JP2503375B2 - Shade feather for camera - Google Patents

Shade feather for camera

Info

Publication number
JP2503375B2
JP2503375B2 JP3118329A JP11832991A JP2503375B2 JP 2503375 B2 JP2503375 B2 JP 2503375B2 JP 3118329 A JP3118329 A JP 3118329A JP 11832991 A JP11832991 A JP 11832991A JP 2503375 B2 JP2503375 B2 JP 2503375B2
Authority
JP
Japan
Prior art keywords
blade
carbon fibers
intermediate layer
carbon fiber
longitudinal direction
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
Application number
JP3118329A
Other languages
Japanese (ja)
Other versions
JPH04345146A (en
Inventor
典義 久我
一尚 衣川
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Seikosha KK
Original Assignee
Seikosha KK
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Seikosha KK filed Critical Seikosha KK
Priority to JP3118329A priority Critical patent/JP2503375B2/en
Publication of JPH04345146A publication Critical patent/JPH04345146A/en
Application granted granted Critical
Publication of JP2503375B2 publication Critical patent/JP2503375B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E40/00Technologies for an efficient electrical power generation, transmission or distribution
    • Y02E40/60Superconducting electric elements or equipment; Power systems integrating superconducting elements or equipment

Landscapes

  • Diaphragms For Cameras (AREA)
  • Shutters For Cameras (AREA)

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、カメラ用遮光羽根に
関し、より具体的には、カメラのフォーカルプレンシャ
ッタやレンズシャッタのシャッタ羽根または絞り羽根等
の高速で運動することが要求される遮光羽根に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a shading blade for a camera, and more specifically, to a shading blade for a camera such as a focal plane shutter of a camera or a shutter blade of a lens shutter or a diaphragm blade which is required to move at high speed. Regarding

【0002】[0002]

【従来の技術】例えばフォーカルプレンシャッタの撮影
領域を上げる等のためシャッタスピードの高速化が図ら
れているが、ジュラルミン板を用いた遮光羽根の構成で
は、剛性を保つため薄型化には限界があり、シャッタス
ピード1/4000秒程度が限界である。従って、より
高速化を図るため、軽量で比剛性の高い炭素繊維強化熱
硬化性樹脂シートを用いた羽根の開発が行われている。
2. Description of the Related Art For example, the shutter speed has been increased in order to increase the photographing area of a focal plane shutter. However, the structure of the light-shielding blade using the duralumin plate has a limit in reducing the thickness because the rigidity is maintained. Yes, the shutter speed is limited to about 1/4000 seconds. Therefore, in order to achieve higher speed, a blade using a carbon fiber reinforced thermosetting resin sheet that is lightweight and has high specific rigidity has been developed.

【0003】この炭素繊維強化熱硬化性樹脂シートを用
いた羽根の構造は従来、炭素繊維を一方向に並べた一方
向強化型プリプレグを、その炭素繊維の方向を直交させ
、または平行になるように、複数枚積層し、熱プレス
により固化させた構造となっている(実開昭60−63
825号公報,実開昭60−65726号公報)。
Conventionally, the structure of a blade using this carbon fiber reinforced thermosetting resin sheet is such that a unidirectional reinforced prepreg in which carbon fibers are arranged in one direction is made to have the directions of the carbon fibers orthogonal or parallel. As described above, it has a structure in which a plurality of layers are laminated and solidified by hot pressing (Actually developed 60-63).
825, and Japanese Utility Model Laid-Open No. 60-65726).

【0004】そして、切口端面の炭素繊維が、羽根の摺
動の際に他の羽根等に傷を付けないように、表面層の炭
素繊維を羽根の長手方向に配向し、中間層の炭素繊維を
羽根の幅方向、即ち摺動方向に配向している。
The carbon fiber of the surface layer is oriented in the longitudinal direction of the blade so that the carbon fiber of the cut end surface does not damage other blades when the blade slides. Are oriented in the width direction of the blade, that is, in the sliding direction.

【0005】[0005]

【発明が解決しようとする課題】しかしながら、打ち抜
き又は切断等による羽根の形への形状抜きの際に、中間
層の炭素繊維が端部付近で引き出され、この引き出され
て端部より突出した炭素繊維が、遮光羽根の使用の際に
他の羽根等を傷付けるという問題点があった。
However, the carbon fiber of the intermediate layer is pulled out in the vicinity of the end when the blade shape is punched out by cutting or cutting, and the carbon which is pulled out and protrudes from the end. There is a problem that the fibers damage other blades when the light-shielding blade is used.

【0006】また、羽根の形への形状抜きの際に、積層
境界面から剥離が生じるという問題点があった。
Further, there is a problem that peeling occurs from the laminated boundary surface when the shape of the blade is removed.

【0007】そこで本発明の目的は、切口端面から炭素
繊維の引出しを防止して使用の際に他の羽根等を傷付け
ることがなく、さらに必要な剛性を確保し、また形状抜
きの際に積層境界面から剥離が生じないカメラ用遮光羽
根を提供することにある。
Therefore, an object of the present invention is to prevent the carbon fibers from being pulled out from the end face of the cut, to prevent the other blades from being damaged during use, to further secure the necessary rigidity, and to laminate when removing the shape. It is to provide a light-shielding blade for a camera that does not peel off from the boundary surface.

【0008】[0008]

【課題を解決するための手段】上記目的を達成するため
に、本発明のカメラ用遮光羽根は、長手方向と実質的に
直交する方向に摺動するものであって、炭素繊維が一方
向に配向されマトリックス樹脂を含浸してなるプリプレ
グシートが積層してあり、積層されたプリプレグシート
のうち、表面層のプリプレグシートは炭素繊維の配向方
向が羽根の長手方向であり、表面層間に挟まれる中間層
のプリプレグシートは炭素繊維の配向方向が羽根の幅方
向であるとともに、中間層は表面層よりも炭素繊維の酸
化程度を大きくしてある。
In order to achieve the above-mentioned object, the light-shielding blade for a camera of the present invention is arranged substantially in the longitudinal direction.
A prepreg sheet that slides in a direction orthogonal to each other, in which carbon fibers are oriented in one direction and is impregnated with a matrix resin is laminated, and the prepreg sheet of the surface layer among the laminated prepreg sheets is carbon. The orientation direction of the fibers is the longitudinal direction of the blade, and the prepreg sheet of the intermediate layer sandwiched between the surface layers has the orientation direction of the carbon fibers in the width direction of the blade, and the intermediate layer has a higher degree of oxidation of the carbon fibers than the surface layer. It's big.

【0009】[0009]

【作用】中間層の炭素繊維は、酸化程度が大きいため、
マトリックス樹脂との結合力が大きくなり、従って形状
抜きの際、中間層の炭素繊維の端部が引き出されこの
面より突出することが減少し、そのため他の羽根を破損
することが抑えられる。
[Function] Since the carbon fiber of the intermediate layer is highly oxidized,
Bonding force between the matrix resin is increased, thus when the shape punching, the ends of the carbon fibers of the intermediate layer is drawn out decreases and protrude from the end <br/> face, damage to other blades therefor
Can be suppressed.

【0010】また、中間層の炭素繊維は、マトリックス
樹脂との結合力が大きくなるため、形状抜きの際の積層
境界面からの剥離が防止される。
Further, since the carbon fiber of the intermediate layer has a large bonding force with the matrix resin, the carbon fiber of the intermediate layer can be prevented from peeling from the laminated boundary surface when the shape is removed.

【0011】[0011]

【実施例】以下、本発明の一実施例を図面に基づいて詳
細に説明する。図2は一枚の遮光羽根1の平面図であ
り、同図A部の端面拡大図を図1に示してある。図1,
図2に示すように、遮光羽根1は3層より構成してあ
り、両表面層2,2には、例えば径7〜10μmの炭素
繊維3が羽根の長手方向に配向してあり、この炭素繊維
マトリックス樹脂4が含浸してある。また、中間層5
同径の炭素繊維6が羽根の幅方向に配向してありマト
リックス樹脂7を含浸させてある。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below in detail with reference to the drawings. FIG. 2 is a plan view of one light-blocking blade 1, and FIG. 1 is an enlarged end view of the portion A in FIG. Figure 1,
As shown in FIG. 2 , the light-shielding blade 1 is composed of three layers, and both surface layers 2 and 2 have carbon with a diameter of 7 to 10 μm, for example.
The fibers 3 are oriented in the longitudinal direction of the blade, and this carbon fiber
Matrix resin 4 are impregnated with. In addition, the intermediate layer 5
Have carbon fibers 6 of the same diameter oriented in the width direction of the blade and impregnated with a matrix resin 7.

【0012】中間層5の炭素繊維6は酸化程度を大きく
してあり、マトリックス樹脂7との結合力が大きくなっ
ている。中間層5は炭素繊維6の酸化程度が大きくなっ
ているため、この炭素繊維の引出しが防止され、そのた
め他の羽根を破損することが抑えられるが、反面では、
その剛性が低くなっている。
The carbon fiber 6 of the intermediate layer 5 has a large degree of oxidation and has a large bonding force with the matrix resin 7. Since the intermediate layer 5 has a large degree of oxidation of the carbon fibers 6, the carbon fibers are prevented from being pulled out, and
Therefore, damage to other blades can be suppressed, but on the other hand,
The rigidity that is lower.

【0013】一方、表面層2は剛性は高いが炭素繊維が
長手方向端面(長手方向の両端部に位置する面、即ち長
手方向に直交する面)から引き出され易い。しかし、炭
素繊維は長手方向に沿って配列しているため、幅方向端
面(幅方向の両端部に位置する面、即ち長手方向に平行
な面)からは突出しない。本発明の遮光羽根は長手方向
に直交する方向に摺動するので、長手方向に平行な端面
(図2の上端面および下端面)から炭素繊維が突出する
と他の羽根と重なり合う際に傷つけ易いが、長手方向に
直交する面(図2の右端面および左端面)から突出して
いても、他の羽根を傷つけることはあまりない。従っ
て、中間層5の酸化程度を大きくすることにより他の羽
根の破損を抑えることができる。
On the other hand, the surface layer 2 has high rigidity but carbon fiber
Longitudinal end faces (faces located at both ends in the longitudinal direction, that is, length
It is easy to pull it out from the surface orthogonal to the hand direction). But charcoal
Since the fibers are arranged along the longitudinal direction,
Surface (surface located at both ends in the width direction, that is, parallel to the longitudinal direction
Surface). The light shielding blade of the present invention is in the longitudinal direction.
Since it slides in the direction orthogonal to, the end face parallel to the longitudinal direction
The carbon fibers project from the upper end surface and the lower end surface in FIG.
It is easy to damage when overlapping with other blades, but in the longitudinal direction
Projecting from orthogonal planes (right end face and left end face in FIG. 2)
However, it does not hurt other feathers very much. Obey
By increasing the degree of oxidation of the intermediate layer 5
It can prevent root damage.

【0014】また、羽根1は、その幅方向には撓み変形
しにくいので、その剛性は、羽根が撓み易い長手方向の
剛性に比して、小さくて済むため、長手方向にできるだ
け高い剛性をもたせ、幅方向には剛性が若干低下して
も、全体として羽根に必要な剛性確保されている。
Further , the blade 1 is bent and deformed in the width direction.
Since it is difficult to do so, its rigidity can be made smaller in the longitudinal direction as compared with the rigidity in the longitudinal direction in which the blades easily bend .
It has high rigidity, and the rigidity decreases slightly in the width direction.
However, the rigidity required for the blades is secured as a whole.

【0015】次にこのカメラ用遮光羽根の製造方法を説
明する。両表面層2,2のプリプレグシートは、従来と
同様に形成する。即ち、炭素繊維3を大気中で400℃
の温度で、数十時間加熱処理して、酸化させ、表面に孔
を形成し、この炭素繊維3を一方向に配向して並べ、こ
れに例えばエポキシ,不飽和ポリエステル等の熱硬化性
樹脂等からなるマトリックス樹脂を含浸し、Bステー
ジ状態のプリプレグシートを形成する。
Next, a method for manufacturing this camera light-shielding blade will be described. The prepreg sheets for both surface layers 2 and 2 are formed in the same manner as the conventional one. That is, the carbon fiber 3 is 400 ° C. in the atmosphere.
At a temperature of several tens of hours for oxidation to form pores on the surface, the carbon fibers 3 are aligned in one direction and arranged, and a thermosetting resin such as epoxy or unsaturated polyester is placed on the carbon fibers 3. The prepreg sheet in the B stage state is formed by impregnating the matrix resin 4 of

【0016】一方、中間層5のプリプレグシートに用い
る炭素繊維6は、大気中で400℃の温度で表面層の炭
素繊維3の加熱時間よりも長く加熱する。加熱時間が長
くなると、過度の酸化が生じてCO2が発生し、炭素繊
維の表面が粗れ、多くの微少な凹凸が生じ表面積が大き
くなる。従って炭素繊維6の表面にケトン,ラワトン,
水酸基,カルボキシル基等の酸素官能基がより多く付着
する。なお、酸化程度が大きくなると、繊維の強度,剛
性が低下するが、羽根の幅方向(図2参照)に必要な
剛性が確保されることを限度として、加熱時間の最大値
が決定される。この炭素繊維6を従来と同様に一方向に
配向して並べ、これに上述と同様のマトリックス樹脂
を含浸し、Bステージ状態のプリプレグシートを形成す
る。
On the other hand, the carbon fiber 6 used for the prepreg sheet of the intermediate layer 5 is heated in the atmosphere at a temperature of 400 ° C. longer than the heating time of the carbon fiber 3 of the surface layer. When the heating time becomes long, excessive oxidation occurs, CO 2 is generated, the surface of the carbon fiber is roughened, and many fine irregularities are generated to increase the surface area. Therefore, on the surface of the carbon fiber 6, ketone, rawton,
More oxygen functional groups such as hydroxyl groups and carboxyl groups attach. Although the strength and rigidity of the fiber decrease as the degree of oxidation increases, the maximum heating time is determined within the limit that the rigidity required in the width direction of the blade 1 (see FIG. 2) is secured. . The carbon fibers 6 are aligned in one direction and arranged in the same manner as in the prior art, and the same matrix resin 7 as described above is arranged thereon.
To form a prepreg sheet in the B stage state.

【0017】次に両表面層2に用いられるプリプレグシ
ートと中間層5に用いられるプリプレグシートとをその
繊維の配向方向が互いに直角となるように積層し、熱プ
レスにより硬化する。するとマトリックス樹脂4,7
硬化して、炭素繊維3,6をそれぞれのマトリックス樹
脂4,7内に固定させ、一枚の繊維強化プラスチック
(FRP)シートを形成する。そして中間層の炭素繊維
6は酸化程度が過度となっているため、特に酸素官能基
がより多く生じているために、マトリックス樹脂との
水素結合,エステル結合等の化学結合が強固に生じ、マ
トリックス樹脂7内に非常に強固に固定される。
Next, the prepreg sheet used for both surface layers 2 and the prepreg sheet used for the intermediate layer 5 are laminated so that the orientation directions of the fibers thereof are at right angles to each other and cured by hot pressing. Then, the matrix resins 4 and 7 are hardened and the carbon fibers 3 and 6 are fixed in the matrix resins 4 and 7, respectively, to form one fiber reinforced plastic (FRP) sheet. Since the carbon fiber 6 of the intermediate layer has an excessive degree of oxidation, in particular, since more oxygen functional groups are generated, chemical bonds such as hydrogen bond and ester bond with the matrix resin 7 are strongly generated, It is very firmly fixed in the matrix resin 7.

【0018】そして、表面層2,2の炭素繊維3の方向
が羽根1の長手方向となるように、また、中間層の炭素
繊維6の配向方向が羽根1の幅方向となるように位置決
めして、羽根1の形に形状抜きを行う。このとき、中間
層の炭素繊維6はマトリックス樹脂7と強固に結合して
いるため、形状抜きの際、中間層5と表面層2,2
の境界面で剥離が生じることが極めて少なくなる。
[0018] Then, as in the direction of the carbon fibers 3 of the surface layers 2 and 2 is the longitudinal direction of the blade 1 and the alignment direction of the carbon fiber 6 of the intermediate layer is positioned such that the width direction of the blade 1 Then, the shape of the blade 1 is removed. At this time, since the carbon fiber 6 of the intermediate layer is firmly bonded to the matrix resin 7, peeling at the boundary surface between the intermediate layer 5 and both surface layers 2 1 and 2 is extremely reduced during shape removal. .

【0019】また、中間層の炭素繊維6はマトリック
ス樹脂7に強固に固定されているため、羽根1の長手方
向に平行な端面(図2の上下の端面)において、この
面より引き出されにくく切口端面において、炭素繊維6
の突出量が少ない。
Further, since the carbon fibers 6 of the intermediate layer 5 are firmly fixed to the matrix resin 7, the longitudinal direction of the blade 1
At the end face parallel to the direction (end surfaces of the upper and lower in FIG. 2), the cut end surface hardly drawn from the end <br/> face, carbon fibers 6
The amount of protrusion is small.

【0020】なお、表面層2,2の炭素繊維は、羽根
1の長手方向に平行な端面において、繊維方向と平行方
向に切り取られるため、繊維の切口がほとんどできず、
端面は滑かである。
Since the carbon fibers 3 of the surface layers 2 and 2 are cut in the direction parallel to the fiber direction on the end face parallel to the longitudinal direction of the blade 1, the cut of the fiber is hardly formed,
The end face is smooth.

【0021】このようにして形成された羽根1は、図3
に示すように、穴部1aを連結軸12,13に取り付け
ることによってアーム10,11に取り付けられ、他の
3枚の羽根15,16,17も同様にアーム9,10,
11に取り付けられる。これらのアーム9,10,11
が羽根受板19に固定され、窓穴部19aが羽根1,1
5,16,17により遮断されてシャッタが構成され
る。回動部18を所定手段(図示せず。)によって回動
させると、平行リンク機構により、羽根1,15,1
6,17が、平行に、かつこの羽根の長手方向と実質的
に直交する方向(図3の上下方向)に摺動して、シャッ
タの開閉が行われる。
The blade 1 thus formed is shown in FIG.
As shown in the figure, the holes 1a are attached to the connecting shafts 12 and 13 so as to be attached to the arms 10 and 11, and the other three blades 15, 16 and 17 are similarly attached to the arms 9, 10, and
It is attached to 11. These arms 9, 10, 11
Is fixed to the blade receiving plate 19, and the window hole portion 19a has blades 1 and 1
The shutter is configured by being blocked by 5, 16, and 17. When the rotating part 18 is rotated by a predetermined means (not shown), the blades 1, 15, 1 are moved by the parallel link mechanism.
6, 17 are substantially parallel to each other and substantially in the longitudinal direction of the blade
The shutter is opened and closed by sliding in a direction orthogonal to (the vertical direction in FIG. 3) .

【0022】ここに羽根1,15,16,17は軽量で
あり、また炭素繊維3で長手方向の剛性が強化され
て、さらに羽根の幅方向の剛性も必要最小限は確保され
ており、高速開閉を支障なく行うことが可能である。
[0022] Here the wing 1,15,16,17 is lightweight, also is enhanced longitudinal rigidity carbon fibers 3, further width direction of the rigidity required minimum vanes are secured, It is possible to open and close at high speed without any problems.

【0023】また、羽根の中間層の炭素繊維6は、
羽根の摺動方向に配向してあるが、炭素繊維6は長手方
向に平行な端面より突出していないので、他の羽根等を
傷付けることがなく、シャッタの耐久性等を向上させる
ことができる。
The carbon fiber 6 of the intermediate layer 5 of the blade 1 is
Although oriented in the sliding direction of the blades, the carbon fiber 6 is long
Since it does not project from the end face parallel to the direction , other blades and the like are not damaged, and the durability of the shutter and the like can be improved.

【0024】なお、羽根1の表面層2,2の炭素繊維3
が図2の左右両端から引出されることがあっても、羽根
はその長手方向と実質的に直交する方向に摺動するた
め、他の羽根を破損する心配はあまりなく、しかも、シ
ャッタ羽根の場合、表面層2,2の炭素繊維3が図2の
左右両端面から引出されたとしても、その部分は図3に
示す羽根受板19で保持されていることが多いのでより
破損しにくい。
The carbon fibers 3 of the surface layers 2 and 2 of the blade 1
Even if it is pulled out from the left and right ends of Fig. 2,
Slides in a direction substantially perpendicular to its longitudinal direction.
Therefore, there is not much risk of damaging other blades, and
In the case of the chatter blade, the carbon fibers 3 of the surface layers 2 and 2 of FIG.
Even if it is pulled out from both left and right end faces, that part is shown in Fig. 3.
Since it is often held by the blade support plate 19 shown,
Hard to break.

【0025】また、表面層2,2の炭素繊維3は羽根の
摺動方向と直角方向に配向してあるため、他の羽根等を
傷付けない。
Further, the carbon fibers 3 of the surface layers 2 and 2 because that is oriented in the sliding direction perpendicular to the direction of the blade, not to damage the other blade or the like.

【0026】上記実施例では、加熱時間を長くして、中
間層の炭素繊維の酸化程度を大きくするとしたが、高濃
度硝酸による薬液酸化法により、炭素繊維の酸化程度を
大きくしてもよい。また、炭素繊維を陽極とした酸性電
解溶液中での電気分解反応により酸化してもよい。
In the above embodiment, the heating time was lengthened to increase the degree of oxidation of the carbon fibers in the intermediate layer. However, the degree of oxidation of the carbon fibers may be increased by a chemical solution oxidation method using high concentration nitric acid. Further, it may be oxidized by an electrolysis reaction in an acidic electrolytic solution using carbon fiber as an anode.

【0027】[0027]

【発明の効果】本発明は、中間層の炭素繊維の酸化程度
を表面層の炭素繊維の酸化程度より大きくしたために、
中間層の炭素繊維をそのマトリックス樹脂に強固に結合
させることができ、形状抜きの際の、積層境界面よりの
剥離が防止され、また羽根の長手方向と平行な端面より
の中間層の炭素繊維のはみ出しが防止され、そのため他
の羽根を破損することが防止される。さらに遮光羽根と
して特に重要な長手方向の剛性が高くなる。
According to the present invention, the degree of oxidation of the carbon fiber of the intermediate layer is made larger than that of the carbon fiber of the surface layer.
The carbon fiber of the intermediate layer can be firmly bonded to the matrix resin, peeling from the lamination boundary surface during shape removal is prevented, and the carbon fiber of the intermediate layer from the end surface parallel to the longitudinal direction of the blade. Is prevented from sticking out and therefore other
It is possible to prevent the blades from being damaged. Furthermore, with shading blades
Then, the rigidity in the longitudinal direction, which is particularly important, becomes high.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の遮光羽根の羽根幅方向の端面部(A
部)の部分拡大斜視図である。
FIG. 1 is an end face portion (A in the width direction of a light-shielding blade of the present invention).
(Part) is a partial enlarged perspective view of FIG.

【図2】遮光羽根の平面図である。FIG. 2 is a plan view of a light shielding blade.

【図3】フォーカルプレンシャッタの平面図である。FIG. 3 is a plan view of a focal plane shutter.

【符号の説明】[Explanation of symbols]

1,15,16,17 カメラ用遮光羽根 2 表面層 3 表面層の炭素繊維 4,7 マトリックス樹脂 5 中間層 6 中間層の炭素繊維 1, 15, 16, 17 Shading blade for camera 2 Surface layer 3 Surface layer carbon fiber 4,7 Matrix resin 5 Intermediate layer 6 Intermediate layer carbon fiber

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 長手方向と実質的に直交する方向に摺動
する遮光羽根において、 炭素繊維が一方向に配向されマトリックス樹脂を含浸し
てなるプリプレグシートが積層してあり、 積層された上記プリプレグシートのうち、表面層のプリ
プレグシートは上記炭素繊維の配向方向が羽根の長手方
向であり、上記表面層間に挟まれる中間層のプリプレグ
シートは上記炭素繊維の配向方向が羽根の幅方向である
とともに、上記中間層は上記表面層よりも上記炭素繊維
の酸化程度が大きいことを特徴とするカメラ用遮光羽
根。
1. Sliding in a direction substantially perpendicular to the longitudinal direction
In the shading blades, the prepreg sheets in which the carbon fibers are oriented in one direction and impregnated with the matrix resin are laminated, and among the laminated prepreg sheets, the prepreg sheet of the surface layer has an orientation direction of the carbon fibers. In the longitudinal direction of the blade, the prepreg sheet of the intermediate layer sandwiched between the surface layers, the orientation direction of the carbon fibers is the width direction of the blade, the intermediate layer has a degree of oxidation of the carbon fibers than the surface layer. A light-shielding blade for cameras that is large.
JP3118329A 1991-05-23 1991-05-23 Shade feather for camera Expired - Fee Related JP2503375B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3118329A JP2503375B2 (en) 1991-05-23 1991-05-23 Shade feather for camera

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3118329A JP2503375B2 (en) 1991-05-23 1991-05-23 Shade feather for camera

Publications (2)

Publication Number Publication Date
JPH04345146A JPH04345146A (en) 1992-12-01
JP2503375B2 true JP2503375B2 (en) 1996-06-05

Family

ID=14733974

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3118329A Expired - Fee Related JP2503375B2 (en) 1991-05-23 1991-05-23 Shade feather for camera

Country Status (1)

Country Link
JP (1) JP2503375B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7038994B2 (en) * 2017-10-16 2022-03-22 国立大学法人金沢大学 Manufacturing method of carbon fiber reinforced plastic, carbon fiber reinforced plastic and cellulosic resin

Also Published As

Publication number Publication date
JPH04345146A (en) 1992-12-01

Similar Documents

Publication Publication Date Title
JP5498219B2 (en) Manufacturing method of optical waveguide having mirror surface and photoelectric composite wiring board
US8329085B2 (en) Process for manufacturing a panel made of a thermoplastic composite
US11401912B2 (en) Flexible balsa wood panel, a rotor blade, a wind turbine and a method
EP2221168B1 (en) Method of making a window skin panel
JP2503375B2 (en) Shade feather for camera
EP2359172B1 (en) Method for forming mirror-reflecting film in optical wiring board
WO2021185263A1 (en) Wind power blade, stringer reinforcement structure thereof, and method
JPS58169102A (en) Reflecting mirror
JP2526832B2 (en) Plate material for shading blades
US20220364548A1 (en) A method and a system for assembling blade parts of a wind turbine blade
JPH0516013B2 (en)
EP3034283A1 (en) Method of forming a laminar composite structure
JP4513005B2 (en) Method for manufacturing flexible optical waveguide
JP4191463B2 (en) Flex beam
EP2886317A1 (en) Method of manufacturing net edge core and a method of bonding net edge core to a substructure
JP2006039231A (en) Method for manufacturing photoelectric wiring consolidated board
JPS63165828A (en) Shutter for optical apparatus and stop laminate
JP2552649Y2 (en) Shade feather for camera
JP2009031582A (en) Method for manufacturing optical waveguide
JP4224259B2 (en) Manufacturing method of opto-electric hybrid board
JP4962265B2 (en) Optical waveguide manufacturing method
JP2010060821A (en) Flexible optical and electrical wiring and manufacturing method thereof
RU2020123363A (en) Vessel hull (device and manufacturing method)
JP3109120B2 (en) Plate material for shading blades
JP2532442Y2 (en) Sliding sheet

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees