EP0020225A1 - Safety release device for a transportable load suspended by an aircraft - Google Patents

Safety release device for a transportable load suspended by an aircraft Download PDF

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Publication number
EP0020225A1
EP0020225A1 EP80400670A EP80400670A EP0020225A1 EP 0020225 A1 EP0020225 A1 EP 0020225A1 EP 80400670 A EP80400670 A EP 80400670A EP 80400670 A EP80400670 A EP 80400670A EP 0020225 A1 EP0020225 A1 EP 0020225A1
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EP
European Patent Office
Prior art keywords
ring
bus bar
hook
safety device
carrier vehicle
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.)
Granted
Application number
EP80400670A
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German (de)
French (fr)
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EP0020225B1 (en
Inventor
-Noel Fulchiron
Bernard Naillon
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.)
Thomson-Brandt SA
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Thomson-Brandt SA
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Filing date
Publication date
Application filed by Thomson-Brandt SA filed Critical Thomson-Brandt SA
Priority to AT80400670T priority Critical patent/ATE2659T1/en
Publication of EP0020225A1 publication Critical patent/EP0020225A1/en
Application granted granted Critical
Publication of EP0020225B1 publication Critical patent/EP0020225B1/en
Expired legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C14/00Mechanical fuzes characterised by the ammunition class or type
    • F42C14/06Mechanical fuzes characterised by the ammunition class or type for fall bombs

Definitions

  • the invention relates to a safety device for dropping a load intended to be suspended from an aircraft for its transport. It also relates to any load equipped with such a device.
  • the object of the present invention is to solve this problem and relates to a combination of means cooperating with each other so that the unlocking of the devices controlling the use of the load carried, can only intervene if the system for attaching this load is well released from the wearer.
  • the invention relates more particularly to a safety device for dropping at least one load suspended from a carrier vehicle, of the aircraft type, characterized in that it comprises: on the one hand, a bus bar capable of occupying a first so-called "safety" position preventing any unlocking at the load level, even if the orders were given, and a so-called "armed” position allowing the execution of these orders; on the other hand a system for attaching the load to the hook of the carrier vehicle, provided with means cooperating with the bus bar so that, as long as the hook is not detached from the attachment member, the translation from the busbar from its "safety” position to its "armed” position is impossible.
  • Figure 1 In Figure 1 are shown locks 1, 2, 3 (by way of example three in number) and the control means associated therewith 4, 5, 6 intended to ensure their unlocking, thereby releasing the member or members contained in a container (not shown in the figure) that they locked.
  • It can be military charges, elementary tanks, modules, intended to be released together or successively, that is to say on demand. All of these organs and their control accessories are attached to the carrier vehicle (not shown) by means of a hanging system.
  • It is for example at least one ring 7, integral with the body containing the elementary modules, into the lumen 80 from which the hook of the carrying means (not visible in the figure), itself integral with the carrier vehicle, penetrates. The separation takes place when the hook is deliberately detached from the ring, thereby releasing the ring-hook connection.
  • a device 10 having the character of a general mechanical control member, is provided.
  • This busbar 10 can occupy two positions: the first so-called “safety” position (the one shown in the figure) and a second position called the “armed” position.
  • the displacement of this bar can be controlled by any known means.
  • a cable 11 which can be a releasable safety cable with an SLC base, is stressed in tension at one of its ends 12.
  • a set of pulleys 13, 14 and 15 and of the spring 16 it acts on the spring 17 which compresses against the stop 18, thereby releasing a movable locking finger 19 which retracts.
  • the bus bar 10 previously held in its safety position by this finger 19 is released and, under the action of the return spring 20, moves back, translates in a given direction (for example that of the arrow 21) towards its position called “army”.
  • Housing 25, 26 and 27 are provided in this bus bar.
  • An example bus lock-bar combination is described below.
  • These housings intended to cooperate with the locks comprise two parts: a first open cavity having a profile with a substantially circular section of diameter D and a second open cavity having a profile with a substantially rectangular section of width D much less than D.
  • the locks in the example described, for example have two parts: the first, of cylindrical section, with a diameter very slightly less than D can move in the first cavity and therefore be unlocked; the second has a thinned section over a length L slightly greater than the thickness of the busbar and can only move in the second cavity over a short stroke corresponding approximately to this length L.
  • the unlocking orders depend on the sequence of operations chosen, either simultaneous or offset.
  • the busbar when moving from its "safety” position to its “armed” position, the busbar pushes through an additional housing 350 on a stud 35 which rotates (see the direction of arrow 36) the ring 7. If this ring 7 is still connected to the hook of the carrier vehicle, the hook-ring connection opposes this rotation and therefore opposes the movement of the busbar 10 from its "safety” position to its “armed” position. Consequently it is necessary that the separation of the ring from the hook of the carrier vehicle is effective for this movement to take place and for the unlocking of the locks 1, 2 and 3 to be possible. It is an extremely reliable security system which constitutes one of the main characteristics of the invention.
  • FIG. 2 is a schematic representation of an alternative embodiment of the combination of a bus bar 10 and a ring 7 cooperating in order to obtain the result stated above, namely the possible movement of the bus bar exclusively in the case where the hook of the carrier vehicle is well separated from the ring.
  • the ring 7 with its thread 70 intended to fix it to the container which must be transported and then released.
  • This ring 7 is connected, in this variant, to the bus bar 10 of the type which was described in the previous variant in the manner described below.
  • the first end of a lever arm or pallet 50 penetrates into the lumen 80 of the ring 7. This arm is articulated around a hinge pin 51.
  • FIG 3 is a schematic representation of another alternative embodiment of a combination according to the invention.
  • the ring does not rotate as in the case of Figure 1, but it rocks. Indeed it is held in place during the entire transport phase thanks to a lug 60 which takes place in a housing 61, provided for this purpose and formed in the bus bar 10 hampering the movement thereof.
  • This lug 60 leans upwards during transport against the structure of the container (not shown). It is held there as long as the hook of the carrier vehicle, by its presence inside the ring prevents a torsion spring 61 from playing its role.
  • FIG. 4 schematically represents an alternative embodiment in which the movement of the ring is vertical.
  • the ring 7 comprises, in addition to the lumen 80 intended to receive the hook of the carrier vehicle, a first cylindrical part 81 comprising a shoulder 82.
  • This cylindrical part 81 is contained in a housing 83 formed in the envelope 84 of the container which must support the ring, a spring 85 is provided between this shoulder 82 and one of the walls 86 of the housing 83.
  • the ring also comprises a second part 87 intended to penetrate into the bus bar 10. This second cylindrical part comprises a portion 90 thinned over a determined length. When the ring is suspended from the carrier hook, the spring 85 is compressed and the cylindrical part 87 is located in the circular section cavity 91 provided for this purpose in the bus bar 10.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)
  • Emergency Lowering Means (AREA)
  • Lock And Its Accessories (AREA)
  • Clamps And Clips (AREA)

Abstract

L'invention concerne un dispositif de sécurité de largage d'une charge suspendue à un aéronef. Une barre dite omnibus (10) occupe deux positions, la première dite de «sécurité», qui interdit le déverrouillage de tout organe de verrouillage lié à la charge, même si des ordres en étaient donnés, et une seconde position dite «armée» qui, en revanche, permet aux ordres donnés d'être exécutés. Avec cette barre, coopère un système d'accrochage de la charge qui comporte un certain nombre de moyens agissant de telle sorte que, tant que le crochet du véhicule porteur est solidaire du système d'accrochage, le déplacement de cette barre est impossible. Un tel système d'accrochage est constitué d'un anneau (7) capable de subir un mouvement, notamment de rotation, de translation dans un plan vertical, ou de basculement, seulement quand le crochet n'est plus présent dans la lumière (80) de l'anneau, ce mouvement libérant un moyen solidaire de l'anneau que entravait le mouvement de la barre. L'invention s'applique notamment au transport et au largage de charges militaires.The invention relates to a safety device for dropping a load suspended from an aircraft. A so-called bus bar (10) occupies two positions, the first called "security", which prohibits the unlocking of any locking member linked to the load, even if orders were given, and a second position called "armed" which , on the other hand, allows given orders to be executed. With this bar, a load hooking system cooperates which comprises a certain number of means acting so that, as long as the hook of the carrier vehicle is secured to the hooking system, the movement of this bar is impossible. Such a fastening system consists of a ring (7) capable of undergoing a movement, in particular of rotation, of translation in a vertical plane, or of tilting, only when the hook is no longer present in the light (80 ) of the ring, this movement releasing a means secured to the ring that hindered the movement of the bar. The invention applies in particular to the transport and dropping of military loads.

Description

L'invention concerne un dispositif de sécurité de largage d'une charge destinée à être suspendue à un aéronef pour son transport. Elle concerne également toute charge équipée d'un tel dispositif.The invention relates to a safety device for dropping a load intended to be suspended from an aircraft for its transport. It also relates to any load equipped with such a device.

Lorsqu'une charge est suspendue à un aéronef en vue d'être transportée vers son lieu de largage, il importe qu'un certain nombre de règles de sécurité soient respectées. Par exemple, s'il s'agit d'une charge militaire, la commande de mise à feu ne doit pouvoir intervenir que lorsque la séparation de la charge de son porteur est effective.When a load is suspended from an aircraft for transport to its drop location, it is important that a number of safety rules are observed. For example, in the case of a military charge, the firing command should only be able to intervene when the separation of the charge from its bearer is effective.

La présente invention a pour objet de résoudre ce problème et concerne une combinaison de moyens coopérant entre eux de telle sorte que le déverrouillage des dispositifs commandant l'utilisation de la charge portée, ne puissent intervenir que si le système d'accrochage de cette charge est bien libéré du porteur. L'invention concerne plus particulièrement un dispositif de sécurité de largage d'au moins une charge suspendue à un véhicule porteur, du type aéronef, caractérisé en ce qu'il comprend : d'une part, une barre omnibus capable d'occuper une première position dite "de sécurité" empêchant tout déverrouillage au niveau de la charge, même si les ordres étaient donnés, et une position dite "armée" permettant l'exécution de ces ordres ; d'autre part un système d'accrochage de la charge au crochet du véhicule porteur, muni de moyens coopèrant avec la barre omnibus de telle sorte que, tant que le crochet n'est pas désolidarisé de l'organe d'accrochage, la translation de la barre omnibus de sa position de "sécurité" vers sa position "armée" est impossible.The object of the present invention is to solve this problem and relates to a combination of means cooperating with each other so that the unlocking of the devices controlling the use of the load carried, can only intervene if the system for attaching this load is well released from the wearer. The invention relates more particularly to a safety device for dropping at least one load suspended from a carrier vehicle, of the aircraft type, characterized in that it comprises: on the one hand, a bus bar capable of occupying a first so-called "safety" position preventing any unlocking at the load level, even if the orders were given, and a so-called "armed" position allowing the execution of these orders; on the other hand a system for attaching the load to the hook of the carrier vehicle, provided with means cooperating with the bus bar so that, as long as the hook is not detached from the attachment member, the translation from the busbar from its "safety" position to its "armed" position is impossible.

L'invention sera mieux comprise à l'aide des explications qui vont suivre et des figures jointes parmi lesquelles :

  • la figure 1 représente schématiquement comment coopèrent entre eux, d'une part, le système d'accrochage d'une charge à son véhicule porteur et d'autre part un dispositif assurant la mise en position de déverrouillabilité de moyens verrouillant les organes essentiels dont le fonctionnement ne doit absolument intervenir que si la séparation entre la charge et son porteur est effective ;
  • les figures 2, 3 et 4 montrent schématiquement des variantes de réalisation d'une combinaison de moyens représentée sur la figure 1.
The invention will be better understood with the aid of the explanations which follow and of the appended figures among which:
  • Figure 1 shows schematically how cooperate with each other, on the one hand, the system for attaching a load to its carrier vehicle and on the other hand a device ensuring the unlocking position of means locking the essential members whose operation must absolutely intervene only if the separation between the load and its carrier is effective;
  • FIGS. 2, 3 and 4 schematically show alternative embodiments of a combination of means shown in FIG. 1.

Pour une plus grande facilité de compréhension les mêmes éléments portent les mêmes références dans toutes les figures.For greater ease of understanding, the same elements have the same references in all the figures.

Sur la figure 1 sont représentés des verrous 1, 2, 3 (à titre d'exemple au nombre de trois) et les moyens de commandes qui leur sont associés 4, 5, 6 destinés à assurer leur déverrouillage, libérant ainsi le ou les organes contenus dans une container (non représenté sur la figure) qu'ils verrouillaient. Il peut s'agir de charges militaires, de réservoirs élémentaires, de modules, destinés à être largués ensemble ou successivement c'est-à-dire à la demande. L'ensemble de ces organes et de leurs accessoires de commande sont accrochés au véhicule porteur (non représenté) au moyen d'un système d'accrochage. Il s'agit par exemple d'au moins un anneau 7, solidaire du corps contenant les modules élémentaires, dans la lumière 80 duquel pénètre le crochet du moyen d'emport (non visible sur la figure), lui même solidaire du véhicule porteur. La séparation a lieu lorsque le crochet est volontairement désolidarisé de l'anneau, libérant ainsi la liaison anneau-crochet.In Figure 1 are shown locks 1, 2, 3 (by way of example three in number) and the control means associated therewith 4, 5, 6 intended to ensure their unlocking, thereby releasing the member or members contained in a container (not shown in the figure) that they locked. It can be military charges, elementary tanks, modules, intended to be released together or successively, that is to say on demand. All of these organs and their control accessories are attached to the carrier vehicle (not shown) by means of a hanging system. It is for example at least one ring 7, integral with the body containing the elementary modules, into the lumen 80 from which the hook of the carrying means (not visible in the figure), itself integral with the carrier vehicle, penetrates. The separation takes place when the hook is deliberately detached from the ring, thereby releasing the ring-hook connection.

Conformément à l'invention, un dispositif 10 dénommé dans la suite de la description "barre omnibus" présentant un caractère d'organe mécanique de commande générale, est prévu. Cette barre omnibus 10, peut occuper deux positions : la première dite position de "sécurité" (celle qui est représentée sur la figure) et une seconde position dite position "armée". Le déplacement de cette barre peut être commandé par tout moyen connu. Par exemple, comme cela est schématiquement représenté sur la figure 1, un cable 11 qui peut être un cable de sécurité largable de culot SLC, est sollicité en traction à l'une de ses extrémités 12. Par un jeu de poulies 13, 14 et 15 et du ressort 16 il agit sur le ressort 17 qui se comprime contre la butée 18, libérant ainsi un doigt de verrouillage mobile 19 qui s'escamote. La barre omnibus 10 précédemment maintenue dans sa position de sécurité par ce doigt 19 se trouve libérée et, sous l'action du ressort de rappel 20, recule, se translate dans un sens donné (par exemple celui de la flèche 21) vers sa position dite "armée".According to the invention, a device 10 called in the following description "bus bar" having the character of a general mechanical control member, is provided. This busbar 10 can occupy two positions: the first so-called "safety" position (the one shown in the figure) and a second position called the "armed" position. The displacement of this bar can be controlled by any known means. For example, as shown diagrammatically in FIG. 1, a cable 11 which can be a releasable safety cable with an SLC base, is stressed in tension at one of its ends 12. By a set of pulleys 13, 14 and 15 and of the spring 16 it acts on the spring 17 which compresses against the stop 18, thereby releasing a movable locking finger 19 which retracts. The bus bar 10 previously held in its safety position by this finger 19 is released and, under the action of the return spring 20, moves back, translates in a given direction (for example that of the arrow 21) towards its position called "army".

Des logements 25, 26 et 27 sont prévus dans cette barre omnibus. Une combinaison verrous-barre omnibus est décrite ci-dessous à titre d'exemple. Ces logements destinés à coopérer avec les verrous comportent deux parties : une première cavité ouverte présentant un profil à section sensiblement circulaire de diamètre D et une seconde cavité ouverte présentant un profil à section sensiblement rectangulaire de largeur D très inférieure à D. Les verrous, dans l'exemple décrit, comportent par exemple deux parties : la première, de section cylindrique, d'un diamètre très légèrement inférieur à D peut se déplacer dans la première cavité et à la limite donc être déverrouillée ; la seconde présente une section amincie sur une longueur L légèrement supérieure à l'épaisseur de la barre omnibus et ne peut se déplacer dans la seconde cavité que sur une faible course correspondant approximativement à cette longueur L.Housing 25, 26 and 27 are provided in this bus bar. An example bus lock-bar combination is described below. These housings intended to cooperate with the locks comprise two parts: a first open cavity having a profile with a substantially circular section of diameter D and a second open cavity having a profile with a substantially rectangular section of width D much less than D. The locks, in the example described, for example have two parts: the first, of cylindrical section, with a diameter very slightly less than D can move in the first cavity and therefore be unlocked; the second has a thinned section over a length L slightly greater than the thickness of the busbar and can only move in the second cavity over a short stroke corresponding approximately to this length L.

Dans la position de sécurité (celle de la figure) les verrous, même s'ils reçoivent l'ordre de déverrouillage, sont bloqués, et l'opération ne peut avoir lieu. En revanche lorsque la barre omnibus 10 est dans sa position dite "armée", ces mêmes verrous se trouvent positionnés dans la seconde cavité 25 b, 26 b, 27 b des logements et sont alors en position de déverrouillabilité et prêts à subir l'action des moyens de déverrouillage 4, 5, 6 pour s'escamoter comme le montre respectivement les flèches 30, 31, 32. Les ordres de déverrouillage sont fonction de la séquence d'opérations choisie, soit simultanés, soit décalés.In the safety position (that of the figure) the locks, even if they receive the unlocking order, are locked, and the operation cannot take place. On the other hand, when the busbar 10 is in its so-called "armed" position, these same locks are positioned in the second cavity 25 b, 26 b, 27 b of the housings and are then in the unlockable position and ready to undergo the action. unlocking means 4, 5, 6 for retracting as shown respectively by the arrows 30, 31, 32. The unlocking orders depend on the sequence of operations chosen, either simultaneous or offset.

Conformément à l'invention, en se déplaçant de sa position de "sécurité", vers sa position "armée", la barre omnibus pousse par l'intermédiaire d'un logement supplémentaire 350 sur un téton 35 qui entraîne en rotation (voir le sens de la flèche 36) l'anneau 7. Si cette anneau 7 est encore relié au crochet du véhicule porteur, la liaison crochet-anneau s'oppose à cette rotation et s'oppose donc au déplacement de la barre omnibus 10 de sa position de "sécurité" à sa position "armée". Par conséquent il faut que la séparation de l'anneau du crochet du véhicule porteur soit effective pour que ce déplacement ait lieu et que le déverrouillage des verrous 1, 2 et 3 soit possible. Il s'agit d'un système de sécurité extrêmement fiable qui constitue l'une des principales caractéristiques de l'invention.According to the invention, when moving from its "safety" position to its "armed" position, the busbar pushes through an additional housing 350 on a stud 35 which rotates (see the direction of arrow 36) the ring 7. If this ring 7 is still connected to the hook of the carrier vehicle, the hook-ring connection opposes this rotation and therefore opposes the movement of the busbar 10 from its "safety" position to its "armed" position. Consequently it is necessary that the separation of the ring from the hook of the carrier vehicle is effective for this movement to take place and for the unlocking of the locks 1, 2 and 3 to be possible. It is an extremely reliable security system which constitutes one of the main characteristics of the invention.

La figure 2 est une représentation schématique d'une variante de réalisation de la combinaison d'une barre omnibus 10 et d'un anneau 7 coopérant en vue de l'obtention du résultat énoncé précédemment, à savoir le déplacement possible de la barre omnibus exclusivement dans le cas où le crochet du véhicule porteur est bien désolidarisé de l'anneau. On retrouve sur cette figure 2, l'anneau 7 avec son filetage 70 destiné à le fixer au container qui doit être transporté puis largué. Cet anneau 7 est relié, dans cette variante, à la barre omnibus 10 du type de celle qui a été décrite dans la variante précédente de la manière décrite ci-dessous. La première extrémité d'un bras de levier ou palette 50 pénétre dans la lumière 80 de l'anneau 7. Ce bras est articulé autour d'un axe d'articulation 51. Il a pour fonction, lorsqu'une pression est appliquée sur sa première extrémité, d'appuyer sur une goupille de verrouillage 55 qui traverse la barre omnibus dans un logement supplémentaire 56 prévu à cet effet et entrave tout déplacement de celle-ci de sa position de sécurité vers sa position armée. Un ressort de rappel 52 qui s'appuie sur une butée 54 tend à soulever la goupille 55. Cette pression s'exerce sur le bras 50 tant que le crochet (non représenté sur la figure) est introduit dans l'anneau 7. Dès que ce crochet est désolidarisé de cet anneau, cette pression disparaît, la goupille 55 entraîne le bras de levier 50 qui remonte dans le sens de la flèche 560. La goupille 55 sort de son logement 56 et libère ainsi la barre omnibus dont le déplacement peut alors être réalisé par tout moyen tel, par exemple, que celui qui a été décrit au moyen de la figure 1. Un dispositif de détection 57 de la position du bras 50 peut également être prévu, ce dispositif pouvant alors commander un circuit électrique.Figure 2 is a schematic representation of an alternative embodiment of the combination of a bus bar 10 and a ring 7 cooperating in order to obtain the result stated above, namely the possible movement of the bus bar exclusively in the case where the hook of the carrier vehicle is well separated from the ring. Found in this figure 2, the ring 7 with its thread 70 intended to fix it to the container which must be transported and then released. This ring 7 is connected, in this variant, to the bus bar 10 of the type which was described in the previous variant in the manner described below. The first end of a lever arm or pallet 50 penetrates into the lumen 80 of the ring 7. This arm is articulated around a hinge pin 51. It has the function, when pressure is applied to its first end, to press on a locking pin 55 which crosses the bus bar in an additional housing 56 provided for this purpose and hinders any movement of the latter from its safety position to its armed position. A return spring 52 which rests on a stop 54 tends to lift the pin 55. This pressure is exerted on the arm 50 as long as the hook (not shown in the figure) is introduced into the ring 7. As soon as this hook is detached from this ring, this pressure disappears, the pin 55 drives the lever arm 50 which rises in the direction of the arrow 560. The pin 55 comes out of its housing 56 and thus frees the bus bar whose movement can then be carried out by any means such as, for example, that which has been described by means of FIG. 1. A device 57 for detecting the position of the arm 50 can also be provided, this device then being able to control an electrical circuit.

La figure 3 est une représentation schématique d'une autre variante de réalisation d'une combinaison conforme à l'invention. Dans ce cas, l'anneau ne tourne pas comme dans le cas de la figure 1, mais il bascule. En effet il est maintenu en place durant toute la phase de transport grâce à un ergot 60 qui prend place dans un logement 61, prévu à cet effet et ménagé dans la barre omnibus 10 entravant le mouvement de celle-ci. Cet ergot 60 s'appuie vers le haut pendant le transport contre la structure du container (non représenté). Il y est maintenu tant que le crochet du véhicule porteur, par sa présence à l'intérieur de l'anneau empêche un ressort de torsion 61 de jouer son rôle. Dès que le crochet est désolidarisé de l'anneau, sous l'action précisément de ce ressort de torsion 61, l'anneau 7 bascule, abaissant l'ergot 60 d'une course supérieure à l'épaisseur de la barre omnibus 10 et permettant du même coup le mouvement de translation de celle-ci de sa position de "sécurité" vers sa position "armée".Figure 3 is a schematic representation of another alternative embodiment of a combination according to the invention. In this case, the ring does not rotate as in the case of Figure 1, but it rocks. Indeed it is held in place during the entire transport phase thanks to a lug 60 which takes place in a housing 61, provided for this purpose and formed in the bus bar 10 hampering the movement thereof. This lug 60 leans upwards during transport against the structure of the container (not shown). It is held there as long as the hook of the carrier vehicle, by its presence inside the ring prevents a torsion spring 61 from playing its role. As soon as the hook is detached from the ring, under the precise action of this torsion spring 61, the ring 7 rocks, lowering the lug 60 by a stroke greater than the thickness of the busbar 10 and allowing at the same time the translational movement of the latter from its "safety" position to its "armed" position.

La figure 4 représente schématiquement une variante de réalisation dans laquelle le mouvement de l'anneau est vertical. L'anneau 7 comporte, oûtre la lumière 80 destinée à recevoir le crochet du véhicule porteur, une première partie cylindrique 81 comportant un épaulement 82. Cette partie cylindrique 81 est contenue dans un logement 83 ménagé dans l'enveloppe 84 du container que doit supporter l'anneau, un ressort 85 est prévu entre cet épaulement 82 et l'une des parois 86 du logement 83. L'anneau comporte en outre une seconde partie 87 destinée à pénétrer dans la barre omnibus 10. Cette seconde partie cylindrique comporte une portion 90 amincie sur une longueur déterminée. Lorsque l'anneau est suspendu au crochet du porteur, le ressort 85 est comprimé et la partie cylindrique 87 se trouve dans la cavité à section circulaire 91 ménagé à cet effet dans la barre omnibus 10. Le mouvement de translation de la barre omnibus est entravé, en revanche, lorsque le crochet est désolidarisé de l'anneau, le ressort 85 se détend et la partie cylindrique 87 descend dans la barre omnibus jusqu'à ce que la portion amincie 90 se trouve face au logement 95. Le mouvement de la barre omnibus peut alors avoir lieu.FIG. 4 schematically represents an alternative embodiment in which the movement of the ring is vertical. The ring 7 comprises, in addition to the lumen 80 intended to receive the hook of the carrier vehicle, a first cylindrical part 81 comprising a shoulder 82. This cylindrical part 81 is contained in a housing 83 formed in the envelope 84 of the container which must support the ring, a spring 85 is provided between this shoulder 82 and one of the walls 86 of the housing 83. The ring also comprises a second part 87 intended to penetrate into the bus bar 10. This second cylindrical part comprises a portion 90 thinned over a determined length. When the ring is suspended from the carrier hook, the spring 85 is compressed and the cylindrical part 87 is located in the circular section cavity 91 provided for this purpose in the bus bar 10. The translational movement of the bus bar is hampered , however, when the hook is detached from the ring, the spring 85 relaxes and the cylindrical part 87 descends into the bus bar until the thinned portion 90 faces the housing 95. The movement of the bus bar can then take place.

Toute la description précédente se réfère au cas où la charge est effectivement accrochée au véhicule porteur avant d'être larguée. Mais avant ce transport néanmoins, ces charges sont le plus souvent entreposées et il convient de prévoir un dispositif de sécurité dit, au sol, se substituant en quelque sorte au crochet du véhicule porteur. Dans le cas de l'anneau tournant (figure 1) une pièce de section carrée est par exemple introduite à l'intérieur de la lumière du ou des anneaux, pièce qui est enlevée au moment de l'accrochage au véhicule porteur. D'autres types de dispositifs de sécurité au sol peuvent également être mis en place, ils n'entrent pas dans le cadre de la présente invention. Ils sont enlevés dès que la charge est accrochée à son véhicule porteur.All of the above description refers to the case where the load is actually attached to the carrier vehicle before being released. However, before this transport, however, these loads are most often stored and it is advisable to provide a safety device called, on the ground, somehow replacing the hook of the carrier vehicle. In the case of the rotating ring (FIG. 1), a piece of square section is for example introduced inside the lumen of the ring or rings, a piece which is removed at the time of attachment to the carrier vehicle. Other types of ground safety devices can also be implemented, they do not fall within the scope of the present invention. They are removed as soon as the load is attached to its carrier vehicle.

Les applications d'une barre omnibus coopérant avec un anneau muni de moyens capables de bloquer ou de permettre le mouvement de translation de cette barre omnibus sont nombreuses. Une telle combinaison s'applique chaque fois que des moyens de verrouillages ne doivent pas pouvoir être déverrouillés, tant qu'une opération ' déterminée n'a pas eu lieu, à savoir par exemple, la désolidarisation d'un anneau et d'un crochet le reliant à un véhicule transporteur. Ce problème se retrouve plus particulièrement dans les applications telles que, par exemple, le transport de charges militaires.The applications of a bus bar cooperating with a ring provided with means capable of blocking or allowing the translational movement of this bus bar are numerous. Such a combination applies whenever locking means must not be able to be unlocked, until a determined operation has taken place, namely for example, the separation of a ring and a hook connecting it to a carrier vehicle. This problem is found more particularly in applications such as, for example, the transport of military loads.

Claims (10)

1. Dispositif de sécurité de largage d'au moins une charge suspendue à un véhicule porteur du type aéronef, caractérisé en ce qu'il comprend : d'une part, une barre omnibus (10) capable d'occuper une première position dite "de sécurité" empechant tout déverrouillage au niveau de la charge, même si les ordres en étaient donné, et une position dite "armée" permettant l'exécution de ces ordres ; d'autre part, un système d'accrochage (7) de la charge au crochet du véhicule porteur muni de moyens coopérant avec la barre omnibus (10) de telle sorte que, tant que le crochet n'est pas désolidarisé du système d'accrochage, la translation de la barre omnibus de sa position de "sécurité" vers sa position "armée" est impossible.1. Safety device for dropping at least one load suspended from a carrier vehicle of the aircraft type, characterized in that it comprises: on the one hand, a bus bar (10) capable of occupying a first position called " security "preventing any unlocking at the level of the load, even if orders were given, and a so-called" armed "position allowing the execution of these orders; on the other hand, a hooking system (7) of the load on the hook of the carrier vehicle provided with means cooperating with the bus bar (10) so that, as long as the hook is not detached from the system attachment, translation of the busbar from its "safety" position to its "armed" position is impossible. 2. Dispositif de sécurité selon la revendication 1, caractérisé en ce que la barre omnibus (10) comporte autant de logements (25, 26, 27) que d'organes verrouillant la charge, les profils respectifs de ces logements et de ces organes de verrrouillage étant tels que, lorsque la barre omnibus (10) est dans la position de sécurité, l'organe de verrouillage ne puisse pas se déplacer dans le logement, tandis que lorsque la barre omnibus (10) est dans sa position armée ce déplacement puisse avoir lieu si un ordre de commande de déverrouillage est donné à l'organe considéré.2. Safety device according to claim 1, characterized in that the bus bar (10) comprises as many housings (25, 26, 27) as there are members locking the load, the respective profiles of these housings and these bodies of the locking being such that, when the bus bar (10) is in the safety position, the locking member cannot move in the housing, while when the bus bar (10) is in its armed position this movement can take place if an unlocking control command is given to the body in question. 3. Dispositif de sécurité selon la revendication 2, caractérisé en ce que ce logement comprend deux parties, une première cavité ouverte présentant un profil - à section sensiblement circulaire de diamètre D, et une seconde cavité ouverte présentant un profil à section sensiblement rectangulaire de largeur D inférieure à D.3. Safety device according to claim 2, characterized in that this housing comprises two parts, a first open cavity having a profile - of substantially circular section of diameter D, and a second open cavity having a profile of substantially rectangular section of width D less than D. 4. Dispositif de sécurité selon l'une des revendications 2 et 3, caractérisé en ce que l'organe de verrouillage comporte une première partie présentant un profil à section sensiblement cylindrique de diamètre très légèrement inférieur à D autorisant le déplacement de cette partie cylindrique dans la première cavité et une seconde partie amincie de longueur L et d'épaisseur très légèrement inférieure à D autorisant le déplacement de cette seconde partie dans la seconde cavité, seulement sur cette longueur L.4. Safety device according to one of claims 2 and 3, characterized in that the locking member comprises a first part having a profile with substantially cylindrical section of diameter very slightly less than D allowing the displacement of this cylindrical part in the first cavity and a second thinned part of length L and of thickness very slightly less than D allowing the displacement of this second part in the second cavity, only on this length L. 5. Dispositif de sécurité selon l'une des revendications 2 à 4, caractérisé en ce que la barre omnibus (10) comporte au moins un logement supplémentaire coopérant avec le système d'accrochage.5. Safety device according to one of claims 2 to 4, characterized in that the bus bar (10) comprises at least one additional housing cooperating with the attachment system. 6. Dispositif de sécurité selon la revendication 5, caractérisé en ce que le système d'accrochage est constitué par au moins un anneau comportant une lumière destinée à recevoir le crochet du véhicule porteur et un téton entraînant en rotation cet anneau lorsque le crochet est désolidarisé de l'anneau et que la barre omnibus (10) est entraînée en translation de sa position de sécurité vers sa position armée, le téton étant guidé alors par un logement supplémentaire prévue à cet effet dans la barre omnibus.6. Safety device according to claim 5, characterized in that the attachment system consists of at least one ring comprising a light intended to receive the hook of the carrier vehicle and a stud driving in rotation this ring when the hook is detached of the ring and that the bus bar (10) is driven in translation from its safety position to its armed position, the stud then being guided by an additional housing provided for this purpose in the bus bar. 7. Dispositif de sécurité selon la revendication 5, caractérisé, en ce que l'anneau (7) est muni d'un bras de levier (50), dont une extrémité est introduite dans la lumière (80) de l'anneau, agissant sur une goupille (55) mobile capable de coulisser dans le logement supplémentaire prévu à cet effet dans la barre omnibus (10) de telle sorte que cette goupille verrouille la barre omnibus tant que le crochet du véhicule porteur est présent à l'intérieur de la lumière de l'anneau et se trouve escamotée sous l'action d'un ressort dès que le crochet est désolidarisé de celui-ci.7. Safety device according to claim 5, characterized in that the ring (7) is provided with a lever arm (50), one end of which is introduced into the opening (80) of the ring, acting on a movable pin (55) capable of sliding in the additional housing provided for this purpose in the bus bar (10) so that this pin locks the bus bar as long as the hook of the carrier vehicle is present inside the light of the ring and is retracted under the action of a spring as soon as the hook is detached from the latter. 8. Dispositif de sécurité selon la revendication 5, caractérisé en ce que l'anneau (7) est muni d'un ergot (60) et subi l'action d'un ressort de torsion, tel que l'ergot soit maintenu en place dans le logement supplémentaire prévu à cet effet dans la barre omnibus (10) tant que le crochet du véhicule porteur est présent à l'intérieur de la lumière de l'anneau et, soustrait de ce logement sous l'action du ressort de torsion, dès que le crochet est désolidarisé de l'anneau.8. Safety device according to claim 5, characterized in that the ring (7) is provided with a lug (60) and subjected to the action of a torsion spring, such that the lug is held in place in the additional housing provided for this purpose in the bus bar (10) as long as the hook of the carrier vehicle is present inside the opening of the ring and, subtracted from this housing under the action of the torsion spring, as soon as the hook is detached from the ring. 9. Dispositif de sécurité, selon la revendication 5, caratérisé en ce que, d'une part, l'anneau (7) comporte deux parties cylindriques, la première (41) de plus grand diamètre comportant un épaulement (82) destiné à soutenir un ressort (85) agissant en compression, et une seconde partie (87) de plus petit diamètre comportant une zone amincie et en ce que, d'autre part, le logement supplémentaire prévu dans la barre omnibus (10) comporte deux cavités ; la première permettant le coulissement de la partie de l'anneau de plus petit diamètre et la seconde cavité uniquement celle de la partie amincie ; l'anneau et la barre omnibus coopérant entre eux de telle sorte que si le crochet du véhicule porteur est présent dans la lumière de l'anneau, le ressort est comprimé, et la partie cylindrique de plus petit diamètre se trouve dans la première cavité ; si le crochet du véhicule porteur est désolidarisé de l'anneau, le ressort se relâche, déplaçant verticalement cette seconde partie cylindrique jusqu'à ce que la partie amincie vienne en regard de la seconde cavité, permettant ainsi le mouvement de translation de la barre omnibus.9. Safety device according to claim 5, characterized in that, on the one hand, the ring (7) comprises two cylindrical parts, the first (41) of larger diameter comprising a shoulder (82) intended to support a spring (85) acting in compression, and a second part (87) of smaller diameter comprising a thinned zone and in that, on the other hand, the housing additional provided in the bus bar (10) has two cavities; the first allowing the sliding of the part of the ring of smaller diameter and the second cavity only that of the thinned part; the ring and the bus bar cooperating with each other so that if the hook of the carrier vehicle is present in the lumen of the ring, the spring is compressed, and the cylindrical part of smaller diameter is located in the first cavity; if the hook of the carrier vehicle is detached from the ring, the spring is released, vertically moving this second cylindrical part until the thinned part comes opposite the second cavity, thus allowing the translation movement of the bus bar . 10. Charge destinée à être suspendue à un aéronef, caractérisée en ce qu'elle est équipée d'un dispositif selon l'une des revendications précédentes.10. Load intended to be suspended from an aircraft, characterized in that it is equipped with a device according to one of the preceding claims.
EP80400670A 1979-05-23 1980-05-14 Safety release device for a transportable load suspended by an aircraft Expired EP0020225B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT80400670T ATE2659T1 (en) 1979-05-23 1980-05-14 SAFETY RELEASE DEVICE FOR A LOAD SUSPENDED FOR TRANSPORTATION ON AN AIRCRAFT.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR7913200A FR2457218A1 (en) 1979-05-23 1979-05-23 SECURITY DEVICE FOR WIDENING A LOAD, SUSPENDED FROM AN AIRCRAFT FOR TRANSPORT, AND LOAD EQUIPPED WITH SUCH A DEVICE
FR7913200 1979-05-23

Publications (2)

Publication Number Publication Date
EP0020225A1 true EP0020225A1 (en) 1980-12-10
EP0020225B1 EP0020225B1 (en) 1983-03-02

Family

ID=9225812

Family Applications (1)

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EP80400670A Expired EP0020225B1 (en) 1979-05-23 1980-05-14 Safety release device for a transportable load suspended by an aircraft

Country Status (17)

Country Link
US (1) US4348936A (en)
EP (1) EP0020225B1 (en)
JP (1) JPS55156799A (en)
AR (1) AR224646A1 (en)
AT (1) ATE2659T1 (en)
BR (1) BR8003222A (en)
CA (1) CA1145174A (en)
DE (1) DE3062181D1 (en)
DK (1) DK224180A (en)
ES (1) ES8200609A1 (en)
FI (1) FI65199C (en)
FR (1) FR2457218A1 (en)
IN (1) IN154506B (en)
NO (1) NO148881C (en)
PT (1) PT71292A (en)
TR (1) TR21268A (en)
ZA (1) ZA803107B (en)

Cited By (1)

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Publication number Priority date Publication date Assignee Title
FR2507303A1 (en) * 1981-06-03 1982-12-10 Lacroix E MOUNTED MACHINE LAUNCHER MODULE WITH REVERSIBLE GENERAL SAFETY

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FR2619902B1 (en) * 1987-08-28 1993-05-14 Thomson Brandt Armements ARMING DEVICE WITH SECURITY FOR A LOADABLE LOAD OF A CARRIER
DE3833817A1 (en) * 1988-10-05 1990-04-19 Messerschmitt Boelkow Blohm DEVICE FOR SECURING AND ARMING SUBMUNITION BODIES
FR2641859B1 (en) * 1988-12-30 1991-03-22 Thomson Brandt Armements SECURITY FOR WIDER AIRPORT LOAD
JPH0649346Y2 (en) * 1989-02-01 1994-12-14 株式会社グリーン Radio-controlled motorcycle toys
GB2532969A (en) * 2014-12-01 2016-06-08 Edo Mbm Tech Ltd Small store suspension and release unit
US11472551B2 (en) * 2019-08-02 2022-10-18 Bae Systems Plc Arming apparatus
US11643208B2 (en) * 2020-02-13 2023-05-09 The Boeing Company Adjustable coupling mechanisms for projectile devices
US11913765B2 (en) * 2021-02-02 2024-02-27 Bae Systems Plc Jettison and arming system
GB2605868B (en) * 2021-02-02 2023-07-12 Bae Systems Plc Aircraft weapon store arming apparatus

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FR499830A (en) * 1917-08-02 1920-02-24 Arthur Henry Gledhill Improvements to devices for dropping bombs or other objects carried by aircraft
FR625895A (en) * 1926-03-19 1927-08-22 Device for protecting the rocket from bombs suspended from an airship
FR636427A (en) * 1928-04-10
FR638575A (en) * 1926-12-14 1928-05-29 Bomb-launching device for airplanes
FR832788A (en) * 1937-01-30 1938-10-03 Ingg Flii Nardi Bomb trigger for aircraft or the like
US3872770A (en) * 1973-04-09 1975-03-25 Motorola Inc Arming system safety device
US3956964A (en) * 1973-04-09 1976-05-18 Motorola, Inc. Arming system safety device

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FR636427A (en) * 1928-04-10
FR499830A (en) * 1917-08-02 1920-02-24 Arthur Henry Gledhill Improvements to devices for dropping bombs or other objects carried by aircraft
FR625895A (en) * 1926-03-19 1927-08-22 Device for protecting the rocket from bombs suspended from an airship
FR638575A (en) * 1926-12-14 1928-05-29 Bomb-launching device for airplanes
FR832788A (en) * 1937-01-30 1938-10-03 Ingg Flii Nardi Bomb trigger for aircraft or the like
US3872770A (en) * 1973-04-09 1975-03-25 Motorola Inc Arming system safety device
US3956964A (en) * 1973-04-09 1976-05-18 Motorola, Inc. Arming system safety device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2507303A1 (en) * 1981-06-03 1982-12-10 Lacroix E MOUNTED MACHINE LAUNCHER MODULE WITH REVERSIBLE GENERAL SAFETY
EP0067732A2 (en) * 1981-06-03 1982-12-22 Etienne Lacroix - Tous Artifices Sa Airplane mounted launcher with resettable safety arrangement
EP0067732A3 (en) * 1981-06-03 1983-01-19 Societe E. Lacroix - Tous Artifices Airplane mounted launcher with resettable safety arrangement
US4479417A (en) * 1981-06-03 1984-10-30 Societe E. Lacroix Missile launcher module in particular for aircraft, with general reversible safety device

Also Published As

Publication number Publication date
NO148881C (en) 1984-01-04
FI801630A (en) 1980-11-24
FR2457218A1 (en) 1980-12-19
FI65199C (en) 1984-04-10
AR224646A1 (en) 1981-12-30
BR8003222A (en) 1980-12-30
DE3062181D1 (en) 1983-04-07
ZA803107B (en) 1981-06-24
EP0020225B1 (en) 1983-03-02
NO148881B (en) 1983-09-26
CA1145174A (en) 1983-04-26
IN154506B (en) 1984-11-03
PT71292A (en) 1980-06-01
ATE2659T1 (en) 1983-03-15
FI65199B (en) 1983-12-30
JPS55156799A (en) 1980-12-06
ES491756A0 (en) 1981-11-01
FR2457218B1 (en) 1983-06-17
US4348936A (en) 1982-09-14
TR21268A (en) 1984-03-15
ES8200609A1 (en) 1981-11-01
NO801540L (en) 1980-11-24
DK224180A (en) 1980-11-24

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