DE392511C - Bracing for aircraft - Google Patents

Bracing for aircraft

Info

Publication number
DE392511C
DE392511C DEL56507D DEL0056507D DE392511C DE 392511 C DE392511 C DE 392511C DE L56507 D DEL56507 D DE L56507D DE L0056507 D DEL0056507 D DE L0056507D DE 392511 C DE392511 C DE 392511C
Authority
DE
Germany
Prior art keywords
bracing
aircraft
eye
lamellas
achieve
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
Application number
DEL56507D
Other languages
German (de)
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.)
JEAN ALFRED LATHAM
Original Assignee
JEAN ALFRED LATHAM
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 JEAN ALFRED LATHAM filed Critical JEAN ALFRED LATHAM
Priority to DEL56507D priority Critical patent/DE392511C/en
Application granted granted Critical
Publication of DE392511C publication Critical patent/DE392511C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • D—TEXTILES; PAPER
    • D07—ROPES; CABLES OTHER THAN ELECTRIC
    • D07B—ROPES OR CABLES IN GENERAL
    • D07B5/00—Making ropes or cables from special materials or of particular form
    • D07B5/005—Making ropes or cables from special materials or of particular form characterised by their outer shape or surface properties
    • D—TEXTILES; PAPER
    • D07—ROPES; CABLES OTHER THAN ELECTRIC
    • D07B—ROPES OR CABLES IN GENERAL
    • D07B1/00—Constructional features of ropes or cables
    • D07B1/06—Ropes or cables built-up from metal wires, e.g. of section wires around a hemp core
    • D07B1/0693—Ropes or cables built-up from metal wires, e.g. of section wires around a hemp core having a strand configuration
    • D—TEXTILES; PAPER
    • D07—ROPES; CABLES OTHER THAN ELECTRIC
    • D07B—ROPES OR CABLES IN GENERAL
    • D07B2201/00—Ropes or cables
    • D07B2201/20—Rope or cable components
    • D07B2201/2001—Wires or filaments
    • D07B2201/2002—Wires or filaments characterised by their cross-sectional shape
    • D07B2201/2003—Wires or filaments characterised by their cross-sectional shape flat

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Joining Of Building Structures In Genera (AREA)

Description

Verspannung für Luftfahrzeuge. Die Erfindung betrifft eine Verspannung für Luftfahrzeuge, Wasserfahrzeuge, Wasserflugzeuge usw. zum Ersatz der bisher üblichen Wanten oder Verspannungen aus Metall- oder Stahlkabeln,, diel sich beim Gebrauch verlängern, häufigen Brüchen ausgesetzt sind und durch Spleißen miteinander verbunden werden mußten.Bracing for aircraft. The invention relates to a bracing for aircraft, watercraft, seaplanes, etc. to replace the previously common Shrouds or braces made of metal or steel cables, which change during use elongate, subject to frequent breaks and bonded together by splicing had to be.

Die Verspannung nach der Erfindung besteht im wesentlichen, aus einer Reihe von auf- oder nebeneinandergelegtenMetallblättern oder Lamellen, die einfach ohne Verbindung miteinander in beliebiger Richtung mit nach außen abnehmender Breite nebeneinandergelegt sind. Die äußeren verbreiterten Enden tragen ein Loch oder Öhr. in welches die anzuschließende Achse oder Welle hineinpaßt. Um den aerodynamischen Wirkungsgrad zu verbessern und ein windschnittiges Profil zu erzielen, kann das Lamellenbündel verleimt oder mit irgendeiner Umhüllung aus beliebigem Stoff versehen sein, um ein glattes Profil zu erzielen.The bracing according to the invention consists essentially of one Series of stacked or juxtaposed metal sheets or lamellas that simply without connection to each other in any direction with an outwardly decreasing width are placed next to each other. The outer widened ends have a hole or an eye. into which the axis or shaft to be connected fits. To the aerodynamic Improving efficiency and achieving a streamlined profile can do that Laminated bundles glued or with any covering from any Fabric should be provided to achieve a smooth profile.

Die Erfindung ist-in der Zeichnung in mehreren Ausführungsformen dargestellt. Die Abb. i zeigt einen Querschnitt durch eine Verspannung aus neben- bzw. aufeinandergelegten Metallamellen a, deren Breite von den mittleren Lamellen aus abnimmt.The invention is shown in several embodiments in the drawing. Fig. I shows a cross-section through a bracing made of juxtaposed or superimposed Metal slats a, the width of which decreases from the central slats.

In Abb. 2 sind die Lamellen a anders, nämlich, senkrecht zur Anbringung nach Abb. i sorgesehen.In Fig. 2 the slats a are different, namely, perpendicular to the attachment as shown in Fig. i.

Zur Erzielung eines windschnittigen Profiles nimmt die Breite der Lamellen nach außen ab, auch kann das die Lamellen a enthaltende Bündel verleimt, verkittet, gestrichen usw. werden, wodurch man auf der. Oberfläche eine glatte Umhüllung b aus beliebigem Stoff schafft.To achieve a streamlined profile, the width of the Lamellas outwards, the bundle containing the lamellas a can also be glued, cemented, painted, etc. Surface a smooth envelope b creates from any material.

Der Anschluß einer so zusammengesetzten, ohne Verspleißung hergestellten Verspannung erfolgt nach den Abb. 3 und d.. Die Enden der Lamellen a sind bei c zu breiten Köpfen mit öhr oder Loch d verbreitert, durch welches die anzuschließende Achse d hindurchgeht. Der Widerstand oder die Beanspruchung jedes Loches oder Auges d ist gleich dem Widerstand oder der Beanspruchung der entsprechenden Metallamelle.The connection of a so assembled, produced without splicing Bracing takes place according to Fig. 3 and d .. The ends of the lamellas a are at c widened to wide heads with an eye or hole d through which the to be connected Axis d passes through. The resistance or stress of each hole or eye d is equal to the resistance or stress of the corresponding metal lamella.

Claims (3)

PATENT-ANsPRticHEi i. Verspannung für Luftfahrzeuge u. dgl., gekennzeichnet durch eine Reihe von Metallamellen (a), die einfach ohne Verbindung miteinander in beliebiger Richtung mit nach außen abnehmenden Breiten nebeneinandergelegt sind. PATENT CLAIM i. Bracing for aircraft and the like by a series of metal lamellas (a) that simply do not connect to each other are placed side by side in any direction with widths decreasing towards the outside. 2. Verspannung nach Anspruch i, dadurch gekennzeichnet, daß die Lamellen (a) verbreitert (c) und mit einem öhr (d) für den Durchtritt der Anschlußachse (e) versehen sind. 2. Bracing according to claim i, characterized in that the lamellae (a) widens (c) and are provided with an eye (d) for the passage of the connection axis (e). 3. Verspannung nach Anspruch i und 2, dadurch gekennzeichnet, daß das Lamellenbündel (a) mit einer aufgebrachten Umhüllung (b) aus beliebigem Stoff versehen ist, um ein glattes Profil zu erzielen. 3. Bracing according to claim i and 2, characterized in that the lamella bundle (a) is provided with an applied covering (b) made of any material in order to achieve a smooth profile.
DEL56507D 1922-10-01 1922-10-01 Bracing for aircraft Expired DE392511C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEL56507D DE392511C (en) 1922-10-01 1922-10-01 Bracing for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEL56507D DE392511C (en) 1922-10-01 1922-10-01 Bracing for aircraft

Publications (1)

Publication Number Publication Date
DE392511C true DE392511C (en) 1924-03-26

Family

ID=7277819

Family Applications (1)

Application Number Title Priority Date Filing Date
DEL56507D Expired DE392511C (en) 1922-10-01 1922-10-01 Bracing for aircraft

Country Status (1)

Country Link
DE (1) DE392511C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019175388A3 (en) * 2018-03-15 2019-10-24 Future Fibres, LLC Multi-strand composite fiber tensioning cable

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019175388A3 (en) * 2018-03-15 2019-10-24 Future Fibres, LLC Multi-strand composite fiber tensioning cable

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