EP0495865A1 - Befestigung von optischen komponenten - Google Patents

Befestigung von optischen komponenten

Info

Publication number
EP0495865A1
EP0495865A1 EP90915503A EP90915503A EP0495865A1 EP 0495865 A1 EP0495865 A1 EP 0495865A1 EP 90915503 A EP90915503 A EP 90915503A EP 90915503 A EP90915503 A EP 90915503A EP 0495865 A1 EP0495865 A1 EP 0495865A1
Authority
EP
European Patent Office
Prior art keywords
support member
frame
lens
optical
frame structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP90915503A
Other languages
English (en)
French (fr)
Inventor
Robert William Fieldings Main Road Musk
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BT& D TECHNOLOGIES Ltd
BT&D Technologies Ltd
Original Assignee
BT& D TECHNOLOGIES Ltd
BT&D Technologies Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BT& D TECHNOLOGIES Ltd, BT&D Technologies Ltd filed Critical BT& D TECHNOLOGIES Ltd
Publication of EP0495865A1 publication Critical patent/EP0495865A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/02Mountings, adjusting means, or light-tight connections, for optical elements for lenses
    • G02B7/023Mountings, adjusting means, or light-tight connections, for optical elements for lenses permitting adjustment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/043Allowing translations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/12Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/3648Supporting carriers of a microbench type, i.e. with micromachined additional mechanical structures
    • G02B6/3656Supporting carriers of a microbench type, i.e. with micromachined additional mechanical structures the additional structures being micropositioning, with microactuating elements for fine adjustment, or restricting movement, into two dimensions, e.g. cantilevers, beams, tongues or bridges with associated MEMs
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/3684Mechanical coupling means for mounting fibres to supporting carriers characterised by the manufacturing process of surface profiling of the supporting carrier
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3801Permanent connections, i.e. wherein fibres are kept aligned by mechanical means
    • G02B6/3803Adjustment or alignment devices for alignment prior to splicing
    • G02B6/3805Adjustment or alignment devices for alignment prior to splicing with a fibre-supporting member inclined to the bottom surface of the alignment means
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/42Coupling light guides with opto-electronic elements
    • G02B6/4201Packages, e.g. shape, construction, internal or external details
    • G02B6/4219Mechanical fixtures for holding or positioning the elements relative to each other in the couplings; Alignment methods for the elements, e.g. measuring or observing methods especially used therefor
    • G02B6/422Active alignment, i.e. moving the elements in response to the detected degree of coupling or position of the elements
    • G02B6/4226Positioning means for moving the elements into alignment, e.g. alignment screws, deformation of the mount

Definitions

  • This invention relates to optical components and optical componen mounts.
  • the invention finds an important application in mountin miniature lenses in optical devices of the kind used for optica communications technology.
  • man of the devices used in such a system transmit light between thei components in the form of a light beam travelling through free space.
  • Th distance over which the light travels as a beam is typically a fe micrometres, but may be up to several millimetres and more.
  • th lens will typically focus the light output of a light source such as a laser for example, onto the end of an optical fibre; in a receiver, the ligh emerging from a fibre end may be collimated by a lens to be incident on photodetector such as a PIN photodiode, for example.
  • the previously mentioned need for good optical alignmen constitutes one of the recurrent problems in the manufacture of optica devices for use in optical communications systems and the like.
  • Adequat alignment present difficult problems owing to the smallness of th components themselves; the high accuracy required of the alignment typically just a few micrometres or less; and to the need to ensure tha alignment will remain stable for the device lifetime of 25 years or more.
  • the present invention is concerned with providing a mounting arrangement for optical devices that provides good long term alignment at a relatively low manufacturing cost.
  • a mounting arrangement for optical components comprises a support member capable of plastic deformation in and parallel to its major plane, the support member being provided with means to mount one or more optical components thereon.
  • a mounting arrangement for miniature optical lenses comprises a support member capable of plastic deformation in and parallel to its major plane, the support member being provided with means to mount one or more optical components thereon.
  • the support member is plastically deformable also in a direction normal to said major plane.
  • a lens mount for a miniature optical lens comprises a support member capable of plastic deformation in and parallel to its major plane. Movement out of the plane may also be provided for.
  • the support member according to the present invention preferably comprises a frame structure.
  • the frame structure defines an essentially enclosed space with mounting locations for optical components being conveniently locate within this space.
  • the frame structure may be provided wit an optical component mount projecting into the interior of the spac defined by the frame structure.
  • mounting locations for optica components may instead, or additionally, be provided on the exterior o the frame structure.
  • the frame structure may be open towards its associated base; that i to say, an essentially enclosed space is defined only once the fram structure has been mounted on its base.
  • Such an open frame structure often enables the mounted optical components to be closer to the base than would be the case for a corresponding closed frame structure.
  • the support member may comprise two or more relatively rigid portions which are linked by relatively deformable portions. Instead, however, the support member may be of similar deformability substantially throughout
  • the corners may provide deformable zones.
  • the material which forms the deformable portions of the support member needs to have low resilience so that the shape imposed by an adjustment is retained.
  • Figure 1 is a perspective schematic view of a lens mount in accordance with the present invention, with Figure la illustrating the adjustability of the lens mount of Figure 1;
  • Figure 2 shows a schematic view of an optical device assembly comprising a plurality of optical components
  • Figures 3a to 3c and Figure 4 are schematic front views of embodiments illustrating various modifications over Figure 1;
  • Figures 5 is a sectional view taken along line V-V of Figure 3a ⁇
  • Figure 6 illustrates a practical arrangement for supplying lens mounts attached to a feeder strip; and Figure 7 illustrates further modifications of the present invention.
  • Figure 1 shows a lens mount 1 comprising an approximately diamond shaped frame portion 2 and integral therewith a straight foot section 3. Projecting into the interior of the frame from its corner opposite the foot section 3 is a lug 4.
  • the lug 4 has an aperture 5 which makes a press fit with a lens 6.
  • the aperture 5 may be of any suitable shape which makes a push fit with the lens 6.
  • the lens 6 is a spherical lens, although other forms of lens may be used such as, for example, a graded index rod lens (not shown).
  • Figure la is a schematic presentation of the manner in which the frame 1 of Figure 1 can be adjusted to position the lens 6 of Figure 1 in the appropriate position.
  • the lens can be moved up or down (U ⁇ — >D), left and right (L ⁇ — >R) and forwards and backwards (F ⁇ — >B).
  • U ⁇ — >D right and right
  • F ⁇ — >B forwards and backwards
  • most practically performed adjustments will be made up of a combination of movements in two or, possibly, all three directions described here.
  • the up-down movement and left-right movement lie generally within the plane defined by the frame, while the front-back movement is arc-like in a direction approximately normal to that plane.
  • the frame 1 is deformed by applying an external force by means of a suitable tool (not shown).
  • the deformation of the frame 1 may occur, essentially, in one of two ways: either the frame as a whole distorts, or distortion is restricted to dedicated portions of the frame, such as the hinge points indicated by empty circles in Figure la.
  • Such hinge points may be points of lower material strength, for example, or be regions of high stress concentration under an applied load. Since self-deformation under operating conditions is clearly undesirable, the material strength of the frame needs accordingly to be chosen such that deformation requires the application of a tool.
  • Figure 2 shows the lens mount 1 mounted on a block 12 together with a light source 13 and an optical fibre 11.
  • the frame 1 and the block 12 are mounted on an intermediate base 10.
  • the frame 1 is affixed to the block 12 by means of two spaced spot welds 7.
  • spot welds 7 In order to enable spot welds to be made, the foot section 3 of the frame 1 extends beyond the corners of the frame 1 itself. Brazing, soldering or organic adhesives may replace the spot welds in appropriate circumstances.
  • the procedure to align the light source 13, the optical fibre 11 and the lens 6 in the lens mount 1 is, essentially, a trial and error method.
  • affixing a lens mount 1 proceeds as follows:- The light source 13 is switched on and the lens mount 1 is positioned to achieve the desired alignment between it, the source 13, and the fibre 11. In this position, the lens mount 1 is attached to the block 12, in the manner described above.
  • the procedure of affixing the lens mount 1 on the block 12 will tend to disturb the previously achieved alignment, especially so in the case of spot welding. Any such misalignment occurring during that procedure is then corrected, with the light source 13 still under power, by deforming the lens mount 1 with a suitable tool (not shown) until the desired optical alignment is obtained.
  • the necessary degree of accuracy in obtaining alignment and hence the exact procedure for obtaining it will largely depend on the particular application. A greater degree of alignment accuracy will normally be required for a single mode fibre than for a multimode fibre, for example.
  • Figures 3a to 3c. show three different embodiments of the approximately diamond shaped frame of Figure 1.
  • the frame of Figure 3a is substantially identical with that of Figure 1, save that its lens is push-fit mounted in a hexagonal aperture 35.
  • the frame of Figure 3b differs from that of Figure 3a primarily in that the centre section of the foot section 3 has been removed, leaving two side portions 33 of the foot section 3. This enables the lug 4 depending from the top of the frame to be longer than in Figure 1 which, in turn, enables the lens to be mounted in a lower position relative to the foot section 3 than would be possible with the frame of Figure 3 .
  • the frame of Figure 3c has a short foot section 38 which would be used in situations where the frame is to be affixed to the front rather than the top of the base 10 of Figure 2.
  • Figure 3c illustrates an approximately square aperture, with rounded corners, where the lens is held in place by the four straight sides of the aperture.
  • FIG. 4 Another embodiment of the invention is shown in Figure 4.
  • the frame shown in Figure 4 is, essentially, an inverted T shape in which the aperture 5 for mounting the lens is located at the far end of the stem 42 of the T, and in which the foot section 43 is formed by the crossbar of the T. Nearest the crossbar, the stem 42 is weakened by two offset slots 47 and
  • slot 47 and 48 permit left to right movement by bending deformation of the bridge 44. Up and down movement of the portion 42 causes shear deformation of the bridge 44, while movement to the back and the front causes a torsional deformation of the bridge 44.
  • Additional zones of weakness may be provided, e.g. with the aid of additional slots (not shown), to obtain a greater range of adjustability.
  • Figure 5 is a section along the line V-V of Figure 3a and illustrates in greater detail the position of the lens 6 within the frame 1. As shown, the lens 6 makes a push fit with the sides of the aperture 35 in the lug 4.
  • the lens 6 is provided with an anti-reflection coating 67.
  • the anti-reflection coating 67 is preferably applied to the lens only after the lens has been inserted into the frame 1.
  • the frame 1 can be used as a convenient clamp for holding the lens 6 during anti-reflection coating and, of course, thereafter.
  • the frames, shown here with lenses 66 inserted, are conveniently formed along a strip 67 and attached to the strip along a break line 68.
  • each frame 61 is snapped off the strip 67 along the break line 68, and attached to a base such as base block 10 in Figure 2.
  • the frame shown there is modified to permit mounting thereon an assembly of a photodiode and a lens , such as is described, for example, in published international patent application WO89/05467 ("Light Sources", BT&D Technologies Ltd).
  • the frame 71 Figure 7 is an open frame having a central section 76 depending on each end via a strip 74 from a support arm 72, 73, whereby the outer ends of the support arm provide the foot section 73 for securing the frame 71 to a base (not shown) such as base 10 of Figure 2.
  • the material of the frame is preferably chosen to closely match the expansion coefficient of the base to which the frame is to be secured. Often the base will form the heat sink for an active device such as a laser or light emitting diode. If the base is a diamond heat sink the frame is preferably made of InvarTM. If the base is copper, the material for the frame may be nickel; and in the case of a silicon base, KovarTM is a material with a suitably matched expansion coefficient
  • the frame can be formed by methods such as mechanical stamping, photo etching, machining, spark erosion, or laser cutting.
  • the aperture for accommodating the lens can be similarly formed.
  • the material thickness, stiffness, deformability and other material parameters are chosen, for a given design of frame, such that in use the frame resists deformation even when subject to moderate shocks, while being sufficiently pliable to be deformed with the aid of an adjustment tool.
  • the frame is designed to have clearly defined deformation zones, the dimensions etc. of its deformable zones will be chosen accordingly.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Lens Barrels (AREA)
  • Optical Couplings Of Light Guides (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Low-Molecular Organic Synthesis Reactions Using Catalysts (AREA)
EP90915503A 1989-10-13 1990-10-12 Befestigung von optischen komponenten Withdrawn EP0495865A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB898923135A GB8923135D0 (en) 1989-10-13 1989-10-13 Mounting optical components
GB8923135 1989-10-13

Publications (1)

Publication Number Publication Date
EP0495865A1 true EP0495865A1 (de) 1992-07-29

Family

ID=10664552

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90915503A Withdrawn EP0495865A1 (de) 1989-10-13 1990-10-12 Befestigung von optischen komponenten

Country Status (8)

Country Link
EP (1) EP0495865A1 (de)
JP (1) JPH05501313A (de)
KR (1) KR920704164A (de)
AU (1) AU6602690A (de)
CA (1) CA2066040A1 (de)
GB (1) GB8923135D0 (de)
IE (1) IE903680A1 (de)
WO (1) WO1991006022A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4142856C1 (de) * 1991-12-20 1993-03-18 Siemens Ag, 8000 Muenchen, De
FR2690996A1 (fr) * 1992-05-07 1993-11-12 Thomson Hybrides Dispositif d'alignement optique entre un composant optoélectronique et un composant optique, et procédé d'alignement.
FR2734065B1 (fr) * 1995-05-12 1997-06-06 Commissariat Energie Atomique Composants microoptiques et microdeflecteurs optomecaniques a deplacement de microlentilles
SE511944C2 (sv) * 1997-06-18 1999-12-20 Ericsson Telefon Ab L M Förfarande för att inrikta optiska byggelement, bärare samt optisk komponent
US6049650A (en) * 1998-04-17 2000-04-11 Seagate Technology, Inc. Structure for micro-machine optical tooling and method for making and using
US6511236B1 (en) * 1999-09-07 2003-01-28 Intel Corporation Optoelectronic assembly and method for fabricating the same
US6227724B1 (en) * 1999-01-11 2001-05-08 Lightlogic, Inc. Method for constructing an optoelectronic assembly
DE19934184A1 (de) * 1999-07-21 2001-01-25 Siemens Ag Optische Kopplungseinrichtung
US6559464B1 (en) * 1999-11-15 2003-05-06 Axsun Technologies, Inc. Optical system active alignment process including alignment structure attach, position search, and deformation
AU3634701A (en) * 1999-11-15 2001-05-30 Axsun Technologies, Inc. Optical component installation process
US7003211B2 (en) 1999-11-15 2006-02-21 Axsun Technologies, Inc. Optical system production system
US6416937B1 (en) * 1999-11-15 2002-07-09 Axsun Technologies, Inc. Optical component installation process
US6625372B1 (en) 1999-11-15 2003-09-23 Axsun Technologies, Inc. Mounting and alignment structures for optical components
US20020043551A1 (en) * 2000-08-25 2002-04-18 Axsun Technologies, Inc. Solid-phase welded optical element attach process
AU2001286607A1 (en) * 2000-08-25 2002-03-13 Axsun Technologies, Inc. Solid-phase welded optical element attach process
US6892444B1 (en) 2000-09-21 2005-05-17 Axsun Technologies, Inc. Optical system manufacturing and alignment system
US7249894B1 (en) 2000-11-07 2007-07-31 Axsun Technologies, Inc. System and process for post alignment polarization extinction ratio compensation in semiconductor laser system
US7124928B2 (en) * 2001-01-16 2006-10-24 Axsun Technologies, Inc. Optical component installation and train alignment process utilizing metrology and plastic deformation
US6543114B2 (en) * 2001-03-08 2003-04-08 Axsun Technologies, Inc. Manufacturing system using solder self-alignment with optical component deformation fine alignment
US7430081B2 (en) 2002-02-28 2008-09-30 Emcore Corporation Sub-micron adjustable mount for supporting a component and method
US7126078B2 (en) 2002-02-28 2006-10-24 Emcore Corporation Sub-micron adjustable mount for supporting a component and method
JP4214406B2 (ja) * 2004-09-27 2009-01-28 日本電気株式会社 光信号入出力機構を有する半導体装置
EP1677133A1 (de) * 2004-12-30 2006-07-05 Rohm and Haas Electronic Materials, L.L.C. Mikrokomponentenhalter und Herstellungsverfahren dafür
DE102005041998B4 (de) 2005-09-05 2018-11-29 Robert Bosch Gmbh Verfahren zur Justage eines abbildenden Elements sowie Messgerät justiert nach einem derartigen Verfahren
DE102007061737A1 (de) * 2007-12-20 2009-06-25 Robert Bosch Gmbh Verfahren zur Montage und Justage einer elektro-optischen Vorrichtung sowie Messgerät montiert und justiert nach einem derartigen Verfahren
US7898752B2 (en) * 2008-11-24 2011-03-01 Corning Incorporated Optical package comprising an adjustable lens component coupled to a multi-directional lens flexure
DE102014007104B3 (de) * 2014-05-15 2015-08-27 MENTOR GmbH & Co Präzisions-Bauteile KG Mehrfach-Halterung mit einer Mehrzahl von Aufnahmen für Lichtleiter
CN109031543A (zh) * 2018-07-26 2018-12-18 武汉光迅科技股份有限公司 一种透镜的固定装置及相应的光模块

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0168820A3 (de) * 1984-07-19 1987-01-14 Siemens Aktiengesellschaft Justiervorrichtung für Lichtwellenleiter
NL8500615A (nl) * 1985-03-05 1986-10-01 Nederlanden Staat Fijninstelmechanisme voor het nauwkeurig positioneren van een instelelement.
JPS62276519A (ja) * 1986-05-26 1987-12-01 Hitachi Ltd 光電子装置およびその製造方法ならびにレンズフレ−ム
FR2606890B1 (fr) * 1986-11-18 1989-06-30 Lyonnaise Transmiss Optiques Dispositif de deplacement de l'extremite d'une fibre optique suivant deux axes orthogonaux

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9106022A1 *

Also Published As

Publication number Publication date
JPH05501313A (ja) 1993-03-11
KR920704164A (ko) 1992-12-19
IE903680A1 (en) 1991-04-24
GB8923135D0 (en) 1989-11-29
WO1991006022A1 (en) 1991-05-02
CA2066040A1 (en) 1991-04-14
AU6602690A (en) 1991-05-16

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