JPS58149030A - Light shielding blade for light controlling device - Google Patents
Light shielding blade for light controlling deviceInfo
- Publication number
- JPS58149030A JPS58149030A JP3133082A JP3133082A JPS58149030A JP S58149030 A JPS58149030 A JP S58149030A JP 3133082 A JP3133082 A JP 3133082A JP 3133082 A JP3133082 A JP 3133082A JP S58149030 A JPS58149030 A JP S58149030A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- blade
- layers
- small
- light
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B9/00—Exposure-making shutters; Diaphragms
- G03B9/08—Shutters
- G03B9/36—Sliding rigid plate
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Diaphragms For Cameras (AREA)
Abstract
Description
【発明の詳細な説明】
本角−は光5#礒砿用の遮光羽根すなわち、シャッター
、レンズ0績1.可動式1光板◆O改嵐に−する。DETAILED DESCRIPTION OF THE INVENTION This horn has a light shielding blade for light 5#, that is, a shutter, and a lens with a score of 0 and 1. Movable 1 light plate ◆ O Kai Arashi -.
上記の如龜迩光羽機は作−カme小さくし、かつ−軸重
充分に保ちながら、4遍に作#させることが4ましい。It is preferable for the above-mentioned light wing machine to operate four times, while keeping the rotational speed small and maintaining sufficient axle load.
そのためには−カー電化する必債がある。従来、この目
的でプラスチックヤチタンなどを!1ムの鋼板に誓えて
l用することや、薄板をさらに部分的に肉抜きすること
などが行なわれている。また、これらの羽根t−急速に
作動させた時に生ずる慣性による材料に働く応力は駆動
部に近いほど大暑いことから、駆msから離れるにした
がって、その厚さt−漸減させib、駆動部付近の厚さ
に比して他の部分の厚さを4くすることも提案されてい
る。To achieve this, there is a need to electrify cars. Conventionally, plastic Yachitan etc. were used for this purpose! Efforts are being made to use a 1mm thick steel plate or to partially thin out a thin plate. In addition, the stress exerted on the material due to inertia that occurs when these blades are operated rapidly is much hotter as they get closer to the drive part, so the thickness of the blades gradually decreases as they move away from the drive part. It has also been proposed to make the thickness of other parts 4 times larger than the thickness of .
しかしながら、これら従来0別根には次のような欠点が
めった。However, these conventional 0 separate roots often have the following drawbacks.
オず、単に比重の小さい材料に替えた4声においては、
強度が不足するか、ま九は@電化が不充分でめった。Ozu, in the case of four voices simply changing to materials with lower specific gravity,
Either the strength was insufficient, or the electrification in Maku was insufficient.
次に、−公的に肉抜き金した態様中駆動部から−れるに
したがって厚嘔t−漸減させ九羽械は、力■工に手間が
かかり製造コストも爾かった。Secondly, the nine-wing machine, in which the thickness was gradually reduced as it was removed from the drive section, was labor intensive and expensive to manufacture.
そこで、本発明は、これらの欠点1に解決し−くて、剛
性が69、襄1’lli容易な遮光羽根を提供すること
t−目的とする。SUMMARY OF THE INVENTION Therefore, it is an object of the present invention to provide a light-shielding blade that overcomes these drawbacks and has a rigidity of 69 mm and is easy to fold.
遮光羽根tmt化するには、薄くすることが縞−に考え
られるが、羽根の曲げ剛性を考えた場合、薄くするには
限界がある。り鵞υ、藩(すればする纜ど−げ剛性(=
1ヤング卓蔵X断面二仄モーメントI、 )が小さくな
るが、ヤング率Eは物質固有の値で変えることはできな
いので、曲げ剛性t−落さずに41!!激化t−図るに
は断面二次モーメント1.t−f&さすに櫃蓋化すれば
よい。ひとつの板t−考えた場合、その断面二次モーメ
ジ)I、t−賂さずに肉抜きして樋量化するには、中立
軸から通い部分1層去するよプも近i鄭分を除去した方
が断面二次モーメント!2の低下は少ない。In order to make the light-shielding blade TMT, it is conceivable to make it thinner, but when considering the bending rigidity of the blade, there is a limit to how thin it can be.り鵞υ、han
1 Young's Takuzo ! Intensification t - To calculate the moment of inertia 1. t-f & just make it into a box. If we consider one plate T, its cross-sectional quadratic mm) I, T- In order to reduce the thickness and increase the gutter volume without cutting, we should remove one layer of the continuous part from the neutral axis. The second moment of area is removed! The decrease in 2 is small.
そこで、本発明者らはクラツド材に着目して研究を進め
たIIa来、%に遮光羽根としては真一層及び−面層が
比弾性係数の高い材料からなシ、中間層が見かけ比重の
小さな材料からなるクラツド材が好ましいことを却)、
更に遮光羽根には駆一部材との結合位置付近から遠ざか
るに従いその傾度は低下しても44質的には差し支えな
いことを見い出し、本発明を成すに至った。Therefore, since IIa, the present inventors have focused their research on cladding materials, and found that as a light-shielding blade, the true and negative layers should be made of a material with a high specific elastic modulus, and the middle layer should be made of a material with a low apparent specific gravity. Although it is preferable to use a clad material consisting of
Furthermore, the inventors have found that there is no problem in terms of quality even if the slope of the light-shielding blade decreases as it moves away from the vicinity of the connection position with the driving member, and the present invention has been completed.
従って、本発明は比弾性係数の高め表面層、六面層よル
見かけ比重の小さい中間層及び比弾性係数の尚い義面ノ
ーの少なくとも3層からなり、駆#部材との結合位置よ
フ鵬れるに従い表面層又は躾面層のいずれか一方から内
層へ向って層数を減少させたこと′f:%値とする光制
御i41輌置用迩光羽@t−提供する。Therefore, the present invention consists of at least three layers: a surface layer with a high specific elastic modulus, a hexagonal layer, an intermediate layer with a low apparent specific gravity, and a prosthetic surface layer with a specific elastic modulus. The number of layers is decreased from either the surface layer or the surface layer toward the inner layer as the temperature increases.
本発明に於いて、表面層及び−面層は、一層だけではな
く複数層から成っていてもよいが、これらの層t−構成
する比弾性係数の南い材料としては、例えば、BN 、
BsN4 + 14cIWsNa 、 S4C
のようなセラミックス、B・のような金属、その他薄恢
状カーボン、薄板状#よう索、薄板状ダイヤモンドなど
かに用される。これらの材料は耐摩耗性、1元性に優れ
、ヤング率Eが^く低比重であるので、遮光羽根材料と
して特に好ましい。これらのA面層または表−ノーの厚
さ比は通常全体に対して1/ 〜V1゜で十分でるる。In the present invention, the surface layer and the surface layer may be composed of not only one layer but also a plurality of layers, but materials with low specific elastic modulus constituting these layers include, for example, BN,
BsN4 + 14cIWsNa, S4C
It is used for ceramics such as B, metals such as B, and other materials such as thin carbon, thin plate-like wire, and thin plate-like diamond. These materials are particularly preferable as light-shielding blade materials because they have excellent abrasion resistance and monotony, and have a high Young's modulus E and low specific gravity. The thickness ratio of these A-side layers or front-to-no layer is usually 1/~V1° with respect to the whole.
0
また中間層も一層又は2以上の多層からなっていてもよ
いが、中間層′に#成する見かけ比重の小さい材料とし
ては、開放中空t−有する構造、閉鎖中空を有する発泡
体構造、繊維臓物構造又はフィルム状でろって、それ自
体低比重のもo、inえばポリエチレン、ポリプロピレ
ン、ポリ塩化ビニル、ポリアミド、エポキシ*m、フェ
ノール樹脂、尿素樹脂、ポリウレタン、ポリスチレン、
不飽和ポリエステル樹脂のようなプラスチックあるいは
、これらのプラスチック上ガラス繊維、カーボンファイ
バー、ポロンファイバー、有機高分子ファイバー、電化
ホウ素ファイバー、ウィスカーなどの繊維で強化したも
のが使用される。0 The intermediate layer may also consist of one layer or two or more layers, but examples of materials with low apparent specific gravity for the intermediate layer include structures with open hollows, foam structures with closed hollows, and fibers. Polyethylene, polypropylene, polyvinyl chloride, polyamide, epoxy*m, phenolic resin, urea resin, polyurethane, polystyrene, etc., which have a visceral structure or film-like structure and have a low specific gravity themselves
Plastics such as unsaturated polyester resins or plastics reinforced with fibers such as glass fibers, carbon fibers, poron fibers, organic polymer fibers, electrified boron fibers, and whiskers are used.
中間層の厚さ比としては、通常全体に対して6/ 〜8
/、。1!直が適切で套る。The thickness ratio of the intermediate layer is usually 6/~8 to the entire thickness.
/,. 1! It is appropriate to be direct.
G
adiJ層は表面層と全く同一の物質でもよいし、異な
る書質でもよい。本発明に於いて表両、71&面の尼−
は厳密ではなく、夾−の応用に際して決められる。The GadiJ layer may be made of the same material as the surface layer, or may have a different quality. In the present invention, the front side, 71 & side ama-
is not strictly determined and is determined upon the application of the weight.
表、裏面層と中間層との接合には、接着剤を用いてもよ
いが、中間層自身を接着剤と兼用させてもよい。An adhesive may be used to bond the front and back layers and the intermediate layer, but the intermediate layer itself may also be used as an adhesive.
次いで、図面を引用して実施例によ〕、本発明kA体的
に説明する。Next, the present invention will be specifically described by way of examples with reference to the drawings.
実施例1
本実施例はたて*aミツオーカルプレンシャッタ羽根に
応用した例で1911g111G6は平函図、同(2)
は断面図である0図中の符号1は表面層、2は中間層、
3は裏面層、4.5は駆l1hs材と結合するための取
付は穴である。Example 1 This example is an example applied to a vertical*a Mitsuo Calplane shutter blade.
0 is a cross-sectional view, code 1 in figure 0 is a surface layer, 2 is an intermediate layer,
3 is the back layer, and 4.5 is a hole for connecting to the 11hs material.
取付は穴4.sO付近においては、表面層1〜裏面層葛
が重ね合わされているが、中央付近では裏面層がなく、
表面層1、中間層重から成)、1ら(先端部1&におい
ては表面層1のみで構成堪れている。Installation is through hole 4. Near the sO, the surface layer 1 to the back layer are superimposed, but there is no back layer near the center;
(The tip portion 1& is composed of only the surface layer 1.).
ここに)いて、表面層1、裏面層3層は他の部材すなわ
ち不図示の案内部中、駆動アーム、重ねて使用されh倫
ovvaと摺動することになるので耐摩耗性の高いこと
が要求される。さらVc表閣層1は先端1&では、単独
で遮光能力を持つ必要が番ることから、透光法が薦〈な
ければならない。Here, the surface layer 1 and the back surface layer 3 are used overlappingly with other members, such as the guide part (not shown), the drive arm, and slide with each other, so they must have high wear resistance. required. Furthermore, since the Vc front layer 1 needs to have a light-shielding ability by itself at the tip 1&, a transparent method is recommended.
ま九、同a11に先411では他の層によシ支持される
ことがないので、比弾性係数が高くなければ、剛性が不
足する。(9) Since the layer 411 prior to a11 is not supported by other layers, the rigidity will be insufficient unless the specific elastic modulus is high.
一方中間層2は、これら表面層1、孤鋪層畠に比して、
!!1度上の要求は少なく(できれば表面層を補強で自
ると良い)、騒く、羽根全体の厚みt提供し、表1&面
層を結び付ける−11をすれば良い。そして、このよう
なり一羽根においては、騒量でめれば、少ない力量で、
遍(遍#させることができるので表面層1〜lIk画層
3はすべて比重(15度〕が小名い方が好ましい。On the other hand, the intermediate layer 2 is, compared to the surface layer 1 and the isolated layer,
! ! There are few requirements for 1 degree higher (if possible, it is better to reinforce the surface layer), and it is sufficient to provide the thickness of the entire blade, 1, and -11 to connect the surface layer. And in a single bird like this, if you get confused by the amount of noise, you can do it with less power.
It is preferable that the specific gravity (15 degrees) of all the surface layers 1 to 3 is small because it can be made to vary.
以上のことから表面層1は、耐摩耗性と迩1 光性
にすぐれヤング率Eが藁く、また比重が小さいことが望
壜れる。例えばセラミックスなどが好適に使用される。From the above, it is desirable that the surface layer 1 has excellent abrasion resistance and optical properties, a high Young's modulus E, and a low specific gravity. For example, ceramics and the like are preferably used.
また中間層2は、比重が小さければ曳くプラスチック等
を用いることができる。さらに裏面層3は、耐jlII
粍性がぁって、比重が小さいものが良いので、鵞うミッ
クス、金属等が使用される。Further, the intermediate layer 2 may be made of plastic or the like if its specific gravity is small. Furthermore, the back layer 3 has a resistance to jlII
It is preferable to use a material that is tough and has a low specific gravity, so a thick mix, metal, etc. are used.
このような構造を有するため樋量の割には剛性の高−羽
根が得られる。また別種の物質を異なる長さにして結合
しているため、単一の物質を先端にゆくにしたがって厚
みt漸減させるいわゆるテーパー状の羽根に比して、劇
作が容易であり、不均一の厚みを持たせるのが1廟でめ
るか、またはそのような材料が市場性を持たず一般的で
ないような物質でも遮光羽根として利用できる自由度t
−有し、かつコストも低廉でるる。With such a structure, a highly rigid blade can be obtained considering the amount of gutter. In addition, since different types of materials are bonded to different lengths, it is easier to create dramas than with so-called tapered blades, in which the thickness of a single material gradually decreases toward the tip. There is a degree of freedom in which materials can be used as light-shielding blades even if it is possible to make them in one temple, or such materials have no marketability and are not common.
- It is also inexpensive.
次に具体的な製造法について述・べろ。Next, let's talk about the specific manufacturing method.
ここでは前面層1はヤング率が^く比較的靭性に−むチ
タン窒化−を用い、中間層2は特に接着性に優れるエポ
キシ事情m’を用い、成面層易は比強度の大きい高力ア
ルミニウム合金を用いる。Here, the front layer 1 is made of titanium nitride, which has a high Young's modulus and is relatively tough, and the middle layer 2 is made of epoxy resin, which has particularly excellent adhesive properties. Uses aluminum alloy.
最初に、表面層1えるチタン蝋化物をホットプレス法t
たはPVD+CVDのような蒸着法で作製し、これに中
間層2九るエポキシllt慮tS分的にライニングする
。ライニングの方法としてはスクリーン印刷が適切であ
る。First, the surface layer 1 is made of titanium waxed by hot pressing method.
Alternatively, the intermediate layer 2 is fabricated by a vapor deposition method such as PVD+CVD, and the intermediate layer 2 is lined with epoxy. Screen printing is a suitable method for lining.
エポキシ樹脂はガラス繊維との濡れ性が良いので、強度
増加のためにガラス繊−強化を施したエポキシ樹脂會用
いてもよい。次に蟲面層37N−る高力アルミニウム合
金を中間層2に重ね合わせて硼着する。3層を摘蕾し九
俵でエツチングによ〕3層をパターニングしfT望形状
に残すこともできる。別の作1ill法としては2層を
基板として3層を真空蒸着によ多積層させることも可−
1でh4゜アルマイト処場が可鰭な高力フルミニ9ム合
金ならば、(同処堀に19)アルマイト層を形成基せ、
ヤング率を向上させてもよい。Since epoxy resin has good wettability with glass fibers, epoxy resins reinforced with glass fibers may be used to increase strength. Next, a high-strength aluminum alloy of 37N is superimposed on the intermediate layer 2 and bonded. It is also possible to pattern the three layers by removing the buds and etching them with nine bales to leave them in the desired shape. As another 1ill method, it is also possible to use two layers as a substrate and laminate three layers by vacuum evaporation.
If the h4゜ alumite place is a flexible high-strength full mini-9mm alloy in 1, form an alumite layer (19 in the same place),
Young's modulus may also be improved.
これによp同じ索材を同一の厚さ比で彊如合わせた均一
なWt#lf:もつ羽根に対し、本発l!110il1
01R梼造をもりた羽根はその重量t80−以上も@滅
でするのである。As a result, compared to the uniform Wt#lf: blade made of the same cable material with the same thickness ratio, the main cable is the same as the one with the same thickness ratio. 110il1
A blade with 01R structure weighs more than t80-.
本実施例においては、3層構造で6るが、4層でも5層
でも、この幼果は得られる。In this example, a three-layer structure is used, but this young fruit can also be obtained with a four-layer structure or a five-layer structure.
実施例2
w&2図は斜視図で弗シ、本例は本発明の羽根を公知の
九て走部シャッタに応用した実施例で参る。その構成と
作動ft説明する。Embodiment 2 Figures w and 2 are perspective views, and this example shows an example in which the blade of the present invention is applied to a known nine-leaf shutter. Its structure and operation will be explained.
第18機6に411設されたピンT、・と、レバーs、
1◎が回@可能に連結されている。411 pins T, · and lever s installed on the 18th aircraft 6,
1◎ is connected so that it can be repeated.
またレバー9.10はシャッタ基板11に植設され丸軸
12,13を中心として回―可能とな−pでいる。ピン
1,8とm12.111とはほぼ平行四辺形を成してい
るため、s1羽根6は、レバー$、1oの回−に従って
ほぼ千行移−する。しかし、第2羽根14、蘂3羽機1
5、第4羽機16および嬉5羽根1Tは講1羽横Gと異
なる動きをする。すなわち、41羽根6上に檀&された
ピン18は、42羽機14と回転q能に結合されておυ
、軸12に回動可能に支持されたアーム18に檀設され
えビシ2・と係合するカム111114&が嬉2羽機1
4の基部に設けられている。それ故、m1羽機14の運
動はピン18を介してピン200動自とカム−14aの
形状によって′Xi!、まる。1層8羽機1Sは軸13
に回転可能に支持され、その基部にピン20と係合する
カム纏11mが設けられている。以下籐4羽機16、箒
6羽根ITも同様にして軸11に回転可能に支持基れ、
ピン20と係合するカム$1@a、IFmがそれぞれ設
けられている。ピン20は壜丸軸12に回転可能に支持
1れ九レバー−とも回転可能に結合してお9軸12を中
心にしてm−する7−ム1−と共に回−する。各羽根の
力A#14m、11m。Further, the levers 9 and 10 are mounted on the shutter base plate 11 and are rotatable around round shafts 12 and 13. Since the pins 1 and 8 and m12.111 form a substantially parallelogram, the s1 blade 6 moves approximately 1,000 times in accordance with the rotation of the levers $ and 1o. However, the second blade 14, the three-legged blade 1
5. The 4th blade 16 and the 5th blade 1T move differently from the horizontal G of the 1st blade. That is, the pin 18 mounted on the 41-blade 6 is rotatably coupled to the 42-blade aircraft 14 and
, a cam 111114 & engaged with the blade 2 is mounted on an arm 18 which is rotatably supported on the shaft 12.
It is provided at the base of 4. Therefore, the movement of the m1 blade 14 is caused by the shape of the pin 200 and the cam 14a via the pin 18 'Xi! ,circle. 1 layer 8 blade aircraft 1S has shaft 13
A cam sleeve 11m is provided at the base of the cam sleeve 11m to engage with the pin 20. Similarly, the rattan 4-blade machine 16 and the broom 6-blade IT are rotatably supported on the shaft 11.
Cams $1@a and IFm that engage with the pin 20 are provided, respectively. The pin 20 is rotatably supported on the bottle shaft 12 and is rotatably connected to the nine levers, and rotates together with the seven levers 1 that rotate about the shaft 12. Power of each blade A#14m, 11m.
1@b、17mは、#l1羽機6が図において1パーチ
ユ121の上方に位置するとき、羽根がm−伏線となっ
て、アパーチュアをおお8 い、嬉1羽機・が7
パーチユア21の下方にyrha’rると蕪、はぼすべ
ての羽根が重なるよう構成されてvhj、この4合、縞
易1機1sから譲S羽根ITオで03枚の羽根は軸11
を中にして回動し、6たかも、JIIを開閉するように
動作する。1@b, 17m, when the #l1 blade 6 is located above the 1 perch 121 in the figure, the blade becomes an m-foreshadow line and covers the aperture, and the #l1 blade is 7.
Below the perch 21, all the blades are arranged so that they overlap, and the 4 blades are arranged so that all the blades overlap.
It rotates with the JII inside and operates to open and close the JII.
フォーカルプレンシャッタにおいては通常このような羽
根膵が2組用意され、一方がシャッタ開き部材、他方が
シャッタ閉じ部材として使用音れる。In a focal plane shutter, two sets of such blades are usually prepared, one of which is used as a shutter opening member and the other as a shutter closing member.
ここにおいて第1有機−は第1図にて説明した如く、一
層によ1構成されピン1.s11遠くなるにしたがって
2層、1層とその層数が減少している。この丸め、蛾も
大暑(遍―する第1羽機6が樋量化されて、従って、羽
is群全体として小さな力量で効率良く羽根1#會−か
すことがで龜る。Here, the first organic layer is further composed of pins 1 and 1, as explained in FIG. As the distance from s11 increases, the number of layers decreases from 2 layers to 1 layer. During this rounding, the moths are also very hot (the first wing 6 is reduced to a sluice), and therefore, the whole group of moths is able to efficiently gather 1 # of wings with little effort.
1危、#111羽根6の平面となっている側藝−倉!s
2羽根14と密着させているため漏光も少ない。1st crisis, #111 blade 6 flat surface! s
Since the two blades 14 are in close contact with each other, there is little light leakage.
なお、嬉1図の実施例1の羽根が、七〇 一端に番る穴
4.sによ)支持されるのに対し、本14施例の講1羽
機6は、その中央部付近會ピン1.@によ)支持1れて
いる点が異なるが、どちら01lII様もシャッタとし
て実用北回―で6ml、本JAIjIが果す効果も同じ
でるる。Note that the blade of Example 1 shown in Figure 1 has 70 holes at one end and 4. In contrast, the single-wing aircraft 6 of this 14th embodiment is supported by the aircraft pin 1 near its center. Although they are different in that they are supported by @1, both 01lII and 6ml are practical as shutters, and the effect of this JAIjI is the same.
1九、本実施例のレバー・も、中は1第1羽機・と同4
111KsJIIIIIcて構成されて−る。そして−
12及びピンス・に支持されている部分とそのii傍は
8層かGll成っているものの、ピン1との遁紬優は一
層のみとな)、中間は8層から成る。これは、軸121
1j)に1−ム1・すなわ珈ピン2・を1g1勅畜せる
ことによ如刹機鮮を纒−する九め、レバー−の軸12と
ピンtoofLtsには入電な力がlji*L、かりそ
OSS力は、ピン20に近いところほど大暑い九め耐久
***九せながらレバー−上湯量化する鑓的で同様の構
造とした。19. The lever of this example is also the same as the 1st wing machine.
It is composed of 111KsJIIIc. And-
Although the part supported by pin 12 and pin 2 and its ii side are made up of 8 layers or Gll, the part supported by pin 1 is only one layer), and the middle part is made of 8 layers. This is the axis 121
1j) By feeding 1g1 of 1-mu 1, ie coffee pin 2, to 1g1, a force is applied to the shaft 12 of the lever and the pin toofLts. , The Kariso OSS force has a similar structure with a lever that increases the amount of hot water as it approaches the pin 20.
これを本実施例の如く厚みにおいて変化さく九レバー・
を用いるかわ如VcII7を中を変化させても、同@0
効畢を得ることがで自るが、本実施例の方が優れている
ので、その説明をする。This is done by nine levers that vary the thickness as in this example.
Even if you change the inside of Kawajo VcII7 using , the same @0
Although it is possible to obtain the desired effect, this embodiment is superior, so it will be explained below.
縞8図及びaI4図は羽@群の平面図でめるが、ここで
は第2図における籐2羽根14から#Is羽根ILK至
る4枚の羽根は省略されている。112図の説明で述べ
良ようにレバー@、IQと軸12,18、ピンT、−は
平行リンクを成している。したがって、レバー自と10
は軸12.18回カにそれぞれ回―すると亀、その間隔
22は必ず小さくなつ九シ大自くなりたりする。例えば
、縞3図においては羽根−が7パーチユ721に遮って
いる場合を示すが、この時にレバーSとレバー100間
隔22は余裕が有る。しかし第4図に至って羽根膵が1
パーチユアの外方に収納され九とき、間#122は小さ
なものとなる。Stripe 8 and aI 4 are plan views of the feather group, but the four blades from rattan 2 blade 14 to #Is blade ILK in FIG. 2 are omitted here. As stated in the explanation of FIG. 112, the levers @, IQ, shafts 12, 18, and pins T, - form parallel links. Therefore, the lever itself and 10
When the axis is rotated 12 and 18 times each, the interval 22 becomes smaller and becomes 90 times larger. For example, in the stripe diagram 3, a case is shown in which the blade is obstructed by 7 parts 721, but at this time, there is enough space 22 between the lever S and the lever 100. However, when we reached Figure 4, the feathered pancreas was 1.
When stored outside the perch, space #122 becomes small.
この丸めレバー9のピン22と結合する付近のレバ−1
0KM接する部分11mが、内薄と □な〕巾を拡大す
ることが困−となる。無通に巾を拡大すると、レバー1
0が第3図、嬉4図の双方の伏線においてピン’io(
glbo突出St−逃げる必誠が生ずるため、レバー1
0が゛属−することによル大滅化してしまいスペースt
ii貴することになる。Lever 1 near the pin 22 of this rounded lever 9
It would be difficult to enlarge the width of the 0KM contacting part 11m with the inner thickness. When the width is expanded to nothing, lever 1
0 is pin 'io (
glbo protruding St - Since it is inevitable to run away, lever 1
Due to 0 becoming a member, the space t becomes annihilated.
ii.
また、j12kAKおける第4羽根11から嬉暴羽楓1
1に主43枚の羽根が、軸13を中心としピン2QIC
よシ回転させられるため、軸1墨とピン211の位置関
係は自由に設定することがで自ず、ピン2・を図中で上
方へ移設で虐る量には臘戚が弗シ、したがって中は)部
分−−の中會増すことは容易ではない。Also, from the 4th feather 11 in j12kAK
1 mainly has 43 blades centered around shaft 13 and pin 2QIC
Since it can be rotated, the positional relationship between shaft 1 and pin 211 can be set freely, and the amount of force required to move pin 2 upwards in the diagram is limited. It is not easy to increase the size of the part.
こOようにレバー■の巾はピン20との結合部付近にお
いて、自由に大会(とれない九め本5AJIl1例の如
く、ピン20に近付くにし九がって層数を増して厚くす
る方法の方が小鑞化と構成の自由go点で有利で番る。In this way, the width of the lever ■ can be adjusted freely near the joint with the pin 20. The latter has an advantage in terms of shading and freedom of composition.
嬉zt3i1〜JI[i4−において、レバー10もレ
バー−と同様な3層からtjelK至る変断面構造とし
ても良いが、レバー1・の役割は41羽機60工“1
ツジ・bが1パーチユ1の長手方向とはぼ平行に
なるように保つことにあるので、引つ彊如力か圧−力し
か加わらないため、特に幼果はない。In JI [i4-], the lever 10 may also have a variable cross-section structure ranging from three layers to tjelK, similar to the lever-, but the role of the lever 1 is 41 blades and 60 pieces.
Since the aim is to keep the rhododendron b almost parallel to the longitudinal direction of each perch, only pulling force or pressure is applied, so there are no particular young fruits.
′A実施例
菖6図を引用して説明する本例は本発明の羽根を九て滝
〕フォーカルプレンシャッタにL用した実施例で弗シ、
同図イ)は斜視図、同図(2)はその断面図である。This example, which will be explained with reference to FIG.
Figure A) is a perspective view, and Figure (2) is its cross-sectional view.
ζこにおいては第1羽機23、レバー240みがf!1
12図と異なる。但し、レバー24は第2図のレバー口
と同じ構造のものでも差し支えない。他の軸1!、13
、ピンT、@。ζ In this case, only the first blade 23 and the lever 240 are at f! 1
This is different from Figure 12. However, the lever 24 may have the same structure as the lever opening shown in FIG. 2. Other axis 1! , 13
, Pin T, @.
1 @、20及C[S[根14はtべて′ts2図と同
じ部位にめ如、同じ働tiをする。また、その他の構成
4I!素も112図と同じであるので省略してらる。1 @, 20 and C[S[root 14 are all located in the same part as in the 'ts2 diagram and have the same function ti. Also, other configurations 4I! The element is also the same as Figure 112, so it has been omitted.
こζで、@1羽根13は、第2図と異な〕その平面部2
3mは、第2羽根14とは対向しておらず、レバー24
.10と対向している。仁の丸め′i!&1羽機23と
嬉2羽根14の間には、−間2sが生じ、漏光しゃすく
なるが、との羽根群とは別の羽根膵中別設の遮光板で7
パーチ21會襦助的に纏うような条件で一層する場合に
は、このことは特に欠点とは亀もず、むしろ次の46図
に示すような利点を有する。In this ζ, @1 blade 13 is different from that in FIG.
3m is not facing the second blade 14 and is not facing the lever 24.
.. It is facing 10. Jin's round'i! There is a -2s interval between the &1 blade 23 and the 2nd blade 14, which reduces light leakage.
When the perch 21 is layered under such conditions as the perch 21, this is not a particular disadvantage, but rather has an advantage as shown in the following Figure 46.
藤鳴−において2・はレバー210回転中心で番〉、ビ
ン2畠がその先端に植設されている。羽礒宜9はビシ2
・によ如レバー21に対して一転可1iiK支持されて
いる。軸2・、レバー0Aびピン28はもう1鳳あシ1
対で羽l12−會支持している。ここでピン2・が1機
210中夫付近でなく項部にある点はgi図−と異なる
。In Fujinari, 2 is located at the center of rotation of the lever 210, and a bottle 2 is installed at its tip. Haisogi 9 is bishi 2
- It is supported by the lever 21 so that it can be rotated in one direction. Shaft 2, lever 0A and pin 28 are one more foot 1
A pair of wings are supporting each other. Here, pin 2 is different from the gi diagram in that it is located at the nuchal part instead of near the 210 midship.
ここで、もし羽根29が先端に行(にしたがりて層の赦
が減少していない時、すなわち図中の砿−で示した2$
aも含んだ形状でるると龜の重心sOaは、羽8210
重心80と異な′)九位置となる。ピン211から重心
sQ壇での長手方向O順MX−は重心番(lalでの處
@X、よjI煩い。このため、羽根2−に一−0澗遮直
が庫わり九時の慣性によりて生ずるモーメントが小さく
なp%ま九重さも211at−含む羽根211よ〕も、
軽いことと相まってピン2@にかかる員担は小さくな)
、耐久性が向上する。1九羽根自体の変形も小さくて済
み、羽根のねじれによって他の部材との閾に無用の摩1
mを生じたプ、引つ掛かつ九シしない。このことは74
6vlAのみならず、蕗2図、第2図における実施例と
も共通の効果で6る。 /さ
らに第5図、第6図の5A施的においてはレバー2Tと
、重心sOの厚み方向の距−Y、が重心Boaとの距m
Y mよりも小さい丸め、レバー2Tによって羽根2
sが急速に駆動された時に、羽根21Bの慣性によって
生ずるねじれが小さくなるので、ヤはり羽根2sの円滑
な運動に寄与する。Here, if the blade 29 goes to the tip (therefore, the thickness of the layer does not decrease, that is, 2$ shown by the circle in the figure)
If the shape also includes a, the center of gravity sOa of the head is feather 8210
The center of gravity is at a position different from 80. From the pin 211 to the center of gravity sQ in the longitudinal direction O order MX- is the center of gravity number (lal 處@X, YOJI troublesome. Therefore, the blade 2- has a 1-0 degree shielding and due to the inertia of 9 o'clock Also, the moment generated by the blade 211 is small, and the weight of the blade 211 is small.
Coupled with its light weight, the amount of effort required for pin 2@ is small.)
, durability is improved. 19 The deformation of the blade itself is small, and the twisting of the blade eliminates unnecessary friction on the threshold with other parts.
The pu that caused the m doesn't catch on. This is 74
Not only 6vlA but also the embodiments shown in Fig. 2 and Fig. 2 have a common effect. /Furthermore, in the case of 5A in FIGS. 5 and 6, the distance between the lever 2T and the center of gravity sO in the thickness direction -Y is the distance m between the center of gravity Boa
Y Round smaller than m, use lever 2T to turn blade 2
When the blade s is driven rapidly, the twist caused by the inertia of the blade 21B is reduced, contributing to smooth movement of the blade 2s.
実施例4
次の3117図(斜視図)は本発明の別の実施例であっ
て、第1図に示した例と若干異な抄貞函層31、中間層
32、Am7m3a七れぞれの巾も長畜も形状も各々異
なるものである。Embodiment 4 The following figure 3117 (perspective view) shows another embodiment of the present invention, in which the widths of the shochu box layer 31, intermediate layer 32, and Am7m3a are slightly different from the example shown in FIG. 1. Each species is different in length, length, and shape.
縞1−においては、−面層1、中間層2、裏1層sO長
す方向のIkさのみ^な)巾については同一で参り九が
、本実施例にかいてはそれに比してさもに一量化YiI
:図ることかで自為ものでるる。穴$4,3iは1ii
lld(D穴4゜iと同一、朧一部材を結合するのに用
いる穴でhる。本実施例の羽根會例えばシャッタに応用
すh4合には、嬶211ail、嬉5図、嬉・−等と同
機に臘み込むことができる。In the case of stripe 1-, the width of the -face layer 1, the intermediate layer 2, and the back layer sO in the longitudinal direction are all the same, but in this example, the width is the same. YiI monomerized into
: It's a deliberate thing, but it's a self-made thing. Hole $4, 3i is 1ii
lld (same as D hole 4゜i, this hole is used to connect the oboro parts. In the blade assembly of this embodiment, for example, when applied to a shutter, there is a You can sit on the same plane as the others.
夷m例S
本例は本部@O構機會嬶i図に示す実施例3と同機なた
て滝)フォーカルプレンシャッタにゐ用しA例で6)、
縞S図にその斜視図上水す。作−はすべて前1の例とF
Qjtaehるが、嬉2の:#1lSFcD作励が、l
id作動、!kOa機81$1,4・と同様に軸41の
回)會ピン4211Cよって回転するように構成されて
いる点が異なり0こζでは、第1から縞lOS機81.
87.11.88.40がすべて本発明の先端に行くに
したがって積層数が減する羽根によって構成されている
。夷m Example S This example is the same as Embodiment 3 shown in Fig.
A perspective view of the striped S diagram is shown above. All works are the previous example and F
Qjtaeh is happy 2nd: #1l SFcD work is l
ID works! The difference is that, like the kOa machine 81$1,4, the shaft 41 is configured to rotate by means of a rotation pin 4211C, and in the 0koa machine 81, the striped lOS machine 81.
87, 11, 88, and 40 are all constituted by vanes in which the number of laminated layers decreases toward the tip of the present invention.
本実施例においては特に羽根の重ね合わせ方に特徴かめ
る。すなわち、1つの羽根を構成する各層のうち歳大面
積となっている層と、他の羽根の同じく最大面積となっ
ている層とが互に接触するように重ね合わせ、を九、さ
らに次の別の羽根との接触は蝋子面積の層相互の重ね合
わせとなっている。This embodiment is particularly characterized by the way the blades are overlapped. That is, among the layers constituting one blade, the layer with the largest area and the layer with the largest area of the other blade are stacked so that they are in contact with each other, and then the following steps are performed: The contact with another blade is the superposition of layers of wax area.
このように全ての羽根に本発明を適用すればシャッタ作
動部0**がさらに軽減で亀、羽根はよ如高速で運−し
、耐久性も向上する。As described above, if the present invention is applied to all the blades, the shutter operating part 0** will be further reduced, the blades will be able to move at a higher speed, and the durability will be improved.
さらに前記の如く交互に裏返しにして羽根′f:Jlね
合わせれば運動時における相互のひつかか如かなくなり
円滑な作IIbt−得ることかで自る。Furthermore, if the blades are alternately turned inside out and laid together as described above, there will be no mutual contact during movement, resulting in smooth operation.
以上の実施例は、薄板tIl数枚重ね合わせて構成した
、公知のたて走9フォーカルプレンシャッタに本発tj
llt応用した例でめったが、同様に薄板を重ね合わせ
て用いる公知のレンズの*n+−わゆみレンズレヤツタ
等はもとよル、分1il1111機を持九ない1枚の板
からなるシャッタ中、単1に漬遮光板に応用することも
で1、岡*C)@釆が得られる。The above embodiments are based on the known vertical running 9 focal plane shutter constructed by stacking several thin plates tIl.
Although it was rare in the application of llt, the *n+- waving lens layer of the known lens, which uses thin plates stacked on top of each other, is also good. 1 can also be applied to a dipping light-shielding plate to obtain 1, Oka * C) @ pot.
実施例・
第9図は本実施例の3秋重ねシャッター羽根評會−明す
るものでTo襲、第一図に)はその斜視−1嬉−mIp
4はg―園ret>ox−r矢視断面−でめる。Embodiment ・ Figure 9 shows the evaluation of the three overlapping shutter blades of this example.
4 is g-ret>ox-r cross section.
本例で使用する遮光羽根は、駆I#部材との結合位置4
sよ)達ざかるにつれて部分的に層歇が少なくな〕、本
夷總繍様も本発明に含まれる。The light shielding blade used in this example is connected to the drive I# member at the position 4.
s)) The present invention also includes the embroidery style in which the layering gradually decreases in parts as it reaches the final stage.
本例は全ての111機が、はソ平行移動をして重ね合わ
ぜ伏線と展開状部の画状lIAをとp得るシャッタ羽根
群に遍し、第9vA(2)の矢印方向から光が入射して
も漏光が少ない。In this example, all 111 planes move parallel to each other to obtain the image shape lIA of the superimposed foreshadowing and the developed part, and the light enters from the direction of the arrow 9vA (2). However, there is little light leakage.
以上のように本発明によれば、鬼かけ比重の小さい中間
層會比弾性係数の^い表、裏面層で挾持す為と共に、各
々の層の長1を変化畜せ、駆動部材との結合位置から離
れるにし九がって重ね層WjLt−少なくしていること
から、作動力量が小さくて済みかつ耐久性に優れ、^遮
で運*−aせることができ、その作動も円滑な遮光羽根
が得られる。As described above, according to the present invention, the intermediate layer with a small specific gravity is held between the front and back layers with a high relative elastic modulus, and the length 1 of each layer can be varied, and the connection with the driving member is improved. Since the overlapping layer WjLt decreases as it moves away from the position, the amount of actuation force is small and it has excellent durability. is obtained.
第1図(イ)は本発明のひとつO実施例1に示す遮光羽
根の平面図でTo)、同図に)はその断面図である。
第2図は本発明の羽根tたて走9シャッタに応用したひ
とつの実施例を示す斜視図である。
1m3図、第4図は第2図を部分的に壜〉出し丸干面図
である。
aS図に)は本発明の羽根を九で走)シャッタに応用し
た別の実施例を示す斜視図でh如、同図■はその断面図
でるる。
第6図CよIss図に)をさらに略記した断面図7・あ
る。
縞7図は本発明のさらに別の実施例の遮光”羽根上水す
斜a図である。
嬉a図は本発明の羽根上次て走シシャッタに応用した例
の斜視図である。
縞9図げ〉は実施例・のシャッター羽根群の#amでT
oシ、同ahは図印のX−Y矢視断E1図である。
〔主tS分の符号のa明〕
1・・・・・・霧面層
2・・・・・・中間層
3・・・・・・裏面層
矛1図
第2囚FIG. 1A is a plan view of a light-shielding blade according to Embodiment 1 of the present invention, and FIG. 1A is a cross-sectional view thereof. FIG. 2 is a perspective view showing one embodiment of the present invention applied to a shutter with nine vertical blades. Figure 1m3 and Figure 4 are partially exposed views of Figure 2. Figure aS) is a perspective view showing another embodiment in which the blade of the present invention is applied to a shutter, and Figure h is a cross-sectional view thereof. There is a sectional view 7 further abbreviated in Figure 6C (Iss diagram). Stripe 7 is a perspective view of a light-shielding blade top water shutter according to yet another embodiment of the present invention. Figure A is a perspective view of an example in which the present invention is applied to a blade top shutter. Stripe 9 〉 is #am of the shutter blade group of the example.
o, ah are X-Y arrow cross-section E1 diagrams of the figures. [A of the sign of the main tS] 1...Fog layer 2...Middle layer 3...Back layer Spear 1 Figure 2nd prisoner
Claims (1)
さい中間層及び弾憔係威の高−裏爾層の少なくとも3層
からな1、駆#部材との一倉位瀘り如−れるに従い表匣
層又は畠−虐Ovhずれか一方から内層へ向って層航會
減少さぜ友ことを脅懺とする光s1御装置用遮光4i機
。It consists of at least three layers: an intermediate layer with a low apparent specific gravity, an inner layer with a high elasticity, and an inner layer with a high elasticity. The light-shielding 4i machine for the optical S1 control device threatens that the layer movement will decrease from either the front layer or the bottom layer toward the inner layer as the temperature increases.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3133082A JPS58149030A (en) | 1982-02-27 | 1982-02-27 | Light shielding blade for light controlling device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3133082A JPS58149030A (en) | 1982-02-27 | 1982-02-27 | Light shielding blade for light controlling device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS58149030A true JPS58149030A (en) | 1983-09-05 |
Family
ID=12328244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3133082A Pending JPS58149030A (en) | 1982-02-27 | 1982-02-27 | Light shielding blade for light controlling device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58149030A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS622029U (en) * | 1985-06-20 | 1987-01-08 | ||
| US6001465A (en) * | 1997-05-12 | 1999-12-14 | Copal Company Limited | Light shielding blade for camera made of para-orientation aromatic polyamide film |
| US12174525B2 (en) | 2020-03-19 | 2024-12-24 | Canon Kabushiki Kaisha | Light shielding blade and image pickup apparatus |
-
1982
- 1982-02-27 JP JP3133082A patent/JPS58149030A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS622029U (en) * | 1985-06-20 | 1987-01-08 | ||
| US6001465A (en) * | 1997-05-12 | 1999-12-14 | Copal Company Limited | Light shielding blade for camera made of para-orientation aromatic polyamide film |
| US12174525B2 (en) | 2020-03-19 | 2024-12-24 | Canon Kabushiki Kaisha | Light shielding blade and image pickup apparatus |
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