JP2607672B2 - Aperture mechanism - Google Patents
Aperture mechanismInfo
- Publication number
- JP2607672B2 JP2607672B2 JP1063096A JP6309689A JP2607672B2 JP 2607672 B2 JP2607672 B2 JP 2607672B2 JP 1063096 A JP1063096 A JP 1063096A JP 6309689 A JP6309689 A JP 6309689A JP 2607672 B2 JP2607672 B2 JP 2607672B2
- Authority
- JP
- Japan
- Prior art keywords
- diaphragm
- aperture
- effective diameter
- blades
- blade group
- 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
- Diaphragms For Cameras (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明は、カメラ用レンズの絞り機構に関するもので
ある。Description: TECHNICAL FIELD The present invention relates to a diaphragm mechanism for a camera lens.
[従来の技術] 第4図乃至第6図は従来のカメラ用レンズの絞り機構
を示している。[Prior Art] FIGS. 4 to 6 show a conventional aperture mechanism of a camera lens.
これは、複数の絞り羽根50の各片面側に固定ダボと称
せられる回転軸51を植設すると共に、他面側に回転ダボ
と称せられるピン52を植設し、蜂の巣と称せられる絞り
羽根容器(光軸を中心とした円形の開口54が設けられて
いる)53に穿設された絞り羽根50と同数の各軸孔55に、
各回転軸51を嵌合するようにして複数の絞り羽根50を収
容し、また風車と称せられるカム部材(光軸中心とした
円形の開口57が設けられている)56に形成された絞り羽
根50と同数の各カム溝58に、各ピン52が嵌合している。This is achieved by implanting a rotating shaft 51 called a fixed dowel on one side of each of the plurality of diaphragm blades 50, and planting a pin 52 called a rotating dowel on the other side, and forming a diaphragm blade container called a honeycomb. (A circular opening 54 is provided around the optical axis.) In each of the shaft holes 55 of the same number as the aperture blades 50 formed in 53,
A plurality of diaphragm blades 50 are accommodated so as to fit the respective rotating shafts 51, and diaphragm blades formed on a cam member 56 (having a circular opening 57 centered on the optical axis) called a windmill Each pin 52 is fitted in the same number of cam grooves 58 as 50.
そして、絞り羽根容器53とカム部材56とを光軸を中心
にして相対回転させることにより、各ピン52が各カム溝
58にならて移動し、絞り羽根容器53とカム部材56との間
に収容されている複数の絞り羽根50が各回転軸51を中心
として傾き、傾いた絞り羽根50の重なり合いによって、
その中央部に形成される絞り有効径の面積を変化させ、
光量の調節を行なうようにしている。By rotating the diaphragm blade container 53 and the cam member 56 relative to each other about the optical axis, each pin 52 is
Moving along 58, the plurality of diaphragm blades 50 housed between the diaphragm blade container 53 and the cam member 56 are tilted around each rotation shaft 51, and by the overlapping of the tilted diaphragm blades 50,
Change the area of the aperture effective diameter formed in the center part,
The amount of light is adjusted.
[発明が解決しようとする課題] ところで、このような従来の絞り機構においては、絞
り込んでいっても絞り有効径以外の部分から光が漏れな
いように、絞り羽根50の外形形状が第6図に示すように
なっている。これは、有効径を決定する機能と、有効径
以外の光線漏れを防ぐ機能との両方の機能を持たせたこ
とにより、絞り羽根の大きさをある程度以上小さくする
ことができなかった。[Problem to be Solved by the Invention] In such a conventional aperture mechanism, the outer shape of the aperture blade 50 is changed so that light does not leak from a portion other than the aperture effective diameter even when the aperture is stopped down as shown in FIG. It is shown as follows. This is because the function of determining the effective diameter and the function of preventing light leakage other than the effective diameter are both provided, so that the size of the aperture blade cannot be reduced to some extent or more.
そのため、絞り羽根容器及びカム部材も小型化でき
ず、絞り機構を内蔵するレンズ鏡筒の筐体の外径も小さ
くできず、レンズ鏡筒の小型・軽量化を阻む原因の一つ
になっていた。Therefore, the aperture blade container and the cam member cannot be reduced in size, and the outer diameter of the housing of the lens barrel having the built-in aperture mechanism cannot be reduced, which is one of the factors that hinder the reduction in size and weight of the lens barrel. Was.
本発明の目的は、絞り有効径以外からの光り漏れを発
生させることなく絞り機構全体の外径を小型化できる絞
り機構を提供するものである。SUMMARY OF THE INVENTION An object of the present invention is to provide a diaphragm mechanism capable of reducing the outer diameter of the entire diaphragm mechanism without causing light leakage from other than the effective diameter of the diaphragm.
[課題を解決するための手段] 本発明の目的を達成するための代表的な絞り機構は、
複数の第1の絞り羽根からなる第1の絞り羽根群と、複
数の第2の絞り羽根からなる第2の絞り羽根群とを光軸
方向に沿って前後に離隔配置した絞り機構であって、前
記第1の絞り羽根群は移動することで絞り有効径を決定
し、前記第2の絞り羽根群は移動することで前記絞り有
効径以外からの漏光を防ぐために前記第1の絞り羽根群
が互いに重なり合わない部分を覆うことを特徴とするも
のである。[Means for Solving the Problems] A typical aperture mechanism for achieving the object of the present invention is:
A diaphragm mechanism in which a first diaphragm blade group composed of a plurality of first diaphragm blades and a second diaphragm blade group composed of a plurality of second diaphragm blades are spaced apart back and forth along the optical axis direction. The first aperture blade group moves to determine an aperture effective diameter, and the second aperture blade group moves to prevent light leakage from other than the aperture effective diameter. Cover portions that do not overlap with each other.
[作 用] 上記の如く構成した絞り機構は、絞り有効径を決定す
る第1の絞り羽根群とは別に、第1の絞り羽群の絞り有
効径以外の互いに重なり合わない部分を覆う第2の絞り
羽根群を設けたので、絞り機構全体の小型化が図れる。[Operation] The diaphragm mechanism configured as described above separates the first diaphragm blade group that determines the diaphragm effective diameter and covers the non-overlapping portions other than the diaphragm effective diameter of the first diaphragm blade group. Since the aperture blade group is provided, the size of the entire aperture mechanism can be reduced.
[実施例] 以下本発明を図面に示す実施例に基づいて詳細に説明
する。EXAMPLES Hereinafter, the present invention will be described in detail based on examples shown in the drawings.
第1図は本発明による絞り機構の一実施例を示す縦断
面図、第2図は第1図のA矢視図、第3図は第1図のB
矢視図を示している。FIG. 1 is a longitudinal sectional view showing an embodiment of a diaphragm mechanism according to the present invention, FIG. 2 is a view as viewed from the direction of arrow A in FIG. 1, and FIG.
FIG.
本実施例は、絞り有効径を決定するための複数の第1
絞り羽根1からなる有効径(D1)決定用絞り羽根群と、
該有効径決定用絞り羽根群において有効径以外からの漏
光を防ぐための複数の第2の絞り羽根6からなる漏光防
止用絞り羽根群から構成している。In the present embodiment, a plurality of first
A group of aperture blades for determining an effective diameter (D 1 ) comprising the aperture blade 1;
The effective diameter determining aperture blade group includes a plurality of second aperture blades 6 for preventing light leakage from other than the effective diameter.
有効径決定用絞り羽根群を構成する複数(本実施例で
は6枚)の第1の絞り羽根1と、漏光防止用絞り羽根群
を構成する複数(本実施例では6枚)の第2の絞り羽根
6とを、中央に円形の開口5aを有する共通蜂の巣5の表
裏両面側に夫々配置し、第3図に示すように、共通蜂の
巣5は表面側に配置される第1の絞り羽根1は、幅が略
一定の弧状に形成され、その一端側に植設された回転中
心となる固定ダボ3が共通蜂の巣5に穿設された有効径
決定用絞り羽根群用の第1軸孔(不図示)に回転可能に
嵌合し、さらに第1の絞り羽根1に植設された回転ダボ
4が中央に開口2aが形成された第1風車2のカム溝2bに
摺動可能に嵌合し、第1風車2を光軸を中心として共通
蜂の巣5に対し回転させことにより、複数の第1の絞り
羽根1が固定ダボ3を中心にして傾き、その重ね合わせ
により有効径が決定される。A plurality of (six in this embodiment) first diaphragm blades 1 constituting an effective diameter determining diaphragm blade group, and a plurality of (six in this embodiment) second diaphragm blades constituting a light leakage prevention diaphragm blade group. The aperture blades 6 are arranged on both front and back sides of a common honeycomb 5 having a circular opening 5a at the center, and as shown in FIG. 3, the common honeycomb 5 is disposed on a front surface side of the first aperture blade 1 Is formed in an arc shape having a substantially constant width, and a fixed dowel 3 serving as a rotation center planted at one end thereof is bored in a common beehive 5 to form a first shaft hole for an effective diameter determining diaphragm blade group ( (Not shown), and a rotary dowel 4 implanted in the first diaphragm blade 1 is slidably fitted in a cam groove 2b of a first windmill 2 having an opening 2a formed in the center. Then, by rotating the first windmill 2 with respect to the common honeycomb 5 about the optical axis, the plurality of first aperture blades 1 move the fixed dowel 3 Slope in the heart, the effective diameter is determined by the superposition.
ところで、第6図の従来の絞り機構では、絞り羽根の
基端部側の幅を広くし、絞りを絞り込むと他の絞り羽根
の先端部側と重なり合うことで、他の絞り羽根間での漏
光を防ぐようにしているが、本実施例では絞り羽根1の
幅を略一定とした弧状に形成して絞り機構の外径の小径
化を図っているため、有効径決定用の第1の絞り羽根1
を絞り込むと、他の第1の絞り羽根1との間に重なり合
わない部分が生じ、そこから漏光することになる。その
ため本実施例では、有効径決定用絞り羽根群の駆動に応
じ、複数の絞り羽根1にて形成される絞り有効径以外の
重なり合わない部分を、漏光防止用絞り羽根群にて覆う
ようにしており、第2図に示すように、共通蜂の巣5の
裏面側に配置される第2の絞り羽根6は、幅が略一定の
弧状に形成されていて、その一端側に植設した固定ダボ
8を、共通蜂の巣5に前記第1軸孔と同心円上に穿設し
た第2軸孔(不図示)に回転可能に嵌合し、さらに第2
の絞り羽根6に植設された回転ダボ9が中央に開口7aが
形成された第2風車7のカム溝7bに摺動可能に嵌合し、
第2風車7を光軸を中心として共通蜂の巣5に対し回転
させことにより、複数の第2の絞り羽根6が固定ダボ8
を中心にして傾き、有効径決定用絞り羽根群の絞り羽根
1間に形成される絞り有効径以外の空所を覆う。By the way, in the conventional diaphragm mechanism shown in FIG. 6, the width at the base end side of the diaphragm blade is widened, and when the diaphragm is stopped down, it overlaps with the distal end side of the other diaphragm blade, so that light leakage between other diaphragm blades is caused. In this embodiment, the outer diameter of the aperture mechanism is reduced by forming the aperture blade 1 in an arc shape having a substantially constant width, so that the first aperture for determining the effective diameter is reduced. Feather 1
When the aperture is stopped down, a portion that does not overlap with the other first aperture blades 1 occurs, and light leaks therefrom. For this reason, in this embodiment, in accordance with the driving of the effective diameter determining aperture blade group, non-overlapping portions other than the aperture effective diameter formed by the plurality of aperture blades 1 are covered with the light leakage prevention aperture blade group. As shown in FIG. 2, the second diaphragm blade 6 disposed on the back side of the common honeycomb 5 is formed in an arc shape having a substantially constant width, and is fixed to the fixed dowel planted at one end thereof. 8 is rotatably fitted in a second shaft hole (not shown) formed concentrically with the first shaft hole in the common honeycomb 5.
A rotary dowel 9 implanted in the aperture blade 6 of the second windmill 7 is slidably fitted in a cam groove 7b of a second windmill 7 having an opening 7a formed in the center.
By rotating the second windmill 7 with respect to the common honeycomb 5 about the optical axis, the plurality of second aperture blades 6 are fixed to the fixed dowels 8.
And covers the space other than the aperture effective diameter formed between the aperture blades 1 of the aperture blade group for determining the effective diameter.
この第2の絞り羽根6は、第1の絞り羽根1よりも短
く形成されていて、有効径決定用絞り羽根群により形成
される絞り有効径に影響を与えないようにしている。The second diaphragm blade 6 is formed shorter than the first diaphragm blade 1 so as not to affect the diaphragm effective diameter formed by the effective diameter determining diaphragm blade group.
なお本実施例では、第1風車2及び第2風車7の外縁
部の同位置に係合凹片2c,7cを設け、不図示の絞り駆動
レバーをこれらの係合凹片2c,7cに係合させ、該絞り駆
動レバーの駆動により第1風車2及び第2風車7を同時
に回転させ、有効径決定用絞り羽根群と漏光防止用絞り
羽根群とを同時の駆動させるようにしている。In the present embodiment, engaging recesses 2c, 7c are provided at the same positions on the outer edges of the first windmill 2 and the second windmill 7, and an aperture drive lever (not shown) is engaged with these engaging recesses 2c, 7c. The first and second windmills 2 and 7 are simultaneously rotated by driving the aperture drive lever, and the aperture blade group for determining the effective diameter and the aperture blade group for preventing light leakage are simultaneously driven.
したがって本実施例によれば、絞り有効径を決定する
ための第1の絞り羽根1の基端部側の幅を狭くすること
ができるので、その分絞り機構全体の外径を小径化で
き、また第1の絞り羽根の形状から生じる漏光を第2の
絞り羽根6にて防ぐことができて所定の絞り効果を得る
ことができる。Therefore, according to the present embodiment, the width at the base end side of the first diaphragm blade 1 for determining the diaphragm effective diameter can be reduced, so that the outer diameter of the entire diaphragm mechanism can be reduced accordingly. Further, light leakage caused by the shape of the first diaphragm blade can be prevented by the second diaphragm blade 6, and a predetermined diaphragm effect can be obtained.
[発明の効果] 以上説明してきたように、本発明によれば、第1の絞
り羽根群と第2の絞り羽根群との役割を分け、第1の絞
り羽根群で形成される絞り有効径以外に形成される漏光
部分を第2の絞り羽根群で覆う構成とすることで、第1
の絞り羽根群の絞り羽根を小さくすることができ、絞り
機構全体外径を小さくできて、絞り機構の小型化が図れ
るといった結果が得られ、絞り機構を装備する例えばカ
メラのレンズ鏡筒の小型軽量化に寄与できる。[Effects of the Invention] As described above, according to the present invention, the roles of the first aperture blade group and the second aperture blade group are divided, and the aperture effective diameter formed by the first aperture blade group. By covering the light leakage part formed in other than the second diaphragm blade group,
The aperture blades of the group of aperture blades can be made smaller, the overall diameter of the aperture mechanism can be reduced, and the aperture mechanism can be downsized. It can contribute to weight reduction.
第1図は本発明による絞り機構の一実施例を示す縦断面
図、第2図は第1図のA矢視図、第3図は第1図のB矢
視図、第4図は従来の絞り機構の縦断面図、第5図は第
4図のD矢視図、第6図は第4図の絞り羽根を示す図で
ある。 1:第1絞り羽根(複数の第1絞り羽根で第1の絞り羽根
群を構成する) 2:第1風車 2a:開口、2b:カム溝、2c:係合凹片 3:固定ダボ、4:回転ダボ 5:共通蜂の巣、5a:開口 6:第2絞り羽根(複数の第2絞り羽根で第2の絞り羽根
群を構成する) 7:第2風車 7a:開口、7b:カム溝、7c:係合凹片 8:固定ダボ 9:回転ダボ D1:絞り有効径FIG. 1 is a longitudinal sectional view showing one embodiment of a diaphragm mechanism according to the present invention, FIG. 2 is a view as seen from an arrow A in FIG. 1, FIG. 3 is a view as seen from an arrow B in FIG. 1, and FIG. FIG. 5 is a view taken in the direction of arrow D in FIG. 4, and FIG. 6 is a view showing the diaphragm blades in FIG. 1: First diaphragm blade (a plurality of first diaphragm blades constitutes a first diaphragm blade group) 2: First windmill 2a: Opening, 2b: Cam groove, 2c: Engagement piece 3: Fixed dowel, 4 : Rotating dowel 5: Common honeycomb, 5a: Opening 6: Second diaphragm blade (a plurality of second diaphragm blades constitute a second diaphragm blade group) 7: Second windmill 7a: Opening, 7b: Cam groove, 7c : Engagement concave piece 8: Fixed dowel 9: Rotating dowel D 1 : Effective aperture
Claims (1)
羽根群と、複数の第2の絞り羽根からなる第2の絞り羽
根群とを光軸方向に沿って前後に離隔配置した絞り機構
であって、前記第1の絞り羽根群は移動することで絞り
有効径を決定し、前記第2の絞り羽根群は移動すること
で前記絞り有効径以外からの漏光を防ぐために前記第1
の絞り羽根群が互いに重なり合わない部分を覆うことを
特徴とする絞り機構。A first group of aperture blades comprising a plurality of first aperture blades and a second group of aperture blades comprising a plurality of second aperture blades are spaced apart back and forth along the optical axis direction. A diaphragm mechanism, wherein the first diaphragm blade group moves to determine a diaphragm effective diameter, and the second diaphragm blade group moves to prevent light leakage from other than the diaphragm effective diameter. 1
A diaphragm mechanism that covers portions where the diaphragm blades do not overlap with each other.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1063096A JP2607672B2 (en) | 1989-03-15 | 1989-03-15 | Aperture mechanism |
| US07/440,645 US5072249A (en) | 1988-11-28 | 1989-11-24 | Diaphragm device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1063096A JP2607672B2 (en) | 1989-03-15 | 1989-03-15 | Aperture mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02242239A JPH02242239A (en) | 1990-09-26 |
| JP2607672B2 true JP2607672B2 (en) | 1997-05-07 |
Family
ID=13219429
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1063096A Expired - Fee Related JP2607672B2 (en) | 1988-11-28 | 1989-03-15 | Aperture mechanism |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2607672B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008203601A (en) * | 2007-02-21 | 2008-09-04 | Olympus Corp | Iris diaphragm mechanism |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5630295A (en) * | 1979-08-21 | 1981-03-26 | Oobayashi Seisakusho:Kk | Stop device for x-ray |
| JPS56138727A (en) * | 1980-03-31 | 1981-10-29 | Matsushita Electric Works Ltd | Iris shutter |
-
1989
- 1989-03-15 JP JP1063096A patent/JP2607672B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH02242239A (en) | 1990-09-26 |
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