DE8633679U1 - Slat for shutters or blinds - Google Patents
Slat for shutters or blindsInfo
- Publication number
- DE8633679U1 DE8633679U1 DE19868633679 DE8633679U DE8633679U1 DE 8633679 U1 DE8633679 U1 DE 8633679U1 DE 19868633679 DE19868633679 DE 19868633679 DE 8633679 U DE8633679 U DE 8633679U DE 8633679 U1 DE8633679 U1 DE 8633679U1
- Authority
- DE
- Germany
- Prior art keywords
- slat
- carbon fiber
- slat according
- fibers
- approximately
- 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
Links
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 14
- 239000004917 carbon fiber Substances 0.000 claims description 14
- 239000000835 fiber Substances 0.000 claims description 12
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 12
- 239000004744 fabric Substances 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 4
- 230000002787 reinforcement Effects 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 239000004760 aramid Substances 0.000 claims description 2
- 229920006231 aramid fiber Polymers 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 claims description 2
- 229920003002 synthetic resin Polymers 0.000 claims description 2
- 239000000057 synthetic resin Substances 0.000 claims description 2
- 229920001169 thermoplastic Polymers 0.000 claims description 2
- 239000004416 thermosoftening plastic Substances 0.000 claims description 2
- 244000309464 bull Species 0.000 claims 1
- 241000446313 Lamella Species 0.000 description 12
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
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
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Diaphragms For Cameras (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Description
Die Erfindung betrifft eine Lamelle für lichtoptische Verschlüsse und Blenden optischer Geräte, z.B. fotographischer Kameras bzw. fotographischer Objektive.The invention relates to a blade for light-optical shutters and apertures of optical devices, e.g. photographic cameras or photographic lenses.
Derartige Lamellen müssen hinsichtlich ihrer Festigkeit und Steifigkeit hohen Anforderungen gerecht werden. Zugleich aber wird eine möglichst geringe Masse gefordert, um immer kürzere Verschlußzeiten realisieren zu können.Such blades must meet high requirements in terms of strength and rigidity. At the same time, however, the mass must be as low as possible in order to be able to achieve ever shorter shutter speeds.
Um diesen Anforderungen wenigstens annähernd gerecht zu werden, werden die Lamellen im Stand der Technik aus Stahl-Titan- oder Aluminiumblech hergestellt, wobei Sickenversteifungen oder geätzte Profilgebung vorgesehen werden können.In order to at least approximately meet these requirements, the slats are manufactured from steel, titanium or aluminum sheet in the state of the art, whereby bead reinforcements or etched profiles can be provided.
Der Erfindung liegt die Aufgabe zugrunde, die Lamellen hinsichtlich ihrer spezifischen Festigkeit und Steifigkeit zu verbessern ohne die Masse der Lamellen erhöhen zu müssen. Angestrebt wird vielmehr eine Verringerung der Masse.The invention is based on the task of improving the slats in terms of their specific strength and rigidity without having to increase the mass of the slats. Rather, the aim is to reduce the mass.
Diese Aufgabe wird erfindungsgemäß gelöst durch einen Strukturfaserverbundwerkstoff, der vorzugsweise Kohlenstoff- oder Aramidfasern aufweist, die in einer Kunstharz-Matrix.vorzugsweise einer Thermoplast-Matrix, eingebettet sind.This object is achieved according to the invention by a structural fiber composite material, which preferably has carbon or aramid fibers embedded in a synthetic resin matrix, preferably a thermoplastic matrix.
Theodor-Heuss-Straße 2 D-3300 BraunschweigTheodor-Heuss-Strasse 2 D-3300 Braunschweig
Bundesrepublik DeutschlandFederal Republic of Germany
Telefon Telex TetegrarTelephone Telex Tetegrar
0531-80079 0952620grammd se Patent Braunschweig0531-80079 0952620grammd se Patent Braunschweig
ttftCCttftCC
Dabei hat sich eine drei- oder mehrlagige Ausbildung der Lamel- ! Ie als vorteilhaft ergeben.A three- or multi-layer design of the lamellae has proven to be advantageous.
j In einer speziellen Ausführungsform ist vorgesehen, daß bei einer dreilagigen Ausbildung die Mittellage ein ca. 60 % j In a special embodiment, it is provided that in a three-layer design the middle layer has an approx. 60 %
'< Kohlenstoffaser-Prepreg ist, das beidseitig mit je einem Kohlenstoffaser-Flies oder -Gewebe verpreßt ist. Dabei verlau- '< Carbon fiber prepreg is pressed on both sides with a carbon fiber fleece or fabric.
; fen die in einem Prepreg unidirektionalen Fasern vorzugsweise in Längsrichtung der Lamelle.; the unidirectional fibers in a prepreg are preferably in the longitudinal direction of the lamella.
In einer Alternativlösung können bei einer dreilagigen Ausbildung der Lamelle auch alle drei Lagen aus dem genannten Prepreg bestehen, wobei dann die Fasern in den beiden Außenlagen in Lamellen-Längsrichtung, in der mittleren Lage jedoch angenähert quer hierzu verlaufen.In an alternative solution, if the lamella is designed in three layers, all three layers can consist of the prepreg mentioned, with the fibers in the two outer layers running in the longitudinal direction of the lamella, but in the middle layer running approximately transversely to this.
Bei einer dreilagigen Ausbildung der Lamelle ist es aber auch möglich, daß nur die beiden Außenlagen aus dem genannten Prepreg bestehen, dessen Fasern wiederum in Lamellen-Längsrichtung orientiert sind, während die mittlere Lage aus einem Kohlenstoffaser-Fl ies oder -Gewebe besteht.However, with a three-layer design of the lamella, it is also possible that only the two outer layers consist of the aforementioned prepreg, whose fibers are again oriented in the longitudinal direction of the lamella, while the middle layer consists of a carbon fiber fleece or fabric.
Die Lamelle ist im Bereich ihrer Drehachse sowie im Angriffsbereich der die Lamelle steuernden Elemente besonders stark be- ; lastet. Erfindungsgemäß können insbesondere in diesen belastungs kritischen Bereichen zusätzliche Verstärkungslagen vorgesehen j werden.The slat is subjected to particularly high loads in the area of its axis of rotation and in the area of action of the elements controlling the slat. According to the invention, additional reinforcement layers can be provided in particular in these load-critical areas.
' Lamellen gemäß der Erfindung sind den herkömmlichen Ausführungsformen hinsichtlich der spezifischen Festigkeit und Steifigkeit überlegen und weisen überdies noch eine geringere Masse auf. i Hierdurch lassen sich kürzere Verschlußzeiten bzw. eine höhere ; Dauerstandfestigkeit erzielen. Als zusätzlicher Vorteil ergibt ' sich bei einem Kohlenstoffaser-Laminat-System noch die sonst \ extra herzustellende matt-schwarze Oberfläche.' Lamellas according to the invention are superior to conventional designs in terms of specific strength and rigidity and also have a lower mass. This allows shorter shutter times and a higher fatigue strength. An additional advantage of a carbon fiber laminate system is the matt black surface that would otherwise have to be produced separately .
In der Zeichnung sind vier als Beispiele dienende Ausführungsformen der Erfindung dargestellt. Dabei zeigen die Figuren 1 bis 4 in jeweils gleicher Darstellung eine dreilagige Lamelle mit unterschiedlichem Aufbau.The drawing shows four embodiments of the invention as examples. Figures 1 to 4 each show a three-layer slat with a different structure in the same representation.
Bei der Lamelle gemäß Figur 1 besteht die mittlere Lage aus einem ca. 60 % Kohlenstoffaser-Prepreg 1, das beidseitig mit je einem Kohlenstoffaser-Flies oder -Gewebe 2 verpreßt ist. Dabei ist erkennbar, daß die in einem Prepreg unidirektional orientierten Fasern in Längsrichtung der Lamelle verlaufen.In the lamella according to Figure 1, the middle layer consists of an approximately 60 % carbon fiber prepreg 1, which is pressed on both sides with a carbon fiber fleece or fabric 2. It can be seen that the unidirectionally oriented fibers in a prepreg run in the longitudinal direction of the lamella.
Bei der Lamelle gemäß Figur 2 bestehen alle drei Lagen aus einem Prepreg 1, wobei die Fasern in den beiden Außenlagen in Lamellen-Längsrichtung und in der mittleren Lage angenähert quer hierzu verlaufen.In the lamella according to Figure 2, all three layers consist of a prepreg 1, with the fibers in the two outer layers running in the longitudinal direction of the lamella and in the middle layer running approximately transversely thereto.
Bei der Ausflihrungsform gemäß Figur 3 sind die Lagen im Vergleich zu der Ausbildung gemäß Figur 1 vertauscht: Die beiden Außenlagen bestehen jeweils aus einem Prepreg 1, wobei die Fasern in Lamellen-Längsrichtung orientiert sind, während die mittlere Lago aus einem Kohlenstoffaser-Flies oder -Gewebe 2 besteht.In the embodiment according to Figure 3, the layers are swapped in comparison to the design according to Figure 1: The two outer layers each consist of a prepreg 1, with the fibers oriented in the longitudinal direction of the lamella, while the middle layer consists of a carbon fiber fleece or fabric 2.
Figur 4 läßt erkennen, daß die dargestellte Lamelle in ihrem Hauptteil dreilagig ausgebildet ist, in ihren belastungskritischen Bereichen jedoch zusätzliche Verstärkungslagen 3 aufweist.Figure 4 shows that the lamella shown is constructed in three layers in its main part, but has additional reinforcement layers 3 in its load-critical areas.
Die in den Figuren 1 bis 3 dargestellten Alternativlösungen lassen sich analog auch für z.B. fünf- oder sieben-lagig ausgebildete Lamellen durchführen.The alternative solutions shown in Figures 1 to 3 can also be implemented analogously for slats with five or seven layers, for example.
Gr/Gru.Gr/Gru.
Claims (1)
• ·•t
·
Gramm + Lins
Gr/Gru.Patent attorneys
Gram + Lins
Gr/Gru.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19868633679 DE8633679U1 (en) | 1986-12-17 | 1986-12-17 | Slat for shutters or blinds |
DE19873736318 DE3736318A1 (en) | 1986-12-17 | 1987-10-27 | Blade (vane, lamella) for shutters or diaphragms |
JP31541787A JPS63165828A (en) | 1986-12-17 | 1987-12-15 | Shutter for optical apparatus and stop laminate |
FR8717569A FR2608793B1 (en) | 1986-12-17 | 1987-12-16 | BLADE FOR SHUTTERS OR DIAPHRAGMS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19868633679 DE8633679U1 (en) | 1986-12-17 | 1986-12-17 | Slat for shutters or blinds |
Publications (1)
Publication Number | Publication Date |
---|---|
DE8633679U1 true DE8633679U1 (en) | 1987-02-05 |
Family
ID=6801209
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19868633679 Expired DE8633679U1 (en) | 1986-12-17 | 1986-12-17 | Slat for shutters or blinds |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS63165828A (en) |
DE (1) | DE8633679U1 (en) |
FR (1) | FR2608793B1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0431931A2 (en) * | 1989-12-07 | 1991-06-12 | Nikon Corporation | Plate member for use as material of light shielding blades |
DE4016187C1 (en) * | 1990-05-19 | 1991-07-11 | Rollei Fototechnic Gmbh & Co. Kg, 3300 Braunschweig, De | Prodn. of multilayer closure or screening lamina - form carbon fibre reinforced, hardenable synthetic resin |
EP0477783A2 (en) * | 1990-09-25 | 1992-04-01 | Nikon Corporation | Member for light shielding blades |
US5202715A (en) * | 1989-12-07 | 1993-04-13 | Nikon Corporation | Plate member for use as material of light shielding blades |
US6001465A (en) * | 1997-05-12 | 1999-12-14 | Copal Company Limited | Light shielding blade for camera made of para-orientation aromatic polyamide film |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009020596A1 (en) * | 2009-02-05 | 2010-08-19 | Prontor Gmbh | Central closure i.e. spring-loaded electromagnetic central closure, for camera, has sectors pivoted in groove when cam ring rotates between opened and closed positions of groove, and drive device driving cam ring in direction of rotation |
JP5614384B2 (en) * | 2011-07-26 | 2014-10-29 | 株式会社豊田自動織機 | Reinforcing fiber sheet, fiber-reinforced composite material, method for producing reinforcing fiber sheet, and method for producing fiber-reinforced composite material |
JP7547742B2 (en) * | 2020-02-28 | 2024-09-10 | ニデック株式会社 | Manufacturing method of fiber-reinforced substrate, manufacturing method of fiber-reinforced substrate and shutter blade |
JP2021134306A (en) * | 2020-02-28 | 2021-09-13 | 日本電産株式会社 | Method for manufacturing fiber-reinforced base material, and method for manufacturing shutter blade |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0668594B2 (en) * | 1986-07-09 | 1994-08-31 | 東邦レーヨン株式会社 | Carbon fiber reinforced thermosetting resin camera shutter blades |
-
1986
- 1986-12-17 DE DE19868633679 patent/DE8633679U1/en not_active Expired
-
1987
- 1987-12-15 JP JP31541787A patent/JPS63165828A/en active Pending
- 1987-12-16 FR FR8717569A patent/FR2608793B1/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0431931A2 (en) * | 1989-12-07 | 1991-06-12 | Nikon Corporation | Plate member for use as material of light shielding blades |
EP0431931A3 (en) * | 1989-12-07 | 1992-05-13 | Nikon Corporation | Plate member for use as material of light shielding blades |
US5202715A (en) * | 1989-12-07 | 1993-04-13 | Nikon Corporation | Plate member for use as material of light shielding blades |
DE4016187C1 (en) * | 1990-05-19 | 1991-07-11 | Rollei Fototechnic Gmbh & Co. Kg, 3300 Braunschweig, De | Prodn. of multilayer closure or screening lamina - form carbon fibre reinforced, hardenable synthetic resin |
EP0477783A2 (en) * | 1990-09-25 | 1992-04-01 | Nikon Corporation | Member for light shielding blades |
EP0477783A3 (en) * | 1990-09-25 | 1992-10-28 | Nikon Corporation | Member for light shielding blades |
US6001465A (en) * | 1997-05-12 | 1999-12-14 | Copal Company Limited | Light shielding blade for camera made of para-orientation aromatic polyamide film |
Also Published As
Publication number | Publication date |
---|---|
FR2608793A1 (en) | 1988-06-24 |
FR2608793B1 (en) | 1990-07-20 |
JPS63165828A (en) | 1988-07-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE68904601T2 (en) | FIBER REINFORCED FRAME, ESPECIALLY AN AIRCRAFT HULL, AND ITS MANUFACTURING METHOD. | |
EP0065087B1 (en) | Flexing spring of compound fibre material | |
DE102004025381B4 (en) | Window frame for aircraft | |
EP3496936A1 (en) | Spar cap made of prefabricated elements with laid fabric and method for producing same | |
DE8633679U1 (en) | Slat for shutters or blinds | |
DE3632472A1 (en) | MOTORCYCLE DISC | |
EP0902148A2 (en) | Solid or hollow section member of fibre-reinforced plastics | |
DE2406348C2 (en) | Torsional vibration damping device | |
DE10002671B4 (en) | Laminated glass for security motor vehicles | |
EP0063260B1 (en) | Concrete pipe with inner lining | |
DE202006004646U1 (en) | Composite of two sandwich panels | |
DE8601811U1 (en) | Self-supporting or supporting body for passenger cars | |
DE3402532C2 (en) | ||
DE3736318A1 (en) | Blade (vane, lamella) for shutters or diaphragms | |
DE3510294C1 (en) | Boom for sailboards | |
DE19737284C1 (en) | Adjustable covering device | |
DE2834849A1 (en) | Process for the production of a translucent synthetic resin hollow chamber profile panel with a structured, light diffusing surface | |
DE102007048003A1 (en) | Producing constructional elements from fiber-reinforced plastic, useful e.g. in motor sports for mudguard of racing car, comprises applying fiber layers on one another and soaking in synthetic resin and masking outer constructional element | |
DE3302770A1 (en) | Energy-absorbing laminate | |
DE69705682T2 (en) | Composite construction | |
DE202014101275U1 (en) | Hollow chamber profile, in particular window or door hollow chamber profile | |
DE8717466U1 (en) | Ridge sealing and ventilation element with underlying sealing strips | |
EP3621065B1 (en) | Insulation element | |
CH637607A5 (en) | Intruder-proof security glass sheet | |
EP0284878A1 (en) | Light construction core, particularly a supporting core for skis |