CA2689280C - Scanning apparatus - Google Patents
Scanning apparatus Download PDFInfo
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- CA2689280C CA2689280C CA2689280A CA2689280A CA2689280C CA 2689280 C CA2689280 C CA 2689280C CA 2689280 A CA2689280 A CA 2689280A CA 2689280 A CA2689280 A CA 2689280A CA 2689280 C CA2689280 C CA 2689280C
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- Prior art keywords
- wedge
- reflector
- polariser
- reflected
- passes
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- 230000003287 optical effect Effects 0.000 claims abstract description 29
- 239000000463 material Substances 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 14
- 239000000377 silicon dioxide Substances 0.000 description 7
- 230000005855 radiation Effects 0.000 description 5
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- 239000005864 Sulphur Substances 0.000 description 4
- 230000010287 polarization Effects 0.000 description 4
- 230000003667 anti-reflective effect Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 3
- 238000003384 imaging method Methods 0.000 description 2
- 239000004810 polytetrafluoroethylene Substances 0.000 description 2
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
- G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
- G02B26/10—Scanning systems
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
- G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
- G02B26/0875—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements
- G02B26/0883—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements the refracting element being a prism
- G02B26/0891—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more refracting elements the refracting element being a prism forming an optical wedge
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/28—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00 for polarising
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Mechanical Optical Scanning Systems (AREA)
- Polarising Elements (AREA)
- Surgical Instruments (AREA)
- Valve Device For Special Equipments (AREA)
- Mechanical Treatment Of Semiconductor (AREA)
- Vehicle Body Suspensions (AREA)
- Ultra Sonic Daignosis Equipment (AREA)
- Apparatus For Radiation Diagnosis (AREA)
Abstract
A scanning apparatus comprises two rotatable bodies arranged to rotate in opposite directions. The first body being a polariser and the second being a mirror or a second polariser. The apparatus is arranged to define an optical path for a polarised beam, wherein the optical path passes through the first body, is reflected at the second body, and is reflected by the first body back to the second body from where it is transmitted or reflected to produce a linear scan. There is also disclosed a scanning system comprising a reflector and an optical wedge containing refractive materials, arranged to counter rotate and arranged so that a beam passing through the optical wedge, is reflected by the reflector and passes back through the optical wedge to produce a linear scan.
Description
SCANNING APPARATUS
This application is a divisional of Canadian patent application serial no. 2,454,194 which is the Canadian national phase of International application no. PCT/GB02/03349 filed 22 July 2002 (22.07.2002) and published 30 January 2003 (30.01.2003) under publication no. WO 03/009048A1.
Background of the Invention Field of the Invention The present invention relates to a scanning apparatus which may be used in a real-time imaging system, and in particular in a real-time mm wave length, or microwave imaging system.
Summary of the Prior Art In optics, there is a requirement to scan beams rapidly across the scene in a linear scan pattern.
For visible light, it is known to achieve a linear scan pattern by the use of two circular rotating reflective discs, which are equally inclined to their axes of rotation, and which rotate at the same speed. A single rotating mirror would produce a conical scan. However, when the second rotating mirror receives a conical scan from the first rotating mirror parts of the conical scan are effectively cancelled out resulting in a linear scan pattern. Alternatively flapping mirrors may be used to achieve a linear scan pattern.
la Such methods are suitable in the visible region where the apertures involved are small. In the infra-red region apertures are frequently about 100 mm and focussing lenses are used to reduce this aperture to around 10 mm. In the mm-wave and microwave regions these apertures are very large ( in the order of 1 m) and it is not practical to use flapping mirrors. Also when making reflective discs, there is considerable displacement of the beam which is received by the second of the mirrors, and therefore the second mirror has to be very large so as to be able to receive the displaced beam.
It is also known, for visible light, to produce a linear scan using two counter rotating prisms. However, such prisms are heavy and therefore not suitable for large aperture systems.
Summary of the Invention The present invention aims to provide a system for producing linear scans which is of suitable size and weight to be used in mm wave length and microwave applications. In other words the invention aims to provide a system which performs the function of the flapping mirrors, in effectively converting conical to linear scans.
In general terms, the invention uses at least one rotating polariser which, depending on the point in the optical path of the beam transmits and reflects the beam, so that the beam can pass through the polariser but then be reflected from another body back to the polariser to be reflected therefrom to cause cancellation of conical scans to produce a linear scan by a double reflection arrangement similar to that described previously.
According to a first aspect, the invention may then provide a scanning apparatus comprising an optical system having first and second rotatable bodies arranged to rotate at the same speed, in opposite directions, having generally parallel axes of rotation and being inclined to those axes of rotation, the optical systems being arranged to define an optical path for a polarised beam so as to form a linear scan, wherein at least a first one of the bodies is a polariser and the optical system is such that the optical path passes through the polariser, is reflected at the second body, and is reflected by the polarises back to the second body. Preferably the axes are coincident.
There are two general possibilities. In the first possibility, the second body is a mirror, or other reflective disc. In this case the optical path is such that, after the optical path has been reflected by the polariser back to the second body, the second body reflects the beam back through the polariser.
In the second possibility, the second body is a polariser and the optical path is such that once the beam is reflected back to the second body it is transmitted through the second body. This is a transmission system, with the beam finally passing through the rotatable body, and emerging from the rotatable body in direction in which it was received.
The polariser may be a circular polariser, or may be a linear polariser.
The invention relies upon changes in the orientation of polarisation which affects whether or not the beam passes through, or is reflected by the polariser.
Reflection is one possible way of altering the orientation of polarisation. However, it may be necessary to include in the optical system quarter wave plates or Faraday rotators to alter the orientation of polarisation. This is particularly the case when linear polarisers are used.
For example the first body may be a linear polariser, and two rotatable quarter wave plates may be located on either side of the polariser. The quarter wave plates rotate about the same axis as the linear polariser, at the same speed and in the same direction as the linear polariser.
In an alternative, a rotatable quarter wave plate is located on one side of the linear polariser, being rotatable about the same axis as the polariser, at the same speed and in the same direction, and a Faraday rotator is located on the other side of the polariser.
The Faraday rotator may be fixed or rotatable.
The quarter wave plate(s) and linear polariser are preferably connected to form a rotating unit.
This application is a divisional of Canadian patent application serial no. 2,454,194 which is the Canadian national phase of International application no. PCT/GB02/03349 filed 22 July 2002 (22.07.2002) and published 30 January 2003 (30.01.2003) under publication no. WO 03/009048A1.
Background of the Invention Field of the Invention The present invention relates to a scanning apparatus which may be used in a real-time imaging system, and in particular in a real-time mm wave length, or microwave imaging system.
Summary of the Prior Art In optics, there is a requirement to scan beams rapidly across the scene in a linear scan pattern.
For visible light, it is known to achieve a linear scan pattern by the use of two circular rotating reflective discs, which are equally inclined to their axes of rotation, and which rotate at the same speed. A single rotating mirror would produce a conical scan. However, when the second rotating mirror receives a conical scan from the first rotating mirror parts of the conical scan are effectively cancelled out resulting in a linear scan pattern. Alternatively flapping mirrors may be used to achieve a linear scan pattern.
la Such methods are suitable in the visible region where the apertures involved are small. In the infra-red region apertures are frequently about 100 mm and focussing lenses are used to reduce this aperture to around 10 mm. In the mm-wave and microwave regions these apertures are very large ( in the order of 1 m) and it is not practical to use flapping mirrors. Also when making reflective discs, there is considerable displacement of the beam which is received by the second of the mirrors, and therefore the second mirror has to be very large so as to be able to receive the displaced beam.
It is also known, for visible light, to produce a linear scan using two counter rotating prisms. However, such prisms are heavy and therefore not suitable for large aperture systems.
Summary of the Invention The present invention aims to provide a system for producing linear scans which is of suitable size and weight to be used in mm wave length and microwave applications. In other words the invention aims to provide a system which performs the function of the flapping mirrors, in effectively converting conical to linear scans.
In general terms, the invention uses at least one rotating polariser which, depending on the point in the optical path of the beam transmits and reflects the beam, so that the beam can pass through the polariser but then be reflected from another body back to the polariser to be reflected therefrom to cause cancellation of conical scans to produce a linear scan by a double reflection arrangement similar to that described previously.
According to a first aspect, the invention may then provide a scanning apparatus comprising an optical system having first and second rotatable bodies arranged to rotate at the same speed, in opposite directions, having generally parallel axes of rotation and being inclined to those axes of rotation, the optical systems being arranged to define an optical path for a polarised beam so as to form a linear scan, wherein at least a first one of the bodies is a polariser and the optical system is such that the optical path passes through the polariser, is reflected at the second body, and is reflected by the polarises back to the second body. Preferably the axes are coincident.
There are two general possibilities. In the first possibility, the second body is a mirror, or other reflective disc. In this case the optical path is such that, after the optical path has been reflected by the polariser back to the second body, the second body reflects the beam back through the polariser.
In the second possibility, the second body is a polariser and the optical path is such that once the beam is reflected back to the second body it is transmitted through the second body. This is a transmission system, with the beam finally passing through the rotatable body, and emerging from the rotatable body in direction in which it was received.
The polariser may be a circular polariser, or may be a linear polariser.
The invention relies upon changes in the orientation of polarisation which affects whether or not the beam passes through, or is reflected by the polariser.
Reflection is one possible way of altering the orientation of polarisation. However, it may be necessary to include in the optical system quarter wave plates or Faraday rotators to alter the orientation of polarisation. This is particularly the case when linear polarisers are used.
For example the first body may be a linear polariser, and two rotatable quarter wave plates may be located on either side of the polariser. The quarter wave plates rotate about the same axis as the linear polariser, at the same speed and in the same direction as the linear polariser.
In an alternative, a rotatable quarter wave plate is located on one side of the linear polariser, being rotatable about the same axis as the polariser, at the same speed and in the same direction, and a Faraday rotator is located on the other side of the polariser.
The Faraday rotator may be fixed or rotatable.
The quarter wave plate(s) and linear polariser are preferably connected to form a rotating unit.
5 The apparatus may have a fixed quarter wave plate to, convert linear polarised radiation into circular polarised radiation before it is received by the first body.
Preferably angle of inclination of the first body is twice the angle of inclination of the second body.
Linear scans may also be achieved by using a rotatable reflector and an optical wedge, wherein the wedge includes refractive materials. The wedge and the reflector are arranged so that their conical scan patterns are the same, but in opposite directions, to produce a linear scan pattern. To achieve this, the wedge and the reflector are arranged to counter-rotate about generally parallel axes, and the reflector is inclined to its axis of rotation, as are the faces of the wedge.
With such an arrangement, a beam passes through the wedge, is reflected by the reflector and passes back through the wedge.
Preferably, the axes of rotation of the wedge and the reflector are coincident, and the median plane of the-wedge is preferably generally perpendicular to the axis of rotation.
Accordingly, in one aspect, the present invention provides a scanning apparatus having a rotatable reflector and a rotatable optical wedge including refractive materials, wherein the wedge and the reflector are arranged to counter-rotate about generally parallel axes, the reflector and the two faces of the wedge being inclined to their respective axes of rotation, such that in use a beam passes through the wedge, is reflected by the reflector and passes back through the wedge to provide a linear scan.
In another aspect, the present invention provides a method of producing a linear scan including the steps of rotating a reflector and an optical wedge in opposite directions to each other, but around generally parallel axes of rotation, the reflector and the two faces of the optical wedge being inclined to the reflector's axis of rotation and the wedge's respective axis of rotation respectively, and directing a beam so that it passes through the optical wedge, is reflected by the reflector back to the optical wedge and passes through the optical wedge to provide a linear scan.
The wedge may be wholly of refractive material, such as silica, but preferably has refractive plates supported on a refractive core. Refractive material, such as sulphur, may be sandwiched between the plates and the core.
Brief Description of the Drawings Embodiments of the invention will now be described in detail, by way of example only, and with reference to the following drawings, in which;
Fig. 1 shows an apparatus according to a first embodiment of the invention;
6a Fig. 2 shows in detail a rotating unit according to an embodiment of the invention;
Fig. 3 shows the path of the beam through the apparatus shown in Fig. 1 and Fig.2;
Fig. 4 shows an apparatus according to a further embodiment of the invention;
Fig. 5 shows an apparatus according to an embodiment of the invention arranged in transmission.
Fig. 6 shows an apparatus according to a further embodiment of the invention;
Fig. 7 shows the wedge of Fig. 6 in detail.
Preferably angle of inclination of the first body is twice the angle of inclination of the second body.
Linear scans may also be achieved by using a rotatable reflector and an optical wedge, wherein the wedge includes refractive materials. The wedge and the reflector are arranged so that their conical scan patterns are the same, but in opposite directions, to produce a linear scan pattern. To achieve this, the wedge and the reflector are arranged to counter-rotate about generally parallel axes, and the reflector is inclined to its axis of rotation, as are the faces of the wedge.
With such an arrangement, a beam passes through the wedge, is reflected by the reflector and passes back through the wedge.
Preferably, the axes of rotation of the wedge and the reflector are coincident, and the median plane of the-wedge is preferably generally perpendicular to the axis of rotation.
Accordingly, in one aspect, the present invention provides a scanning apparatus having a rotatable reflector and a rotatable optical wedge including refractive materials, wherein the wedge and the reflector are arranged to counter-rotate about generally parallel axes, the reflector and the two faces of the wedge being inclined to their respective axes of rotation, such that in use a beam passes through the wedge, is reflected by the reflector and passes back through the wedge to provide a linear scan.
In another aspect, the present invention provides a method of producing a linear scan including the steps of rotating a reflector and an optical wedge in opposite directions to each other, but around generally parallel axes of rotation, the reflector and the two faces of the optical wedge being inclined to the reflector's axis of rotation and the wedge's respective axis of rotation respectively, and directing a beam so that it passes through the optical wedge, is reflected by the reflector back to the optical wedge and passes through the optical wedge to provide a linear scan.
The wedge may be wholly of refractive material, such as silica, but preferably has refractive plates supported on a refractive core. Refractive material, such as sulphur, may be sandwiched between the plates and the core.
Brief Description of the Drawings Embodiments of the invention will now be described in detail, by way of example only, and with reference to the following drawings, in which;
Fig. 1 shows an apparatus according to a first embodiment of the invention;
6a Fig. 2 shows in detail a rotating unit according to an embodiment of the invention;
Fig. 3 shows the path of the beam through the apparatus shown in Fig. 1 and Fig.2;
Fig. 4 shows an apparatus according to a further embodiment of the invention;
Fig. 5 shows an apparatus according to an embodiment of the invention arranged in transmission.
Fig. 6 shows an apparatus according to a further embodiment of the invention;
Fig. 7 shows the wedge of Fig. 6 in detail.
Detailed Description Referring first to Fig. 1 a rotating mirror 1 is inclined at around 11 and a rotating unit 3, (shown in more detail in Fig. 2) which includes a linear polariser inclined at an angle of around 22 . A fixed quarter wave plate 5 is located in front of the rotating unit 3 to convert a linearly polarised beam to a circularly polarised beam.
Fig. 2 shows the rotating unit 3 in detail. This comprises an inclined linear polariser 10 positioned between two quarter wave plates 13 and 15. The quarter wave plates in this embodiment have fast axes of +450, though other directions are possible.
A linearly polarised beam is converted by the fixed quarter wave plate 5 to a right circularly polarised beam In this embodiment, the incident beam is horizontally polarised and the fixed quarter wave plate 5, which has a fast axis at +450 produces right-handed circularly polarised beam. Though other directions are possible, for example, left circularly polarised beam may alternatively be used).
Referring to Fig.3, the right circularly polarised beam passes through the first quarter wave plate 13 of rotating unit 3 which converts the beam to linear polarised. The beam then passes through the polariser 10 and through the second quarter wave plate-15 of'hhe rotating unit, where it is converted to circular polarised light. The beam then reaches the rotating mirror 1, which rotates in the opposite direction from rotating unit 3 but at the same speed, and the beam is reflected from the counter-rotating mirror 1.
The beam then passes back to the rotating unit 3 where it passes through the quarter wave plate 15. This time the light is reflected at the inclined polariser 10, because the plane of polarisation has been rotated through 90 when reflected at the rotating mirror 1 and transmitted by the quarter wave plate 15. The beam then passes to the counter rotating mirror 1 where it is reflected again, the handedness of the circularly polarised radiation undergoing a further change, and passes back through the rotating unit 3, this time passing through the linear polariser 10.
In isolation, the rotating unit 3 and the counter rotating mirror 1 produce conical scans, but in this tandem arrangement, with the rotations at the same speed and in opposite directions. Parts of the conical scans are effectively cancelled out to produce a linear scan.
This cancellation is virtually complete if the inclination of the inclined polariser 10 is twice that of the counter-rotating mirror 1.
Fig. 2 shows the rotating unit 3 in detail. This comprises an inclined linear polariser 10 positioned between two quarter wave plates 13 and 15. The quarter wave plates in this embodiment have fast axes of +450, though other directions are possible.
A linearly polarised beam is converted by the fixed quarter wave plate 5 to a right circularly polarised beam In this embodiment, the incident beam is horizontally polarised and the fixed quarter wave plate 5, which has a fast axis at +450 produces right-handed circularly polarised beam. Though other directions are possible, for example, left circularly polarised beam may alternatively be used).
Referring to Fig.3, the right circularly polarised beam passes through the first quarter wave plate 13 of rotating unit 3 which converts the beam to linear polarised. The beam then passes through the polariser 10 and through the second quarter wave plate-15 of'hhe rotating unit, where it is converted to circular polarised light. The beam then reaches the rotating mirror 1, which rotates in the opposite direction from rotating unit 3 but at the same speed, and the beam is reflected from the counter-rotating mirror 1.
The beam then passes back to the rotating unit 3 where it passes through the quarter wave plate 15. This time the light is reflected at the inclined polariser 10, because the plane of polarisation has been rotated through 90 when reflected at the rotating mirror 1 and transmitted by the quarter wave plate 15. The beam then passes to the counter rotating mirror 1 where it is reflected again, the handedness of the circularly polarised radiation undergoing a further change, and passes back through the rotating unit 3, this time passing through the linear polariser 10.
In isolation, the rotating unit 3 and the counter rotating mirror 1 produce conical scans, but in this tandem arrangement, with the rotations at the same speed and in opposite directions. Parts of the conical scans are effectively cancelled out to produce a linear scan.
This cancellation is virtually complete if the inclination of the inclined polariser 10 is twice that of the counter-rotating mirror 1.
Fig. 4 shows an alternative embodiment in which the rotating unit 20 consists of a quarter wave 23 plate and a linear polariser 21. The apparatus also has a Faraday rotator 25, which rotates the plane of polarization by 45 .
In the embodiment shown in Fig.4, the fixed quarter wave plate 5 converts a linearly polarised beam in to a circularly polarised beam. This circularly polarised beam is received by the rotating unit 20 and is converted into a linear beam by the quarter wave plate 23. The beam then passes through the linear polariser 21 and is then received by the Faraday rotator 25 which rotates the plane of the polarisation of the incident beam by 45 .
This beam is then incident at the rotating mirror 1 where it is reflected.
The beam passes back through the Faraday rotator 25 where it undergoes a further rotation of 45 in its plane of polarisation.
The beam is now polarised at right angles to the transmission axis of the inclined polariser 21 of the rotation unit 3. The polarises 21 therefore reflects the incident beam in a conical scan pattern. This reflected beam now passes through the Faraday rotator 25 again and the plane of polarisation is rotated through 45 . The beam is then reflected at the mirror 1, and passes through the Faraday rotator, the plane of polarization being rotated through 45 so that the beam is then able to pass through the inclined polariser 21 and then through the quarter wave plate 23 of the rotating unit 20.
In this way, there are two reflections at the rotating mirror and one at the inclined polariser 21, which is positioned at twice the angle of the rotating mirror It is also possible for two rotating units similar to that described in Fig. 1 to be used in series. This arrangement is shown in Fig. 5. The second unit 40 rotates about its axis with the same speed, but in the opposite direction from the first unit 30, and has a Faraday rotator between the quarter wave plate and the polariser. In this embodiment, it is not necessary to have a rotating mirror, because the polariser in the second rotating unit 40 can act as a mirror. The beam passes through the first rotating unit 30 as described for the first embodiment. The beam then passes to the second rotating unit 40 and is reflected from the inclined polarizer of the second unit.
The reflection at the inclined polariser of the second unit rotates the polarization of the beam through 90 , so that when the beam passes back to the first polarizing unit, it is reflected by the inclined polariser (and the polarization is rotated through 90 ).
This time when the beam reaches the second rotating unit 40 it passes through the inclined polariser and via a second quarter wave plate 5a which is fixed.
In an alternative embodiment shown in Fig. 6, the rotating unit is a rotating wedge 41 which rotates in the opposite direction from, and at the same speed as, the rotating mirror 1. The rotating wedge 1 is mounted on a drive shaft 42, and a gear box 43 and a motor 44 are used to control the speed and direction.
Fig. 7 shows the wedge 41 of this embodiment in more detail. The wedge 41 has a sulphur layer 46 sandwiched between two silica plates 47a and 47b, which are coated with anti-reflective PTFE layers 49a and 49b. The rotation of the wedge 41 is further balanced by balance weights 45a and 45b.
At microwave frequencies sulphur has a refractive index of 1.89 which is close to that of silica (1.94).
The silica plates are angled to produce a wedge which will deviate a beam through an angle given by:
6 = 2 Sin (n Sin a/2) - a at the condition of the minimum deviation, where a is the apex angle of the wedge. For small deviations, this approximates to:
0 = (n-i) a =
where n is the refractive index of the wedge.
The anti-reflective layer should have a refractive index which is the square root of the refractive index of the silica and have an optical thickness of ?./4 where X is the wavelength of the radiation. PTFE is therefore an appropriate material for the anti-reflective layer, as it has a refractive index of 1.44 which approximates to the square root of the refractive index of silica (1.89).
Its thickness should be 1.39 mm for radiation having a wavelength of 8mm (i.e. 35GHz). Alternative materials and thicknesses can be selected by the person skilled in the art. For example, it may be possible to achieve a suitably refractive wedge using a body of silica material, thus omitting the sulphur.
A beam incident on the arrangement of Figs. 6 and 7 passes twice through the wedge 46 as it is reflected by the rotating mirror 1.
In the embodiment shown in Fig.4, the fixed quarter wave plate 5 converts a linearly polarised beam in to a circularly polarised beam. This circularly polarised beam is received by the rotating unit 20 and is converted into a linear beam by the quarter wave plate 23. The beam then passes through the linear polariser 21 and is then received by the Faraday rotator 25 which rotates the plane of the polarisation of the incident beam by 45 .
This beam is then incident at the rotating mirror 1 where it is reflected.
The beam passes back through the Faraday rotator 25 where it undergoes a further rotation of 45 in its plane of polarisation.
The beam is now polarised at right angles to the transmission axis of the inclined polariser 21 of the rotation unit 3. The polarises 21 therefore reflects the incident beam in a conical scan pattern. This reflected beam now passes through the Faraday rotator 25 again and the plane of polarisation is rotated through 45 . The beam is then reflected at the mirror 1, and passes through the Faraday rotator, the plane of polarization being rotated through 45 so that the beam is then able to pass through the inclined polariser 21 and then through the quarter wave plate 23 of the rotating unit 20.
In this way, there are two reflections at the rotating mirror and one at the inclined polariser 21, which is positioned at twice the angle of the rotating mirror It is also possible for two rotating units similar to that described in Fig. 1 to be used in series. This arrangement is shown in Fig. 5. The second unit 40 rotates about its axis with the same speed, but in the opposite direction from the first unit 30, and has a Faraday rotator between the quarter wave plate and the polariser. In this embodiment, it is not necessary to have a rotating mirror, because the polariser in the second rotating unit 40 can act as a mirror. The beam passes through the first rotating unit 30 as described for the first embodiment. The beam then passes to the second rotating unit 40 and is reflected from the inclined polarizer of the second unit.
The reflection at the inclined polariser of the second unit rotates the polarization of the beam through 90 , so that when the beam passes back to the first polarizing unit, it is reflected by the inclined polariser (and the polarization is rotated through 90 ).
This time when the beam reaches the second rotating unit 40 it passes through the inclined polariser and via a second quarter wave plate 5a which is fixed.
In an alternative embodiment shown in Fig. 6, the rotating unit is a rotating wedge 41 which rotates in the opposite direction from, and at the same speed as, the rotating mirror 1. The rotating wedge 1 is mounted on a drive shaft 42, and a gear box 43 and a motor 44 are used to control the speed and direction.
Fig. 7 shows the wedge 41 of this embodiment in more detail. The wedge 41 has a sulphur layer 46 sandwiched between two silica plates 47a and 47b, which are coated with anti-reflective PTFE layers 49a and 49b. The rotation of the wedge 41 is further balanced by balance weights 45a and 45b.
At microwave frequencies sulphur has a refractive index of 1.89 which is close to that of silica (1.94).
The silica plates are angled to produce a wedge which will deviate a beam through an angle given by:
6 = 2 Sin (n Sin a/2) - a at the condition of the minimum deviation, where a is the apex angle of the wedge. For small deviations, this approximates to:
0 = (n-i) a =
where n is the refractive index of the wedge.
The anti-reflective layer should have a refractive index which is the square root of the refractive index of the silica and have an optical thickness of ?./4 where X is the wavelength of the radiation. PTFE is therefore an appropriate material for the anti-reflective layer, as it has a refractive index of 1.44 which approximates to the square root of the refractive index of silica (1.89).
Its thickness should be 1.39 mm for radiation having a wavelength of 8mm (i.e. 35GHz). Alternative materials and thicknesses can be selected by the person skilled in the art. For example, it may be possible to achieve a suitably refractive wedge using a body of silica material, thus omitting the sulphur.
A beam incident on the arrangement of Figs. 6 and 7 passes twice through the wedge 46 as it is reflected by the rotating mirror 1.
Claims (5)
1. A scanning apparatus having a rotatable reflector and a rotatable optical wedge including refractive materials, wherein the wedge and the reflector are arranged to counter-rotate about generally parallel axes, the reflector and two faces of the wedge being inclined to their respective axes of rotation, such that in use a beam passes through the wedge, is reflected by the reflector and passes back through the wedge to provide a linear scan.
2. A scanning apparatus according to claim 1 wherein the axes of rotation of the wedge and the reflector are coincident.
3. A scanning apparatus according to claim 1 wherein a median plane of the wedge is generally perpendicular to the axis of the wedge's rotation.
4. A scanning apparatus according to any one of claims 1 to 2 wherein the wedge comprises refractive plates supported on a refractive core.
5. A method of producing a linear scan including the steps of rotating a reflector and an optical wedge in opposite directions to each other, but around generally parallel axes of rotation, the reflector and two faces of the optical wedge being inclined to the reflector's axis of rotation and the wedge's respective axis of rotation respectively, and directing a beam so that it passes through the optical wedge, is reflected by the reflector back to the optical wedge and passes through the optical wedge to provide a linear scan.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0117750.0 | 2001-07-20 | ||
| GBGB0117750.0A GB0117750D0 (en) | 2001-07-20 | 2001-07-20 | Scanning apparatus |
| CA2454194A CA2454194C (en) | 2001-07-20 | 2002-07-22 | Scanning apparatus |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2454194A Division CA2454194C (en) | 2001-07-20 | 2002-07-22 | Scanning apparatus |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2689280A1 CA2689280A1 (en) | 2003-01-30 |
| CA2689280C true CA2689280C (en) | 2011-07-12 |
Family
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2454194A Expired - Fee Related CA2454194C (en) | 2001-07-20 | 2002-07-22 | Scanning apparatus |
| CA2689280A Expired - Fee Related CA2689280C (en) | 2001-07-20 | 2002-07-22 | Scanning apparatus |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2454194A Expired - Fee Related CA2454194C (en) | 2001-07-20 | 2002-07-22 | Scanning apparatus |
Country Status (9)
| Country | Link |
|---|---|
| US (2) | US7038821B2 (en) |
| EP (1) | EP1410093B1 (en) |
| JP (1) | JP4170901B2 (en) |
| AT (1) | ATE285082T1 (en) |
| CA (2) | CA2454194C (en) |
| DE (1) | DE60202297T2 (en) |
| ES (1) | ES2233837T3 (en) |
| GB (1) | GB0117750D0 (en) |
| WO (1) | WO2003009048A1 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7142340B2 (en) | 2003-10-31 | 2006-11-28 | Hewlett-Packard Development Company, L.P. | Optical scanner apparatuses and optical scanning methods |
| EP1730576A2 (en) * | 2004-03-30 | 2006-12-13 | Farran Technology Limited | Scanning apparatus |
| EP1733270A2 (en) * | 2004-03-31 | 2006-12-20 | Koninklijke Philips Electronics N.V. | Projection system with scanning device |
| US7719773B2 (en) * | 2007-11-12 | 2010-05-18 | Ricoh Company, Ltd. | Zoom lens unit and imaging apparatus |
| WO2009126546A1 (en) * | 2008-04-07 | 2009-10-15 | University Of Florida Research Foundation, Inc. | High-precision monolithic optical assemblies and methods for fabrication and alignment thereof |
| US20110040605A1 (en) * | 2009-08-17 | 2011-02-17 | Geoffrey Prentix Evertz | Electronic voting system |
| ES2387484B1 (en) | 2009-10-15 | 2013-08-02 | Alfa Imaging S.A. | SWEEP MULTIESPECTRAL SYSTEM. |
| US20200081129A1 (en) * | 2018-09-10 | 2020-03-12 | Veoneer Us, Inc. | Detection system for a vehicle |
| US12092278B2 (en) | 2022-10-07 | 2024-09-17 | Magna Electronics, Llc | Generating a spotlight |
| US12228653B2 (en) | 2022-10-07 | 2025-02-18 | Magna Electronics, Llc | Integrating a sensing system into headlight optics |
| US12202396B1 (en) | 2023-12-19 | 2025-01-21 | Magna Electronics, Llc | Line-scan-gated imaging for LiDAR headlight |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1282675B (en) * | 1967-03-21 | 1968-11-14 | Eltro G M B H & Co Ges Fuer St | Device for the sinusoidal deflection of a bundle of rays by means of a mirror |
| US3881802A (en) * | 1974-04-18 | 1975-05-06 | Bendix Corp | Wedge-prism optical scanner |
| US4042933A (en) * | 1976-03-19 | 1977-08-16 | The United States Of America As Represented By The Secretary Of The Navy | Antenna line scan system for helicopter wire detection |
| US4168126A (en) * | 1977-07-05 | 1979-09-18 | Altman Associates, Inc. | Electro-optical measuring system using precision light translator |
| US4544228A (en) * | 1982-09-14 | 1985-10-01 | Spectra-Physics, Inc. | Scanning method using a rotating prism |
| US4871904A (en) * | 1987-12-28 | 1989-10-03 | Symbol Technologies, Inc. | Multidirectional optical scanner |
| EP0633541A1 (en) * | 1993-07-06 | 1995-01-11 | Opticon Sensors Europe B.V. | Scanning device |
| GB9707654D0 (en) * | 1997-04-16 | 1997-06-04 | Secr Defence | Scanning apparatus |
-
2001
- 2001-07-20 GB GBGB0117750.0A patent/GB0117750D0/en not_active Ceased
-
2002
- 2002-07-22 CA CA2454194A patent/CA2454194C/en not_active Expired - Fee Related
- 2002-07-22 DE DE60202297T patent/DE60202297T2/en not_active Expired - Lifetime
- 2002-07-22 US US10/484,173 patent/US7038821B2/en not_active Expired - Fee Related
- 2002-07-22 EP EP02745666A patent/EP1410093B1/en not_active Expired - Lifetime
- 2002-07-22 AT AT02745666T patent/ATE285082T1/en not_active IP Right Cessation
- 2002-07-22 JP JP2003514327A patent/JP4170901B2/en not_active Expired - Fee Related
- 2002-07-22 CA CA2689280A patent/CA2689280C/en not_active Expired - Fee Related
- 2002-07-22 ES ES02745666T patent/ES2233837T3/en not_active Expired - Lifetime
- 2002-07-22 WO PCT/GB2002/003349 patent/WO2003009048A1/en not_active Ceased
-
2006
- 2006-03-06 US US11/367,554 patent/US7106482B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1410093A1 (en) | 2004-04-21 |
| US7038821B2 (en) | 2006-05-02 |
| US7106482B2 (en) | 2006-09-12 |
| US20040240019A1 (en) | 2004-12-02 |
| DE60202297D1 (en) | 2005-01-20 |
| US20060146387A1 (en) | 2006-07-06 |
| CA2454194A1 (en) | 2003-01-30 |
| ATE285082T1 (en) | 2005-01-15 |
| CA2689280A1 (en) | 2003-01-30 |
| CA2454194C (en) | 2010-12-07 |
| EP1410093B1 (en) | 2004-12-15 |
| JP4170901B2 (en) | 2008-10-22 |
| WO2003009048A1 (en) | 2003-01-30 |
| DE60202297T2 (en) | 2005-12-15 |
| ES2233837T3 (en) | 2005-06-16 |
| JP2004536342A (en) | 2004-12-02 |
| GB0117750D0 (en) | 2001-09-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20170724 |