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| United States Patent | 4233847 |
| Link to this page | http://www.wikipatents.com/4233847.html |
| Inventor(s) | Walker; Clifford G. (915 Weatherly Rd., Huntsville, AL 35803) |
| Abstract | An accelerometer utilizing a laser source and a resonant cavity formed by a
pair of spaced mirrors. A birefringent isotropic material is disposed in
the resonant cavity. Light generated by the laser is reflected back and
forth between the mirrors and through the birefringent material to
generate a pair of orthogonally polarized beams. The optical path of one
beam is changed in response to acceleration forces acting on a proof mass
carried on the birefringent material. The pair of beams produced have
different phases. The phase difference will be by an amount proportional
to the difference in refractive indexes along and perpendicular to the
optic axis of the birefringent material. |
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Title Information  |
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Drawing from US Patent 4233847 |
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Passive laser accelerometer |
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| Publication Date |
November 18, 1980 |
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Title Information  |
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| Market Size |
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Estimate the gross annual revenues of the relevant market
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| Reasonable Royalty |
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Market Review  |
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Description  |
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BACKGROUND OF THE INVENTION
The present invention relates to a passive laser accelerometer which
utilizes a laser external of a resonant cavity having a birefringent
material therein which produces a pair of orthoganally polarized beams
differing in phase.
Other laser accelerometers are known in which the laser source is
positioned in the resonant cavity which results in mode locking problems.
Under low input accelerations the phases of the two oscillations
lock-together and the output beat frequency remains unchanged. To obtain
an output the birefringent material must be stressed beyond the lock-in
value.
Additionally, mounting the birefringent material in the resonant cavity
provides residual strains in the birefringent material and the laser and
birefringent material are in such close proximity that the birefringent is
heated, creating more undesirable residual strains in the birefringent
material.
In one embodiment of the invention the system is implemented in an
integrated optics format. The principle of integrated optics is disclosed
in the publication "Spectrum", pages 22-29, December 1978, entitled
"Integrated Optical Spectrum Analyzer: an Imminent Chip".
SUMMARY OF THE INVENTION
An accelerometer including a pair of spaced mirrors forming a resonant
cavity having a birefringent material therein. A proof mass is carried on
the birefringent material. A laser generates light which is reflected back
and forth between the mirrors. Part of the laser energy passes through one
mirror and a polarizer, and onto a detector. The output of the detector is
a beat frequency proportional to the input acceleration. Prior to using
the detector output a voltage is generated and applied to a sensing
element to fix the cavity length. The beat frequency depends only on the
change in refractive index and is proportional to the acceleration induced
optical path difference. With the birefringent material in the resonant
cavity, the laser oscillates in two orthogonal plane polarized modes. The
directions of polarization is along and perpendicular to the optic axis of
the element.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a diagrammatic view of the passive laser accelerometer of the
present invention.
FIG. 2 is a diagrammatic view of an alternate arrangement of the passive
laser accelerometer of the present invention.
FIG. 3 is a diagrammatic view of the passive laser accelerometer of the
present invention using integrated optics.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As shown in FIG. 1, accelerometer 10 includes a laser 12 and a power supply
14. A reflecting mirror 16 (which may be spherical or plane) is in spaced
relation with a partially transmitting plane mirror 18 to form a resonant
cavity 20. A birefringent material 22 having a proof mass 24 thereon is
carried in the resonant cavity. Secured perpherally to plane mirror 18 is
a piezoelectric crystal 26. The crystal is shown to be toroidal but may be
of other shapes. A plane polarizer 28 is in spaced relation with crystal
26 and a detector 30 is spaced from polarizer 28. The detector may be an
optical processor or a photo diode assembly. The output of the detector is
a beat frequency proportional to the input acceleration. A voltage source
32 is provided to generate a voltage which is applied to piezoelectric 26
(through connecting circuit 34) to fix cavity length.
In operation, laser 12 is energized by power supply 14 producing a laser
beam with frequency Vo. Mirror 16 reflects the beam into resonant cavity
20 and through the birefringent material (double refracting) sensor 24
onto plane mirror 18 and is reflected back through the sensor 22 to mirror
16 producing a resonant condition. Part of the laser energy is allowed to
pass through mirror 18, polarizer 28 and into the detector system 30 which
may be an optical processor or a photo diode scheme. The output of the
detector is a beat frequency proportional to the input acceleration. Prior
to using the detector output a voltage must be generated and applied to
the crystal 26, through the connecting circuit 34. This voltage (K.sub.I
(.lambda.)/volt) applied to the piezoelectric element 26 will fix the
cavity length 20 and produce the proper beat frequency (.DELTA.V). The
change in cavity length per volt will depend on the selected constant
K.sub.I. The voltage is applied by any of many conventional means (a
potentiometer, for example) until the cavity length is changed for maximum
output. The proof mass 24 is attached to the birefringent (double
refracting) material 22 and under acceleration stresses induces optical
birefringence of the photoelastic photoelastic material 22. In order to
observe a beat frequency (.DELTA.V), a plane polarizer 28 is inserted at
45 degrees to the two orthogonal planes of polarization. This is necessary
in order to resolve the orthogonal plane polarized waves along a direction
containing a component of each. The beat frequency (.DELTA.V) depends only
upon the differential change in refractive index and is not influenced by
any change in cavity length that may arise from mechanical vibration or
thermal expansion. The acceleration sensitive birefringent material may be
a gas, liquid, or solid, however, the solid photoelastic material 22
provides greater sensitivity.
The signal beam and local oscillator beam in the cavity 20 are coincident.
This enables both beams to see the same reflector surface and the same
optical path everywhere, except through the sensor 24. It is possible in
this type of laser for each beam to retain its identity by its state of
polarization. With an input acceleration stress the optical path is
different for polarization in the coincident beam and the two waves are
combined, thus obtaining a beat frequency (.DELTA.V) proportional to the
acceleration induced optical path difference. With the sensor 22 in the
cavity 20 the laser will oscillate in two orthogonal plane polarized
modes. The directions of polarization will be along and perpendicular to
the optic axis of the element. Two orthogonal modes will differ in phase
by an amount proportional to the difference in refractive indexes along
and perpendicular to the optic axis of the element 24.
In the embodiment shown in FIG. 2 wherein like numerals refer to like
parts, circular polarized waves are used to reduce noise in the
birefringent material. In this embodiment the beam is directed through a
polarizer 36 and through a quarter wave plate 38. A partially transmitting
mirror 19 and into cavity 20. The circular beam is passed through
birefringent element 22 and becomes elliptical and is reflected back and
forth between mirrors 16 and 19. A portion of the elliptical beam is
passed through mirror 18 and a second quarter wave plate 40, polarizer 28
and detector 30. Operation of this embodiment is the same as described in
conjunction with FIG. 1.
In the embodiment shown in FIG. 3 wherein like numerals refer to like
parts, the accelerometer is made in an integrated optics format.
A laser 12 (solid state preferably) is energized by power source 14 which
directs a beam through a polarizer 36, quarter wave plate 38, partially
transmitting mirror 19, birefringent material 22, and then through an
electro-optics phase modulator 42, disposed in the resonant cavity 20,
mirror 18, a second quarter wave plate 40, polarizer 28 and detector 30.
Operation of this embodiment is the same as in FIG. 2.
FIG. 3 shows the system implemented in an integrated optics format.
Polarizer 36, mirrors 19 and 18 are made of a simple grating structure
etched in base 44. The quarter wave plate (.lambda./4) 38 could be a
passive element material material with a width equal to (.lambda./4) or an
active element, a polarizing modulator. The electro-optic phase modulator
is an active element that changes the index of refraction in proportion to
an applied voltage thus changing the effective length of the optical
resonant cavity to ensure a resonant peak. The most straight forward
electro-optic modulation of a guided-wave mode produces a phase
retardation as the mode propagates through an electrically induced
birefringent medium. The phase modulation can be obtained by propagating a
mode with a propagation in the Y-Z direction and applying an electric
field in the X direction. The piezoelectric element 18 in FIGS. 1 & 2
physically moves the mirror 18 as a function of the applied voltage.
The primary goal of integrated optics is to integrate a variety of discrete
optical elements, both active and passive, into a monolithic, miniaturized
planar structure. In other words, it is an optical analogy of integrated
circuit technology in the electronics industries. By this analogy, it is
reasonable to assume that optical systems in the integrated optics
configuration can be made more efficient, comPact and stable at lower
cost. In the embodiment shown in FIG. 3, which is a monolithic structure,
galium-aluminum-arsenide is used as the substrate. Other substrates may be
resorted to such as silicon or lithium-niobate, however, in this structure
an interface must be used between the laser and the substrates and the
detectors.
The polarizers used herein may be any of many types available, such as
H-sheet polaroid, a molecular analog of the wire grid.
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Description  |
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