CA1284372C - Radiation deflector assembly - Google Patents
Radiation deflector assemblyInfo
- Publication number
- CA1284372C CA1284372C CA000520797A CA520797A CA1284372C CA 1284372 C CA1284372 C CA 1284372C CA 000520797 A CA000520797 A CA 000520797A CA 520797 A CA520797 A CA 520797A CA 1284372 C CA1284372 C CA 1284372C
- Authority
- CA
- Canada
- Prior art keywords
- deflector
- radiation
- waveguides
- substrate
- assembly according
- 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.)
- Expired - Fee Related
Links
Landscapes
- Mechanical Light Control Or Optical Switches (AREA)
- Optical Couplings Of Light Guides (AREA)
- Spectrometry And Color Measurement (AREA)
- Instruments For Measurement Of Length By Optical Means (AREA)
Abstract
RADIATION DEFLECTOR ASSEMBLY
ABSTRACT
A radiation deflector assembly, primarily for deflecting optical radiation, comprises three waveguides mounted in V-shaped grooves (2, 3, 4) of a substrate (1) which are substantially coplanar. A cantilevered beam (6) integral with the substrate (1) is positioned in a cavity (5) of the substrate such that when the beam (6) is in a first position radiation passes between optical waveguides in two of the grooves (2,3) and when the beam is in a second position optical radiation passes between optical waveguides in another two of the grooves (2,4).
Control means including electrodes (8,9) is responsive to control signals to generate a suitable electrostatic field for moving the beam (6) between the two positions.
ABSTRACT
A radiation deflector assembly, primarily for deflecting optical radiation, comprises three waveguides mounted in V-shaped grooves (2, 3, 4) of a substrate (1) which are substantially coplanar. A cantilevered beam (6) integral with the substrate (1) is positioned in a cavity (5) of the substrate such that when the beam (6) is in a first position radiation passes between optical waveguides in two of the grooves (2,3) and when the beam is in a second position optical radiation passes between optical waveguides in another two of the grooves (2,4).
Control means including electrodes (8,9) is responsive to control signals to generate a suitable electrostatic field for moving the beam (6) between the two positions.
Description
~ 23334/GB
RADIATION DEFLECTOR ASSEMBLY
The invention re1ates to radiation deflector assemblies of the kind comprising at least three radiation waveguides; a controllable radiation deflector positioned such that when the deflector is in a first position radiation passes between one combination of two of the waveguides, and when the deflector is in a second position radiation passes between another combination of two of the waveguides; and control means responsive to control signals for controlling the position of the deflector. Such assembliess are hereinafter referred to as of the kind described.
Radiation deflector assemblies of the kind described find particular application as switches in optical 1' transmission systems. IBM Technical Disclosure Bulletin Vol 27, No 2 of July 1984 ~pages 11-12) describes a solid-state array of mirrors positioned beneath three groups of optical fibres. In a relaxed position, optical radiation impinging on the mirrors from one group of 2~ fibres is reflected towards another group. When the mirrors are in a deflected position, optical radiation is instead reflected towards the third group of fibres.
- The major problem with this arrangement is that it is difficult accurately to align the optical fibres with the mirrors. Alignment is important when large arrays of mirrors are concerned so as to maximise the number of mirrors per unit area.
~ In accordance with the present invention, a i radiation deflector assembly of the kind described is characterised in that the waveguides and the deflector are mounted in a common substrate.
The invention deals with the alignment problem by mounting both the waveguides and the deflector in the same substrate.
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Preferably, the waveguides are substantially coplanar, and conveniently the direction of movement of the deflector is in substantially the sa~le plane as the plane of the waveguides. In alternative arrangements, S however, the waveguides may extend in different planes.
The invention is particularly suitable where the substrate comprises a single crystal of for example silicon, since anisotropic etching techniques may be used to define grooves of the same or different depths into 1~ which the waveguides are mounted.
The invention is particularly suitable for deflecting radiation in the optical waveband and ;typically a large number o~ radiation deflector assemblies according to the invention will be assembled together to cons~itute an optical switch array.
In some arrangements, the deflector may comprise a piston member which moves to and fxo between the 'irst and second positions. Preferably, however, the deflector comprises a cantilevered arm which is controlled to pivot betweer. the first and secon2 position~.
It is particularly convenient i' the deflector is integrally formed with the substrate. This can be achieved using conventional etching techniques or laser etching technology.
25Preferably, the deflector is adapted to deflect the radiation in both the first and secona positions although in some examples, radiation could pass directly fro~ one waveguide to another when the deflector is in the first position and be deflected towards another waveguide when the deflector is in the second position.
` The deflector will typically comprise a radiation reflector but other deflectors are possible such as a - re'ractor or diffractor.
In some examples, the waveguides could be formed by diffusing a suitable material into the substrate but .
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convenien-tly each waveguide is mounted in a groove formed in a surface of the substrate, typically a V-shaped groove.
As has previously been mentioned, the substrate may comprise silicon but other substrate materials are ; possible such as silica cr lithium niobate or III-V
; compounds such as gallium arsenide.
The position of the deflector can be controlled using conventional electrostatic techniques or by thermal methods similar to those described in our copending Canadian Patent Application, serial number 520,799 entitled "Movable Member Mounting".
An example of an optical reflection assembly according to the invention for use in an optical switch array will now be described with reference to the accompanying drawing which is a schematic perspective view of the assembly.
The optical element or assembly shown in the drawing includes a substrate comprising a single crystal silicon slice 1 in the upper surface of which three V-shaped grooves 2-4 have been etched using an anisotropic masking and etching technique. The grooves 2-4 all have substantially the same depth and are effectively coplanar.
~S Each groove 2-4 termina-tes in a cavity 5 formed in the ; substrate 1. Monomode optical fibres (not shown) are positioned in each of the grooves 2-4 with their ends facing into the cavity 5.
A cantilevered, vertically hinged silicon beam 6 is positioned in the cavi-ty 5 and is integrally formed with the remainder of the substrate 1. The beam 6 acts as an optical reflector.
The beam can pivot about its end 7 between first ` and second positions in response to an electrostatic field generated by a pair of electrodes, one of which 8 is - mounted to the substrate and the other of which is B
., ; mounted to the facing surface of the beam 6. If the beam is at ground potential, the second electrode is not required. The electrodes are connected to electrical control apparatus including a power source ~not shown~.
In its first position, the reflector 6 reflects optical radiation passing along the optical fibre in the ;~ groove 2 into the optical fibre in the groove 3. In its second position, optical radiation impinging on the reflector 6 from the fibre in the groove 2 is reflected l~ into the fibre in the groove 4. The element shown in the drawing can thus be used as an optical switch to switch incoming radiation in the optical fibre in the groove 2 into eithex the optical fibre in the groove 3 or the optical fibre in the groove 4.
: 15 .~
: ~n . 30 :``
. ~ .
.
. .
. .
RADIATION DEFLECTOR ASSEMBLY
The invention re1ates to radiation deflector assemblies of the kind comprising at least three radiation waveguides; a controllable radiation deflector positioned such that when the deflector is in a first position radiation passes between one combination of two of the waveguides, and when the deflector is in a second position radiation passes between another combination of two of the waveguides; and control means responsive to control signals for controlling the position of the deflector. Such assembliess are hereinafter referred to as of the kind described.
Radiation deflector assemblies of the kind described find particular application as switches in optical 1' transmission systems. IBM Technical Disclosure Bulletin Vol 27, No 2 of July 1984 ~pages 11-12) describes a solid-state array of mirrors positioned beneath three groups of optical fibres. In a relaxed position, optical radiation impinging on the mirrors from one group of 2~ fibres is reflected towards another group. When the mirrors are in a deflected position, optical radiation is instead reflected towards the third group of fibres.
- The major problem with this arrangement is that it is difficult accurately to align the optical fibres with the mirrors. Alignment is important when large arrays of mirrors are concerned so as to maximise the number of mirrors per unit area.
~ In accordance with the present invention, a i radiation deflector assembly of the kind described is characterised in that the waveguides and the deflector are mounted in a common substrate.
The invention deals with the alignment problem by mounting both the waveguides and the deflector in the same substrate.
' 35 . ~
;' .~`
. . .
. . .
.~., .
L~
Preferably, the waveguides are substantially coplanar, and conveniently the direction of movement of the deflector is in substantially the sa~le plane as the plane of the waveguides. In alternative arrangements, S however, the waveguides may extend in different planes.
The invention is particularly suitable where the substrate comprises a single crystal of for example silicon, since anisotropic etching techniques may be used to define grooves of the same or different depths into 1~ which the waveguides are mounted.
The invention is particularly suitable for deflecting radiation in the optical waveband and ;typically a large number o~ radiation deflector assemblies according to the invention will be assembled together to cons~itute an optical switch array.
In some arrangements, the deflector may comprise a piston member which moves to and fxo between the 'irst and second positions. Preferably, however, the deflector comprises a cantilevered arm which is controlled to pivot betweer. the first and secon2 position~.
It is particularly convenient i' the deflector is integrally formed with the substrate. This can be achieved using conventional etching techniques or laser etching technology.
25Preferably, the deflector is adapted to deflect the radiation in both the first and secona positions although in some examples, radiation could pass directly fro~ one waveguide to another when the deflector is in the first position and be deflected towards another waveguide when the deflector is in the second position.
` The deflector will typically comprise a radiation reflector but other deflectors are possible such as a - re'ractor or diffractor.
In some examples, the waveguides could be formed by diffusing a suitable material into the substrate but .
- , .
~., .
:
r~-~
convenien-tly each waveguide is mounted in a groove formed in a surface of the substrate, typically a V-shaped groove.
As has previously been mentioned, the substrate may comprise silicon but other substrate materials are ; possible such as silica cr lithium niobate or III-V
; compounds such as gallium arsenide.
The position of the deflector can be controlled using conventional electrostatic techniques or by thermal methods similar to those described in our copending Canadian Patent Application, serial number 520,799 entitled "Movable Member Mounting".
An example of an optical reflection assembly according to the invention for use in an optical switch array will now be described with reference to the accompanying drawing which is a schematic perspective view of the assembly.
The optical element or assembly shown in the drawing includes a substrate comprising a single crystal silicon slice 1 in the upper surface of which three V-shaped grooves 2-4 have been etched using an anisotropic masking and etching technique. The grooves 2-4 all have substantially the same depth and are effectively coplanar.
~S Each groove 2-4 termina-tes in a cavity 5 formed in the ; substrate 1. Monomode optical fibres (not shown) are positioned in each of the grooves 2-4 with their ends facing into the cavity 5.
A cantilevered, vertically hinged silicon beam 6 is positioned in the cavi-ty 5 and is integrally formed with the remainder of the substrate 1. The beam 6 acts as an optical reflector.
The beam can pivot about its end 7 between first ` and second positions in response to an electrostatic field generated by a pair of electrodes, one of which 8 is - mounted to the substrate and the other of which is B
., ; mounted to the facing surface of the beam 6. If the beam is at ground potential, the second electrode is not required. The electrodes are connected to electrical control apparatus including a power source ~not shown~.
In its first position, the reflector 6 reflects optical radiation passing along the optical fibre in the ;~ groove 2 into the optical fibre in the groove 3. In its second position, optical radiation impinging on the reflector 6 from the fibre in the groove 2 is reflected l~ into the fibre in the groove 4. The element shown in the drawing can thus be used as an optical switch to switch incoming radiation in the optical fibre in the groove 2 into eithex the optical fibre in the groove 3 or the optical fibre in the groove 4.
: 15 .~
: ~n . 30 :``
. ~ .
.
. .
. .
Claims (10)
1. A waveguide deflector assembly comprising at least three radiation waveguides, a controllable radiation deflector positioned such that when the deflector is in a first position radiation passes between one combination of two of the waveguides and when the reflector is in a second position radiation passes between another combination of two of the waveguides; and control means responsive to control signals for controlling the position of the deflector characterised in that the deflector is integrally formed with a substrate; and the waveguides are in a fixed position relative to the substrate.
2. A radiation deflector assembly comprising at least three radiation waveguides; a controllable radiation deflector positioned such that when the deflector is in a first position radiation passes between one combination of two of the waveguides and when the deflector is in a second position radiation passes between another combination of two of the waveguides; and control means responsive to control signals for controlling the position of the deflector characterised in that the waveguides and the deflector are mounted in a common substrate.
3. An assembly according to claim 1, wherein the radiation waveguides are substantially coplanar.
4. An assembly according to claim 1, wherein each waveguide comprises a waveguide member mounted in respective groove formed in the substrate.
5. An assembly according to any one of claims 1, 2 or 3, wherein the deflector is integrally formed with the substrate.
6. An assembly according to any one of claims 1, 2 or 3, wherein the deflector comprises a cantilevered arm.
7. An assembly according to any one of claims 1, 2 or 3, wherein the deflector is adapted to deflect radiation in both the first and second positions.
8. An assembly according to any one of claims 1, 2 or 3, wherein the deflector comprises a radiation reflector.
9. An assembly according to any one of claims 1, 2 or 3, wherein the waveguides and deflector are adapted to guide and deflect optical radiation respectively.
10. An assembly according to any one of claims 1, 2 or 3, wherein the substrate is a single crystal.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8526189 | 1985-10-23 | ||
GB858526189A GB8526189D0 (en) | 1985-10-23 | 1985-10-23 | Fabry-perot interferometer |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1284372C true CA1284372C (en) | 1991-05-21 |
Family
ID=10587147
Family Applications (6)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000520797A Expired - Fee Related CA1284372C (en) | 1985-10-23 | 1986-10-17 | Radiation deflector assembly |
CA000520799A Expired - Fee Related CA1277525C (en) | 1985-10-23 | 1986-10-17 | Movable member mounting |
CA000520800A Expired - Fee Related CA1278910C (en) | 1985-10-23 | 1986-10-17 | Mounting a component to a substrate |
CA 520796 Expired - Fee Related CA1333452C (en) | 1985-10-23 | 1986-10-17 | Fabry-perot interferometer |
CA000520801A Expired - Fee Related CA1276781C (en) | 1985-10-23 | 1986-10-17 | Positioning optical components and waveguides |
CA000520798A Expired - Fee Related CA1271552A (en) | 1985-10-23 | 1986-10-17 | Wavelength selection device and method |
Family Applications After (5)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000520799A Expired - Fee Related CA1277525C (en) | 1985-10-23 | 1986-10-17 | Movable member mounting |
CA000520800A Expired - Fee Related CA1278910C (en) | 1985-10-23 | 1986-10-17 | Mounting a component to a substrate |
CA 520796 Expired - Fee Related CA1333452C (en) | 1985-10-23 | 1986-10-17 | Fabry-perot interferometer |
CA000520801A Expired - Fee Related CA1276781C (en) | 1985-10-23 | 1986-10-17 | Positioning optical components and waveguides |
CA000520798A Expired - Fee Related CA1271552A (en) | 1985-10-23 | 1986-10-17 | Wavelength selection device and method |
Country Status (2)
Country | Link |
---|---|
CA (6) | CA1284372C (en) |
GB (1) | GB8526189D0 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6670208B2 (en) | 2000-06-23 | 2003-12-30 | Nec Corporation | Optical circuit in which fabrication is easy |
US11226457B2 (en) * | 2020-05-28 | 2022-01-18 | Cisco Technology, Inc. | Laser and photonic chip integration |
-
1985
- 1985-10-23 GB GB858526189A patent/GB8526189D0/en active Pending
-
1986
- 1986-10-17 CA CA000520797A patent/CA1284372C/en not_active Expired - Fee Related
- 1986-10-17 CA CA000520799A patent/CA1277525C/en not_active Expired - Fee Related
- 1986-10-17 CA CA000520800A patent/CA1278910C/en not_active Expired - Fee Related
- 1986-10-17 CA CA 520796 patent/CA1333452C/en not_active Expired - Fee Related
- 1986-10-17 CA CA000520801A patent/CA1276781C/en not_active Expired - Fee Related
- 1986-10-17 CA CA000520798A patent/CA1271552A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB8526189D0 (en) | 1985-11-27 |
CA1277525C (en) | 1990-12-11 |
CA1271552A (en) | 1990-07-10 |
CA1276781C (en) | 1990-11-27 |
CA1333452C (en) | 1994-12-13 |
CA1278910C (en) | 1991-01-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKLA | Lapsed |