Coherent light generators – Particular resonant cavity – Folded cavity
Reexamination Certificate
2000-05-31
2001-10-30
Font, Frank G. (Department: 2877)
Coherent light generators
Particular resonant cavity
Folded cavity
C372S098000, C372S099000, C372S107000, C356S340000, C356S340000, C356S329000
Reexamination Certificate
active
06310904
ABSTRACT:
CROSS-REFERENCE TO RELATED APPLICATION(S)
None.
BACKGROUND OF THE INVENTION
The present invention is a measurement method to facilitate the production of self-aligning laser gyroscope blocks.
One embodiment of this invention is application to a ring laser gyroscope (RLG). A RLG is commonly used to measure the angular rotation of a vehicle, such as an aircraft. Such a gyroscope has two counter-rotating laser light beams which move within a closed loop path or “ring” with the aid of successive reflections from multiple mirrors. The closed path is defined by an optical cavity which is interior to a structural gyroscope frame or “block”. In one type of RLG, the block includes planar top and bottom surfaces that are bordered by six planar sides that form a hexagon-shaped perimeter. Surfaces on each of the sides define mounting areas for components such as mirrors and electrodes. For example, three planar non-adjacent sides of the block form the mirror mounting surfaces for three mirrors at the corners of the optical path, which is triangular in shape.
Operationally, upon rotation of the RLG about its input axis (which is perpendicular to and at the center of the planar top and bottom surfaces of the block), the effective path length of each counter-rotating laser light beam changes, and a frequency differential is produced between the beams that is nominally proportional to angular rate. This differential is then measured by signal processing electronics to determine the angular rotation of the vehicle.
A typical RLG block has three electrodes, which are disposed one on each of three non-adjacent planar side surfaces, and three mirrors, one of which has a concave reflective surface while the other two mirrors have planar reflective surfaces. The curved mirror serves two main purposes. First, the curvature of the reflective surface controls the diameter and the primary mode of the counter-rotating laser light beams. Second, the curvature of the reflective surface is used to align the counter-rotating laser light beams within the optical cavity so that the light beams are at substantially maximum intensity to minimize RLG bias errors. In particular, this latter purpose is accomplished due to the inherent attributes of the concave reflective surface. By nature, the angle of the surface of a concave mirror varies in accordance with its curvature. Therefore, an incident laser light beam can be redirected or “steered” by translating (i.e., moving) the curved mirror within the plane of its respective block mounting surface.
In practice, with the two planar mirrors already mounted on the block, the concave mirror is translated to selectively steer the light beam within the optical cavity via a conventional mirror movement mechanism. During translation of the concave mirror, a detector, such as a photodiode, senses the intensity of the laser light out put from the cavity through one of the planar mirrors that is partially transmissive. The photodiode generates an electrical signal representative of the intensity of the laser light output from the optical cavity. This signal is monitored by a voltmeter during such translations of the concave mirror until a mirror position is found exhibiting a maximum output on the voltmeter. This mirror position indicates that the counter-rotating laser light beams are at substantially maximum intensity and therefore are optimally aligned within the aperture of the optical cavity. The concave mirror is then secured to its mounting surface on the block at the optimum mirror position to complete the laser light beam alignment process.
Though the above described alignment mechanism and process adequately aligns the counter-rotating laser light beams within the optical cavity of the block so as to minimize RLG bias errors, there is at least one disadvantage. The mechanism and process described requires a great deal of handling of the concave mirror, particularly when translating the mirror about its mounting surface to identify the mirror's optimum mirror mounting position. The greater the extent of concave mirror manipulation, the better the chance of introducing contaminants (i.e., dirt) to or damaging the delicate reflective surface of the mirror. Any damage and/or contamination increases the likelihood of bias errors and degrades RLG performance. If the bias errors are too great and/or the RLG performance too corrupted, the RLG must be rebuilt or scraped. This increases the manufacturing cost of producing the RLG's.
There is a need for improved device and method for achieving optical alignment of an optical cavity such as the optical cavity of an RING. In particular, there is a need for a mirror alignment device and method that reduces the amount of mirror handling needed to align the light beams within the optical cavity. In addition, the device and method should reduce the likelihood of mirror reflective surface damage and/or contamination during alignment, to reduce the number of RLG's needing to be rebuilt or scrapped. Moreover, the mirror alignment device and method should be relatively easy and inexpensive to practice and should facilitate automation of assembly.
BRIEF SUMMARY OF THE INVENTION
The present invention is a method for locating the optimal position for a concave mirror alignment device on a RLG block so as to minimize RLG bias errors. A preferred embodiment of method includes the following steps: 1) mount a “log” onto a CNC machine; 2) select several points along the length of the log for measurement; 3) measure the mirror mounting surface radial distances at each of the several points from the “front” of the log; 4) measure the surface radial distances at each of the several points from the “rear” of the log; 5) determine the radius, and ultimately the diameter, of a circle tangent to the mirror mounting sides of the log, for each of the several selected points; 6) determine a “best fit” equation to describe the diameters as a function of position along the log; 7) determine the offset along the x axis for the mirror mounting device of each block within the log.
REFERENCES:
patent: 4777639 (1988-10-01), Whitehouse
patent: 4831632 (1989-05-01), Simms
patent: 4861160 (1989-08-01), Hammons et al.
patent: 4884283 (1989-11-01), Rahn et al.
patent: 5960025 (1999-09-01), Thorland et al.
Altmann Gerald R.
Carlson David W.
Sittler Daniel L.
Thorland Rodney H.
Font Frank G.
Fredrick Kris T.
Honeywell International , Inc.
Rodriguez Armando
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