Method and apparatus for making an electromagnetic beam combiner
A beam combiner includes a first beam-input face, a beam-output face, and first and second reflectors. The first beam-input face receives first and second beams of electromagnetic energy respectively having a first and second wavelengths. The first reflector reflects the first received beam toward the beam-output face, and the second reflector passes the first beam from the first reflector and reflects the received second beam toward the beam-output face. In one alternative, the first beam-input face also receives a third beam of electromagnetic energy having a third wavelength, the beam combiner includes a third reflector that reflects the received third beam toward the beam-output face, and the first and second reflectors pass the third beam from the third reflector. In another alternative, the beam combiner includes a second beam-input face that receives a third beam directed toward the beam-output face, and the first and second reflectors pass the third beam
Latest Patents:
Electronic color images, such as television images, are typically generated using three electromagnetic beams that each represent a different primary color. For example, a color-television screen typically includes an array of pixels that are each split into three phosphorescent regions: red (R), green (G), and blue (B). Three corresponding electron beams, one each for R, G, and B, are aligned such that they simultaneously strike the R, G, and B regions of the same pixels as the beams sweep across the screen. These beams cause the R, G, and B regions of a pixel to phosphoresce, and the human eye integrates the light generated by the phosphorescing R, G, and B regions of all the pixels to perceive a color image. By adjusting the respective intensities of the beams, the color television can generate a pixel having virtually any color. Alternatively, the R, G, and B beams can be light beams that the human eye perceives and integrates directly.
A problem with the image generator 100 is that its maximum image scan angle φ is 2θ less than the maximum image scan angle of a single-beam image generator (not shown). The maximum scan angle φ is the angle over which the mirror 110 can scan an image onto the display area 102. Specifically, the rightmost portion of the area 102 is defined by the rightmost position of the B beam, i.e., the position of the B beam when the mirror 110 is in its right most position. Likewise, the leftmost position of the area 102 is defined by the leftmost position of the R beam. When the B beam is in its rightmost position, and is thus at the rightmost edge of the area 102, the R beam is 2θ beyond the rightmost edge of the area 102. Likewise, when the R beam is in its leftmost position, and is thus at the leftmost edge of the area 102, the B beam is 2θ beyond the leftmost edge of the area 102. Consequently, 2θ of the sweep angle of the mirror 110 is wasted. That is, if the mirror 110 scanned only a single beam—the R beam for example—then φ would increase by 2θ. This 2θ reduction in the maximum scan angle φ may be significant in applications such as a virtual retinal display (VRD) where the maximum scan angle φ of the mirror is small to begin with.
To overcome the problem of a reduced scan angle in a multi-beam image generator such as the generator 100, one can combine the multiple beams into a single, composite beam.
The X-cube 200 is a combination of four right-angle prisms 204, 206, 208, and 210 having vertices that meet at the center axis 212 (in the Z dimension) of the X-cube and form two interfaces 214 (dash line) and 216 (solid line). Before the X-cube 200 is assembled, the internal prism faces that form the first interface 214 are treated with an optical coating that reflects red light but passes green and blue light. Similarly, the prism faces that form the second interface 216 are treated with an optical coating that that reflects blue light but passes green and red light. Furthermore, either before or after the X-cube 200 is assembled, the external faces 218, 220, 222, and 224 of the prisms 204, 206, 208, and 210 are polished to an optical finish since they respectively receive and project the R, G, B, and composite beams of light.
First, the operation of the X-cube 200 is discussed where the R, G, and B beams 104, 106, and 108 include only their single center rays (solid line). This discussion also applies to thin beams—such as beams that are a single pixel wide—that are much narrower than the faces 218, 220, 222, and 224 of the X-cube 200. That is, this discussion also applies to collimated beams that are neither converging toward a focus nor diverging as they pass through the X-cube 200. The R, G, and B beams 104, 106, and 108 enter the X-cube 200 at the respective faces 220, 218, and 222, and the X-cube projects the composite beam 202 from the face 222. Specifically, the G beam 106 propagates through the face 218 to the center axis 212, passes through the interfaces 214 and 216, and exits the face 222 as part of the composite beam 202. The R beam 104 propagates through the face 220 to the center axis 212, and is reflected out of the face 222 by the interface 214 as part of the composite beam 202. Similarly, the B beam 108 propagates through the face 224 to the center axis 212, and is reflected out of the face 222 by the interface 216 as part of the composite beam 202. As long as the prisms 204, 206, 208, and 210 are properly dimensioned and aligned, the composite beam 202 is a single ray, i.e., is no wider than the R, G, and B beams 104, 106, and 108.
Therefore, referring to
Next, the operation of the X-cube 200 is discussed where the R, G, and B beams 104, 106, and 108 are wider than a single ray (dashed line), i.e., have diameters/widths that are on the order of the widths of the faces 218, 220, 222, and 224. For example, such wide R, G, and B beams may respectively include the R, G, and B components of an entire image as opposed to merely a single pixel of the image. The operation is similar to that described above for the narrow-beam case, but because the R, G, and B beams are wider, they intersect the interfaces 214 and 216 at regions that are centered about the center axis 212. Furthermore, the interfaces 214 and 216 reverse the R and B beams such that the R and B image components in the composite beam 202 are the “mirror images” of the R and B image components in the R and B beams. But this reversal can easily be accounted for by “reversing” the contents of the R and B beams before they enter the X-cube 200.
Image-projection devices, such as overhead projectors, often include an X-cube that operates in the wide-beam mode.
Still referring to
Another problem is that for the X-cube 200 to function correctly, it may be necessary to rotate the polarization of the G beam 106 by 90° (relative to the polarization of the R and B beams) before it enters the X-cube. One way to accomplish this rotation is to insert a half-wave retarder (not shown) into the path of the G beam before it enters the face 218. Unfortunately, this may increase the cost of an image generator that includes the X-cube.
SUMMARY OF THE INVENTIONIn one aspect of the invention, a beam combiner includes a first beam-input face, a beam-output face, and first and second reflectors. The first beam-input face receives first and second beams of electromagnetic energy respectively having a first and second wavelengths. The first reflector reflects the first received beam toward the beam-output face, and the second reflector passes the first beam from the first reflector and reflects the received second beam toward the beam-output face. In one alternative, the first beam-input face also receives a third beam of electromagnetic energy having a third wavelength, the beam combiner includes a third reflector that reflects the received third beam toward the beam-output face, and the first and second reflectors pass the third beam from the third reflector. In another alternative, the beam combiner includes a second beam-input face that receives a third beam directed toward the beam-output face, and the first and second reflectors pass the third beam.
Such a beam combiner can be less expensive than an X-cube because it is easier to manufacture. For example, the beam combiner often requires fewer precision cuts and has a less-stringent alignment tolerance because the most or all of the machining can be done after the combiner is assembled. Furthermore, the combiner can often be manufactured in bulk using off-the-shelf materials, thus further reducing the cost and manufacturing complexity.
In addition, such a beam combiner does not require the use of a half-wave retarder.
BRIEF DESCRIPTION OF THE DRAWINGSThe foregoing aspects and many of the attendant advantages of this invention will become more readily appreciated as the same become better understood by reference to the following detailed description, when taken in conjunction with the accompanying drawings, wherein:
The following discussion is presented to enable a person skilled in the art to make and use the invention. The general principles described herein may be applied to embodiments and applications other than those detailed below without departing from the spirit and scope of the present invention. The present invention is not intended to be limited to the embodiments shown, but is to be accorded the widest scope consistent with the principles and features disclosed or suggested herein.
The beam combiner 300 includes three sections 306, 308, and 310, which are bonded together and which are made from a transparent material such as glass or polymer suitable for optical applications. The combiner 300 also includes an input face 312 having a length of 3W and a rectangular cross section in the X-Z plane, and includes an output face 314 having a height of W and a square cross section in the Y-Z plane. In one embodiment, W=5.5 millimeters (mm), and in another embodiment W=3.5 mm. Both the input face 312 and the output face 314 are flat, optical-quality surfaces. The manufacture of the combiner 300 is discussed below in conjunction with
The first section 306 has a parallelogram-shaped cross section in the X-Y plane with a height and width of W and includes a segment input face 316, which forms part of the combiner input face 312, and a reflector face 318 for reflecting the R beam 104 toward the combiner output face 314. In one embodiment, the face 318 is made reflective by application of a conventional optical coating. One can select the reflective and transmissive properties of this coating (and the other coatings discussed below) according to the parameters of the beam-combiner system. The angle α between the input face 316 and the reflector face 318 is an acute angle. In a preferred embodiment, α=45° to allow the R beam 104 to have a maximum width in the X dimension equal to W. That is, if α=45°, then all portions of a W-width R beam will project onto the reflector face 318 as long as the R beam is properly aligned with the input face 316. If, however, the combiner 300 is designed for a R beam 104 having a width less than W, then the region of the face 318 that is reflective can be limited to the area that the R beam will strike. Alternatively the angle α can be made greater than 45°. But because the angle α is the same for all of the segments 306, 308, and 310, one should consider the effect on the other segments 308 and 310 before altering the value of α. Furthermore, if α does not equal 45°, then the angle of the R beam from the beam source 304 is adjusted such that the reflected R beam remains normal to the output face 314.
Similarly, the second section 308 has a parallelogram-shaped cross section in the X-Y plane with a height and width of W and includes a segment input face 320, which forms part of the combiner input face 312, and includes a reflector face 322, which lies along an interface between the sections 306 and 308 and passes the reflected R beam 104 and reflects the G beam 106 toward the combiner output face 314. In one embodiment, the face 322 is made reflective by application of a conventional optical coating to either or both the face 322 and the face of the section 306 that interfaces with the face 322. The angle α between the input face 320 and the reflector face 322 is an acute angle, and is preferably equal to 45° to allow the G beam 106 to have a maximum width in the W dimension equal to W. If, however, the combiner 300 is designed for a G beam 106 having a width less than W, then the region of the face 322 that is reflective can be limited to the area that the G beam will strike. Alternatively the angle α can be made greater than 45°. But because the angle α is the same for all of the segments 306, 308, and 310, one should consider the effect on the other segments 306 and 310 before altering the value of α. Furthermore, if α does not equal 45°, then the angle of the G beam from the beam source 304 is adjusted such that the reflected G beam remains normal to the output face 314.
The third section 310 has a triangular-shaped cross section in the X-Y plane and includes the combiner output face 314, a segment input face 324, which has a width of W and which forms part of the combiner input face 312, and a reflector face 326, which lies along an interface between the sections 308 and 310 and passes the reflected R and G beams 104 and 106 and reflects the B beam 108 toward the combiner output face. In one embodiment, the face 326 is made reflective by application of a conventional optical coating to either or both the face 326 and the face of the section 308 that interfaces with the face 326. The angle α between the input face 324 and the reflector face 326 is an acute angle, and is preferably equal to 45° to allow the B beam 108 to have a maximum width in the X-dimension equal to W. If, however, the combiner 300 is designed for a B beam 108 having a width less than W, then the region of the face 326 that is reflective can be limited to the area that the B beam will strike. Alternatively the angle α can be made greater than 45°. But because the angle α is the same for all of the segments 306, 308, and 310, one should consider the effect on the other segments 306 and 308 before altering the value of α. Furthermore, if α does not equal 45°, then the angle of the B beam from the beam source 304 is adjusted such that the reflected B beam is normal to the output face 314. Moreover, an angle β between the section input face 324 and the output face 314 is substantially a right angle in a preferred embodiment.
The beam source 304 includes three beam-generating sections 328, 330, and 332 for respectively generating the R, G, and B beams such that they traverse paths having substantially the same optical length. This causes the images of the R, G, and B light-emitting points in the combined beam to occur at the same distance from the output face 314 of the beam combiner 300, and thus allows focusing of all three colors to the same plane with a single focusing lens located after the output face of the beam combiner. For purpose of illustration, assume that the center rays (shown in solid line) of the R, G, and B beams enter the respective centers (in the X dimension) of the faces 316, 320, and 324 as shown in
Although the preceding discussion approximates optical path length as actual path length, one of skill in the art will realize that the optical path length through a medium other than free space is typically longer than the actual path length due to the medium having an index of refraction that is greater than one. Consequently, one can more precisely equalize the optical path lengths that the R, G, and B beams traverse by accounting for the indices of refraction of the segments 306, 308, and 310 and the medium between the beam combiner and the beam source 304 when determining the respective distances between the beam-generating sections 328, 330, and 332 and the input face 312.
Moreover, the beam source 304 is preferably aligned with the beam combiner 300 such that the center rays (solid line) of the R, G, and B beams 104, 106, and 108 are respectively aligned with the centers (in the X dimension) of the section input faces 316, 320, and 324. However, even if the center rays are not aligned with the face centers, the R, G, and B beams will be aligned such that, in the composite beam 302, the center rays of all three beams will be approximately collinear.
Still referring to
The R beam 104 propagates the distance D from the beam-generating section 328 to the beam-input face 316, and is substantially normal to the beam-input face. Preferably, the center ray of the R beam is aligned with the center of the face 316 in the X dimension. Next, the R beam propagates the distance W/2 from the face 316 to the reflector 318. Then, the reflected R beam, which is substantially parallel to the face 316, propagates the distance 2W from the reflector 314 to the reflector 326, and then propagates another W/2 to the beam-output face 314 as part of the composite beam 302, which is substantially normal to the beam-output face. Therefore, as stated above, the optical length of the R-beam path from the beam-generator section 328 to the beam-output face 314 is D+3W.
The G beam 106 propagates the distance W+D from the beam-generating section 330 to the beam-input face 320, and is substantially normal to the beam-input face. Preferably, the center ray of the G beam is aligned with the center of the face 320 in the X dimension. Next, the G beam propagates the distance W/2 from the beam-input face 320 to the reflector 322. Then, the reflected G beam, which is substantially parallel to the face 320 and substantially coincident with the reflected R beam 104, propagates the distance W from the reflector 322 to the reflector 326, and then propagates another W/2 to the beam-output face 314 as part of the composite beam 302. Therefore, as stated above, the optical length of the G-beam path from the beam-generator section 330 to the beam-output face 314 is D+3W.
The B beam 108 propagates the distance 2W+D from the output of the beam-generating section 332 to the beam-input face 324, and is substantially normal to the beam-input face. Preferably, the center ray of the B beam is aligned with the center of the face 324 in the X direction. Next, the B beam propagates the distance W/2 from the beam-input face 324 to the reflector 326. Then, the reflected B beam which is substantially parallel to the face 324 and substantially coincident with the reflected R and G beams, propagates a distance of W/2 from the reflector 326 to the beam-output face 314 as part of the composite beam 302. Therefore, as stated above, the optical length of the B-beam path from the beam-generator section 332 to the beam-output face 314 is D+3W.
Still referring to
Alternatively, if the composite beam 302 is a pixel beam, i.e., includes the R, G, and B components of a single pixel, then the R, G, and B beams respectively include the instantaneous red, green, and blue components of the pixel. One can use a scanner such as the scanning mirror 110 of
Alternate embodiments of the beam combiner 300 and beam source 304 are contemplated. In one such embodiment, the R, G, and B beams may enter the input face 312 of the beam combiner 300 in an order other than the order (R-G-B) shown. For example, instead of the beam-generator section 328 generating the R beam and the beam-generator section 332 generating the B beam, the section 328 can generate the B beam and the section 332 can generate the R beam such that the R and B beams enter the combiner sections 310 and 306, respectively. Where the beams do not enter the input face 312 in the same order in which they appear in the electromagnetic spectrum (RGB or BGR), the reflective coatings that form the reflectors 318, 322, and 326 are more complex, requiring a band-pass response instead of a low-or high-pass response . Furthermore, the input face 312 may have other than a rectangular cross section, and the output face may have other than a square cross section. Moreover, one of the sections 306 or 308 may be omitted so that the combiner 300 generates the composite beam 302 from only two beams, such as R and B, R and G, or G and B. In addition, one can add additional sections that are similar to the sections 306 and 308 so that the combiner 300 generates the composite beam 302 from more than three beams. Furthermore, the widths of the segment input faces 316, 320, and 324 need not be equal. But to allow transfer of all the energy in the R, G, B beams to the combined beam 302 in this situation, the widths of the beams 104, 106, and 108 where they enter the respective segment input faces 316, 320, and 324 are typically no greater than the widths of the respective segment input faces. Moreover, where the width of the face 324 is greater than the width of the face 320, the segment 310 has a truncated triangular shape (flat bottom). In addition, although the segment input faces 316, 320, and 324 are shown as being coplanar to form a planar input face 312, the segment input faces need not be coplanar, and thus the input face 312 need not be planar. For example, the segment input face 316 may extend further toward, or abut, the beam-generator section 328. Similarly, the segment input face 320 may extend further toward, or abut, the beam-generator section 330, and the segment input face 324 may extend further toward, or abut, the beam-generator section 332. Depending on the system parameters, this may reduce the distance between the beam combiner 300 and the beam source 304, and thus may reduce the overall size of a module that includes the combination of the beam combiner and beam source. Furthermore, extending the segment input faces 316, 320, and 324 such that they respectively abut (or nearly abut) the beam-generator sections 328, 330, and 332 inherently equalizes the optical path lengths because the R, G, and B beams are propagating through only one material having a single index of refraction before emerging from the output face 314.
The beam combiner 400 includes three sections 406, 408, and 410 that are bonded together and that are made from a transparent material such as glass or polymer suitable for optical applications. The combiner 400 includes an input face 412, which is also the input face of the section 410, and which has a length W and a square cross section in the X-Z plane, and includes an output face 414 having a height W and a square cross section in the Y-Z plane. Both the input face 412 and the output face 414 are flat optical-quality surfaces. The manufacture of the combiner 400 is discussed below in conjunction with
The first section 406 has a parallelogram-shaped cross section in the X-Y plane, a width of S in the X dimension, and includes a reflector face 418 for reflecting the R beam toward the combiner output face 414. Because S is significantly smaller than the width W of the segment 306 of
Similarly, the second section 408 has a parallelogram-shaped cross section in the X-Y plane, a width of S in the S dimension, and includes a reflector face 422, which lies along an interface between the sections 406 and 408 and which passes the reflected R beam and reflects the G beam toward the combiner output face 414. Again, because S is significantly smaller than the width W of the segment 308 of
Like the third section 310 of
Using known geometrical principles, the length of the path traversed by the R-beam center ray from the beam generator (not shown in
Because the R beam passes through the B and G reflector faces 422 and 426 before striking the R reflective face 418, and because the G beam passes through the B reflector face 426 before striking the G reflective face 422, the spectra of the R and G beams and the faces 422 and 426 are non overlapping so that the combiner 400 does not generate artifacts such as “ghost” images. Specifically, if the face 422 or 426 reflects any of the R beam, or if the face 426 reflects any of the G beam (such reflections are shown in dashed line), then one or more unwanted beams 428 (dashed line) will emanate from the beam output face 414 in addition to the composite beam 402. These unwanted beams 428 may cause unwanted artifacts in the generated image. Consequently, it is preferred that the R beam contain no wavelengths that are within the spectrum of wavelengths that the faces 422 and 426 reflect, and that the G beam contain no wavelengths that are within the spectrum of wavelengths that the face 426 reflects. One technique for accomplishing this is to tune the beam generator (not shown in
In another embodiment, the level of artifacts such as “ghost” images is reduced or eliminated by making S large enough so that the unwanted beams 428 of the R and G beams are sufficiently spaced from the composite beam 402.
Furthermore, if the R beam (or a portion thereof) incident on the input face 412 is shifted to the left such that the beam is not incident on the face 426, then the R beam (or portion thereof) does not generate a corresponding unwanted beam 428. Likewise, if the R beam (or a portion thereof) is shifted further to the left such that it is not incident on the face 422, then the R beam (or portion thereof) does not generate unwanted beams 428 corresponding to the faces 422 and 428. A similar analysis applies to the G beam.
Still referring to
Alternate embodiments of the beam combiner 400 are contemplated. In one such embodiment, the R, G, and B beams may enter the input face 412 of the beam combiner 400 in an order other than the order (R-G-B) shown. For example, instead of the B beam entering the combiner 400 closest to the output face 414, one may swap the positions of the R and B beams. Furthermore, the ends of the sections 406 and 408 need not be coplanar with the input face 412. Conversely, the R or G beams may be incident on the sections 406 and 408 instead of on the section 410. Moreover, one of the segments 406 or 408 may be omitted so that the combiner 400 generates the composite beam 402 from only two beams. In addition, one can add additional sections that are similar to the sections 406 and 408 so that the combiner 400 generates the composite beam 402 from more than three beams. Furthermore, the input face 412 may have other than a rectangular cross section, and the output face 414 may have other than a square cross section.
The beam combiner 500 includes three sections 506, 508, and 510 that are bonded together and that are made from a transparent material such as glass or polymer suitable for optical applications. The combiner 500 includes two input faces 512 and 514 having a length 2W and a height W, respectively, and includes an output face 516 having a height W. The input face 512 has a rectangular cross section in the X-Z plane, and the input face 514 and the output face 516 each have a square cross section in the Y-Z plane. The input faces 512 and 514 and the output face 516 are flat optical-quality surfaces. The manufacture of the combiner 500 is discussed below in conjunction with
The first section 506, which effectively replaces the section 306 of
The second section 508 and the third section 510 are similar or identical to the second and third sections 308 and 310 of
Referring to
The operation of the beam combiner 500 is similar to the operation of the beam combiner 300 of
Alternate embodiments of the beam combiner 500 are contemplated. In one such embodiment, the R, G, and B beams may enter the input faces 512 and 514 of the beam combiner 500 in an order other than the order (R-G-B) shown. For example, instead of the input face 514 receiving the R beam and the input face 522 receiving the B beam, the input face 514 can receive the B beam and the input face 522 can receive the R beam. Furthermore, the cross section of the input face 512 may be other than rectangular, and the cross sections of the faces 514 and 516 may be other than square. Moreover, one can omit the section 508 so that the combiner 500 generates the composite beam 502 from only two beams. In addition, one can add additional sections that are similar to the section 508 so that the combiner 500 generates the composite beam 502 from more than three beams.
As an alternative, the beam combiner may be assembled such that input faces 518 and 522 are not coplanar, but rather are parallel planes. For example, face 522 may be raised by a distance W toward the blue light source. This results in a beam combiner that provides inherent optical path length equalization.
First, one conventionally coats the surfaces of transparent slabs 600, 602, and 604 with the desired wavelength-sensitive reflective optical coatings as discussed above in conjunction with
Next, one bonds the optically coated slabs 600, 602, and 604 together using a conventional optical adhesive.
Then, one cuts the bonded slabs along the appropriate dashed cut lines to form the combiner. To form the combiner 300 of
Next, one conventionally polishes the beam-receiving and beam-projecting surfaces of the cut slabs to an optical-quality finish. For example, to form the combiner 300 (
Although one can cut and polish the slabs before bonding them together, this may increase the manufacturing complexity and cost because one must properly align the cut and polished pieces before bonding.
First, one conventionally coats the surfaces of three or more transparent slabs. The example of
Next, one bonds the optically coated slabs 700, 702, 704, 706, and 708 together using a conventional optical adhesive. The ends of the slabs are staggered as shown to maximize the number of combiners that can be formed.
Then, one cuts the bonded slabs along the horizontal lines 722a-722h to form individual plates 724a-724g. At this point, one can, but does not need to, polish the tops and bottoms of the plates (the optically coated sides have already been polished) to an optical-quality finish, as discussed above.
Next, one cuts the plates 724a-724g in half along the vertical lines 726a-726g.
Then, to form either combiners 300 (
To form the combiners 500 (
Referring to
In operation, the beam source 802 temporally modulates the intensities of the R, G, and B beams to change the color and other characteristics of the image beam 820 on a pixel-by-pixel basis.
Alternate embodiments of the image-beam generator 800 are contemplated. For example, by modifying the locations of the R, G, and B beam generators 804, 806, and 808, the generator 800 can incorporate the beam combiner 300 (
In operation, the image-beam generator 800 directs the image beam 820 onto the mirror 902 via the optical train 818. The mirror 902 is operable to sweep the beam 820 through a pupil 906 and across the retina 904 by rotating back and forth about an axis 908.
Claims
1-59. (canceled)
60. A method, comprising:
- attaching an hypotenuse of a triangular first slab of transparent material to a first side of a rectangular second slab of transparent material to form an interface operable to reflect a first wavelength of electromagnetic energy and to pass second and third wavelengths of electromagnetic energy, the second slab having a second side opposite the first side; and
- attaching a first side of a third slab of transparent material to the second side of the second rectangular slab to form an interface operable to reflect the second wavelength and to pass the first wavelength.
61. The method of claim 60, further comprising:
- wherein the third slab is rectangular; and
- planing beam-input ends of the second and third slabs such that the beam-input ends are substantially coplanar with a beam-input end of the first slab.
62. The method of claim 60 wherein the first, second, and third slabs comprise glass.
63. The method of claim 60 wherein:
- the third slab is substantially triangular; and
- the first side of the third slab comprises the hypotenuse of the third slab.
64. The method of claim 60, further comprising coating the hypotenuse of the first slab with a material operable to reflect the first wavelength of electromagnetic energy and to pass the second and third wavelengths of electromagnetic energy.
65. The method of claim 60, further comprising coating the first side of the second slab with a material operable to reflect the first wavelength of electromagnetic energy and to pass the second and third wavelengths of electromagnetic energy.
66. The method of claim 60, further comprising coating the first side of the third slab with a material operable to reflect the second wavelength of electromagnetic energy and to pass the third wavelength of electromagnetic energy.
67. The method of claim 60, further comprising coating the second side of the second slab with a material operable to reflect the second wavelength of electromagnetic energy and to pass the third wavelength of electromagnetic energy.
68. A method, comprising
- attaching a first side of a rectangular first slab of transparent material to a first side of a rectangular second slab of transparent material to form an interface operable to reflect a first wavelength of electromagnetic energy and to pass second and third wavelengths of electromagnetic energy;
- attaching a second side of the rectangular first slab to a first side of a rectangular third slab of transparent material to form an interface operable to reflect the first wavelength and to pass the second and third wavelengths;
- attaching a second side of the rectangular second slab to a first side of a rectangular fourth slab of transparent material to form an interface operable to reflect the second wavelength and to pass the third wavelength;
- attaching a second side of the rectangular third slab to a first side of a rectangular fifth slab of transparent material to form an interface operable to reflect the second wavelength and to pass the third wavelength;
- cutting through the attached first, second, third, fourth, and fifth slabs to form a combination slab;
- cutting the combination slab in sections such that a first section includes portions of the first, second, and fourth slabs and that a second section includes portions of the first, third, and fifth slabs;
- polishing the cut edges and the largest surfaces of the first and second sections of the combination slab; and
- forming beam combiners by cutting the first and second sections of the combination slab in directions substantially perpendicular to the respective cut edges of the sections.
69. The method of claim 68, further comprising planing edges of the first and second sections of the combination slab opposite the respective cut edges after cutting the combination slab in sections.
70. The method of claim 68, further comprising planing opposite edges of the combination slab before cutting the combination slab in sections.
71. The method of claim 68 wherein the first, second, third, fourth, and fifth slabs have substantially equal thicknesses.
72. The method of claim 68 wherein the first slab is thicker than the second, third, fourth, and fifth slabs.
73. The method of claim 68 wherein:
- the first slab is thicker than the second, third, fourth, and fifth slabs; and
- the second, third, fourth, and fifth slabs have substantially equal thicknesses.
74. The method of claim 68, further comprising treating second sides of the fourth and fifth slabs to reflect the third wavelength.
75. The method of claim 68, further comprising:
- prior to cutting the first, second, third, fourth, and fifth slabs to form the combination slab, attaching a second side of the rectangular fourth slab to a first side of a rectangular sixth slab of transparent material to form an interface operable to reflect the first wavelength of electromagnetic energy and to pass the second and third wavelengths of electromagnetic energy, and attaching a second side of the rectangular sixth slab to a first side of a rectangular seventh slab of transparent material to form an interface operable to reflect the second wavelength and to pass the third wavelength;
- wherein cutting through the attached first, second, third, fourth, and fifth slabs further comprises cutting through the sixth and seventh slabs to form a combination slab;
- wherein cutting the combination slab in sections further comprises cutting the combination slab in sections such that a third section includes portions of the fourth, sixth, and seventh slabs;
- wherein polishing the cut edges further comprises polishing the cut edges and the largest surface of the third section of the combination slab; and
- wherein forming beam the combiners further comprises forming the combiners by cutting the third section of the combination slab in directions substantially perpendicular to the respective cut edges of the third section.
76. A method, comprising
- attaching a first side of a rectangular first slab of transparent material to a first side of a rectangular second slab of transparent material to form an interface operable to reflect a first wavelength of electromagnetic energy and to pass second and third wavelengths of electromagnetic energy;
- attaching a second side of the rectangular second slab to a first side of a rectangular third slab of transparent material to form an interface operable to reflect the second wavelength and to pass the third wavelength;
- cutting through the attached first, second, and third slabs to form a combination slab;
- cutting an edge of the combination slap formed by a second side of the first slab;
- polishing the cut edge and the largest surface of the combination slab; and
- forming beam combiners by cutting the combination slab in directions substantially perpendicular to the cut edge.
Type: Application
Filed: Dec 14, 2006
Publication Date: Apr 26, 2007
Applicant:
Inventors: Mathew Watson (Bellevue, WA), Mark Freeman (Snohomish, WA)
Application Number: 11/639,610
International Classification: G02B 27/14 (20060101);