The present invention relates to a blade driving device used in an imaging device, or the like.
Blade driving devices are used to change the state of an opening by driving one or more blade members that advance into the opening, and are used in a variety up optical units, such as camera units, for diaphragms, shutters, diaphragm-shutters, filters, and the like.
As a conventional blade driving device, the electromagnetic driven-type, which uses a magnet and a coil as a driving source, typically is well known, and linear actuators, known as voice coil motors (VCMs) are used in order to reduce the size and thickness.
Moreover, in conventional blade driving devices, those that are provided with mechanisms wherein a plurality of blade members are linked by a lever member that is borne at a center portion are well known, and a structure has been proposed wherein a magnet is installed on the lever member when a linear actuator, as described above, is used as a driving source (referencing Japanese Unexamined Patent Application Publication 2001-281724).
With the prior art described above, there is a problem in that the structure is such that, when the magnet of the linear actuator is equipped on the lever member, the magnet is contained within the width of the lever member, making it impossible to use a magnet of an adequately large volume, and thus impossible to produce enough propulsion to drive the blade member smoothly. Moreover, while one may consider provision of a magnet with a large volume that extends beyond the width of the lever member, it would not be possible to attach the magnet stably to the lever member, and thus there would be a problem in that it would not be possible to secure balanced operation of the lever member, nor smooth movement.
Moreover, when the magnet is installed at a place that is away from the rotational center of the lever member, as in the prior art, when a large (heavy) magnet is installed, the moment of inertia when the lever member rotates around the rotary shaft will be large, and thus the overshoot, when controlling the position of the lever member with the linear actuator, will be large. Because of this, there is a problem in that it is difficult to control the position with good responsiveness. In particular, when controlling the size of an aperture, there is a problem in that it is not possible to achieve the desired diaphragm value (AV value or F value) with good sensitivity.
The present invention is proposed in order to handle problems such as these. That is, objects of the present invention are to reduce the thickness of a blade driving device, to enable driving of a blade member with adequate propulsion while achieving smooth movement with balanced operation of the lever member in a mechanism wherein a plurality of blade members are linked by a lever member, and to enable positional control with good responsiveness.
In order to solve such a problem, the lens driving device according to the present invention is provided with the following structures:
A blade driving device, comprising: a base member; a pair of blade members supported on the base member; a lever member, with respective end portions connected to the blade members, wherein the bearing portion, provided in the center, is borne on a rotary shaft that is provided on the base member; and a linear actuator for causing the lever member to rotate around the rotary shaft, wherein: in the lever member, a containing portion, for containing the magnet of the linear actuator, is provided integrally with the bearing portion.
Examples according to the present invention will be explained below in reference to the drawings. Identical reference symbols in the different drawings below indicate positions with identical functions, and redundant explanations in the various drawings are omitted as appropriate.
As illustrated in
The blade members 2 and 3 are provided with openings 2A and 3A, where the area of opening varies depending on the amount of overlap of the openings 2A and 3A, and can move to arbitrary positions from the fully open state to the fully closed state or from the fully closed state to the fully open state. The blade members 2 and 3 are provided with guide holes (elongated holes) 2B and 3B for engaging a guiding portion 10B the base member 10. The guide holes 2B and 3B are provided extending along the direction of movement of the blade members 2 and 3. The shapes of the blade members 2 and 3 are not limited thereto. In a form wherein the base member 10 has an opening and the blade members 2 and 3 advance into this opening, the blade members 2 and 3 have the curved portions, or the like, that define the opening.
The lever member 4 comprises a bearing portion 4A in a center portion thereof, and comprises respective connecting portions 4B and 4C at both end portions thereof. The bearing portion 4A of the lever member 4 is borne on the rotary shaft 10C, where the connecting portion 4B is connected to the connecting hole 2C of the blade member 2, and the connecting portion 4C is connected to the connecting hole 3C of the blade member 3.
A linear actuator 5 comprises a magnet 5A and a coil (flat coil) 5B. The magnet 5A of the linear actuator 5 is attached to the lever member 4, and the coil 5B of the linear actuator 5 is attached to the base member 10. The linear actuator 5 produces a propulsive force through an electric current in the coil 5B, causing the lever member 4 to rotate around the rotary shaft 10C, to cause the pair of blade members 2 and 3 to slide in mutually opposing directions, to adjust the amount of overlap of the openings 2A and 3A.
The lever member 4 comprises a containing portion 4D for containing the magnet 5A. The containing portion 4D is equipped integrally with the bearing portion 4A, where, in the example in the figure, a rectangular containing portion 4D is provided on the side of the bearing portion, and are one side of the rotary shaft 10C.
Such a blade driving device 1, by providing the bearing portion 4A of the lever member 4 integrally with the containing portion 4D for the magnet 5A, makes it possible to hold the magnet with stability, without disrupting the balanced operation of the lever member 4, even when the containing portion 4D is made larger in order to contain a magnet 5A that has a large volume, enabling the lever member 4 to be operated smoothly.
Moreover, even when magnet 5A of a large volume is installed in the containing portion 4D, the magnet 5A, which is a heavy object, can be held in that the vicinity of the rotary shaft 10C, which can keep the moment of inertia small when the lever member 4 rotates around the rotary shaft 10C. This enables control with good responsiveness by keeping the amount of overshoot small when performing positional control of the blade members 2 and 3 through causing the lever member 4 to rotate under servo control of the linear actuator 5.
Moreover, when producing a large propulsive force through increasing the volume of the magnet 5A, this can keep the moment of inertia of the magnet 5A, of a given volume, small when compared to the case of storing the magnet 5A in a containing portion 4D that is rectangular, as described above. This enables control with good responsiveness by keeping the amount of overshoot even smaller when performing positional control of the blade members 2 and 3 through causing the lever member 4 to rotate under servo control of the linear actuator 5.
Moreover, when producing a large propulsive force through increasing the volume of the magnet 5A when the magnet 5A is held in the containing portion 4D2, this can keep the moment of inertia of the magnet 5A, of a given volume, even smaller when compared to a containing portion 4D that is rectangular or a containing portion 4D1 that is fan-shaped, as described above. This enables control with good responsiveness by keeping the amount of overshoot even smaller when performing positional control of the blade members 2 and 3 through causing the lever member 4 to rotate under servo control of the linear actuator 5.
A more specific embodiment will be explained below.
In the example in the figure, the base member 10 is provided with a lens frame containing portion 11, which is recessed into a U-shape, at the outer peripheral edge. The base member 10, as described above, comprises: a supporting face 10A, a guiding portion 10B, and a rotary shaft 10C, and also a coil supporting portion 10D for supporting the coil 5B, a bonding part 10E for bonding the base member 10 and the cover member 7, and so forth.
The blade supporting units 6A and 6B are plate-shaped members for forming a blade chamber 6 for containing the thin blade members 2 and 3, where the opening 6X is provided at a position that corresponds to the openings 2A and 3A of the blade members 2 and 3. Moreover, the blade supporting units 6A and 6B are provided with holes 6Y into which the guiding portion 10B of the base member 10 is inserted, and also with holes 6Z in the range of movement of the connecting portions 4B and 4C of the lever member 4, corresponding to the connecting holes 2C and 3C of the blade members 2 and 3.
The cover member 7 comprises a recessed portion 7X corresponding to the lens frame containing portion 11 of the base member 10, and a bonding part 7Y, for bonding to the bonding part 10E of the base member 10. A yoke 9, for positioning the magnet 5A, is attached to the cover member 7.
The magnet 5A, which is contained in the containing portion 4D of the lever member 4, is magnetized toward the left and the right of the rotary shaft 10C, and magnetized in the direction of thickness of the base member 10. Additionally, the coil 5B is positioned so as to be perpendicular to the lines of magnetic force of the magnet 5A, to structure a linear actuator 5 for causing the lever member 4 to rotate around the rotary shaft 10C.
When the linear actuator 5 is driven to cause the lever member 4 to rotate, the blade members 2 and 3 that are connected to the connecting portions 4B and 4C of the lever member 4 will move along the protruding portions 6C of the blade supporting units 6A and 6B, to adjust the area of opening within the openings 6X through the state of overlap of the openings 2A and 3A of the blade members 2 and 3 and the openings 6X of the blade supporting units 6A and 6B.
Note that the yoke 9 is disposed on the cover member 7 so as to face the vicinity of the magnet 5A, to hold the non-powered position of the lever member 4 in a position wherein the magnet 5A is attracted to the yoke 9.
With such a blade driving device 1, the magnet 5A of the linear actuator 5 is contained in a containing portion 4D that is integrated with the bearing portion 4A of the lever member 4, thus enabling installation on the lever member 4 in a stabilized state, even when the magnet 5A is provided with a large volume. Through this, this enables the blade members 2 and 3 to be moved with a high propulsive force, while the magnet 5A is installed in a stabilized state.
Moreover, the magnet 5A that is equipped on the lever member 4 being positioned in the vicinity of the rotary shaft 10C makes it possible to keep the moment of inertia relatively small, even when the weight of the magnet 5A is large. This enables highly responsive control through suppressing overshoot when rotating the lever member 4, through positional control by the linear actuator 5, to position the blade members 2 and 3 at an arbitrary position between the fully open position in the fully closed position. This enables, for example, diaphragm control with high sensitivity.
While embodiments according to the present invention were described in detail above, referencing the drawings, the specific structures thereof are not limited to these embodiments, but rather design variations within a range that does not deviate from the spirit and intent of the present invention are also included in the present invention. Moreover, insofar as there are no particular contradictions or problems in purposes or structures, or the like, the technologies of the various embodiments described above may be used together in combination.
Number | Date | Country | Kind |
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2016-241068 | Dec 2016 | JP | national |
This is a U.S. National Phase Application under 35 U.S.C. § 371 of International Patent Application No. PCT/JP2017/042234, filed Nov. 24, 2017, which claims priority of Japanese Patent Application No. 2016-241068, filed Dec. 13, 2016. The entire contents of which are hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/JP2017/042234 | 11/24/2017 | WO | 00 |