MOUNTING AND ALIGNMENT STRUCTURES FOR OPTICAL COMPONENTS

Abstract: An alignment structure (100) maintains an optical fiber in a bore (113). The structure is fixed on a bench and is passively or actively aligned with a light source. Then the structure may be welded or soldered to the optical bench whereby the alignment may suffer due to heat transfer. To correct this, the alignment structure can be plastically deformed to correct the alignment after the components have been fixed. The alignment structure has a substantially constant cross section in a z-axis direction as well as flexible links in order to allow displacements orthogonal to the optical axis. This movements will be initiated by seizing the component with a micro-positioner at a handle (136) and displacing it over the elastic limit to achieve permanent deformation.

Description: Mounting and Alignment Structures for Optical Components RELATED APPLICATIONS This application claims the benefit of the filing date of U.S. Provisional Application No. 60/165,431 , filed November 15, 1999, which is incorporated herein by this reference in its entirety. This application also claims the benefit of the filing date of U.S. Provisional Application No. 60/186,925, filed March 3, 2000, which is incoφorated herein by this reference in its entirety. BACKGROUND OF THE INVENTION Component alignment is of critical importance in semiconductor and/or MEMS (micro electro-mechanical systems) based optical system manufacturing. The basic nature of light requires that light generating, transmitting, and modifying components must be positioned accurately with respect to one another, especially in the context of free-space-optical systems, in order to function properly and effectively in electro-optical or all optical systems. Scales characteristic of semiconductor and MEMS can necessitate sub-micron alignment accuracy. Consider the specific example of coupling a semiconductor diode laser, such as a pump laser, to a fiber core of a single mode fiber. Only the power that is coupled into the fiber core is usable to optically pump a subsequent gain fiber, such as a rare- earth doped fiber or regular fiber, in a Raman pumping scheme. The coupling efficiency is highly dependent on accurate alignment between the laser output facet and the core; inaccurate alignment can result in partial or complete loss of signal transmission through the optical system. Moreover, such optical systems require mechanically robust mounting and alignment configurations. During manufacturing, the systems are exposed to wide temperature ranges and purchaser specifications can explicitly require temperature cycle testing. After delivery, the systems can be further exposed to long-term temperature cycling and mechanical shock. Solder joining and laser welding are two common mounting techniques. Solder attachment of optical elements can be accomplished by performing ahgnment with a molten solder joint between the element to be aligned and the platform or substrate to which it is being attached. The solder is then solidified to "lock-in" the alignment. In some cases, an intentional offset is added to the alignment position prior to solder solidification to compensate for subsequent alignment shifts due to solidification shrinkage of the solder. In the case of laser welding, the fiber, for example, is held in a clip that is then aligned to the semiconductor laser and welded in place. The fiber may then also be further welded to the clip to yield alignment along other axes. Secondary welds are often employed to compensate for alignment shifts due to the weld itself, but as with solder systems, absolute compensation is not possible. Further, there are two general classes of alignment strategies: active and passive. Typically in passive alignment of the optical components, registration or alignment features are fabricated directly on the components or component carriers as well as on the platform to which the components are to be mounted. The components are then mounted and bonded directly to the platform using the alignment features. In active alignment, an optical signal is transmitted through the components and detected. The alignment is performed based on the transmission characteristics to enable the highest possible performance level for the system. SUMMARY OF THE INVENTION The basic problem with conventional mounting and alignment techniques is that they are incompatible with high-speed production processes that are capable of yielding a consistently high-quality product. Passive alignment can be performed quickly, but there are typically problems associated with producing high performance products. In contrast, active alignment production processes can be well optimized over time to yield the high performance devices. These processes, however, are typically very slow. For example, in laser welding, the optical fiber bracket must be first welded. The weld must be allowed to cool and then alignment subsequently checked. Subsequent welding may then be necessary, followed by further cooling and rechecking cycles. Moreover, these conventional techniques are difficult to deploy in the manufacture of more-complex optical systems that offer higher levels of functionality. For example, laser welding has been successfully used to align the end of an optical fiber to a single laser diode chip in a small, i.e., less than five-centimeter module. It would be desirable, however, to integrate more functionality, such as filtering, multiplexing, demultiplexing, and/or switching capabilities in modules of similar dimensions. The present invention concerns mounting and alignment structures for optical components, especially micro optic components having a size of typically less than a millimeter. The structures are preferably deployed in all-optical, electro-optical, electro-mechanical-optical devices/subsystems/systems. These structures are used to connect the optical components to an optical circuit board or optical bench. The optical components include active devices, such as lasers or other devices offering higher levels of functionality, such as integrated lasers/MEMS, e.g., tunable Fabry- Perot active devices. Still further, the optical components in other implementations are passive devices such as beam splitters, passive, such as thin film, filters, mirrors, birefringent material, polarizers, crystals, prisms, and/or diffractive elements, for example. More specifically, the invention is directed to a generalized mounting system that allows optical components to be connected to an optical bench and then subsequently aligned, i.e., either passively or actively, in manufacmring or subsequent calibration or recalibration, alignment or realignment processes. In general, according to one aspect, the invention features a mounting and alignment structure for optical components. The structures typically comprise a quasi- extrusion portion. This portion is "quasi-extrusion" in the sense that it has a substantially constant cross section in a z-axis direction as would be yielded in an extrusion manufacmring process. The invention, however, is not limited to only forming the structures via extrusion For example, in the preferred embodiment, the structures are manufactured using a photolithography and metahzation, such as metal electroplating, processes According to the invention, the quasi-extrusion portion comprises at least one base, having a laterally-extending base surface, and an optical component interface At least one armature connects the optical component interface with the base In the preferred embodiment, the base surface is securable to an optical bench In the preferred embodiment, the base surface is bonded to the optical bench via solder holding, such as solder bonding with an 80/20 gold/tin ratio, or other eutectic solder In alternative embodiments, however, laser welding, epoxy bonding, ultrasonic welding, or adhesive/cast bonding are used In one embodiment, the base surface further compπses alignment features that are adapted to mate with opposite-gender alignment features of an optical bench This passive alignment technique is used to facilitate initial positioning of the alignment structure on the optical bench In the preferred embodiment, optically detectable ahgnment features or marks are used to position the structures on the bench Depending on the implementation, one or two bases are provided In two base configurations, one is typically located on either side of a medial axis of the structure In the preferred embodiment, the interface comprises a port for enabling an optical signal to pass transversely through the quasi-extrusion portion This enables optical access to an optical component installed on the optical component interface In some implementations, an optical signal is reflected off of the optical component to pass back through the port In other implementations, the optical signal passes through the optical component, in the case of a lens, for example In other implementations, the interface is configured as an open clamp or U- shaped cut-out. This configuration is useful for mounting optical components such as optical fibers to a bench. Also preferably, the handle is provided to facilitate grasping and manipulation of the alignment strucmre. In one implementation, the handle is integral with the optical component interface. In other embodiments, handles are provided integral with the armature(s) and/or integral with the base(s). In the preferred embodiments, the armamre comprises at least one flexure. The flexure is typically a region of the armamre that has a reduced cross-sectional area. Preferably, at least two flexures are provided along the armamre. The flexures are preferably separated by a laterally-extending segment of the armature. Other flexures of the strucmre are preferably separated by vertically-extending segments. Providing laterally and vertically extending segments allows for the manipulation and consequently alignment of the optical component on the structure in a two-dimensional x-y plane with a minimal of linkage between alignments along the x-axis with alignment along the y-axis. The use of discrete flexures, however, is not a requirement. In other embodiments, the flexure is distributed in the fashion of a leaf spring across a region of the armamre and in fact, the armature itself can act or function as a distributed flexure. In general, according to another aspect, the invention also features a mounting and alignment strucmre for an optical component having a substantially-constant cross section in an x-y axis plane. The rigidity of the strucmre to strain in the x-y plane is greater than in the direction of a z-axis. The strucmre comprises at least one base having a laterally extending base surface and an optical component interface. The above and other features of the invention including various novel details of construction and combinations of parts, and other advantages, will now be more particularly described with reference to the accompanying drawings and pointed out in the claims. It will be understood that the particular method and device embodying the invention are shown by way of illustration and not as a limitation of the invention. The principles and features of this invention may be employed in various and numerous embodiments without departing from the scope of the invention. BRIEF DESCRIPTION OF THE DRAWINGS In the accompanying drawings, reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale; emphasis has instead been placed upon illustrating the principles of the invention. Of the drawings: Fig. 1 is a perspective view of a first embodiment of a mounting and alignment strucmre according to the present invention; Fig. 2 is a front plan view of the first embodiment mounting and alignment strucmre; Fig. 3 A is a perspective view showing a second embodiment of the mounting and alignment strucmre according to the present invention; Fig. 3B is a front plan view showing the dimensions of the second embodiment structure; Fig. 4 is a perspective view showing a third embodiment of the mounting and alignment strucmre according to the present invention; Fig. 5 A is front plan view showing fourth embodiment of the inventive mounting and alignment stmcmres; Fig. 5B is perspective view showing a related embodiment of the inventive mounting and alignment structures; Fig. 6 is front plan view showing fifth embodiment of the inventive mounting and alignment stmcmres; Fig. 7 is a front plan view of a sixth embodiment of the mounting and alignment stmcmres according to the present invention; Fig. 8 is a front plan view of a seventh embodiment of the inventive mounting and alignment strucmres; Figs. 9 and 10 show eighth and ninth embodiments of the inventive mounting and alignment stmcmres; Fig. 11 is a front plan view of a tenth embodiment of the inventive mounting and alignment stmcmres in which separate stmcmres are integrated onto a single base according to the invention; Fig. 12 is a plan view showing an eleventh embodiment of a mounting and alignment stmcmre according to the present invention; Fig. 13 is a plan view showing twelfth embodiment of the present invention; Fig. 14 is a plan view showing a thirteenth embodiment of an inventive mounting and alignment stmcmre for passive component alignment; Figs. 15A and 15B are front plan views showing the fourteen embodiment of the mounting and alignment stmcmre and it deployment for mounting a second optical component in proximity to another optical component, Fig. 15C is an exploded perspective view showing a MEMS filter for mounting on the fifteenth embodiment; Figs. 16A, 16B, 16C are cross-sectional views of the plating and lithography processes used to fabricate the mounting and alignment strucmres according to the invention; Figs. 17A-17F illustrate a process for manufacturing mounting and alignment stmcmres that have non-constant cross-sections along a z-axis for portions of stmcmres; Fig. 18A and 18B are a perspective diagram illustrating the process steps associated with installing optical components on the mounting and alignment stmcmres and mounting and alignment structures on the optical bench; Fig. 19 is a perspective drawing of a laser optical signal source that couples a beam into an optical fiber held by a mounting and alignment stmcmre, according to the present invention; Fig. 20 is a process diagram illustrating the optical system active alignment process according to the present invention; Fig. 21 is a perspective top view showing the jaws of an aligner engaging the handle of a mounting and alignment stmcmre to deform the structure during an alignment process; Fig. 22 is a plot of force and optical response on the vertical axis as a function of displacement or strain on the horizontal axis illustrating the inventive alignment process; Fig. 23 is the plot of force along the y-axis as a function of displacement illustrating constraints in the selection of the yield force; Fig. 24 is a perspective view showing a fifteenth, composite stmcmre embodiment of the invention; Fig. 25 is a schematic perspective view of a sixteenth, dual material embodiment of the invention; Fig. 26 is a schematic diagram illustrating a production line for optical systems, according to the present invention; and Figs. 27A, 27B, and 27C are partial plan views of the mounting and alignment stmcmres showing three different configurations for the alignment channels. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Mounting and alignment structure configuration Fig. 1 shows an exemplary mounting and alignment stmcmre, which has been constructed according to the principles of the present invention. Generally, the alignment structure 100 comprises a base 1 10, an optical component interface 112, and left and right armamres 114A, 1 14B, which either directly connect, or indirectly connect, the base 110 to the interface 1 12. The base 1 10 comprises a laterally-extending base surface 1 16. In the illustrated example, the base surface 116 extends in a plane of the x and z axes, generally. The base base-surface comprise alignment feamres. In some embodiment, these feamres are adapted to mate with preferably opposite-gendered alignment feamres of an optical bench. In the specific illustrated implementation, the alignment feamres are used by machine vision to match to alignment marks or feamres of a 5 bench. Specifically, the alignment feamres comprise a wide, U-shaped cut out region 120. Three female alignment channels 1 18 are further provided that extend along the entire depth of the stmcmre in the direction of the z-axis. The U-shaped cut-out region 120 has the added advantage of minimizing the contact area and thus stress in the interface between the stmcmre and the bench or other surface to which it is o attached. In the illustrated implementation, each of the armamres 1 14A, 1 14B comprises two segments 122 and 124. Specifically, and for example, armamre 1 14B comprises two segments, 122B and 124B. The vertically-extending segments 122A, 122B, i.e., extending at least 5 partially in the y-axis direction, have two flexures 126A, 126B along their length, in the illustrated embodiment. These flexures are regions of reduced cross-sectional area in the segments, which regions extend in the direction of the z-axis. The vertically- extending segments 122 facilitate the positioning of an optical component, installed on the interface 112, along the x-axis; the flexures 126A, 126B facilitate the pivoting 0 of the segments 122A, 122B in a plane of the x and y axes. A puφose of the flexures is to isolate regions of microstructural change, such as occurring in plastic deformation, in order to make the yield forces, for example, readily predictable. Also, the flexures localize deformation on the armatures and consequently decrease the amount of force/movement required in the optical component before plastic 5 deformation is initiated in the armamre. Horizontally-extending (i.e., extending in the direction of the x-axis) segment 124A, 124B each comprise, in the illustrated embodiment, two flexures 128A, 128B. These flexures are also regions of reduced cross-sectional area in the respective segments, the flexures extending in the direction of the z-axis. 5 The horizontally-extending segments 124A, 124B allow the positioning of an optical component, installed on the optical component interface 1 12, generally vertically along the y-axis. Armamre deformation is facilitated by respective flexures 128A, 128B. In one implementation, the optical component is bonded to the optical l o component interface 1 12, and specifically bonding surface 132. This bonding is accomplished either through polymeric adhesive bonding or preferably solder bonding. In other implementations, thermocompression bonding, laser welding, reactive bonding or other bonding method are used. In the illustrated embodiment, the component interface further includes 15 stmcmre-component alignment feamres 1 13. In the illustrated embodiment, the stmcmre-component alignment feamres comprise slots extending in the z-axis direction from the component bonding surface 132. As a result, corresponding male- projections of an optical component are engaged the slots 1 13 to locate and align the optical component over the optical port 134 both along the x-axis and y-axis. 2 o The optical component interface, in some implementations, comprises a port 134 for enabling an optical signal to pass transversely through the structure. This enables optical access to the optical component by either facilitating the propagation of an optical signal to and/or away from the component. To facilitate the grasping and placement of the structure 100, a handle 136 is 25 also preferably provided on the stmcmre. In the illustrated embodiment, the handle 136 comprises two V- or U-shaped cut out regions on either side, near the top of the top of the stmcmre. In the illustrated example, they are integral with the optical component interface 112. The handle 136 enables the manipulation of the stmcmre 100 when attached to the bench 10. Specifically, the right cut-out is engaged to displace the stmcmre to the left, for example. To displace the stmcmre vertically or in the y-axis direction, both cut-out are engaged enabling the structure to be pressed down toward the bench 10 or pulled away from the bench To further facilitate grasping and installation on the bench, wing portions 121 A, 12 IB are provided on each armature. These are used by heated vacuum chuck to enable manipulation of the stmcmre and subsequent heating for solder bonding. The short distance between the wings 121 and the base surface 1 16 facilitate good heat transfer. Fig. 2 is a front plan view of the first embodiment of the mounting and alignment stmcmre 100, illustrated in Fig. 1. This view illustrates the constmction of the left and right armatures 1 14A, 1 14B, and specifically how the armamres are constructed from respective horizontally-extending segments 124 and vertically extending segments 122. Also shown is the extent of the bonding surface 132. Typically, a solder material is first applied to the surface 132. Later, the optical components and/or stmcmres are heated and brought into contact with each other to effect the solder bonding. In other embodiments, epoxy bonding processes are used in which epoxy is first applied to the surface 132. Fig. 3 A shows a second embodiment of the mounting and alignment stmcmre. This embodiment shares a number of similarities with the first embodiment illustrated in Figs. 1 and 2. Specifically, the mounting surface 1 16 has slot-like alignment channels 118 for visual alignment. Turning to the armatures 1 14A, 1 14B, vertically-extending portions 122A, 122B are provided similar to the first embodiment. Two horizontally extending portions 154, 155, however, are provided on each armamre on each side of the mounting and alignment stmcture 100. Specifically, the armamre 1 14B comprises two horizontally extending segments 154B, 155B, which extend generally from the vertically extending portion 122B to the optical component interface 1 12. Specifically, a linkage portion 158B connects the distal ends both of the horizontally- extending portions 154B, 155B to the vertically-extending portion 122B of armature 1 14B. The second embodiment of Fig. 3 A illustrates a further configuration for the optical component interface 112. Specifically, the optical interface 112 of the second embodiment comprises a V or U-shaped cut-out region or slot 152 extending through the mounting and alignment stmcmre 100 in the direction of the z-axis. This open- slot configuration allows a fiber, schematically illustrated as F to be installed vertically in the direction of arrow 159 down into the slot 152. In the typical implementation, the fiber F is then bonded to the surface 132 in the bottom of the slot. Solder bonding is preferably used, but other alternatives such as epoxy bonding exist. In the preferred embodiment, the depth of the slot relative to the locations of the attachment points of the armatures is designed to resist any rocking in response to z-axis forces exerted on the stmcmre by the fiber. Specifically, some movement in response to z-axis forces is unavoidable. Slot depth is controlled, however, so that the fiber axis does not move in response to these forces. In alternative embodiments, the handles 136 are engaged and the U-shaped slot crimped closed by applying force along arrow 157 to secure the optical component, such as fiber Fig 3B shows exemplary dimensions of the third embodiment Specifically, the height h of the illustrated embodiment is 1 1 millimeters (mm) Generally the stmcmres typically have height of greater than 0 5 mm to promote manipulation To provide adequate clearance in standard packages, the stmcmres are typically less then 2 0 mm in height The width w of the illustrated stmcmre is 1 9 mm Here again, the width is preferably greater than 0 5 mm to facilitate stable installation on the bench To provide acceptable component packing densities and clearance between components the width w of typically less than 4 mm is desirable Fig 4 shows a third embodiment mounting and alignment stmcmre 100 that shares many similarities with the stmcmres described in connection with Figs 1-3 It has a base 1 10 and laterally-extending base surface 1 16 Further, the third illustrated embodiment has an optical component interface 1 12 with an optical port 152 In this example, the handle 136 is more pronounced, extending vertically upward from the interface 1 12 V-shaped alignment feamres 210 are provided on the base surface for engaging complementary V-shaped alignment trenches in the bench One of the more distinguishing characteristics is the armatures 1 14A and 1 14B Instead of having segments that extend parallel to the x and y axes, each armature comprises two diagonally extending segments 212, 214 that intersect substantially at a right angle with respect to each other Further, the armamres have no discrete flexure system but instead have a relatively constant cross-section along the length of the armamres Further, the optical component interface 112 comprises a relatively closed slot- shaped optical component mounting slot 152. In one embodiment, a fiber is inserted into the slot 152 and then the slot is crimped closed to secure the fiber therein. Further, a handle 136 is provided extending vertically from the optical component interface 1 12. In the illustrated example, the handle 136 has right and left extensions on either side of the slot 152. Another distinction relative to the third embodiment of Fig. 4 relative to the previously is the use of a z-axis flexure. Specifically, the base 1 10 comprises a front plate portion 422 and a rear plate portion (not shown). Thus, the base 1 10 is a hollow box-configuration. The use of the Z-axis armamre allows controlled flexing when stress is exerted in a rotational manner around the x-axis or θ direction. Fig. 5A shows an embodiment in which the base is divided into two separate base portions 110 A, 1 10B to promote a stable structure-bench interface while simultaneously minimizing the contact area subject to thermal expansion mismatch stresses. In order to make the device more robust during manufacturing of the stmcmre and during its installation on the optical bench, a spring-like connecting element 310 connects the two halves of the base 1 10A, 1 10B. This element is clipped prior to installation or intentionally collapsed. Fig. 5B shows a related embodiment with similar reference numerals indicating similar parts. This embodiment is notable in that the angle between vertically-extending segments 126 and the horizontally-extending segments 124 form an obtuse angle. In some applications this configuration facilitates alignment. Fig. 6 shows a fifth embodiment, being closely related to the fourth embodiment of Fig. 5. Here, the optical component interface comprises two separate, divided portions 112A, 1 12B. In this embodiment, an optical component, such as an optical fiber f is inserted into the volumetric region between the two halves 112 A, 112B of the interface. The two halves 112A, 112B are snapped closed around the fiber F. Fig. 7 shows a sixth embodiment of a mounting and alignment stmcmre. This embodiment is notable relative to the previously discussed embodiments in that the armatures 114A, 1 14B have continuous flexures distributed across the length of the armatures. The flexures are not located at specific flexure points as illustrated in some of the previous embodiments. In this embodiment, the armamres act as distributed flexing components that are subject to plastic deformation. Fig. 8 shows a seventh embodiment of the mounting and alignment stmcmres. This embodiment is notable in that the armamres 114A, 114B are relatively rigid such that they will resist any flexing or plastic deformation. Specifically, the armamres 1 14A, 1 14B have no discrete flexures as discussed relative to Fig. 1 nor do they have a continuous flexure system as illustrated in Fig. 7 as illustrated by the fact that the armatures are relatively thick. As a result, the embodiment of Fig. 8 is typically used mostly for mounting fibers that pass outside of the module or package through a fiber feed-through. The seventh embodiment resists strain to any stress exerted on, for example, a fiber F held in the interface 1 12. Typically, the seventh embodiment is used in conjunction with a second mounting and alignment stmcture. The first mounting and alignment stmcmre is proximate to the end of the fiber and enables alignment of the fiber end in the x, y plane. The seventh embodiment alignment stmcmre is used to minimize the stress transmitted through the fiber to the stmcmre used for fiber-end alignment. Fig. 9 illustrates an eighth embodiment with continuous flexure armatures 114A, 114B and an optical interface 112 that would be appropriate for an optical component other than an optical fiber. Specifically, a mirror or lens is mounted on the optical interface 112 by bonding such as solder or epoxy bonding. The port 134 enables optical access to that component in which an optical signal is reflected by the optical component or passes through the component thus also passing through the port 134. Fig. 10 shows ninth embodiment where the base 1 10 is a relatively wide one- piece base. Fig. 1 1 shows another embodiment in which four stmcmres 100A-100D are integrated on a common base 110. This system is useful for holding optical components, such as optical fibers for four physically parallel optical channels or paths. According to the invention, each optical fiber is separately aligned with separate alignment characteristics of the stmcmres. The common base, however, enables multiple, simultaneous passive alignment of the structures/fibers in a single pick and placement step. Fig. 12 shows a non-laterally symmetric mounting and alignment stmcmre according to an eleventh embodiment. It comprises a base 110 and an armamre 114 extending from the base vertically. The armature comprises a vertical segment 122 and a horizontally extending segment 124. The horizontally extending segment 124 terminates in a component interface 112. A handle 136 extends vertically from this interface. Fig. 13 shows a non-laterally symmetric mounting and alignment stmcmre according to a twelfth embodiment of the present invention. In this case, the base 110 extends in a vertical, y-axis direction such that it may be attached onto a side-wall of a module or another mounting and alignment stmcture. It further has an horizontally extending armamre 1 14 and a component interface 112 adapted to hold a fiber concentrically in the center or abut against a fiber to improve its alignment. Fig. 14 is a plan view of a mounting stmcmre for exclusively passive mounting of an optical component. Specifically, the thirteenth embodiment has a base 112 and an integral optical component interface 112. It further has a port 134 for enabling access to the optical component. This embodiment does not have armamres and consequently is only susceptible to small alignment shifts. It is used mostly to hold components when their horizontal or vertical positioning is non-critical, such as, for example, a fold mirror in some system designs. Fig. 15A shows a mounting and alignment stmcmre for mounting relatively large MEMS filter device, a current implementation. Specifically, the fourteenth embodiment mounting and alignment stmcmre has a divided base 1 10 A, HOB. From each base, respective armatures 1 14 A, 1 14B extend. The armamres each comprise a vertically extending portion 122 A, 122B and a horizontally extending portion 124A, 124B. The optical component interface 112 is relatively large and is designed to hold an optical component mounted to the mounting surface 132, for example. The handle 136 is integral with the interface in this embodiment. Fig. 15B illustrates the deployment of the fourteenth embodiment alignment stmcmre 1 OOB with one of the previously discussed alignment stmcmres 1 OOA. In typical installation and alignment, the mounting and alignment stmcmre 100A is first installed on an optical bench 10. Alignment stmcmre is then preferably deformed, in an active alignment process, for example, such that the optical component is properly located relative to the optical path. Subsequently, after the alignment of the optical component held by mounting and alignment stmcture 100A, the mounting stmcmre 100B is installed with its own optical component. Then, this second alignment stmcmre 100B is then tuned, in an active alignment process, for example, so that the second optical component is properly located in the optical path. The relative size differences between alignment stmcmre 100A and 100B allows series alignments of their respective optical components even though the optical components are mounted in close proximity to each other on the bench 10. Mounting structure manufacturing Figs. 16A-16C are cross-sectional views of the mounting and alignment stmcmres 100 during the manufacmring process. Specifically, as illustrated in Fig. 16A, a thick PMMA resist layer 414 is bonded to a seed/release layer 412 on a substrate 410. The depth d of the PMMA layer 414 determines the maximum thickness of the subsequently manufactured quasi-extmsion portion of the mounting and alignment stmcmre. As a result, the depth determines the rigidity of the mounting and alignment stmcmre 100 to forces along the Z-axis. In the preferred embodiment, the depth and consequently Z-axis thickness of the mounting and alignment stmcmres is in the range of 500-1000 microns. Thicker stmcmres are typically used for strain relief-type stmcmres. According to present processes, the stmcmres, and consequently the depth of the PMMA layer is as deep as 2000 microns to produce stmcmres of same thickness. Fig. 16B illustrates the next fabrication step in the mounting and alignment stmcmre 100. Specifically, the thick PMMA resist layer is patterned by exposure to collimated x-rays. Specifically, a mask 416, which is either be a positive or negative mask having the desired pattern for the stmcture, is placed between the x-ray source such as a synchrotron and the PMMA layer 414. The PMMA layer 414 is then developed into the patterned layer 414A as illustrated in Fig. 16B. Fig. 16C shows the formation of the quasi-extmsion portion of the mounting stmcmre 100. Specifically, in the preferred embodiment, the quasi-extmsion portion is formed via electroplating. The preferred plating metal is nickel according to the present embodiment. Nickel alloys, such as a nickel-iron alloy, are used in alternative embodiments. Alternatively gold or a gold alloy is used in still other embodiments. Currently, alternative metal and alloys include: silver, silver alloy, nickel copper, nickel cobalt, gold cobalt and alloys laden with colloidal oxide particles to pin the microstructures. Figs. 17A-17F illustrate a process of manufacmring the z-axis flexure 422 previously discussed with reference to Fig. 4. Specifically, as illustrated in Fig. 17A, after the formation of the quasi-extmded portion of the mounting and alignment stmcmre, the substrate 410 is removed from the seed layer 412. Thereafter, an additional photoresist 420 layer is coated and then patterned as illustrated in Fig. 17B for one plate of the z-axis flexure. Thereafter, a further electroplating step is performed to fabricate the plate of the z-axis flexure 422 onto the existing cross- sectionally constant section 100. In Fig. 17D, a second photoresist is formed and then patterned on the reverse side of the stmcmre 100 and first PMMA layer 414. The etching is performed through the seed layer 412. Another plating step is performed and the second plate of the z- axis flexure 428 is manufactured as illustrated in Fig. 17E. Thereafter, as illustrated in Fig. 17F, the remaining photoresist layer 424, seed layer 412, and PMMA layer 414 are removed leaving the hollow box-shaped stmcture illustrated. This box shaped stmcmre forms the bottom base section 422 of the mounting and alignment stmcmre illustrated in Fig. 4. Mounting structure-optical component bench installation Fig. 18A illustrates the process associated with installing optical components on the optical bench 10. The bench is preferably constructed from mechanically robust, chemically stable, and temperamre stable material, such as silicon, beryllium oxide, aluminum nitride, aluminum silicon carbide, beryllium copper. It is typically metal or ceramic coated with gold or a gold alloy for example. Specifically, in a step 450, optical component 20 is installed on a first mounting and alignment stmcture 100-1. Specifically, the optical component 20 is preferably bonded to the mounting and alignment stmcmre 100- 1. In the preferred embodiment, a solder bonding is used in which solder is first applied to a periphery of the optical component and/or the bonding surface 132 of the optical component interface 112. Then the optical component is brought into contact with the mount surface 132 of the structure's component interface 112. The solder is then melted and allowed to solidify. Also in the preferred embodiment, complimentary alignment features in the optical component 20 and the interface 112 facilitate alignment and proper seating between the component 20 and stmcmre 100-1. Specifically, in alignment channels 113 (see Figs. 1 and 2) are formed on the structure's interface. Marks or projections 450 on the optical component 20 engage the slots 1 13 to ensure reproducible installation of the component 20 on the stmcmre 100-1. In other embodiments, the component 20 is epoxy bonded or bonded using another adhesive bonding technique to the stmcmre. Then, in a structure-bench mounting step 452, the stmcmre 100-1 is brought into contact with the optical bench 10 and bonded to the bench. In the preferred embodiment, solder bonding is used in which the bench is held in a heated chuck of a pick-and-place machine while the preheated stmcmre is brought into contact with the bench. The heat is then removed to solidify the solder. As illustrated in connection with alignment stmcmre 100-2, for other optical components, the mounting steps are reversed. In this example, the mounting and alignment stmcmre 100-2 is contacted and bonded to the bench in a structure-bench bonding step 454. Thereafter, the optical fiber is seated in the U-shaped port 152 of the mounting and alignment stmcmre 100-2. Thereafter, the fiber is either bonded to the interface bonding surface 132 or the U-shaped slot is crimped such that the fiber is secured in the bottom of the U-shaped port. Thus, the fiber endface EF is secured to the optical bench in proximity to the optical component, such as thin film filter or mirror 20, held by stmcmre 100-1. Fig. 18B also illustrates the process associated with installing MEMS-type optical components on the optical bench 10. Specifically, in this embodiment, a front mirror 470 is first bonded over a reflective membrane of the MEMS device 472 in a first bonding step 474. Then, the MEMS device 472 is bonded to the alignment stmcmre 100 in a second bonding step 476. Then in a bench-bonding step 478, the composite MEMS/structure is bonded to the bench 10. Mounting structure deformation in alignment Fig. 19 is a perspective view of a fiber optic laser optical signal source system, which has been constmcted according to the principles of the present invention. Specifically, the laser source system 610 comprises a laser chip 612, which has been mounted on a hybrid substrate 614. Typically, this substrate supports the electrical connections to the chip 612 and possibly also comprises a thermoelectric cooler for maintaining an operating temperamre of the chip 612. The hybrid substrate 614 is in m installed on an optical bench portion 10 of a package substrate 622. A detector 616 is located behind the chip 612 on the bench 10 to detect rear facet light and thereby monitor the operation of the laser 612. Light emitted from a front facet 618 of the chip 612 is collected by a fiber f for transmission outside the optical system 610. In one implementation, the light propagating in fiber f is used to optically pump a gain fiber, such as a rare-earth doped fiber or regular fiber in a Raman pumping scheme. In other implementations, the laser chip 612 is modulated in response to an information signal such that the fiber transmits an optical information signal to a remote detector. In still other implementations, the laser chip 612 is operated to mn in a CW mode with modulation performed by a separate modulator such as a Mach-Zehnder interferometer. An optical component mounting and alignment stmcmre 100, according to the invention, is installed on the optical bench portion 10 of the package substrate 622. As discussed previously, the optical bench has alignment feamres 620, which mate with opposite-gender alignment features on the base surface of the mounting and alignment stmcmre 100 as described previously in connection with Fig. 1, for example. As also discussed previously, the fiber f is installed in the U-shaped port 152, which is part of the optical component interface 1 12 of the mounting and alignment stmcmre 100. Fig. 20 is a process diagram illustrating the active alignment process that is used in conjunction with the deformable optical component mounting stmcmres in the manufacture of an optical signal source as illustrated in Fig. 19, for example. Specifically, in step 650, a laser die 614 and alignment stmcture 100 are mounted to the optical bench 10 in a pick-and-place and bonding process. Specifically, a pick-and-place robot locates the die 614 and the alignment stmcmre 100 on the optical bench 10 using passive alignment. The alignment process is preferably accomplished using machine vision techniques and or alignment feamres in the laser bench 10, and mounting and alignment stmcture 100, and die 614, or 5 explicitly relative to a defined coordinate system of the bench 10/module 622. In step 652, once the laser hybrid 614 and stmcmre 100 are attached to the bench 10, wire bonding is performed to the laser hybrid. Then, in step 654, the laser 612 is electrically energized to determine whether or not the laser is functioning properly. 0 If the laser is not functioning, then the optical system is rejected in step 656. If, however, the laser is determined to be operational in step 654, the bench is moved to an alignment fixture of the production system in step 658. In step 660, the fiber f is inserted into the U-shaped port 152 of the optical component interface 1 12 and bonded there. In the preferred embodiment, the fiber is 5 solder bonded to bonding surface 132. In step 664, the alignment system grasps or engages the mounting and alignment stmcmre 100 to deform the mounting and alignment stmcmre 100 in response to a strength or magnitude of a signal transmitted by the fiber f from the laser 612. o Fig. 21 illustrates the engagement between the alignment system and the mounting and alignment stmcture 100 to align the fiber f. Specifically, the two jaws 710A, 710B engage the handles 136 of the mounting and alignment stmcmre 100 and then move the mounting and alignment stmcmre to displace the fiber f in an x-y plane, which is orthogonal to the axis of the fiber f. Simultaneously, the magnitude of the signal transmitted by the fiber is monitored until a maximum signal is detected in step 666 of Fig. 20. Of note is the fact that the right and left cut-outs of the handle 136 enable the jaws of alignment system to both pull and push the stmcmre away and toward the bench 10, as needed to achieve an optimal alignment. Returning to Fig. 20, once the maximum signal is detected in step 666, the alignment system further deforms the mounting and alignment stmcmre 100 such that when the mounting and alignment stmcmre is released, it will elastically snap-back to the desired alignment position detected in step 666. In other words, the mounting and alignment stmcmre is plastically deformed such that it will have proper alignment when the jaws 710A, 710B of the alignment system disengage from the mounting and alignment stmcmre 100. If it is subsequently determined in step 670 that the optical component, i.e., the fiber is not at the position associated with the maximum coupling, the deformation step 668 is performed again until the position is within an acceptable tolerance. Fig. 22 is a plot illustrating the alignment process. Specifically, the figure of merit or the coupling efficiency of light into the optical fiber is plotted as a function of displacement of the optical fiber. Specifically, the coupling efficiency is maximized when the fiber is located at the best alignment position and falls off on either side of this position. Fig. 22 also illustrates force or stress as a function of strain or displacement during the several steps of the alignment process. Specifically, in a first step 710, force is exerted on the mounting and alignment stmcmre, such that it undergoes elastic deformation. In this regime, there is a substantially linear relationship between the applied force, on the y-axis and the displacement or strain on the x-axis. Once the yield force level is exceeded, however, the mounting and alignment stmcmre 100 undergoes plastic deformation as illustrated by line 720. This plastic deformation results in permanent deformation to the mounting and alignment stmcmre. When force is removed, the mounting and alignment stmcmre undergoes elastic "snap-back" as illustrated by step 722. That is, with the force removed, the stmcmre undergoes some elastic movement. However, because the yield force level was exceeded, the mounting and alignment stmcmre has been permanently deformed as indicated by distance Δi. Even with this plastic deformation, the fiber is still not at the best alignment position. As a result, another cycle of plastic deformation is performed. Specifically, force is applied such that the mounting alignment stmcmre undergoes elastic deformation as illustrated by line 724. Once the new yield force level has been exceeded a second time, it then undergoes plastic deformation as indicated by line 726. The yield force has increased during this second alignment cycle due to work hardening. Force is then removed and the mounting and alignment stmcmre undergoes elastic snap-back as illustrated by line 728. This second plastic deformation step, since it exceeded the yield force, resulted in movement toward the best alignment position of Δ 2 . Nonetheless, if optimal alignment is to be achieved, more plastic deformation must be performed. Specifically, again the elastic deformation is performed in step 730 until the yield force is reached. Then, a small amount of plastic deformation is performed as indicated by line 732. Force is removed and the mounting alignment stmcmre now snaps back to the best alignment position as indicated by line 734. The graph insert shows the figure of merit during the alignment process. During the first plastic deformation cycle, the position passes through the best alignment position, but after force is removed, the elastic snap-back pulls it out of best alignment. During the second deformation cycle, the best alignment position is again passed and exceeded. This second cycle, however, improves the alignment once force is removed. Finally, the third cycle brings the fiber into the best alignment position. Mounting structure design criteria 5 Fig. 23 presents a plot of force, Fy, as a function of displacement that can be employed in accordance with the invention to design the armatures for a given application. The yield force is the force at which the stmcmre begins to undergo plastic deformation from an elastic deformation regime. The lower bound on Fy (1200) is constrained by environmental shock, i.e., o acceleration, and by the possible forces to which the mounting stmcmre might be subjected during handling. Some specifications require optical systems to withstand 5000 g shock-tests. Typically with some optical elements, yield forces of greater than 0.5 Newtons are typically required. This number, however, can be reduced as the size and thus mass of optical elements is reduced. Were there no minimum yield force 5 constraint, the unavoidable forces produced during handling, including fabrication, heat treatment, plating, pick and place, alignment, packaging, and other processes, could cause plastic deformations of the flexure joints. More seriously, any shock to an aligned system might misalign it, defeating one of the puφoses of the invention. The upper bound on Fy (1250) is constrained by three factors. First, the force o required to cause plastic deformation of an armature or flexure must not be so high as to weaken or destroy the bond between the mounting stmcmre and the substrate. Second, the yield force must not be so high as to cause significant elastic deformation in the micromanipulator that is applying the force. Third, the force required to deform the armamre or flexure must not be so high as to damage other portions of the 5 integrally- formed mounting stmcmre. In addition to constraining the armamre yield force, it is also preferred to constrain how much displacement is required in order to reach the yield point. The lower bound (line 1300) is dictated first by the physical range of the stmcmre. A mounting stmcmre only functions as desired if there is enough plastic deformation range to reach the aligned position. Generally, the alignment stmcmres need to enable movement or placement of the optical component of 0 to 50 microns. The typically alignment algorithms require plastic deformation that yields 4 to 5 microns of movement in the position of the optical component to reach alignment. The second constraint on the minimum stiffness is determined by the amount of "overshoot" deemed acceptable by the alignment algorithm. If the stmcmres are too elastic, then they must be pressed a long distance beyond the desired alignment point in order to make even a small alignment adjustment. The final constraint is the maximum stiffness of the flexures (line 1350). Were work hardening not an issue, there would be no constraint on maximum stiffness (except, of course, material limitations). With nickel and nickel alloys, however, work hardening occurs. Therefore, the stiffness upper bound is selected so that line 1250 is not exceeded even with work hardened created by successive plastic deformation cycles performed during the search for the correct alignment. In the preferred embodiment, F Y y , i.e., the yield force in the direction of the y- axis, is less than 3 Newtons (N), typically between 0.2 and 1 N. The yield force along the x-axis, Fy , x is similarly limited to less than about 3 Newtons, typically between 0.2 and 1 N. Yield forces below 0.2 N are viable if smaller optical component are used, however. These lower limits are related to the mass of the optical component that the stmcmre must restrain without unintended plastic deformation. Thus, lower yield forces are possible with smaller components in subsequent product generations. In contrast, the yield force the z-axis direction, i.e., Fγ j Z or Fy^, is much larger to promote alignment in only the x-y plane. Preferably, F y> z or F y, Θ are greater than 5 N or 10 N. Further, especially in versions of the alignment stmcmres that are used to secure fiber pigtails to benches. Thermal expansion mismatches resulting 5 stresses on the fibers. The objective is to design the stmcmres so that such stresses result in as little movement in the fiber endface as possible. Especially any rocking motion is desirably avoided by balancing the stmcmres by selecting the location of where the armamres attach to the fiber component interface. Further embodiments l o Fig. 24 illustrates another embodiment of the invention in which the stmcmre 100 is a composite of an extrusion-like portion 101, which has a constant cross section along the z-axis, and two z-axis flexure pieces 102, which control rotation around the x-axis or in the direction of angle Θ x , thereby determining the resistance to force components along the z-axis. Preferably on the z-axis flexure pieces 101 are is separately fabricated and bonded to base surface of portion 101. Base surfaces of the pieces are then bonded to the bench. Fig. 25 is an example mounting stmcmre provided by the invention wherein two different materials (indicated as "A" and "B") are employed in the mounting stmcmre for minimizing any change in optical axis location due to thermal expansion 20 and/or contraction of the stmcmre. In one example configuration, the "A" material is selected, in combination with the design of that region of the stmcmre, to expand upward due to temperamre change, while the "B" material and its corresponding mounting design feamres are selected for a tendency to expand downward due to temperature change. These opposing expansion tendencies result in a compensating 5 action that produces stability in stmcmre geometry and position across a range of operational temperatures. Optical system production line Fig. 26 schematically illustrates the manufacmring sequence for optical systems according to the principles of the present invention. Generally, process comprises precision pick and place to locate the optical component to an accuracy of better than 10 microns, better than two microns in the preferred embodiment, followed by active alignment in which the position of the component is trimmed to an accuracy of about a micron, preferably better than a micron. Specifically, an alignment stmcmre supply 2010, such as a gel pack or other machine-vision compatible holder, is provided along with a similarly configured optical component supply 2012. Each of the supplies is accessed by a pick-and-place machine 2014. Specifically, the pick-and-place machine applies the optical components to the alignment stmcmres and bonds the components. Typically, either the alignment stmcmres and/or the optical components are solder coated or solder performs are used. The pick-and-place machine heats the alignment stmcmre and the optical components and brings the two pieces into contact with each other and then melts and resolidifies the solder. In the current embodiment, the pick-and-place machine is manufactured by Karl Siiss, France, type FC-1 0 or FC-250. These pick-and-place machines have a vacuum chuck for picking-up the optical components and a holder for holding the alignment stmcmres. The alignment stmcmres, with the affixed optical components are then fed to a separate or the same pick-and-place machine, which has access to an optical bench supply 2018. In this second pick-and-place operation, the pick-and-place machine 2016 holds the optical bench on a vacuum chuck or holder and then applies the alignment stmcmre, with the optical component, to the optical bench using its vacuum chuck. The bench and stmcmre are then heated to effect the solder bonding. Further, by matching alignment feamres of the benches and alignment feamres of the mounting stmcmres, placement accuracies of less than 5 microns are attainable. In the preferred embodiment, the stmcmres are located on the bench with accuracies of better than 2-3 microns in a production environment. In the preferred embodiment, the optical benches, with the alignment stmcmres affixed thereto are then fed to an alignment system. This alignment system 2020 has the jaws 710A, 710B which grasp the handle of the alignment stmcmre 100 to effect alignment. In the preferred embodiment, this alignment is active alignment in which the magnitude of the optical signal 2022 is detected by a detector 2024. The alignment stmcmre 100 is manipulated and deformed until the optical signal 2022, detected by the detector 2024, is maximized. Alignment search strategies such are a hill-climbing approach or spiral scan approach are preferably utilized. In other situations, such as when installing optical fibers on the bench 10, the alignment stmcmre is preferably installed first without the fiber attached by the pick and place machine 2016. Then at the alignment system, the fiber is fed through a fiber feed-through in the module and attached, such as by solder bonding, to the alignment stmcmre 100. Then the alignment system manipulates the stmcmre to effect alignment. Once aligned, the optical bench and module is then passed to a lid sealing operation 2026 where the final manufacmring steps are performed such as lid sealing and baking, if required. Figs. 27A, 27B, and 27C illustrate three different configurations for the alignment channels 1 18 introduced in Fig. 1. Fig. 27A is the simplest design, but has a drawback associated with implementation in machine vision applications when the base surface is pre-coated with solder, or other bonding agent. Solder fills in the creases and smoothens the channel's edges making alignment based on the features potentially less accurate. 5 Figs. 27B and 27C show channels incoφorating cavities in the feamres that facilitate the identification of edges 118A even after solder coating. The resulting clear edge feamres, even after coating, facilitate alignment during bench installation. While this invention has been particularly shown and described with references to preferred embodiments thereof, it will be understood by those skilled in l o the art that various changes in form and details may be made therein without departing from the scope of the invention encompassed by the appended claims.

Claims: CLAIMS What is claimed is: 1. A mounting and alignment stmcmre for optical components, comprising a quasi-extmsion portion having a substantially constant cross-section in a z- axis direction, the quasi-extmsion portion including: at least one base having a laterally-extending base surface; an optical component interface; at least one armature connecting the component interface with the base; and a handle to enable manipulation of the stmcture during and/or after installation.. 2. A stmcture as claimed in claim 1, wherein the base surface is securable to an optical bench. 3. A stmcture as claimed in claim 1 , wherein the base surface is securable to an optical bench via solder bonding. 4. A stmcmre as claimed in claim 1, wherein the base surface is securable to an optical bench via epoxy bonding. 5. A stmcture as claimed in claim 1, wherein the base surface is securable to an optical bench via laser welding. 6. A stmcture as claimed in claim 1, wherein the base surface comprises an alignment feature used to locate the stmcmre on an optical bench. 7. A stmcture as claimed in claim 1, further comprising two bases, one on each side of a medial axis of the stmcmre. 8. A stmcture as claimed in claim 7, further comprising two armamres, one armamre extending from each base to the optical component interface. 9. A stmcmre as claimed in claim 1, wherein the interface comprises a port for enabling an optical signal to pass transversely through the stmcmre. 10. A stmcture as claimed in claim 9, wherein the port is a closed hole. 1 1. A stmcture as claimed in claim 9, wherein the port is a substantially U- shaped cut-out region. 12. A stmcmre as claimed in claim 1, wherein the interface comprises an open clamp for receiving an optical component that extends are least partially in a direction of the z-axis. 13. A stmcture as claimed in claim 12, wherein the optical component is an optical fiber. 14. A stmcmre as claimed in claim 1, wherein the handle comprises at least one cut-out region in the stmcmre. 1 . A stmcture as claimed in claim 14, wherein the handle is integral with the optical component interface. 16. A stmcture as claimed in claim 1, wherein the armamre comprises at least one flexure. 17. A stmcture as claimed in claim 16, wherein the flexure comprises a region of the armamre having a reduced cross-sectional area. 18. A stmcture as claimed in claim 1, wherein the armamre comprises at least two flexures. 19. A stmcmre as claimed in claim 18, wherein the flexures are separated by a laterally-extending segment of the armamre. 20. A stmcmre as claimed in claim 19, wherein the flexures have a reduced cross-sectional area relative to the segment. 21. A stmcture as claimed in claim 18, wherein the flexures are separated by a vertically-extending segment of the armamre. 22. A stmcture as claimed in claim 21, wherein the flexures have a reduced cross-sectional area relative to the segment. 23. A stmcture as claimed in claim 1, wherein the armamre comprises at least three flexures. 24. A stmcture as claimed in claim 23, wherein two of the flexures are separated by a laterally-extending segment of the armamre and two of the flexures are separated by a vertically-extending segment of the armamre. 25. A stmcture as claimed in claim 24, wherein the flexures have a reduced cross-sectional area relative to the segment. 26. A stmcture as claimed in claim 1 , wherein the armamre comprises a U- shaped flexure cut-outs in the armature. 27. A stmcture as claimed in claim 1, wherein the stmcture comprises at least two armamres symmetrically extending from either side of the interface. 28. A mounting and alignment stmcmre for an optical component, the stmcmre comprising: at least one base having a laterally extending base surface; and an optical component interface; wherein a rigidity of stmcmre to strain in a direction of an optical path at the optical component is greater than in a plane that is orthogonal to the optical path. 29. A stmcture as claimed in claim 28, wherein the base surface is securable to an optical bench. 30. A stmcmre as claimed in claim 28, wherein the base surface comprises an alignment feature to facilitate placement on an optical bench. 31. A stmcmre as claimed in claim 28, wherein the interface comprises a port for enabling an optical signal to pass transversely through the stmcmre to enable optical access to an optical component installed on the optical component interface. 32. A stmcmre as claimed in claim 31, wherein the port is a closed hole. 33. A stmcture as claimed in claim 31, wherein the port is a substantially U- shaped cut-out region. 34. A stmcture as claimed in claim 28, wherein the interface comprises a slot for receiving an optical component that extends are least partially in a direction of the z-axis. 35. A stmcmre as claimed in claim 34, wherein the optical component is an optical fiber. 36. A stmcmre as claimed in claim 28, further comprising a handle for facilitating grasping of the stmcmre and placement on an optical bench. 37. A stmcture as claimed in claim 36, wherein the handle is integral with the optical component interface. 38. A stmcmre as claimed in claim 28, further comprising flexures extending in the direction of the z-axis to control rigidity in the x-y plane. 39. A stmcture as claimed in claim 28, wherein a yield force in the direction of the optical path is over 5 times a yield force in a direction that is orthogonal to the optical path. 40. A stmcmre as claimed in claim 28, wherein a yield force in the direction of the optical path is over 10 times a yield force in a direction that is orthogonal to the optical path. 41. A stmcture as claimed in claim 28, wherein a yield force in the direction of the optical path is over 5 Newtons. 42. A stmcture as claimed in claim 28, wherein a yield force in a direction that is orthogonal to optical path is less than 1 Newton. 43. A stmcmre as claimed in claim 42, wherein a yield force in the direction of the optical path is over 5 Newtons. 44. A mounting and alignment stmcmre for optical fiber, comprising: at least one base having a laterally-extending base surface; an optical fiber interface including an open slot for receiving the optical fiber extending traversely therethrough; interface; and at least one plastically-deformable armamre connecting the fiber interface with the base. 45. A mounting and alignment stmcmre for optical fiber, comprising: at least one base; and an optical component interface including alignment feamres for facilitating installation of an optical component on the interface. 46. A strucmre as claimed in claim 45, wherein the alignment feamres physically engage complimentary features of an optical component. 47. A strucmre as claimed in claim 45, wherein the alignment feamres comprise slots 48. A strucmre as claimed in claim 47, wherein the slots extend in a z-axis direction. 49. A strucmre as claimed in claim 45, further comprising at least one armamre connecting the component interface with the base. 50. A strucmre as claimed in claim 49, wherein the armamre is deformable to effect alignment of the optical component relative to an optical path. 51. A mounting and alignment strucmre for an optical component, the strucmre comprising: at least one base having a laterally extending base surface; and an optical component interface; wherein the strucmre undergoes plastic deformation in response to forces of less than 3 Newtons in a direction orthogonal to an optical path at the optical component. 52. A stmcmre as claimed in Claim 51, wherein the stmcmre undergoes plastic deformation in response to forces of between 0.2 and 1 Newton in a direction orthogonal to an optical path at the optical component. 53. A stmcmre as claimed in Claim 51 , wherein the stmcmre undergoes plastic deformation in response to forces of less than 1 Newton but not less than 0.2 N in a direction orthogonal to an optical path at the optical component. 54. A stmcmre as claimed in Claim 51, wherein the stmcmre resists plastic deformation in response to forces of greater than 5 Newton in a direction parallel to an optical path at the optical component. 55. A mounting and alignment stmcmre for optical components, comprising a quasi-extmsion portion having a substantially constant cross-section in a z- axis direction, the quasi-extmsion portion including: at least one base having a laterally-extending base surface; an optical component interface; armamre connecting the component interface with the base; and at least one flexure in the armamre. 56. A stmcture as claimed in claim 55, wherein the flexure comprises a region of the armamre having a reduced cross-sectional area. 57. A stmcture as claimed in claim 55, wherein the armamre comprises at least two flexures. 58. A stmcture as claimed in claim 57, wherein the flexures are separated by a laterally-extending segment of the armamre. 59. A structure as claimed in claim 58, wherein the flexures have a reduced cross-sectional area relative to the segment. 60. A strucmre as claimed in claim 57, wherein the flexures are separated by a vertically-extending segment of the armature. 61. A structure as claimed in claim 60, wherein the flexures have a reduced cross-sectional area relative to the segment. 62. A strucmre as claimed in claim 55, wherein the armamre comprises at least three flexures. 63. A strucmre as claimed in claim 62, wherein two of the flexures are separated by a laterally-extending segment of the armamre and two of the flexures are separated by a vertically-extending segment of the armature. 64. A structure as claimed in claim 63, wherein the flexures have a reduced cross-sectional area relative to the segment. 65. A structure as claimed in Claim 51, wherein the structure undergoes plastic deformation in response to forces of less than 1 Newton in a direction orthogonal to an optical path at the optical component.

Inventors: FLANDERS DALE C, MASGHATI MONA, RACZ LIVIA M, WHITNEY PETER S, FLANDERS, DALE, C., MASGHATI, MONA, RACZ, LIVIA, M., WHITNEY, PETER, S.
Applicants: AXSUN TECH INC, FLANDERS DALE C, MASGHATI MONA, RACZ LIVIA M, WHITNEY PETER S, AXSUN TECHNOLOGIES, INC., FLANDERS, DALE, C., MASGHATI, MONA, RACZ, LIVIA, M., WHITNEY, PETER, S.
Application year: 2000
Main classification: G02B7
IPC codes: G02B6, G02B7, G02B27