Optical system for flying spot scanning apparatus

Abstract: Disclosed is an optical system useful for a flying spot scanning apparatus. The optical system includes a laser tube (1), an optoelectronic integrated circuit (3) which divides a laser beam (B1, B2) into a plurality of beams (B3) and individually modulates respective beams, a focusing lens (7) forming a beam waist on the optical system thereof, deflection mirror (8) reciprocatingly deflecting the beams to scan a recording medium (18), and a second-surface concave mirror (15) receiving the beams thereon. The recording medium is disposed optically behind the concave mirror, the recording medium being fed in a predetermined direction (A) while the recording spot scans the recording medium.

Description: BACKGROUND OF THE INVENTION The present invention relates generally to an improvement of an apparatus for recording an image on a recording medium, and particularly to an optical system for use in a so-called flying spot scanning system (hereinafter referred to as "flying spot scanner"). There have been several proposals for improvement of the flying spot scanner. One of them is shown in the United States Patent US-A-4,034,408, wherein a laser beam emitted from a light source is modulated by an optical modulator in response to image signals, which is then deflected by a multifaced rotating polygon and is condensed by an f -theta lens which is provided immediately after the polygon, whereby a recording spot of the laser beam scans a recording medium which is fed in a direction perpendicular to the direction in which the recording spot runs, to record a desired image on the recording medium. Another proposal is shown in a publication "KOGAKU" (Japanese Journal of Optics) Vol. 6, No. 2, pp. 67-74, entitled "The Correcting Method of Beam Scanning Distortion Using the Parabolic Mirror". In order to correct a distortion on a recording plane, a laser beam emitted from a light source is first expanded by a beam expander, which is then deflected by a galvanometer mirror and is in turn reflected by a parabolic mirror which is directed toward a recording medium, whereby the recording spot of the laser beam scans the recording medium, to record a desired image thereon. Recently it has been demanded to record a desired image onto a recording medium of relatively large size, e.g. of approximately 500 mm to 1000 mm in an effective recording width, with high resolution, which requires the diameter of the recording spot to be fine, e.g. up to approximately 3 µm to 10 µm at half-width power thereof. However, conventional apparatuses cannot meet such demands satisfactorily. The reasons are discussed hereinbelow. Generally, the more the recording medium becomes large in size, the more undesirable abberations caused will become also large. The diameter of a recording spot W o can be expressed by: W o = k ·λ· F where k is a constant, λ is a wave length and F is an F-number. In an apparatus shown in the United States Patent US-A-4,034,408, when the diameter of the recording spot W o is intended to reduced, e.g. up to approximately 3 µm to 10 µm, an f -theta lens having a small F-number has to be prepared, as long as both k and λ are kept constant. It will be impractical, though not impossible in a theoretical sense, to obtain such an f -theta lens as meeting the conditions required. It may, of course, be possible to correct the abberations by using only a paraxial region of the f -theta lens, but, in this case the apparatus as a whole will become undesirably large in size because it makes the optical path considerably long, which is apparently disadvantageous. Furthermore, should an f -theta lens be available as can enable a recording spot to be reduced up to approximately 3 µm to 10 µm, it will be required to prepare a specific polygon having a large reflecting surfaces enough to scan a whole recording width of a recording medium. Such multi-faced rotating polygon will have a diameter of 500 mm and have to be controlled so as to ensure the recording spot to scan a recording medium at a predetermined rotation rate, which will apparently be impracticable and costly. In the case of an apparatus shown in the publication "KOGAKU", abberations, particularly coma and astigmatism, cannot be corrected by means of a parabolic mirror. Accordingly, the diameter of the recording spot cannot be reduced up to approximately 3 µm to 10 µm. SUMMARY OF THE INVENTION In view of the foregoing, it is a principal object of the present invention to provide an improved optical system particularly useful for a so-called flying spot scanning apparatus. It is another object to provide an optical system which ensures recording on a relatively large size recording medium, e.g. of 500 mm to 1000 mm in width, with a fine recording spot, e.g. approximately of 3 µm to 10 µm in half-width thereof. It is a further object to provide an optical system which can make a flying spot scanning apparatus compact as a whole. It is a further object to provide an optical system which can correct undesirable abberations. The aforementioned objects are accomplished by the present invention as defined by the appended claims. The present invention has the following useful advantages: A recording spot focused on a recording medium can be extensively reduced up to 3 µm to 10 µm, whereby resolution power can be increased, while the effective scanning length can be made to be long to the extent of 500 mm to 1000 mm. Curvature of field can be effectively reduced, by which a substantially flat image plane can be produced. A deflection mirror can be efficiently minimized, whereby the scanning speed can be sufficiently increased. Undesirable abberations, particularly coma and astigmatism, can be efficiently corrected, whereby a fine recording spot can be produced. Furthermore, the flying spot scanning apparatus can be made compact as a whole. Other novel features and advantages of the present invention will become apparent in the course of the following detailed description taken together with the accompanying drawings, which are directed only to the understanding of the present invention and not to the restriction of the scope of the invention. BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a schematic perspective view of a flying spot scanning apparatus according to a first embodiment embodying the present invention; Figure 2 is a schematic partial side view of Figure 1; Figure 3 is a schematic partial plane view of Figure 1; Figure 4 is a side view of Figure 3; Figures 5-(A) to 5-(C) are respectively a spot diagram according to the first embodiment of the present invention; Figure 6 is a schematic partial plane view of a second embodiment embodying the present invention; Figures 7-(A) to 7-(C) are respectively a spot diagram according to the second embodiment of the present invention; Figure 8 is a schematic partial plane view of a third embodiment embodying the present invention; Figure 9 is a side view of Figure 8; Figures 10-(A) to 10-(C) are respectively a spot diagram according to the third embodiment of the present invention; Figure 11 is a schematic partial plane view of a fourth embodiment embodying the present invention; Figure 12 is a side view of Figure 11; Figures 13-(A) to 13-(C) are respectively a spot diagram according to the fourth embodiment of the invention; Figure 14 is a perspective view of a part of the flying spot scanning system; Figures 15-(A) to 15-(C) are respectively a spot diagram according to a fifth embodiment of the invention; and Figure 16 is a side view of a part of the optical system according to a sixth embodiment. DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS Referring to Figures 1 to 4, a laser beam B₁ emitted from a light source 1 first passes through a condenser lens 2, by which the laser beam B₁ is condensed and a beam B₂ emerges therefrom. The beam B₂ then enters an opto-electronic integrated circuit (hereinafter referred to as OEIC) 3, in which the beam is divided into twenty-one beams, which are in turn individually modulated thereby, to emerge therefrom. These beams B₃ are transmitted through a field lens 4 to impinge upon a folding mirror 5. In Figure 1 the laser beams impinging upon the folding mirror 5 are denoted by B₄ , and those reflected thereby are denoted by B₅ . The laser beams B₅ then pass through a collimater lens 6, by which the beams are corrected to be well-collimated beams B₆ . These beams B₆ are received by a focusing lens 7, by which the beams are focused on a recording surface S of a recording medium 18 through optical elements including a deflection mirror 8, a beam directing device 11 and a concave mirror 15. The deflection mirror 8 comprises a rectangular mirror and is controlled by a galvanometer 10 coaxially mounted on a drive shaft thereof. A pulse encoder 9 is also mounted on the drive shaft, which is used for outputting clock pulses for use in reading out image signals from a memory. The laser beams B₇ impinging upon the deflection mirror 8 are deflected to the concave mirror 15 and they traverse the reflecting surface of the concave mirror through the beam directing device 11. The beam directing device 11 comprises a pair of triangular prisms having a thin metal film on a border plane therebetween, which allows only the laser beams B₈ to transmit therethrough. The beams B₉ reflected from the concave mirror 15 are directed by the thin metal film of the directing device 11 to the recording surface S of the recording medium 18. The recording medium 18 is fed in a direction A at a predetermined velocity, while the laser beams scan the recording surface S in a direction perpendicular to the direction A . In this embodiment the flying spot scanning apparatus is so arranged that an effective scanning length be approximately 1000 mm, and that the diameter of the recording spots on the recording surface be 5.5 µm at half-width power. The source of the laser beam 1 comprises e.g. an Ar-laser tube, from which Ar-laser of a wave length of 488 nm is emitted. The OEIC 3 comprises an assembly of both an optical waveguide device for dividing a laser beam into a plurality of (e.g. twenty-one) beams and an optical modulator provided at the exit of the waveguide device for individually modulating the respective laser beams in response to image signals. The OEIC 3 may, of course, be replaced with a conventional optical beam splitter and an optical modulator which are separately installed. The collimater lens 6 is positioned, by a distance corresponding to the focal length of the collimater lens, away from the exit of the OEIC 3, so that the respective twenty-one beams are collimated to enter the incident surface of the focusing lens 7, whereby the respective laser beams B₆ emerged therefrom are overlapped each other on the incident surface of the focusing lens 7. The focusing lens 7 comprises a so-called objective lens which makes parallel incident rays focus upon a point, which comprises a single optical unit including two lenses. The focal length and effective aperture of the focusing lens 7 is designed so that the diameter of the respective laser beams comes into 5.5 µm at half-width power on the recording surface S . The lens data thereof are listed hereinbelow. The intensity of the respective laser beams B₆ represents a normal distribution on the incident surface of the focusing lens 7, while the diameter of the respective beams B₇ emerged therefrom is defined to 182 mm, and thus the peripheral intensity of the respective beams will come into e⁻² times (i.e. 13 %) of that at the center thereof. The field lens 4 is provided for adjusting the laser beams so that the respective principal rays of the laser beams B₇ be consistent with each other at a point on the rotating axis Z of the deflection mirror 8, whereby the height of the deflection mirror 8 can be lowered efficiently. The angles formed by respective adjacent principal rays of the beams B₆ are approximately the same (i.e. they are approximately 0.63 seconds), and on this condition the twenty-one recording spots of 5.5 µm in diameter are aligned at intervals of 5.5 µm in the direction of the arrow A on the recording plane S . In this embodiment the rotating axis Z of the deflection mirror 8 is positioned at a distance of 227.782 mm from the exit surface of the focusing lens 7. The deflection mirror 8 is also arranged so that the rotating axis Z thereof is positioned approximately at the focal point of the concave mirror 15. The deflection mirror 8 is reciprocatingly rotated by the galvanometer 10 up to a predetermined rotation angle ϑ₁ , by which the laser beams B₇ are deflected to traverse the reflecting surface of the concave mirror 15. In this embodiment the deflecting surface of the mirror 8 is designed to be 220 mm in width and 180 mm in height, and its effective rotation angle ϑ₁ is adjusted to be ±9 degrees, thence the scanning angle ϑ₂ of the beams deflected by the deflection mirror 8 comes into ±18 degrees. The concave mirror 15 comprises a second-surface spherical mirror, which includes an optical glass plate forming a first-surface of the mirror and an aliminized or silvered reflecting surface coated on the back surface thereof. By way of compactness, the concave mirror 15 is formed into a spherical band extending in the direction of scanning. Conditions of the concave mirror 15 are listed hereinbelow. The radius r₁ of the first-surface M₁ : -3626.372 mm The radius r₂ of the second-surface M₂ : -3807.674 mm The distance between the first- and second-surfaces at the center thereof: 40 mm The refractive index of the glass plate: 1.52224 The focal length of the concave mirror 15: 1936.057 mm The ratio of r₁ to r₂ comes into 0.952, as can be understood from the above conditions. In this embodiment the deflection mirror 8 is positioned at a distance of 1512.336 mm from the center of the first-surface of the concave mirror. The distance V given by subtracting the distance between the focusing lens 7 and the deflection mirror 8 from the back focus of the focusing lens 7, comes into 1881.922 mm, thence the focal length f M can be expressed by: f M = 1.03 V The ratio of f M to V comes into 1.03, and the ratio of the distance b between the deflection mirror and the concave mirror to the distance V , comes into 0.795. In such a case where the distance V is approximately equal to the focal length f M of the concave mirror 15, an image surface formed by the scanning spots will come into flat. As can be understood, the glass plate of the second-surface mirror 15 functions as a thick meniscus lens having a considerably long focal length, which eliminates coma and astigmatism caused by the inconsistency between the radius center of the concave reflecting surface M₂ and the rotating axis Z of the deflection mirror 8. The beam directing device 11 is disposed between the deflection mirror 8 and the concave mirror 15, which allows only the beams B₈ to transmit therethrough and directs the beams B₉ to the recording surface. In this embodiment the beam directing device 11 is formed into a square pole, extending in the scanning direction, formed by a pair of triangular prisms cemented each other, which has a thickness of 45 mm in both the horizontal and vertical directions and whose refractive index is 1.52224. The beam directing device is positioned so that the exit surface of the beams B₈ be at a distance of 47.953 mm from the center of the first surface M₁ of the concave mirror, and that the exit surface of the beams B₉ be at a distance of 199.042 mm from the recording surface (i.e. image surface) S . As arranged is the flying spot scanning apparatus as mentioned above, in accordance with the rotating angle ϑ₁ of the deflection mirror 8 (i.e. ±9 degrees), the effective scanning length will come into 1000 mm on the image plane S , and the diameter of the recording spots will come into 5.5 µm at half-width power. Figures 5-(A) to 5-(C) respectively show a spot diagram, on the image plane, of the 21th beam among the row of twenty-one beams, which are in a case where the image height is of 0 mm, 350 mm and 500 mm, respectively. The frame size of these diagrams is of 10 µm square, from which it will be apparently understood that the lateral abberation of the recording spot falls within approximately ±4 µm at most. According to the embodiment as mentioned above, the Strehl definition can attain more than 0.90 on every scanning spot aligned on the recording surface. Interval variations between respective adjacent scanning spots, which are aligned in the direction A , are no more than 2.2 % (i.e. 0.12 µm) even at the image height of 500 mm. SECOND EMBODIMENT Referring to Figures 1, 6 and 7, in this embodiment the basic structure of the system is substantially the same as shown in the first embodiment, except the beam directing device 11. Respective optical elements are so designated that the effective scanning length be 420 mm, and that the diameter of the scanning spots be 3 µm at half-width power. The focusing lens 7 comprises a single optical unit including three lenses, whose lens data are shown hereinbelow. The deflection mirror 8 is disposed at a distance of 167 mm from the focusing lens 7 and of 811.723 mm from the concave mirror 15, so that the distance V given by subtracting the distance between the focusing lens and the deflection mirror 8 from the back focus of the focusing lens 7 comes into 1008.812 mm. The rotating angle ϑ₁ is designed to be ±7 degrees in this embodiment. The concave mirror 15 comprises a second-surface mirror similar to one in the first embodiment, conditions of which are listed hereinbelow. The radius r₁ of the first-surface M₁ : -1995.230 mm The radius r₂ of the second-surface M₂ : - 2019.7780 mm The distance between the first- and second-surfaces at the center thereof: 30 mm The refractive index of the glass plate: 1.52224 The focal length of the concave mirror 15: 1003.275 mm The ratio of r₁ to r₂ comes into 0.988, as can be understood from the above conditions. From the aforementioned conditions, it will be understood that the focal length f M can be expressed by: f M = 0.995 V The ratio of f M to V comes into 0.995, and the ratio of the distance b between the deflection mirror and the concave mirror to V comes into 0.81. Furthermore, in this embodiment a so-called half-mirror made of a thin film is employed instead of the beam directing device 11, which functions substantially in the same manner as the beam directing device 11 employed in the first embodiment. The half-mirror is positioned at a distance of 50 mm from the concave mirror and of 81.188 mm from the recording surface S . In this embodiment, in accordance with the rotating angle ϑ₁ = ±7 degrees, the effective scanning length comes into 420 mm on the recording surface S , and the diameter of the recording spots comes into 3 µm at half-width power thereon. Figures 7-(A) to 7-(C) respectively show a spot diagram, on the image plane, of the 21th beam among the row of twenty-one beams, which are in a case where the image height is of 0 mm, 147 mm and 210 mm, respectively. The frame size of these diagrams is of 10 µm square, from which it will be apparently understood that the lateral abberation of the recording spot falls within approximately ±2 µm at most. The Strehl definition can attain more than 0.96 on every scanning spot aligned on the image plane. Interval variations between respective adjacent scanning spots, which are aligned in the direction A , are no more than 1.4 % even at the image height of 210 mm. THIRD EMBODIMENT Referring to Figures 1, 8 and 9, in this embodiment the basic structure of the system is also substantially the same as shown in the first and second embodiments, except the beam directing device 11 or the half-mirror. The laser beams B₈ deflected by the deflection mirror 8 is directed directly to the concave mirror 15 by eliminating the beam directing device 11 in the first embodiment and the half-mirror in the second embodiment, whereby the intensity of the respective beams is secured not to be reduced. As can be clearly seen in Figure 9, the laser beams B₈ are somewhat inclined to strike the concave mirror 15. Respective optical elements are so designed that the effective scanning length be 560 mm, and that the diameter of the scanning spots be 5.6 µm at half-width power. The focusing lens 7 comprises a single optical unit including two lenses, whose lens data are shown hereinbelow. The deflection mirror 8 is positioned at a distance of 225 mm from the focusing lens and of 990.845 mm from the concave mirror 15, so that the distance V given by subtracting the distance between the focusing lens and the deflection mirror 8 from the back focus of the focusing lens 7, comes into 1166.645 mm. The rotating axis of the deflection mirror 8 is inclined by 8 degrees relative to a vertical axis, whose rotating angle ϑ₁ is designed to be ±8 degrees. The concave mirror 15 comprises a second-surface mirror similar to ones in the first and second embodiments, conditions of which are listed hereinbelow. The radius r₁ of the first-surface M₁ : -2291.604 mm The radius r₂ of the second-surface M₂ : -2311.511 mm The distance between the first- and second-surfaces at the center thereof: 20 mm The refractive index of the glass plate: 1.52224 The focal length of the concave mirror 15: 1152.281 mm The ratio of r₁ to r₂ comes into 0.991, as can be understood from the above conditions. From the aforementioned conditions, it will be understood that the focal length f M can be expressed by: f M = 0.988 V The ratio of f M to V comes into 0.988, and the ratio of the distance b between the deflection mirror and the concave mirror to V comes into 0.85. Because of the inclination of the beams B₈ , the optical axis of the concave mirror 15 (i.e. normal axis of the reflecting surfaces of M₁ and M₂ ) is inclined by 7.373 degrees relative to the optical axis along the beams B₇ . In this embodiment a total reflection mirror 11 b is installed and is positioned at a distance of 80 mm from the concave mirror 15 and of 50 mm from the recording surface S . The reflection mirror 11 b is so arranged that the normal axis thereof forms an angle of 45.18 degrees relative to the recording surface. In this embodiment, in accordance with the rotating angle ϑ₁ = ±8 degrees, the effective scanning length comes into 560 mm on the recording surface S , and the diameter of the recording spots comes into 5.6 µm at half-width power thereon. Figures 10-(A) to 10-(C) respectively show a spot diagram, on the image plane, of the 21th beam among the row of twenty-one beams, which are in a case where the image height is of 0 mm, 200 mm and 280 mm, respectively. The frame size of these diagrams is of 10 µm square, from which it will be apparently understood that the lateral abberation of the recording spot falls within approximately ±3.5 µm at most. According to this embodiment, the Strehl definition can attain more than 0,90 on every scanning spot aligned on the recording surface. Interval variations between respective adjacent scanning spots, which are aligned in the direction A , are no more than 1.9% even at the image height of 280 mm. FOURTH EMBODIMENT Referring to Figures 1, 11 and 12, in this embodiment the basic structure of the system is also substantially the same as shown in the precedent embodiments, except the concave mirror 15. A meniscus lens having a considerably long focal length 15 a and a concave first-surface mirror 15 b are installed instead of the concave second-surface mirror 15 employed in the precedent embodiments. In this embodiment respective optical elements are so designed that the effective scanning length be 550 mm, and that the diameter of the scanning spots be 8.4 µm at half-width power. The focusing lens 7 comprises a single optical unit including two lenses, whose lens data are show hereinbelow. The deflection mirror 8 is positioned at a distance of 144.083 mm from the focusing lens 7 and of 663.320 mm from the meniscus lens 15 a , so that the distance V given by subtracting the distance between the focusing lens 7 and deflection mirror 8 from the back focus of the focusing lens, comes into 1100 mm. The rotating angle ϑ₁ is designed to be ±8 degrees. The meniscus lens 15 a is positioned at a distance of 274.396 mm from the concave mirror 15 b , whose concave surface is directed toward the deflection mirror 8. By way of compactness, the meniscus lens 15 a is formed into a spherical band similarly to the precedent embodiments. Conditions of the meniscus lens 15 a is shown hereinbelow. The ratio of the distance V to the focal length f N of the meniscus lens comes into -0.01. The concave mirror 15 b comprises a parabolic first-surface mirror with a thin metal coating on the front incident surface of the mirror, whose focal length f M is 1096.694 mm. The focal length f M can also be expressed by: f M = 0.997 V The ratio of f M to V comes into 0.997, and the ratio of the distance b between the deflection mirror and the concave mirror to V comes into 0.88. The concave mirror 15 b is disposed at a distance of 957.424 mm from the deflection mirror 8. A half-mirror 11 a is installed between the meniscus lens 15 a and the concave mirror 15 b for transmitting only the beams B₈ therethrough and directing the beams reflected by the concave mirror 15 b to the recording surface S . The half-mirror 11 a is made of a thin film as employed in the second embodiment, which is positioned at a distance of 50 mm from the concave mirror 15 b and of 89.225 mm from the recording surface. In this embodiment undesirable abberations, particularly coma and astigmatism caused by using the parabolic mirror 15 b , can effectively be corrected by means of the meniscus lens 15 a . Figures 13-(A) to 13-(C) respectively show a spot diagram, on the image plane, of the 21th beam among the row of twenty-one beams, which are in a case where the image height is of 0 mm, 200 mm and 275 mm, respectively. The frame size of these diagrams is of 20 µm square, from which it will be apparently be understood that the lateral abberation of the recording spot falls within approximately ±5 µm at most. The Strehl definition can attain more than 0.92 on every scanning spots aligned on the image plane. Interval variations between respective adjacent scanning spots, which are aligned in the direction A , are no more than 2.0 % even at the image height of 275 mm. FIFTH EMBODIMENT In this embodiment the basic structure of the system is also substantially the same as in the fourth embodiment. However, both the meniscus lens 15 a and the concave mirror 15 b shown in Figures 11 and 12 are formed into a parabolically-bent shape, as typically shown in Figure 14. In this case the word "parabolically-bent shape" depicts that a band of a plane mirror is bent so as to form a parabolic curve in a plan view. In other words, it has a curvature in the horizontal direction and has no curvature in the vertical direction. In this embodiment respective optical elements are so designed that the effective scanning length be 560 mm, and that the diameter of the scanning spots be 9.2 µm at half-width power. Both the focusing lens 7 and the deflection mirror 8 are the same designs and are positioned at the same positions as shown in the fourth embodiment. The distance V given by subtracting the distance between the focusing lens and the deflection mirror from the back focus of the focusing lens, comes into 1100 mm. The meniscus lens 15 a of the spherically-bent shape is positioned at a distance of 654.305 mm from the deflection mirror 8 and of 335.742 mm from the parabolically-bent shaped concave mirror, whose concave incident surface is directed toward the deflection mirror 8. Hereinbelow is shown the conditions of the meniscus lens 15 a . The ratio of the distance V to the focal length f N comes into less than 0.01. As mentioned above, the concave mirror 15 b is formed into a parabolically-bent shape, whose focal length f M is designed to be 1000 mm, thence this can be expressed by: f M = 0.91 V The ratio of f M to V comes into 0.91, and the ratio of the distance b between the deflection mirror and the concave mirror to V comes into 0.91. The half-mirror 11 a is positioned at a distance of 50 mm from the concave mirror 15 b and of 50 mm from the recording surface S . Figures 15-(A) to 15-(C) respectively show a spot diagram, on the image plane, of the 21th beam among the row of twenty-one beams, which are in a case where the image height is of 0 mm, 200 mm and 280 mm, respectively. The frame size of these diagrams is of 30 µm square, from which it will be apparently be understood that the lateral abberation of the recording spot falls within approximately ±7 µm at most. The Strehl definition can attain more than 0.90 on every scanning spots aligned on the image plane. Interval variations between respective adjacent scanning spots, which are aligned in the direction A , are no more than 0.026 % even at the image height of 275 mm. In comparison with the fourth embodiment, these will be apparently more excellent and ideal than those in the fourth embodiment. The reason of excellence in this embodiment is that the optical length between the deflection mirror and the recording surface is kept approximately constant independently of the rotating angle of the deflection mirror by using the parabolically-bent shaped mirror. In view of the aforementioned results, it will be apparently understood that the flying spot scanning apparatus according to the present invention has excellent optical characteristics and is approximately ideal for recording an image on a recording medium. In the aforementioned embodiments it will be apparent that the deflection mirror may be positioned at a position within the range of: 0.9 < f M / V < 1.05 where f M is a focal length of the concave mirror, and V is a distance given by subtracting the distance between the focusing lens and the deflection mirror from the back focal length of the focusing lens. The concave mirror may be disposed at a position within the range of: 0.75 < b / V < 0.95 where b is a distance between the deflection mirror and the concave mirror. In a case where the concave mirror comprises a second-surface mirror, the concave mirror may be designed so that the following formula be satisfied. 0.95 < r₁ / r₂ < 1.0 where r₁ is a radius of the first surface of the concave mirror, and r₂ is a radius of the second surface thereof. In a case where the concave mirror comprises a first-surface mirror, a meniscus lens to be disposed optically before the concave mirror may be designed so that the following formula be satisfied. | V / f N | < 0.02 where V is a distance given by subtracting a distance between the focusing lens and the deflection mirror from the back focal length of the focusing lens, and f N is a focal length of the meniscus lens. In the precedent embodiments the laser beams B₆ received by the focusing lens 7 are collimated by the collimater lens 6. However, it is not necessary to employ such collimater lens. The following is an embodiment where such collimater lens is not employed. SIXTH EMBODIMENT Referring to Figure 1 and 16, in this embodiment the basic structure of the system is substantially the same as shown in the precedent embodiments, except the field lens 4 and the collimater lens 6. By way of easiness of explanation, all optical elements employed in this embodiment are assumed to use ones shown in the first embodiment, though it is apparently applicable to incorporate this embodiment to any one of the precedent embodiments. The focusing lens 7 comprises a single optical unit including three lenses, whose lens data are shown hereinbelow. The focusing lens 7 is positioned at a distance of 2103.302 mm from the exit of the modulator 3. Assuming that a beam waist of the respective laser beams is formed at the exit of the modulator 3 and that the diameter of the beam waist is 5.5 µm at half-width power, another beam waist of 5.5 µm in diameter at half-width power will be formed, by the focusing lens, at a position of 2109.704 mm away from the exit surface of the focusing lens. It will be apparently understood that the position where the beam waist is formed by the focusing lens corresponds to the back focal length of the focusing lens 7 employed in the first embodiment. Accordingly, recording can be made substantially in the same manner as in the first embodiment, by disposing the deflection mirror 8 at a position of 227.782 mm away from the focusing lens.

Claims: An optical system for a flying spot scanning apparatus, comprising: a light source for emitting a light beam; optical modulator means for modulating said light beam; a focusing lens for forming a recording spot of the light beam on an optical axis thereof; deflection means disposed optically between the focusing lens and a recording surface for reciprocatingly deflecting the light beam to move the recording spot on the recording surface; and reflection means, disposed optically between the deflection means and the recording surface, having a focal length f M , the reflection means extending along a direction where the recording spot runs thereon, characterized in that the deflection means is disposed at a position where a distance V given by subtracting the distance between the focusing lens and the deflection means from the distance, along the optical path of the light beam, between the focusing lens and the recording spot formed by the focusing lens on the recording surface is approximately equal to the focal length f M , that the reflection means comprises a concave optical glass plate having a front surface and a back surface, and a concave reflection surface disposed optically behind the concave optical glass plate, the radius r1 of the front surface being approximately equal to the radius r2 of the back surface, and that the reflection means is disposed at such a position that the following formula is satisfied: 0.75 < b/V < 0.95 where b is the distance between the deflection means and the concave reflection surface. An optical system as set forth in claim 1, wherein the deflection means is positioned at a position where the following formula is satisfied: 0.9 < f M /V < 1.05. An optical system as set forth in claim 2, wherein the reflection means is a second-surface mirror comprising the concave optical glass plate whose back surface being coated by metal film. An optical system as set forth in claim 3, wherein the concave optical glass plate is so designated that the following formula is satisfied: 0.95 < r1/r2 < 1.0. An optical system as set forth in claim 2, wherein the reflection means comprises a meniscus lens having a focal length f N , and a first-surface mirror having a concave reflection surface. An optical system as set forth in claim 5, wherein the meniscus lens is so designated that the following formula is satisfied: V/f N < 0.02. An optical system as set forth in claim 4 or 6, wherein the reflection means is formed into a spherical band extending along a direction where the light beam is deflected by the deflection means. An optical system as set forth in claim 4 or 6, wherein the reflection means is formed into a parabolic band extending along a direction where the light beam is deflected by the deflection means. An optical system as set forth in claim 4 or 6, wherein the reflection means is formed into a parabolically-bent band extending along a direction where the light beam is deflected by the deflection means.

Inventors: KATSUYAMA MIKIZO C O DAINIPPON, NAGATA SHINICHI C O DAINIPPON, WAKIMOTO ZENJI C O DAINIPPON S, KATSUYAMA, MIKIZO C/O DAINIPPON SCREEN MFG. CO, LT, NAGATA, SHINICHI C/O DAINIPPON SCREEN MFG. CO, LTD, WAKIMOTO, ZENJI C/O DAINIPPON SCREEN MFG. CO, LTD.
Applicants: DAINIPPON SCREEN MFG, DAINIPPON SCREEN MFG. CO., LTD.
Application year: 1988
Main classification: H04N1
IPC codes: H04N1, G02B27