately 2π and a phase due to Sagnac effect because of the propagation through loop 210; and (d) reflection at BS 230, transmission at BS 220, propagation in clockwise direction in loop 210 for a certain number of times and then transmission again through BS 220 and then through BS 230, with total phase of approximately n and a phase due to Sagnac effect because of the propagation through loop 210. Trajectories (a) and (b) and trajectories (c) and (d) may have substantially the same length.
When loop 210 is not rotating relative to inertial frame 240 the phase in trajectories (a) and (b) may be substantially opposite and the phase of trajectories (e) and (d) may be substantially opposite, thus, for example, the probability to exit at port o may be substantially zero, due to, for example, full destructive interference. However, when loop 210 is rotating relative to inertial frame 240 the particle beams propagating clockwise and counterclockwise through loop 210 may add opposite phase shifts proportional to the rotation frequency Ω and to the number of passes through loop 210. These phase shifts may increase the probability for a positive output of particles at port o, wherein the probability may depend on the rotation frequency Ω. Therefore, for example, the rotation frequency Ω and/or changes in the rotation frequency Ω may be deduced by measurement of output transmission at port o.
In the embodiment of the present invention shown in
In this embodiments of the present invention, for example, the output transmission probability at port o as a function of the rotational phase φ(Ω), which may be notated
Accordingly, for example, the output transmission probability
The sensitivity of the output transmission at port o to changes in the rotation frequency Ω in this embodiment of the present invention, may be defined as the minimum change in the rotation frequency Ω which may generate a noticeable (beyond noise level) change in the output transmission at port o. This minimum change may be represented by
wherein
A Sagnac interferometer according to embodiments of the present invention may provide high rotational sensitivity due to, for example, the ability to propagate particles in loop 210 for a large number of times, thus, for example, enlarging the effective area A and/or the rotational sensitivity of the Sagnac interferometer. Therefore, for example, the actual size of a Sagnac interferometer according to embodiments of the present invention may be very small, for example, having a loop radius of 1 cm. This may enable, for example, implementation of such SI on an atom chip.
The maximum velocity of the atoms in this embodiment may be limited by the magnetic force by which the SI may be bounded to an atom chip. For example, the SI may be bounded to the chip by magnetic field gradients of approximate order of Gauss/μm, which may be generated, for example, by wires on the chip, for example, about 10 μm from the surface of the chip. The centrifugal force mv2/r of the circulating atoms should be below the magnetic force bounding the SI to the chip. For example, the maximum velocity of the atoms may be about 10 m/sec.
As described above with reference to
While certain features of the invention have been illustrated and described herein, many modifications, substitutions, changes, and equivalents will now occur to those of ordinary skill in the art. It is, therefore, to be understood that the appended claims are intended to cover all such modifications and changes as fall within the true spirit of the invention.
This application claims the benefit of U.S. provisional application Ser. No. 60/877,591, which is incorporated in its entirety herein by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IL07/01611 | 12/26/2007 | WO | 00 | 10/28/2010 |
Number | Date | Country | |
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60877591 | Dec 2006 | US |