DE727599C - Hot rope hook for bomb loading devices on aircraft - Google Patents

Hot rope hook for bomb loading devices on aircraft

Info

Publication number
DE727599C
DE727599C DEH162510D DEH0162510D DE727599C DE 727599 C DE727599 C DE 727599C DE H162510 D DEH162510 D DE H162510D DE H0162510 D DEH0162510 D DE H0162510D DE 727599 C DE727599 C DE 727599C
Authority
DE
Germany
Prior art keywords
hook
aircraft
hot
rope hook
loading devices
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
DEH162510D
Other languages
German (de)
Inventor
Richard Toepfer
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.)
Heinkel Flugzeugwerke E GmbH
Original Assignee
Heinkel Flugzeugwerke E GmbH
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 Heinkel Flugzeugwerke E GmbH filed Critical Heinkel Flugzeugwerke E GmbH
Priority to DEH162510D priority Critical patent/DE727599C/en
Application granted granted Critical
Publication of DE727599C publication Critical patent/DE727599C/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/22Taking-up articles from earth's surface

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)

Description

Heißseilhaken für Bombenladeeinrichtungen bei Flugzeugen Gegenstand der Erfindung ist ein Heißseilhaken für Bo:mb:enladeeinrichtu,ngen bei Flugzeugen, der mittels Kardangelenk am Heißseilende befestigt ist und sich mit seinem dem Maul abgekehrten Ende ,gegen die zu fassende Last anlegt.Hot rope hook for bomb loading equipment on aircraft The invention is a hot rope hook for loading equipment in aircraft, which is attached to the end of the hot rope by means of a cardan joint and which is connected to its mouth remote end, bears against the load to be grasped.

Es ist bereits bekannt, die Beweglichkeit eines sich gegen die zu fassende Last anlegenden H:eißseilhakens gegenüber dem mit ihm in Verbindung stehenden Heißseil durch eine über den oberen Hakenteil vorstehende Schulter zu sichern. Bei einer bekannten Anordnung dieser Art ist der Heißseilhaken zweiarmgausgebildet und mit seinem einen Arm drehbar in einem joch- o. dgl. -förmi,gen Lagerteil angeordnet, das .am Heißseilende b;efestigt ist und die sich Besen die zu fassende Last anlegende Schulter trägt.It is already known the agility of one against the too hoisting rope hook to hold the load opposite to the one in contact with it To secure the hot rope by a shoulder protruding over the upper part of the hook. at In a known arrangement of this type, the hot cable hook is designed with two arms and with one arm rotatable in a yoke or the like arranged in a bearing part, the end of the hot rope is fixed and the broom is applying the load to be grasped Shoulder carries.

Gemäß. der Erfindung wird bei einem kardanisch am Heißseilende aasgelenkten Heißseilhaken diese Anordnung dadurch vereinfacht, daß das sich gegen die Last anlegende, dem Maul ,abgekehrte Hakenende durch ,eine über den Kardanring hinaus vorstehende, ,an den den Kardanring tonfassenden Gabelteilen sitzende Schulter gebildet ist. Diese Ausführung erfordert weder einen zweiarmigen Heißseilhaken noch ein besonderes, den Iiardanring umgebendes joch- o. dgl. -förmiges Lagerteil für den Haken.According to. the invention is aasgelenkten with a gimbal at the end of the hot rope Hot rope hook simplifies this arrangement by the fact that the through the mouth, facing away from the hook end, a protruding beyond the gimbal ring, , on which the gimbal tone holding fork parts seated shoulder is formed. This version does not require a two-armed hot rope hook or a special, the yoke surrounding the Iardan ring or the like. -shaped bearing part for the hook.

In der beiliegenden Zeichnung ist der Erfindumgsgegenstand in beispielsweiser Ausführungsform, dargestellt. Es zeigt: Abb. i eise Amvendungsbeispiel des erfindungsgemäßen Heißseilhakens, Abb. a eine Vorderansicht mit teilweisem Längsschnitt, Abb. 3 eine Seitenansicht und Abb. d. einen Querschnitt durch den Iiarda.nring.In the accompanying drawing, the subject of the invention is shown by way of example Embodiment shown. It shows: Fig. 1 an example of use of the invention Hot rope hook, Fig. A a front view with a partial longitudinal section, Fig. 3 a Side view and Fig. D. a cross section through the Iiarda.nring.

Es bezeichnet a einen Heißseilhaken und b ein Heißseil, dessen Ende z. B. durch Eingießen in dein trichterförmigen Ansatz eines Kopfstückes c befestigt ist. Das Kopfstück c ist mit Bolze:ng im Iiardanring @d und zusammen mit dem Isardanring d mit Bolzen e in einer Gabelung des Hakens a, schwenkbar gelagert. Um die Beweglichkeit des Kardaiiringes;d bei an der Last anliegendem Haken a zu sichern, besitzen die Gabelteile des Hakens a Schultern h, die über den Umfang des Iiardanringes;d hinaus vorstehen.It denotes a hot rope hook and b a hot rope, the end of which z. B. is attached by pouring into your funnel-shaped approach of a head piece c. The head piece c is pivotably mounted with a bolt: ng in the Iiardanring @d and together with the Isardanring d with bolt e in a fork of the hook a. In order to ensure the mobility of the cardai ring; d when the hook a is in contact with the load, the fork parts of the hook a have shoulders h which protrude beyond the circumference of the Iardan ring; d.

Claims (1)

PATENTANSPRUCH: Heißseilhak e:n für Bombenladeeinrichtungen bei Flugzeugen, der mittels Kardangelenk .am Heifz'>seilende befestigt ist und sich an seinem dem Maul abgekehrten Ende gegen die zu fassende Last anlegt, dadurch gekennzeichnet, daß das sich gegen die Last anlegende, dem Maul ab-,gekeh rte Hakenende durch eine über den Kardanring (d) hinaus vorstehende, an den den ILardanrin,g umfassenden Gabelteilen sitzende Schulter (h) ,gebildet ist.PATENT CLAIM: Hot rope hook e: n for bomb loading devices on aircraft, which is attached to the Heifz '> rope end by means of a cardan joint and attaches to its Mouth facing away from the end against the load to be grasped, characterized in that that the end of the hook, which rests against the load and is turned away from the mouth, is protruding beyond the cardan ring (d) to the one encompassing the I-cardan ring, g Fork parts seated shoulder (h), is formed.
DEH162510D 1940-06-16 1940-06-16 Hot rope hook for bomb loading devices on aircraft Expired DE727599C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEH162510D DE727599C (en) 1940-06-16 1940-06-16 Hot rope hook for bomb loading devices on aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEH162510D DE727599C (en) 1940-06-16 1940-06-16 Hot rope hook for bomb loading devices on aircraft

Publications (1)

Publication Number Publication Date
DE727599C true DE727599C (en) 1942-11-06

Family

ID=7183673

Family Applications (1)

Application Number Title Priority Date Filing Date
DEH162510D Expired DE727599C (en) 1940-06-16 1940-06-16 Hot rope hook for bomb loading devices on aircraft

Country Status (1)

Country Link
DE (1) DE727599C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2531402A1 (en) * 2010-02-01 2012-12-12 Dart Aerospace Ltd. Helicopter cargo basket mounting assembly and method of using same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2531402A1 (en) * 2010-02-01 2012-12-12 Dart Aerospace Ltd. Helicopter cargo basket mounting assembly and method of using same
EP2531402A4 (en) * 2010-02-01 2013-07-17 Dart Aerospace Ltd Helicopter cargo basket mounting assembly and method of using same

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