RAPIDLY SWITCHABLE LINE SELECTOR FOR PULSED LASERS

Abstract: This invention allows forcing successive pulses of a pulsed laser to be on different spectral lines. This invention can support a higher pulse repetition frequency than the prior art and the alignment of the laser does not change during a pulse. There are five implementations or embodiments of this invention. The first embodiment includes a set of diffraction gratings (25-30) on the face (24) of a wheel (23) each grating being set at an angle to select a different spectral line. The wheel is rotated, and as each grating moves into the end-reflector position of the laser's optical path, the laser is fired. The second embodiment includes a single fixed diffraction grating (58) and a set of plane mirrors (49-54) on the face (47) of the wheel (45), each mirror being set at an angle to reflect onto the diffraction grating and select a different spectral line. The wheel is rotated and as each mirror moves into the end-reflector position of the laser's optical path, the laser is fired. Alternate embodiments include a small spinning fold mirror (65) that reflects the beam in a circle about the axis (15) of the laser in an embodiment that includes (a) a circular array of diffraction gratings (73, 75) arranged about the laser axis such that the tilt of the gratings and the orientation of the grooves vary as one goes around the circle and successively fires the laser at each grating; (b) both a circular array of mirrors (77-79) and a corresponding array of diffraction gratings (80, 81) such that the grooves of all of the gratings are parallel and the gratings are all tilted in the same direction; and (c) two spinning fold mirrors (59, 59') and two circular arrays of mirrors (77, 79, 87, 89) giving a double fold plus a single diffraction grating (99) wherein the optical paths are not parallel but arrive at the grating at different angles for selecting different spectral lines.

Description: RAPIDLY S ITCHABLE LINE SELECTOR FOR PULSED LASERS BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates general ly to a rapidly switchable I i ne selector for pulsed lasers, and more particularly to a system that al lows forcing successive pulses of a pulsed laser to be on di fferent and distinct spectra I I i nes . 2. Descr iption of the Prior Art The only prior art known to the inventor that has actual ly been demonstrated to work are systems using a rapid mechanical motion to change a diffraction grating's al ignmeπt. In one prior art system, the rapid mechanical motion of the diffraction grating is done by a dr ive that changes the angle of the diffraction grating, as with a pointing mirror. . In the other known pr ior art system, a set of diffraction gratings is mounted on the faces of a spinning hexagonal prism. As each of the diffraction gratings comes into the correct al ignment angle, the laser Is fired on a different spectral l ine. The spinning pr ism arrangement of the pr ior art has two major disadvantages, which wi l l be discussed in terms of an infrared CO laser. The primary disadvantage is a I imitation of the maximum pulse repetition rate. The di ffraction grating is changing al ignment during the pulse, and if it turns too rapidly, the laser wi l l go out of al ignment dur ing the pulse, cl ipping the pulse, and reducing the optical energy contained in it. The al ignment time is not just the time during which there is signi f icant power in the p lse, but must also include the time for the pulse to bui ld up out of the noise. The times invol ed are about 0.1 to 0.3 usec for pulse bui ld-up from the noise, 0.1 to 0.2 usec for the main pulse, and another usec i-f the energy in the tai l is also to be used, the total time being appro imately 0.2 to 2 usec. The al ignment tolerance of the laser is about 50 urad, so if the diffraction grating rotates faster than 50 urad/usec, the pulse wi l l be cl ipped. Significant energy can be extracted with al ignment times as smal l as 0.1 usec, w ich a1.1 ows rotation rates up to 500 urad/usec, but with somewhat reduced energy. These numbers convert to 50 pulses per second with ful l energy at a prism rotation of 8.3 Hz (500 RPM) and 500 pulses per second with reduced energy at a prism rotation of 83 Hz (5000 RPM) for a hexagonal rotating prism. The achievable pulse repetition rate scales with the number of faces on the prism, but so does the physical size of the prism, because the size of a face is determined by the laser beam size, which is approximately 1 centimeter. A second major disadvantage of this prior art system is the requirement for precise timing of the firing of the laser relative to the angular position of the spinning prism. The af ignment tolerance is, as stated above, 50 urad, and this is achieved with a precision optical encoder wheel on the same shaft as the prism. Tire prior art spinning prism system is not without it's advantages. It has the abil ity for random access to any spectral l ine by choosing the firing time relative to the angular position of the prism. But this advantage is offset by the previously described disadvantages. The present invention solves substantial ly al l of the problems of the prior art systems and avoids the disadvantages of the prior art whi le providing- many advantages thereover . BRIEF SUMMARY OF THE INVENTION The present invention describes a rapidly switchable I i ne selector for pulsed lasers. The invention al lows forcing successive pulses of a pulsed laser to be on different spectral I ines. This invention can support a higher pulse repetition frequency than was possible in the prior art, and the al ignment of the I aser -does not change during a pulse. There are several implementations of the present invention. In a first embodiment, a set of diffraction gratings is set on a face of a wheel . Each di ffraction grating is set at an angle to select a different spectral I i ne . The wheel is rotated, and as each grating moves into the end- reflector position of the laser's optical path, the laser is f i red . In a second embodiment of the present invention, a single fixed diffraction grating is used and a set of plane mirrors are mounted on the face surface of a rotating wheel . Again, each of the plane mirrors on the face of the wheel is set at a different angle to reflect onto the diffraction grating and select a different spectral I ine. The wheel is rotated, and as each mirror moves into the end-reflector position of the laser's optical path, the I aser is f I red . A third embodiment of the present invention has the primary advantage that it does not require the spinning of a large wheel equipped with gratings or mirrors, but needs only to spin a smal l fold mirror. In this embodiment, a set of diffraction gratings are placed in a circle around a smal l rotating fold mirror within the laser's resonator cavity. The rotating mirror subsequently reflects each of the gratings into the optical position of the end-reflector of the resonator cavity. As each grating comes into position, the laser is fired. I f the polarizations of al l the spectral I ines are to be the same, then the or ien ation of the grooves of the diffraction grating and the directions of ti lt of the gratings vary as one goes around the circle of diffraction gratings, which could lead to some difficulty in af ignment. Sti l l another embodiment of the present invention, similar to the last, el iminates the difficulty leading to possible al ignment problems by introducing one more fold in the optical path. Now the grooves of al I of the gratings are paVal lel and the gratings are al l i lted in the same d i rect ion . Lastly, in yet another embodiment, the optical paths are brought together again so that only one diffraction grating is required in the end-reflector position. This embodiment has to have each path select a different spectral . I ine, and this is done by setting the angles of the additional fold mirrors so the paths are not al I paral lel as they arrive at the grating but are incident on the grating at —dif erent angles, thereby selecting different spectral l ines. This embodiment uti l izes a combination double fold mirror with two rings of plane mirrors, one about each of the fold mirror faces. The common concept present in al l of the embodiments is to switch the laser along different path o s, each adjusted to select a different and distinct spectral l ine. ^ Each of the above- ident i f ied embodiments does just that. These and other objects and advantages of the present invention wi l l be more ful ly understood after reading the detai led description of the preferred embodiments, the claims, and the drawings, which are briefly described here inbe I ow. BRIEF DESC IPTION OF THE DRAWI GS In the accompanying drawings: FIG. 1 is a schematic representation of a prior art system for selecting different spectral l ines for a pulsed I aser ; FIG. 2 is a perspective I l lustration depicting one embodiment of the rapidly switchable I ine selector for pulsed lasers of the present invention; FIGS. 3A , 3B, and 3C i l lustrate different angles at which the diffraction grating disks may be mounted on the face surface of the wheel of FIG. 2; FIG. 4 is a perspective i l lustration of a second embodiment of the rapidly switchable l ine selector for pulsed lasers of the present invention; FIG. 5A is a front view of the mirror wheel of FIG. 4; FIGS. 5B, 5C , and 5D i l lustrate var ious mounting angles of the mirrored disks on the front surface of the mirror wheel of FIG. 5A; FIG. 6 is a schematic I l lustration of a pulsed laser system using a third embodiment to accompl ish spectral I ine sw i tch i ng ; FIG. 7 is a schematic i l lustration of a pulsed laser system representing sti l l another embodiment of the present j nveπt ion; and FIG. 8 is a schematic diagram of a pulsed laser system I l lustrating yet a further embodiment of the present i nvent ion. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The rapidly switchable I ine selector system for pulsed lasers of the present Invention al lows the forcing of successive pulses of a pulsed laser to be on different and distinct spectral l ines. The present system can support a much higher pulse repetition frequency than was previously possible in the pr ior art, and the al ignment of the laser does not change dur ing a pulse. In a f irst embodiment of the present invention, a set of diffraction gratings are provided on the face of a rotat ing wheel . Each diffraction grating is set at a unique angle to select a different spectral l ine. As the wheel is spun or rotated, each of the diffraction gratings moves to the end-reflector position of the laser's optical path and the laser is fired to produce output at a pre- selected different and distinct spectral l ine from that of the previous firing. In FIG, 1 , a system of the prior art Is shown. A laser is shown as passing an optical beam 15 through an output mirror 13. A rotating hexagonal prism or wheel 17 is provided with six different and distinct faces. Each of the faces includes a diffraction grating 21 , and the wheel 17 is rotated about it's central axis 19 In a clockwise direction. As the beam 15 diffracts from the diffraction grating, the wavelength that is diffracted back upon the incident direction changes as the prism rotates, and hence different spectral I ines are selected for the optical pulse out of the laser 11. As each diffraction grating of each of the surfaces 21 comes into the correct optical al ignment, the laser 11 is fired. The spinning prism method is the closest prior art known and it has two major disadvantages and one good feature. A first or p imary major disadvantage is the l imitation on the maximum pulse repetition rate. The diffraction grating is changing al ignment continuously during the pulse, and if it turns or rotates too rapidly, the laser wi l l go out of al ignment during the pulse, thereby cl ipping the pulse and reducing the optical energy contained in it. The al ignment time is not just the time during which there is significant power in the pulse, but it must also include the time for the pulse to bui ld up out of the noise. The times involved are general ly about 0.1 to 0.3 usec for pulse bui ld-up from the noise, 0.1 to 0.3 usec for the main pulse, and another 1 usec if the' energy in the tai l is also to be used. T is results in a total time of 0.2 to 2.0 usec. The al ignment tolerance of the laser is about 50 urad, so if the diffraction grating rotates faster than 50 urad/usec, the pulse wi l l be cl ipped. Significant energy can be extracted with al i gnment t imes as sma I I 0.1 usec , which al lows rotation rates of up to 500 urad/usec, but with somewhat reduced energy. These numbers convert into 50 pulses per second with ful l energy at a pr ism rotation of 8.3 Hz (500 RPM) and 500 pulses per second with reduced energy at a pr ism rotation of 83 Hz (5000 RPM) , for a hexagonal prism. The achievable pulse repetition rate scales with the number of faces on the prism, but so does the physical size of the pr ism, because the size of a face is determined by the laser beam size, which is appro imately 1 centimeter per face. Another major disadvantage of the pr ior art system is the requirement for precise timing of the fir ing of the laser relative to the angular position of the spinning prism. ' The al ignment tolerance is, as stated above, 50 urad, and this is achieved with a precision optical encoder wheel on the same shaft as the prism. The advantage of this system l ies in It's abi l ity for random access to any particular spectral l ine by choosing the fir ing time relative to the angular position of the prism. The present invention is I imited to a fixed set of spectral I ines, although the set can be changed simply by real igning the gratings in the f irst implementation or the mirrors in the second implemen ation, etc. FIG. 2 i l lustrates a pulsed I aser system uti l izing the rapidly switchable I ine selector of the irst embodiment of the present invention. In FIG. 2, the pulsed laser 11 has it's optical output beam 15 passing through an output mirror 13. In the end-reflector position is a di ffraction grating disk 25 mounted on the face 24 of a r-otating circular wheel 23. The wheel 23 has a body portion 33 including a general ly planar face 24 and an outer peripheral r im 36. The wheel is dr iven in a clockwise direction by shaft or a le 31 about an axis of rotation 32 so as to spin the various diffraction grating disks 25, 26, 27, 28, 29, and 30 sequential ly into the end-re lec or position as the wheel rotates. it wi l l be real ized that the set of diffraction grating disks disposed on the face of the wheel 23 of the present invention can include different numbers of diffraction grating disks "n" other than six, where "n" is a positive whole number. Each of the gratings is set at an angle to select a different spectral I ine. As the wheel 23 is spun or rotated, and as each of the gratings 25-30 moves into the end-reflector position of the laser's optical path, the laser is fired. If the laser axis is paral lel to the axis of rotation of the wheel , then each grating must be set in the wheel at it's Littrow angle, but If the angle between the laser axis and the axis of rotation is set equal to the average Littrow angle of the gratings, then the angles of the gratings in the wheel are reduced. This can be important if the power to drive the wheel is a factor because the angled gratings wi l l act as fan blades to blow air around. FIGS. 3A, 3B, and 3C each show a diffraction grating disk 25, 26, 27 having a body portion 34 with it's lower surface 44 secured to the face 24 of the wheel body 33 so that the diffraction grating surface 35 is disposed at a required angle to produce the necessary spectral I ine. In FIG. 3A, for example, the intersection of the plane of the diffraction grating face 35 and the face 24 of the wheel body 33 form an angle θι , whi le an angle Qi. is shown as being formed in FIG. 3B, and an angle © 5 is forme d in FIG. 3C. Each of the angles is adjusted by the positioning of the angle of the diffraction grating surface 35 so as to produce a predetermined spectral I ine -as the diffraction grating face 35 passes in the end-reflector position of the laser's optical path and the laser is f i red . FIG. 4 shows a pulsed laser system using the rapidly switchable I ine selector system as the second embodiment of the present invention. In FIG. 4, the laser 11 is shown as outputting an optical beam 15 through an output mirror 13. The end-reflector position is provided by a plural i ty of "n" general ly circular mirrored disks 49, 50, 51 , 52, 53, and 54 where "n" is a positive whole number. The isks 49- 54 are adhered to or carr ied by the general ly planar front surface 47 of a circular wheel 41. The wheel 41 includes a body portion 45 sustaining the front planar face 47 and having an axle or shaft 55 for driving the wheel -in a clockwise direction about an axis of rotation 43. In this embodiment, the single fi ed diffraction grating 58 . is used in conjunction with a set of plane mirrors 49-54 disposed on the front surface or face 47 of a wheel 41. Each of the circular d i sk- I I ke mirrors 49-54 is set at a different angle to reflect a beam 60 onto the diffraction grating 58 and select a different and distinct spectral I ine. As the wheel 41 is spun or rotated, each of the general ly circular mirrored disks 49-54 wi l l come into the end-re lector position of the laser's optical path and the I aser wi l l be fired. Each of the laser fir ings wi l l result in a different and distinct spectral l ine. FIG. 5A shows a front view or face iew of an alternate embodiment to the diffraction grating wheel 23 of FIG. 2. In FIG. 5A, a general ly circular mirror wheel 41 is shown as having a general ly planar front surface 47, a body portion 45 and an outer peripheral r im 46. A plural ity of mirrors 49, 50, 51 , 52, 53, and 54 are shown as being secured or attached to or on or carried by the surface 47 of the wheel 41. The wheel rotates about it's central axle or axis 43. FIGS. 5B, 5C , and 5D show three of the mirrors 49, 50, and 51 as being mounted in different angular posi tions about the surface 47 of the wheel 41 of the present Invention. Each of the circular disk mirrors 49, 50, 51 is shown as having a body portion 56 and a mirror surface 57. The wheel body is represented by reference numeral 45 and it wi l l be seen that the back, bottom, or lower surface 62 of the mirrored body 56 is secured onto the planar face 47 of the body portion 45 of the wheel 41 so that the mirror face 57 provides different required angles for producing the different spectral l ines. It wi l l be seen that the angular placement of the first mirrored disk 49 produces an angle ι , whi le " the second mirrored disk 50 produces an angle θt , and the third mirrored disk 51 produces an angle ©•? . These angles wi l l result in the production of three different spectral I ines as the mirrored surfaces are rotated and each mirror surface passes into the end-reflector position of the laser's optical path and the laser is fired so as to select a different and distinct spectral I ine for each mirror. The difference between the first embodiment and the second I ies in replacing the wheel of diffraction gratings with a wheel of mirrors, each of which reflects the optical beam differently onto a single diffraction grating. Each of the mirrors is set at an angle to reflect onto the grating and select a different and distinct spectral I ine so that as the wheel is spun or rotated, and as each mirror moves into the reflector position of the lasers optical path, the laser is fired. As with the first embodiment, the angle between the laser axis and the rotation axis can be chosen to reduce the angles between the mirrors and the wheel face to reduce the fan action. Uti l izing six optical positions for the circular mirrored disks 49-54 of the present invention, a wheel rotation rate of 83 Hz (5000 RPM) wil l provide a pulse repetition rate of 500 Hz. If the optics on the wheel have one centimeter apertures, the wheel is only- three centimeters in diameter. By going to a 15 centimeter diameter wheel with 30 optical positions rotating at 166 Hz ( 10,000 RPM ) the pulse repetition rate can be made 5000 Hz with ful l laser energy in each pulse. The common concept among al l of the embodiments of the present invention is to provide a method and system or apparatus to switch the laser among different optical paths. Each of the paths must be adjusted to select a unique different and distinct spectral I ine. With this in mind, yet another embodiment of the present invention can be descr ibed. In the remaining embodiments, the var iat ions on the rapidly switchable I ine selection method of the present invention have the advantage that the they do not have to spin a large wheel with diffraction gratings or mirrors carried on it's face, but need only spin a relatively smal l , l ightweight, fold mirror. In the first embodiment of this concept, a set of diffraction gratings are placed in a circle around a sma I I rotating fold mirror disposed within the resonator cavity. The rotating mirror sequential ly reflects each of the gr-at i ngε onto the optical position of the end-reflector of the resonator cavity. As each grating comes into position, the laser is fired. Whi le only two gratings are shown in FIG. 6, it wi l l be real ized that they are in the plane, of the paper, but more are distributed around a circle perpendicular to the pLane of the paper. I f the polar ization of al l of the spectral l ines are to be the same, then the orientation of the grooves and the directions of ti lt of the diffraction gratings vary as one goes around the circle of gratings. This could lead to some al ignment difficulties. In FIG. 6, a pulsed laser 11 is shown as generating or outputting an optical beam or laser beam 15 through an output mirror 13. A rotating fold mirror assembly 59 is shown as having a body portion 71 , an axle or shaft 67 for rotating the mirror face 61 , and an axis of rotation- 69, A point of incidence 65 shows the optical beam 15 reflected off of the mirrored surface 61 and the reflected beam 63 being then reflected onto the surface of the diffraction grating 73 of one of the "n" diffraction gratings 73 of the circle or set, where "π" is a positive whole number. For example, if a six diffraction grating circle were used, the lower or bottom diffraction grating 75 would be the fourth, whi le the second and third and fifth and sixth would be out of the plane of paper of FIG. 6. In order to solve the possible al ignment problem that could result in the embodiment of FIG. 6, the embodiment of FIG. 7 is proposed. In this embodiment, any potential al ignment difficulty is el imiπated by introducing one more fold into the optical path. Now the grooves of al I of the gratings are paral lel and the diffraction gratings themselves are al l ti lted in the same direction. in FIG. 7, the laser 11 is.shown as outputting the laser beam 15 through an output mirror 13. The system i.πcludes a rotating fold mirror assembly 59 having a body portion 71 and an axle or rotating shaft 67 for rotating the diagonal face 61 of the mirror about the a is of rotation 69. The optical beam 15 is shown as striking the mirrored surface 61 of the fold mirror assembly 59 at the point of impingement or incidence 65 and then as reflected beam 63 to the face of a plane mirror 77. The mirror 77 is part of a circular array of mirrors disposed about a plane drawn through the point of impingement 65 and perpendicular to the axis of rotation 69. For example, the mirror 77 could be the first in a set of six mirrors whi le the bottom or opposite mirror 79 would be the fourth, and similarly, for different numbers of mirrors in the circular array. Mirror 77 is shown as having a point of impingement or point of incidence 83 on it's face, which reflects optical beam 85 onto the face of a diffraction grating 81. In fact, as the mirrored surface 61 of the fold mirror 59 rotates, the beam reflected off of the point of incidence 65 and represented by reference numeral 63' wil l be .reflected off the surface of the mirror 79 to also Impinge on the corresponding paired diffraction grating surface of the grating 80. In this manner, the extra fold al lows the grooves of al l of the diffraction gratings to be paral lel and the planes of al l of the di ffraction gratings are ti lted in the same general direction so as to pass the reflected optical beam off of the mirrored surface and onto the corresponding paired diffraction grating of the circular array of gratings of FIG. 7. It wi l l be seen that there is one diffraction grating for each plane mirror such as diffraction grating 81 in the circular array corresponding circular to mirror 77 of the circular array. Simi larly, the mirror 79 corresponds to the di ffraction grating 80 of the corresponding array of di ffraction grat i ngs . The idea * can be carried sti l l further as shown in the embodiment of FIG. 8. In FIG. 8, the paths ar e brought together again or folded back so that only one single diffraction grating 99 is required for the entire system. Whi le we sti l l have to have a different path selected to produce a different spectral l ine, this is done by setting the angles of the additional fold mirrors so the paths are not a I- 1 paral lel as they arr ive at the diffraction grating, but are incident on the grating at different angles, thereby selecting different spectral I ines, FIG. 8 shows a laser 11 having a laser output beam 15 passing through an output mirror 13. A double fold mirror assembly 101 includes a first fold mirror assem ly 59 and a second fold mirror assembly 59' . The first mirror assembly 59 has a fold mirror body 71 , a diagonal mirrored surface 61 , and a rotating shaft 67 shared in common with the second fold mirror assembly 59' . The second fold mirror assembly 59' includes a body portion 71 ' and a slanted or diagonal mirrored surface 61 ' . The point of incidence or impingement 65 is shown on the front surface 61 of th ' e fold mirror body 71 so the beam 15 is reflected as reflected beam 63 to impinge on impingement point 83 of the mirror 77 of a simi lar mul ti-mirror array as previously descr ibed with reference to FIG. 7. This beam then reflects off of the surface of the mirror 77 as reflected beam 85, which is again ref I ected -off the point of impingement 91 of a mirror 87 of a second circular mirror array as reflected beam 93. Beam 93 then strikes the point of impingement or incidence 95 of the surface 61' of the folded mirror 71 ' , and the reflected beam 97 strikes the single diffraction grating 99. Similarly, it wil l be understood that the system of FIG. 8 uses two circular arrays " of plane mirrors ith one being in a circle whose plane is general ly perpendicular to the a is of rotation of the shaft 67 and paral lei to the second circular array of mirrors, 87, 89 whose plane is also perpendicular to the axis of rotation of the shaft 67 and general ly paral lel with the plane of the first circular array of mirrors 77, 79. In this manner, as each of the mirrors of the first array including mirrors 77 and 79 pass into the optical path and reflect the beam to - a corresponding mirror of the second circular array, the second circular array folds back or reflects back the beam off of the surface of a second rotating mirror so that al I of the optical beams terminate on the single diffraction grating 99. Again, since different optical paths are selected by the ti lt angles of the mirrors of both the circular arrays, different and distinct spectral l ines are selected each time the laser is pulsed. Each time the pair of mirrors passes into the optical path of the laser, and occupies the end-reflector position, the laser is pulsed. In this specification, the graphic symbol used in the drawings and assigned reference numbers 11 or 13 is referred to as a "laser". it wi l l be understood that the laser actual ly includes the gain media, resonant cavity, output mirror, corrective optics, and end reflector. However the term wi l l be used herein to mean al I parts of the complete laser not otherwise shown. I t wi I I be read i I y seen by those having ordinary ski l l in the art that various modifications, variations, substitutions, changes, and alterations can be made in the apparatus, the method, and the system of the present invention without changing the spirit and scope thereof, which Is l imited only by the appended claims.

Claims: CLA I S L What is Claimed is: 1. A method for rapidly switching a pulsed laser between different and distinct spectral l ines, said laser having an optical path, an end-reflector position in the optical path, and a resonant cavity, comprising the steps of: providing a rotatable wheel ; placing said wheel in the optical path of the I aser ; arranging a plural ity of diffraction gratings about the face of the wheel ; orienting the angle of each of said diffraction gratings with respect to the plane of the wheel for selecting different and distinct spectral l ines; rotating said wh-βel ; sequential ly passing each one of said plural ity of diffraction gratings into the end-reflector position of the laser's optical path; and firing the laser each time one of said different and distinct diffraction gratings is in said end-reflector position for sequential ly producing said different and distinct spectral l ines. 2. A system for forcing successive pulses of a pulsed laser to be on different spectral l ines comprising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a wheel operabfy disposed at least partial ly within said optical path; a plural ity of diffraction gratings operably carried by a face of said wheel ; means for setting each of said plural ity of diffraction gratings at a predetermined angle adapted for selecting a different spectral I ine; means for rotating said wheel ; and means responsive to each of said plural i y of diffract ion gratings moving into the end-reflector posi tion in said optical path for firing said pulsed laser. 3. A system for rapidly switching a pulsed laser between different and distinct spectral l ines compr ising: a laser having a resonant cavity, an ' optical path, and an end-reflector position in said optical path; a rotatable wheel having an axis of rotation and a substantial ly planar face; a plural i ty of diffraction grating means on a circle ceπte'red on the axis of said wheel , operably disposed about the face of said wheel , said wheel being disposed with respect to the optical path of said laser so that the axis of the optical path is displaced a predetermined distance lateral ly from said axis such that the optical beam engages the diffraction gratings disposed on the face of the wheel as the wheel is rotated, sa-id diffraction gratings being or iented to select different and distinct spectral I ines; means for rotating said wheel to sequent ial ly place each of said plural ity of diffraction gratings into the end-reflector position of the laser's optical path; and means for fir ing said laser when each of said diffraction gratings are sequential ly p I aced ■ i n said end- ref I ector pos i t i on . 4. The system of Claim 3 wherein the face of each of said di ffraction gratings is set at an angle with respect to the plane of the face of the wheel to produce said different and distinct spectral I ines. 5. A rapidly switchable spectral I ine selector apparatus for a pulsed laser system including a laser having a resonant cavity and an optical path, said l ine selector apparatus comprising: means for providing a plural i ty of "n" different and distinct optical paths, each of said "n" optical paths defining a different and distinct one of a set of "n" optical spectral I ines for. said laser, where "n" is a positive whole number and n-≥ 2; means for sequential ly directing the laser's optical beam along different and distinct ones of said set • of "n" optical paths; and means for firing said pulsed laser each time one of said optical beams is directed along one of said set of "π" selected optical paths for generating one of said different and distinct spectral l ines associated therewith. 6, The I ine selecting apparatus of Claim 5 wherein said means for providing a plural ity of "n" different and distinct optical paths includes: a wheel having a planar face and an axis of rotation; a plural i y of "n" mirrors arranged about the face of said wheel ; a single di-ffract ion grating at the end-reflector position of the laser's optical path; means for rotating said wheel about said axis of rotation such that each of said "n" mirrors sequential ly rotates into a fold position in the laser's optical path to direct the beam onto the single diffraction grating, each at a different and predetermined angle of incidence; and said laser firing means being responsive to each of said "n" mirrors sequential ly occupying said fold position of the laser's optical path for firing said laser and generating a predetermined different and distinct spectral l ine corresponding to each particular one of the optical paths produced by said "n" mirrors. 7. The I ine selector apparatus of Claim 6 wherein said means for sequential ly directing the optical beam along different and distinct ones of said "n" optical paths include means for or ienting ' said wheel general ly perpendicular to the optical path of the laser with the optical path of the laser spaced a predetermined distance to one side of the axis of rotation thereof such that each of the "n" mirrors wi l l sequential ly pass into the fold position of the laser's optical path for Initiating the firing of said laser at each predetermined different and distinct spectral I ine. 8. The I ine selecting apparatus of Claim 6 wherein each of said "n" mirrors is set at a different and distinct angle with respect to the plane of the face of said wheel for sequential ly selecting said different and distinct opt i ca I paths . 9. A method for rapidly switching a pulsed laser between different and distinct spectral I ines, said laser having an optical path, an end-reflector position in said optical path, and a resonant cavity, comprising the steps of: providing a rotatable wheel ; placing said wheel In a fold position of the optical path of said laser; arranging a plural ity of plane mirrors about the face of the whee I ; positioning a diffraction grating in the end- reflector position of the laser's optical path; orienting the angle that each of said plane mirrors makes wi th the plane of the face of the wheel for providing different and distinct optical paths and ' angles of incidence of the paths in the diffraction grating to the end-reflector position; rotating the wheel ; sequential ly passing each one of said plural ity of mirrors into the fold position of the laser's optical path; and firing the laser each time one of said mirrors moves into said fold position for generating said different and distinct spectral l ines. 10. A system for rapidly switching a pulsed laser between different and distinct spectral l ines comprising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a rotatable wheel having an axis of rotation and a substantial ly planar face; a plural ϊty of mirror means operatfvely disposed about the face of the wheel , and on a circle centered on the axis of said wheel, each of said mirror means being oriented at a different and distinct angle, said wheel being disposed with respect to the optical path of said laser so that the axis of the optical path is spaced a predetermined distance lateral ly from said axis such that the optical beam engages each of said mirror means as the wheel is rotated; means for rotating said wheel to sequential ly place each of the plural i ty of mirror means into the fol position of the laser's optical path; diffraction grating means operably disposed for receiving the optical beam reflected from said plural ity of the mirror means for selecting a different spectral l ine corresponding to the angle of each of said mirror means; and means for firing said pulsed laser at a different spectral l ine when each of the mirror means are sequential ly placed in said fold position. 11. The system of Claim 10 wherein each of said circular disks has it's mirrored surface placed at an angle with respect to the planar face of the wheel for producing said different and distinct spectral l ines. 12. A system for forcing successive pulses of a pulsed laser to be on different spectral l ines compr ising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a wheel operably disposed at least partial ly within said optical path; a diffraction grating; a plural i ty of mirrors operably disposed on a face of said wheel ; means for setting each of said mirrors at a predetermined angle for reflecting the impinging pulses onto said diffraction grating for selecting a di fferent spectral I ine for each mirror; means for rotating said wheel ; and means responsive to each successive one of said plural ity of mirrors moving into the end-reflector position of said optical path as said wheel is rotated for firing said pulsed laser to generate each of said different spectra I I i nes . 13. The l ine selector apparatus of Claim 5 wherein said means for providing a plural i ty of "n" different and distinct optical paths includes: a fold mirror means having a diagonal mirror face and an axis of rotation operably disposed at least partial ly within the resonant cavity of said laser; a set of "π" diffraction gratings arranged in a circular array around said rotatable folding mirror ; and means for rotating said fold mirror, the mirror face of said rotating fold mirror being continuously operably disposed in the optical path of said laser for continuously reflecting the optical beam to said circular array of diffraction gratings for subsequently intercepting said diffraction gratings with the optical beam as they sequential ly come into the end-reflector position of the laser's optical path for initiating the firing of said laser for producing- said different and distinct spectral I ines. 14. A method for rapidly switching a pulsed laser between different and distinct spectral l ines, said laser having an optical path, an end-reflector position in said optical path, and a resonant cavity, comprising the steps of: rotating a fold mirror in the optical path of sa id I aser ; arranging a circular array of diffraction gratings about said fold mirror; continuously reflecting the optical path off of said fold mirror and to said circular array of diffraction grat ings; sequential ly intercepting each of said plural ity of diffraction gratings as each comes into the eπd- reflector position of the laser's optical path and firing the laser on each occurrence of a diffraction grating coming into the end-reflector position of said optical path for producing said different and distinct spectral l ines. 15. A system for rapidly switching a pulsed laser between- d i fferent and distinct spectral l ines comprising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a rotatable fold mirror having an axis of rotation and a diagonal mirror face; a circular array comprising a plural ity of diffraction gratings disposed in a circular path about the diagonal mirror face of said fold mirror; the diagonal face of said fold mirror being continuously in the optical path of said laser for directing an optical beam reflected therefrom to said circular path defined by said circular array of diffraction gratings for sequential ly intercepting each of said plural i ty of di ffraction gratings as it moves Into the end- reflector position of the laser's optical path; and means for firing the laser each time one of said plural i ty of diffraction gratings comes .into said end- reflector position for producing said plural i ty of different and distinct spectral l ines. 16. The I ine selector apparatus of Claim 5 wherein said means for providing a plural i ty of "n" different and distinct optical paths compr ises: a fold mirror having a diagonal mirror face and an axis of rotation operably disposed within the resonant cavity of the laser; a set of "n" plane mirrors arranged in a circular array around said rotatable fold mirror; and a corresponding set of "n" diffraction gratings arranged in a circular array adjacent said circular array of mirrors, one of said "n" diffraction gratings being -associated with each one of said "n" mirrors, said diffraction gratings occupying the end-reflector positions of said distinct optical paths; means for rotating said fold mirror, the mirror face of said rotating fold mirror being continual ly operably disposed in the optical path of said laser for continuously reflecting the optical beam to said circular array of mirrors for sequential ly intercepting the faces of each of said mirrors and reflecting the intercepted beam onto said diffraction gratings as they come into the end- reflector position of the laser's optical path for initiating the fir ing of the laser and the generation of said different and distinct spectral l ines. 17. A method for rapidly switching a pulsed laser between different and distinct spectral l ines, said laser having an optical path, an end-reflector position in said optical path, and a resonant cavity, comprising the steps of: rotating a fold mirror whose diagonal mirror face is directly in the optical path of the laser; arranging a set . of "n" plane mirrors in a circular array where "n" is a positive Integer; arranging a set of "n" diffraction gratings In a circular path paral lel to the circular path of said mirrors so that each of said "n" diffraction gratings is directly across from one of said "n" mirrors; directing the laser beam reflected from the diagonal mirror face of the rotating fold mirror to the circular path and sequentially onto the face of each of the "n" mirrors in said path for sequential ly reflecting the beam from said mirrors onto said corresponding circular array of diffraction gratings thereby sequent ia I I y -p I ac ing said gratings in the end-reflector position of the laser's optical path; and firing said laser each time one of said diffraction gratings passes into the end-reflector position of the laser's optical path for generating said different and distinct spectral I ines. 18. A system for rapidly switching a pulsed laser between different and distinct spectral l ines comprising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a fold mirror having an axis of rotation and diagonal mirror face, said mirror face being continuously disposed within the optical path of said laser; a circular array including a plural ity of mirrors arranged in a circle about said fold mirror; a corresponding plural ity of diffraction gratings arranged in a circular array about the axis of rotation of said fold mirror, each of the plural ity of mirrors in said first circular array corresponding to a distinct one of the diffraction gratings in said second circular array so that as the optical path is continuously moved In a circle about said first circular array and sequential ly reflected off of each of the mirrors in said array to impinge upon each of the corresponding diffraction gratings in said second circular array as each comes into the end-reflector position of the laser's optical path; and means for firing the laser each time a di fferent one of said plural I ty of diffraction gratings to said second circular array comes into said end-reflector position for generating said different and dist inct spectra I I i nes . 19. The I ine selector apparatus of Claim 5 wherein said means for providing a plural i ty of "n" different and distinct optical paths includes: a first and second fold mirror means each having a diagonal mirror surface and an axis of rotation, said first and second fold mirror means having their diagonal mirrors oriented in different directions and their axis of rotation being formed through a common rotational shaft for rotating the diagonal mirror surfaces of each s imu I aneous I y; a single fixed position diffraction grating means; a first circular array of "n" fold mirrors; a second circular array of "n" fold mirrors; each of the "n" mirrors of said first set corresponding to one of the "n" mirrors of said second set, and the mirror face of each of said fold mirrors of said first circular array being disposed toward the face of a corresponding one of the "n" mirrors of said second c i rcu I ar array ; means for setting the angles of the second circular array of fold mirrors so that the optical paths therefrom are not al l paral lel as they arr ive at the single diffraction grating, but are incident on the gratings at different angles for selec ing said different spectral i i nes; means for rotating the diagonal faces of said fold mirrors; means for sequential ly directing the optical beam reflected from the diagonal mirror surface of the first rotating fold mirror sequential iy onto ones of the faces of the "n" mirrors of the first circular array, the mirrors of said first circular array sequential ly directing the reflected beam to the surfaces of the corresponding ones of the mirrors of the second circular array, and each of the mirrors of the second circular array being arranged to reflect the incident beam onto the rotating diagonal mirror face of the second fold mirror, said second fold mirror directing the optical beam onto the face of the single diffraction grating thereby selectively and sequential ly changing the angle of incidence on the diffraction grating and thereby producing said different and distinct spectral l ines corresponding thereto. 20. A method for rapidly switching a pulsed laser between different and distinct spectral l ines, said laser having an optical path, an end-reflector position in said optical path, and a resonant cavity, comprising the steps of: connecting a shaft between a pair of first and second fold mirrors whose diagonal mirror faces are directed in different directions from one another; arranging a first set of "n" plane mirrors in a first circular array about the face of the first one of said fold mirrors; arranging a second corresponding set of "η." plane mirrors in a second circular array about the face of the second one of said fold mirrors; orienting the reflective faces of each of said first and second circular arrays of "n" mirrors opposite one another so that they face general ly toward one another such that each of said second set of "n" mirrors receives a beam reflected from a corresponding one of the first set of "n" mirrors; positioning a single diffraction grating in the end-reflector position of the laser's optical path; and rotating the common axis of said first and second fold mirrors for simultaneously rotating the diagonal faces of each in synchronism with one another; impinging the laser beam on the diagonal mirror face of the first rotating fold mirror; reflecting said beam therefrom and impinging i t on a face of one of the "n" mirrors in said . first circular array; reflecting said beam onto the face of a corresponding mirror in the second circular array; reflecting said beam onto the diagonal mirror face of the second rotating fold mirror; impinging the beam onto the single diffraction grating occupying the end-reflector position of the laser's opt leal path ; and selecting different and distinct spectral l ines as each of the mirror pairs of the first and second arrays pass into the laser's optical path with the rotation of said fold mirrors to bring the reflected beam to the single diffraction grating at different angles of incidence. 21. A system for rapidly switching a pulsed laser between different and distinct spectral l ines compr ising: a laser having a resonant cavity, an optical path, and an end-reflector position in said optical path; a first rotatable fold mirror having a shaft, an axis of rotation, and a first diagonal mirror surface; : a second rotatable fold mirror having a shaft, an axis of rotation, and a second diagonal mirror surface; means for connecting the rotatable shafts of said first and second fold mirrors commonly together for synchronizing the rotation of said first diagonal mirror surface with the rotation of said second diagonal mirror surface to produce a double fold mirror configura ion; a first circular array of mirrors disposed about said first fold mirror; a corresponding second circular array of mirrors disposed about said second fold mirror, the number of mirrors in said first circular array being equal to the number of mirrors in said second circular array and each of the ' mirrors in said first circular array corresponding to exactly one of the mirrors in said second circular array for forming mirror pairs operably disposed in the end- reflector position of the laser's optical path; a single diffraction grating means; the faces of the mirrors in said first circular array being general ly disposed toward the faces of.the mirror in said second circular array such that when the optical beam from said laser is reflected off of the rotating diagonal face of the first fold mirror, the reflected beam impinges on the faces of one of the. mirror pairs before it is reflected to impinge upon the second rotating diagonal mirror surface of the second fold mirror to be final ly reflected onto the surface of said single diffraction grating means; means for simultaneously rotating both of said fold mirrors in synchronism with one another for reflecting the optical beam from said laser to said mirror pairs and folding the beam back to the diagonal face of the second fold mirror and to said single diffraction grating so that each of the corresponding pairs of mirrors are sequential ly placed into the laser's optical path such that the beam arrives at said single diffraction grating means at different and distinct angles for each optical path taken; and means for fir ing said laser each time a di fferent one of said pairs of corresponding mirrors sequential ly passes into said optical path position, thereby generating said different and distinct " spectral I ines.

Inventors: FINK DAVID, FINK, DAVID
Applicants: HUGHES AIRCRAFT CO, HUGHES AIRCRAFT COMPANY
Application year: 1988
Main classification: H01S3
IPC codes: G02B26, H01S3