DISPLACED APERTURE BEAMSPLITTER FOR LASER TRANSMITTER/RECEIVER OPTO MECHANICAL SYSTEM

Abstract: A single aperture opto-mechanical system for transmitting two small-aperture laser beams (10, 11) and single received laser beam (12). An in-coming beam (12) is received along a path that is essentially parallel with the path of transmitted beams (10, 11). The small-aperture transmitted beams (10, 11) each pass through a hole (28, 29) in a metal mirror beamsplitter (5) that is positioned to reflect the received light energy (12) at a 90 DEG angle through a narrow band-pass filter (6) and focused by an aspheric glass lens (7) that directs the received beam energy (12) onto a receiver detector (8). The out-going beams (10, 11) are transmitted through the top and bottom of portions of the afocal beam expanders (18) optical aperture which is specifically achromatized for the two displaced transmitted beams (10, 11) at the two wavelengths such that they exit the beam expander (18) off axis from the optical center line and maintain parallel alignment to within a few micro-radians. The objective lens (1) is movable in a plane orthogonal to the optical axis of the beam expander (18) for steering the two transmitted beams (10, 11) and the receiver beam path (12).

Description: DISPLACED APERTURE BEAMSPLITTER FOR LASER TRANSMITTER/RECEIVER OPTO MECHANICAL SYSTEM Technical Field: The present invention relates to an opto-mechanical system incorporating a pair of transmitted laser beams and a received beam that share common optics. The opto-mechanical system has particular utilities for portable devices used for distance measuring applications. Background of the Invention: In a typical rangefinder application, the line-of-sight (LOS) of a high quality visual optical path used for locating and identifying a target is aligned with the LOS of a second optical path associated with an eye-safe laser. The eye-safe laser beam reflects off the target and becomes a return optical signal that is received along a path that is aligned with the transmitted eye-safe laser. A receiver detector senses the received beam to acquire information that can be used to determine the distance to the object. The receiver detector, the laser cavity optical system for producing the eye-safe laser beam, and the visible aiming beam, produced by a laser diode and collimating optics, cannot be mounted on an optical bench coaxially, they must be separated. Prior art rangefinding applications typically use complex and expensive multiple-bounce dichroic beamsplitters to yield coaxial laser transmitter and aiming beam optical paths and separate the received laser beam from the transmitted beams. Splitting the transmitted paths from the receiver path typically requires dichroic optical coatings on the beamsplitter. Prior art beamsplitters may require as much as four tightly toleranced regions of different optical coatings. Prior art beam steering methods typically require repackaging of the aiming light to accommodate complex beamsplitters with added cost and weight to the overall opto-mechanical package. Critical to rangefinder applications is the angular alignment of the three laser beam paths must be held to tight tolerances. This places difficult alignment and retention requirements on the optical elements typically used to combine the two transmitted paths. For example, one laser is often transmitted through a beamsplitter (usually tilted at 45E) and combined with the first beam. This causes the angular alignment sensitivity and retention of the beamsplitter to be twice as sensitive as the angular requirement between the two beams, requiring costly optical alignment at manufacturing time. In use, each of the two LOS paths must be steered from their respective nominal position. The two LOS paths and the received path are manipulated in unison in a manner that ensures that all paths have essentially the same deviation from their nominal position. Prior art beam steering methods for multi-wavelength systems require wedges or prism pairs for LOS steering. Summary of the Invention: The present invention is comprised of one eye-safe transmitted laser beam, a visible transmitted light beam, and a single received laser beam that all share a single aperture optical system. The two pencil-thin transmitted beams are co-aligned within 150 micro-radians in the same direction but have optical axes that are displaced laterally. Lateral displacement of the two transmitted beams eliminates the requirement for complex beam combining optics, which relaxes the opto-mechanical tolerances. The in-coming beam is received along a path that is essentially parallel with the path of the transmitted laser beams within 500 micro-radians. One variation of the present invention provides for a receiver path and detector for sensing the received laser beam. Other specific variations of the present invention provide mechanical and optical methods for expanding, aligning, and steering the three parallel beams as well as separating the in-coming receiver laser beam from the two out-going transmitted laser beams. An exemplary embodiment of the present invention utilizes for one of the out-going transmitted beams an infrared eye-safe laser having a wavelength of 1.533Φm. The second out-going transmitted beam is produced by a laser diode in the visible red spectrum having a wavelength of 0.655Φm and is used as an aiming light for boresighting the unit to a weapon. The in-coming received beam is the reflection or scattering of the transmitted infrared eye-safe laser beam off the target. Due to the very small size of the transmitted beams in comparison to the receiver aperture, a standard glass beamsplitter with anti-refection and dichroic coatings is not needed to separate the received beam from the transmitted beams. In one variation of a specific embodiment, the small-aperture transmitted beams each pass through a hole in a metal mirror beamsplitter that is positioned to reflect a substantial amount of the received laser energy at a 90E angle. The preferred embodiment of the beamsplitter is a simple aluminum mirror with a thin highly reflective metallic coating with holes that allow the laser transmitter and aiming beams to pass through the mirror. The mirror provides about 98% reflectivity for the receiver beam and 100% throughput for the transmitted beams. The beamsplitter has indexing features that provide self-alignment of the beamsplitter to the laser mount, thereby reducing optical alignment cost. In another specific embodiment of the present invention, the out-going transmitted beams are magnified by four times by Galilean telescope beam expander optics. Magnification of the transmitted laser beams by the beam expander optics allows for substantially smaller and lighter laser sources than would be possible without the beam expander optics. The two out-going beams are transmitted through the top and bottom portions of the afocal beam expander?s optical aperture. The beam expander is also used by the receiver path in conjunction with the beamsplitter, receiver lens and filter. The objective lens of the beam expander in the preferred embodiment is a cemented doublet, comprised of a positive high-refractive-index crown lens having a bi-convex shape and a very high-refractive-index flint lens having a meniscus-concave shape. The negative lens "eyepiece" of the beam expander in the preferred embodiment has a bi-concave-shape and is formed of a low-index crown glass. The design of the afocal Galilean telescope beam expander optics is not a conventional achromatic design. The novel aspects of the design of the beam expander optics lie in the methods where the objective lens is specifically achromatized at the 1.533Φm and 0.655Φm wavelengths at the displaced apertures of the two transmitted beams such that they exit the beam expander telescope off-axis from the optical center line and maintain relative angular alignment to within a few micro-radians. The design of the beam expander optics also achieves a very flat wavefront (with almost no residual aberrations) for the full aperture of the receiver path to obtain the image quality required at the receiver detector. The Galilean telescope beam expander does not have an intermediate image, thus the transmitted laser beam does not get concentrated at a focus; this prevents ionization of the air. In a specific embodiment of a rangefinder, the received beam passes through a narrow band-pass filter for filtering out all wavelengths except the desired 1.533Φm, and is focused by an aspheric glass lens that directs the received beam energy onto a receiver detector. The receiver detector in the preferred embodiment is a light detecting diode. The optical system has the capability of being steered over a +/- 0.5E field of view (FOV). The objective lens is movable in a plane orthogonal to the optical axis of the objective lens. In one exemplary embodiment, the objective lens can be moved by as much as 0.775mm away from the initial position of the optical axis for steering the transmitted beams and the receiver beam path up to an angle of 0.5E while maintaining the required angular alignments between the two transmitted beams and the received beam. The methods of the present invention provide various opto-mechanical systems for rangefinding and boresight applications. Ruggedness, small size, and light weight are significant advantages for applications that require portability. Specific embodiments may have one or more advantages over methods of prior art including: (1) less weight, (2) smaller physical size, (3) decrease in manufacturing cost, and (4) increased ruggedness. Brief Description of the Drawings: FIG. 1 shows a ray-trace diagram of the present invention. FIGS. 2a and 2b shows a beamsplitter of the present invention. FIG. 3 illustrates a method of the present invention for steering the LOS. Detailed Description of Preferred Embodiments: FIG. 1 shows a ray-trace diagram of an embodiment, which exemplifies different specific aspects of the present invention. Transmitted laser beams 10, 11 pass through small holes 28, 29 in a metal mirror beamsplitter 5 and are magnified by four times by Galilean telescope beam expander optics 18 comprised of an objective lens 1 and a negative lens 4. The transmitted beams pass through respective top and bottom portions of the expander optics 18 that have a close proximity to the periphery of the objective 1 and negative 4 lenses. A received beam 12 is received through the aperture of the objective lens 1 , which is shared by the two out-going transmitted beams 10, 11. The external portions 110, 111 of both transmitted beams 10, 11 that are out-going from the Galilean telescope beam expander optics have optical axes that are essentially parallel to the optical axis of the external portion 112 of the received beam 12 that is in-coming to the shared Galilean telescope beam expander optics. In FIGS. 1 and 3, the transmitted beam external portions 110, 111 and the incoming received beam external portion 112 are shown in the ray-trace diagram as extending from surface R1 of the objective lens 1 through the sealing window 9. The eye-safe laser beam 10 has a wavelength of 1.533Φm, a diameter of 0.8mm prior to magnification and an optical axis that is located 3.35mm from the optical axis of the beam expander 18. The aiming beam 11 has a wavelength of 0.655Φm, has a diameter of 2mm prior to magnification, and is located 2.77mm from the beam expander?s 18 optical axis. The incoming laser beam 12 has a wavelength of 1.533Φm and is received through objective lens 1 of the beam expander optics 18 shared by the two transmitted beams 10, 11. The received beam 12 is essentially coaxial with the optical axis of the beam expander 18 and has a diameter of 34.76mm. An iterative process is used to design the afocal Galilean telescope beam expander optics using a design and simulation computer software program. Design and simulation programs are well known to those skilled in the art. The essential program input parameters include the type of telescope, the wavelengths of the transmitted and received laser beams, and that good aberration correction is required. In the exemplary design shown in Figure 1 , the sealing window 9 is formed of Schott BK7 glass and is 2.41 mm thick. The objective lens 1 of the beam expander 18 is a cemented doublet comprised of a bi-convex shaped lens 2 and a meniscus-concave lens 3. The bi-convex shaped lens is made of a very high-refractive-index crown glass Schott LaKN13. It has a thickness of 7.24mm along the optical center line, an outer radius R1 of 62.87mm, and an inner radius R2 of -52.19mm that is equal to the inner radius of the meniscus- concave lens. The meniscus-concave lens is made of a very high-refractive- index flint glass Schott SFL6, has an outer radius R3 of -377.4mm, and a thickness of 1.52mm along the optical centerline. The negative lens 4 is located along the optical axis of the objective lens 62.74mm from the objective lens. The negative lens 4 is formed of low-index crown glass Schott BK7 and has a bi-concave shape having a first radius R4 of -96.08mm, a second radius R5 of 13.07mm, and a thickness of 1.52mm along the optical center line. Energy from the received laser beam 12 is separated from the two transmitted beams 10, 11 by a metal mirror beamsplitter 5. About 98% of received beam energy is reflected off the metal mirror beamsplitter 5 and passed through a narrow band pass filter 6 formed of a silicon substrate for filtering out all wavelengths except the desired 1.533Φm. An aspheric glass lens 7 (Geltech part number 350240) focuses the received beam 12?s energy onto the receiver detector 8. The receiver detector 8 in the preferred embodiment is a light detecting diode (EG&G part number 30718E). In the exemplary embodiment shown in FIG. 1 , the receiver detector 8 inlet path is essentially orthogonal to the optical axis of the beam expander optics 18. A beamsplitter 5, positioned at a 45E angle from the optical axis of the beam expander optics 18, separates the received beam 12 from the two transmitted beams 10, 11 , and bends the received beam 12 path 90E into the receiver detector 8. An exemplary beamsplitter 5 of the present invention is shown in FIG. 2. The beamsplitter 5 is preferably formed of aluminum 23 with a thin nickel plating 21 on one surface that is optically polished to provide a highly smoothed surface 24. This nickel surface can then be coated with aluminum with a further protective coating of SiO x or, alternatively, either plated with gold or coated with gold with a further protective coating of SiO x . Either process results in a highly reflective mirror surface. Alternately, the beamsplitter 5 may be formed of copper that is optically polished on one side 24 and then overcoated with a protective layer of SiO x . Two small holes 28, 29 which are oversized somewhat as compared to the diameter of the transmitted beams 11 , 10 are formed in the metal mirrors to allow the two transmitted beams 11 , 10 to pass through. One specific embodiment utilizes an indexing feature 25 on the beamsplitter 5 to achieve self-alignment of the beamsplitter 5 to a laser mount, eliminating costly manual optical alignment. Self-alignment is accomplished by positioning the notch 25 on the beamsplitter 5 to a mating projection 30 on the laser mount such that the two orthogonal edges of the notch 25 are firmly pressed against two respective surfaces of the projection 30 on the laser mount. The two edges of the notch 25 and respective surfaces on the mating projection 30 on the laser mount are accurately machined to a few micro- meters to provide an accurate x-y location as well as accurate rotational position of the beamsplitter 5 to the mount. The beamsplitter 5 can then be rigidly bonded to three machined pads on the mount that are held to tight tolerances to achieve a three-point kinematic attachment of the beamsplitter 5 on the laser mount. Now referring to FIG. 3, a variation of the present invention provides the capability for steering the LOS of both the transmitted 110, 111 and received beam 112 over a +/- 0.5E field of view (FOV). The objective lens 1 is movable in all directions within the plane that is orthogonal to the optical axis of the objective lens 1. In the exemplary embodiment, the objective lens can be moved by as much as 0.775mm away from the initial position of the objective lens 1 for steering the external portions 110, 111 of the two transmitted beams 10, 11 , and the external portion 112 of the received beam 12 up to an angle of 0.5E from their respective nominal positions. The external portions 110, 111 , 1 12 of the three beams maintain the required relative angular alignment. FIG. 3 shows the objective lens 1 ? in a position displaced from the centered position 1 such that the external portions of the in-coming beam 112 and the external portions of the transmitted beams 110 and 111 each have an optical axis that is at a desired angle from their respective nominal positions 110, 111 , 112. The present invention, therefore, is well adapted to carry out and attain the advantages mentioned herein as well as other ends and advantages made apparent from the disclosure. While preferred embodiments of the invention have been described for purposes of disclosure, numerous changes and modifications to those embodiments described herein will be readily apparent to those skilled in the art and are encompassed within the spirit of the invention and the scope of the following claims.

Claims: CLAIMS What is claimed is: 1. An opto-mechanical system comprising: a Galilean-telescope beam expander (18) including a large- aperture objective lens (1) and a negative lens (4) defining an associated optical axis, for receiving a large-aperture beam (12) having a first wave length and propagating in an in-coming direction along said optical axis; a first small-aperture beam (10) having said first wavelength and propagating in an out-going direction opposite to said incoming direction, such that said first small-aperture beam (10) is displaced from said optical axis and is transmitted through a second peripheral portion of said Galilean-telescope beam expander remote from said first peripheral portion; a second small-aperture beam (11) having a second wavelength different from said first wavelength and also propagating in said outgoing direction, such that said second small-aperture beam (11) is displaced from said optical axis and from said first small-aperture beam (10) and is transmitted through a second peripheral portion of said Galilean-telescope beam expander (18) remote from said first peripheral portion; and a beamsplitter (5) for separating said large-aperture beam (10) from said optical axis after said large-aperture beam (12) has entered said objective lens (1) and has exited from said negative lens (5); wherein a respective external-portion (110), (111) of each of said small-aperture beam out-going from said objective lens (1) are both essentially parallel to an external-portion of said large-aperture beam (112) in-coming to said objective lens (1). 2. The opto-mechanical system of claim 1 wherein said beamsplitter (5) is an opaque mirror (5) formed with two holes (28), (29) for substantially separating said large-aperture beam (12) from both said first and said second small-aperture beams (10), (11). 3. The opto-mechanical system of claim 2 further comprising: a laser mount; and wherein said opaque mirror (5) is formed with an indexing feature (25) for self-alignment of said mirror to said laser mount. 4. The opto-mechanical system of any one or more of claims 1 - 3: wherein said first wavelength is 1.533Φm and said second wavelength is 0.655Φm. 5. The opto-mechanical system of any one or more of claims 1 - 4: wherein said large-aperture objective lens is a cemented doublet comprised of a bi-concave-shaped lens (2) formed of positive, high-refractive-index crown glass and a meniscus-concave shaped lens (3) formed of very high-refractive-index flint glass; and wherein said negative lens (4) has a bi-concave shape and is formed of low-index crown glass. 6. The opto-mechanical system of any one or more of claims 1 - 4: wherein said objective lens (1) is movable in the directions essentially orthogonal with the optical axis of said Galilean-telescope beam expander (18) for steering said respective external-portions (110), (111) of said first and said second small-aperture beams (11), (12) outgoing from said objective lens (1), and for steering said externa-portions (112) of said large-aperture beam (12) in-coming to said objective lens (1). 7. The method for determining distance to an object comprising the steps of: providing a Galilean-telescope beam expander (18) including a large-aperture objective lens (1) and a negative lens (4) defining an associated optical axis, for receiving a large-aperture beam (12) having a first wave length and propagating in an in-coming direction along said optical axis; providing a first small-aperture beam (10) having said first wavelength and propagating in an out-going direction opposite to said incoming direction, such that said first small-aperture beam (10) is displaced from said optical axis and is transmitted from said negative lens (4) to said objective lens (1) through a first peripheral portion of said Galilean-telescope beam expander (18); providing a second small-aperture beam (11) having a second wavelength different from said first wavelength and also propagating in said out-going direction, such that said second small-aperture beam (11) is displaced from said optical axis and from said first small- aperture beam (10) and is transmitted through a second peripheral portion of said Galilean-telescope beam expander (18) remote from said first peripheral portion; and providing a beamsplitter (5) for separating said large-aperture beam (12) from said optical axis after said large-aperture beam (12) has entered said objective lens (1) and has exited from said negative lens (4); wherein a respective external-portions (110), (111) of each of said small-aperture beam (10), (11) out-going from said objective lens (I) are both essentially parallel to an external-portion (112) of said large-aperture beam (12) in-coming to said objective lens (1); providing a distant object; reflecting said first small-aperture beam (10) off said distant object to produce said large-aperture beam (12). 8. The method of claim 7 for determining the distance to an object: wherein said beamsplitter (5) is an opaque mirror (5) formed with two holes (28), (29). 9. The method of any one or more of claims 7, 8 for determining the distance to an object further comprising the step of: providing a detector (8) for sensing said large-aperture beam (12); and sensing said large-aperture beam (12). 10. The method of any one or more of claims 7 - 9 for determining distance to an object: wherein said objective lens (1) is movable in the directions essentially orthogonal with said optical axis of said Galilean-telescope beam expander (18) for steering said respective external-portions (110), (111) of said first and said second small-aperture beams (10), (I I) outgoing from said objective lens (1), and for steering said external-portions (112) of said received beam (12) in-coming to said objective lens (1).

Inventors: CHEN PAN-FEY F, NOYES GARY R, PATEL ASHOK B, PURER EDNA M, CHEN, PAN-FEY, F., NOYES, GARY, R., PATEL, ASHOK, B., PURER, EDNA, M.
Applicants: RATHEON COMPANY
Application year: 1999
Main classification: G02B26
IPC codes: G01S7, G02B27