FR2605671A1 - Security locking device for inspection doors and trap doors - Google Patents
Security locking device for inspection doors and trap doors Download PDFInfo
- Publication number
- FR2605671A1 FR2605671A1 FR8614691A FR8614691A FR2605671A1 FR 2605671 A1 FR2605671 A1 FR 2605671A1 FR 8614691 A FR8614691 A FR 8614691A FR 8614691 A FR8614691 A FR 8614691A FR 2605671 A1 FR2605671 A1 FR 2605671A1
- Authority
- FR
- France
- Prior art keywords
- lever
- button
- axis
- allows
- keeper
- 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
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C3/00—Fastening devices with bolts moving pivotally or rotatively
- E05C3/12—Fastening devices with bolts moving pivotally or rotatively with latching action
- E05C3/122—Fastening devices with bolts moving pivotally or rotatively with latching action flush
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lock And Its Accessories (AREA)
Abstract
Description
DISPOSITIF DE VERROUILLAGE AVEC SECURITE
POUR PORTES DE VISITE ET TRAPPES
La présente invention concerne un dispositif de verrouillage et deverrouillage rapide, avec sécurité, destine aux portes et trappes d'accës. portes de visite et autres des appareils civils et militaires, comme avions, missiles, fusees. satellites, et machines roulantes, comme trains a grande vitesse, chars, etc...SECURITY LOCKING DEVICE
FOR VISIT DOORS AND DOORS
The present invention relates to a fast locking and unlocking device, with security, intended for doors and access hatches. inspection doors and the like for civil and military aircraft, such as planes, missiles, rockets. satellites, and rolling machines, like high speed trains, tanks, etc ...
Le nombre de dispositifs par porte ou trappe est variable en fonction de la dimension de celle-ci et des efforts auxquels elle est soumise. The number of devices per door or hatch is variable depending on the size of the latter and the forces to which it is subjected.
Selon une forme et un nombre de piëces préférentiel, ce dispositif assure l'interchangeabilite pour tout dispositif de merne reference, et, de ce fait la réduction du coût du materiel de rechante, ainsi que le cout de fabrication a 1 assemblage du materielA
Le dispositif, selon l'invention, permet une pose simple et précise, et d'être réalisé dans le méme materiau que la partie des éléments de l'appareil sur lequel il est assemble, et ainsi d'utiliser des él@mants de fixation de même nature, afin d'éviter le couple galvanique.According to a shape and a preferential number of parts, this device provides interchangeability for any device of the same reference, and, therefore, the reduction of the cost of the repairing material, as well as the manufacturing cost to 1 assembly of the material.
The device according to the invention allows a simple and precise installation, and to be made in the same material as the part of the elements of the device on which it is assembled, and thus to use fixing elements of the same kind, in order to avoid galvanic torque.
Le dispositif, selon l'invention, possède un double verrouillage a l'aide d'un levier de sécurité monte sur la gache, ce qui permet son utilisation dans les zones des appareils les plus sollicités par les variations de pression lors de conditions de vol difficiles. The device according to the invention has a double locking using a safety lever mounted on the keeper, which allows its use in the areas of the aircraft most stressed by pressure variations during flight conditions difficult.
Le dispositif se compose : d'une cage-boîtier (1) en forme de profil oméga, à l'intérieur de laquelle sont assemblées une gâche (2). une detente-poussoir (3) qui ont chacune un point de basculement autour d'un axe
A l'intérieur de la gâche (2) et de la détente-poussoir (3) sur un alésage fonctionnel est montée une entretoise (6) ou (8)
La gàche est équipee d'un levier de securité (9) monte sur un axe (10) a l'intérieur d'un logement (15) qui permet le basculement de celui-ci.The device consists of: a box cage (1) in the shape of an omega profile, inside which a keeper (2) is assembled. a detent-pusher (3) which each have a tilting point around an axis
A spacer (6) or (8) is mounted inside the strike plate (2) and the push-trigger (3) on a functional bore.
The striker is equipped with a safety lever (9) mounted on an axis (10) inside a housing (15) which allows the tilting thereof.
Un ressort de rappel (4) de la gâche au déverrouillage et de pression de la détente-poussoir (3) et du levier de secu- rité (9) en position verrouillage est monte sur l'entretoise (6) å l'intérieur d'un logement (14) de la gâche 2}. A return spring (4) for the strike plate when unlocked and for pressing the trigger trigger (3) and the safety lever (9) in the locked position is mounted on the spacer (6) inside 'a housing (14) of the strike 2}.
Deux axes-rivets (5) et (7) assurent le montage de l'ensemble
La cage-boîtier comporte trois perçages (31) sur chacune des ailes (30) pour permettre la fixation de l'ensemble a la porte ou trappe.Two rivet pins (5) and (7) ensure the assembly of the assembly
The housing cage has three holes (31) on each of the wings (30) to allow the assembly of the assembly to the door or hatch.
Les epaisseurs variables de verrouillage sont assurées par la variation des cotes a et b', qui definissent ainsi la référence spécifique de chaque dispositif. The variable locking thicknesses are ensured by the variation of the dimensions a and b ', which thus define the specific reference of each device.
Le dispositif peut étre réalise en alliage d'aluminium de préférence 2024 etat T351), en acier cadmi@ ou chrome, en acier inoxydable, en matière composite du type stratifié, fibre de carbone ou en plastique dur, en titane ou tout autre matériau entrant dans la fabrication d'aëronefs. The device can be made of aluminum alloy preferably 2024 state T351), of cadmi @ or chrome steel, of stainless steel, of composite material of the laminated type, carbon fiber or hard plastic, of titanium or any other incoming material. in the manufacture of aircraft.
Selon des variantes, le point d'articulation de la gache (2) peut étre deplac@ cote X @ Y pour assurer un jeu minimum entre la gâche (2) et le poussoir (3) en position fermee (verrouillé) et la découpe fonctionnelle de la porte ou trappe. According to variants, the hinge point of the keeper (2) can be moved @ dimension X @ Y to ensure a minimum clearance between the keeper (2) and the pusher (3) in the closed position (locked) and the functional cutout from the door or hatch.
Dans ce cas, la cote "d" est adaptée, ainsi que la forme frontale de la gâche. In this case, the dimension "d" is adapted, as well as the frontal shape of the strike.
Les figures 1 et 3 presentent, en coupe, le dispositif selon l'invention en position fermés (verrouillé). Figures 1 and 3 show, in section, the device according to the invention in the closed position (locked).
La figure 2 présente, en coupe, le dispositif en position ouverte (déverrouillé). Figure 2 shows, in section, the device in the open (unlocked) position.
Le dispositif représenté sur les figures 1, 2 et 3, comporte une cage-boitier en forme de Omega (1) ayant des dimensions de l'ordre de 5,1 cm de long, 1,4 cm de haut, 3,8 cm de large, comportant un embrévement (11) qui permet d'assurer la position angulaire de la gâche au dëverrouillage, trois perçages (31) sur chacune des ailes et deux trous (12) sur chaque fianc (13 >
Une gache (2) qui comporte un logement (14) pour le ressort de rappel (4), une découpe en forme de fenêtre (15) pour loger le levier de securite (9) de deux alesages (16) et (17) pour le passage respectif de l'entretoise (6) et de l'axe (10). The device represented in FIGS. 1, 2 and 3 comprises a cage in the shape of an Omega (1) having dimensions of the order of 5.1 cm long, 1.4 cm high, 3.8 cm wide, comprising a recess (11) which ensures the angular position of the strike when unlocked, three holes (31) on each of the wings and two holes (12) on each side (13>
A keeper (2) which comprises a housing (14) for the return spring (4), a window-shaped cutout (15) for housing the safety lever (9) of two bores (16) and (17) for the respective passage of the spacer (6) and the axis (10).
Un levier de securite (9) en forme de té, comportant un embrevement 19) sur la partie opposée aux branches (153 du te pour permettre le maintien en position du ressort (4). A safety lever (9) in the shape of a tee, comprising a member 19) on the part opposite the branches (153 of the tee to allow the spring (4) to be held in position.
Le levier (9) est assemble sur la gâche (2) a l'aide de l'axe (10). The lever (9) is assembled on the keeper (2) using the pin (10).
Une detente-poussoir (3) qui possède une partie prolongee vers l'intérieur du dispositif (20) constituant une buté positive en position repos et en position verrouillage. Sur cette partie. une découpe (21) permet le passage du levier de securite lors du basculement pour dëverrouillage. Sur chaque bras (20) de la fourche, un embrevement (20) assure le maintien en place de chaque branche du ressort de rappel (4). A detent-pusher (3) which has a part extended towards the inside of the device (20) constituting a positive stop in the rest position and in the locking position. On this part. a cutout (21) allows the passage of the safety lever during tilting for unlocking. On each arm (20) of the fork, a removal (20) ensures the holding in place of each branch of the return spring (4).
Un ressort de rappel (4) qui assure une triple fonction
pression de deverrouillage de la détente-poussoir (3).A return spring (4) which performs a triple function
release pressure of the trigger (3).
- Pression de deverrouillage du levier- de securite (1). - Unlocking pressure of the safety lever (1).
Rappel de la gache (2) lors du déverrouillage. Reminder of the keeper (2) when unlocking.
Deux entretoises (6) et (8) qui, montées respectivement su la gache (2) et la detente-poussoir (3), permettent de diminuer la flexion des axes-rivets (5) et (7) en position fermée et, en char-ge, d'assurer le montage du r-essort de rappel (4), ainsi que l'écartement fonctionnel de la cage-boltier, lors de l'assemblage par rivetage. Two spacers (6) and (8) which, mounted respectively on the keeper (2) and the push-button (3), make it possible to reduce the bending of the rivet pins (5) and (7) in the closed position and, in load, to ensure the mounting of the return spring (4), as well as the functional spacing of the bolt cage, during assembly by riveting.
Deux axes-rivets (5) et (7j qui assurent le montage final de l'ensemble. Two rivet pins (5) and (7j which ensure the final assembly of the assembly.
La position du ressort de rappel (4), l'entraxe et la position des axes-rivets (5) et (7), par rapport au point d'enclenchement du becquet (23), de la gâche (2) et de la face (24) et gorge (25) du poussoir (3) sont tels que celui-ci tend â déplacer positivement le point de verrouillage lorsque l'effort augmente sur la gâche. Lorsque la gâche (2) et la detente-poussoir (3) sont en position verrouillée, le levier- de sécurité (9) est rabattu sur la detente-poussoir (3) et se loge dans l'enbrevement en forme de té (26) de la detente-poussoir (3j. The position of the return spring (4), the center distance and the position of the rivet pins (5) and (7), relative to the point of engagement of the spoiler (23), the keeper (2) and the face (24) and groove (25) of the pusher (3) are such that it tends to positively move the locking point when the force increases on the keeper. When the keeper (2) and the push-button (3) are in the locked position, the safety lever (9) is folded back on the push-button (3) and is housed in the tee-shaped recess (26 ) of the trigger release (3d.
Le dispositif devient ainsi doublement verrouille et seu le déclenchement du levier de s@curite (9) permet son ouve ture, par une pression ensuite sur la detente-poussoir (3ss. The device thus becomes doubly locked and only the triggering of the safety lever (9) allows its opening, by a pressure then on the trigger-trigger (3ss.
Le dispositif. selon l'invention est particulièrement destiné au verrouillage des portes de visite et trappes equipant les aeronefs, fusees, missiles et satellites exposes' a des grandes variations de pression ou â des pressions treimportantes. The device. according to the invention is particularly intended for locking the inspection doors and hatches fitted to aircraft, rockets, missiles and satellites exposed to large pressure variations or to significant pressures.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8614691A FR2605671B1 (en) | 1986-10-23 | 1986-10-23 | SECURITY LOCKING DEVICE FOR VISIT DOORS AND DOORS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8614691A FR2605671B1 (en) | 1986-10-23 | 1986-10-23 | SECURITY LOCKING DEVICE FOR VISIT DOORS AND DOORS |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2605671A1 true FR2605671A1 (en) | 1988-04-29 |
FR2605671B1 FR2605671B1 (en) | 1995-04-21 |
Family
ID=9340094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8614691A Expired - Lifetime FR2605671B1 (en) | 1986-10-23 | 1986-10-23 | SECURITY LOCKING DEVICE FOR VISIT DOORS AND DOORS |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2605671B1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1197619A1 (en) * | 2000-10-10 | 2002-04-17 | Hartwell Corporation | Blowout latch |
CN109533273A (en) * | 2018-11-28 | 2019-03-29 | 中国特种飞行器研究所 | A kind of simple quick-release lid |
EP3882422A1 (en) | 2020-03-17 | 2021-09-22 | LISI Aerospace | Lock for panel of an aircraft |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4365831A (en) * | 1980-04-04 | 1982-12-28 | Hartwell Corporation | Channel latch |
FR2556399A1 (en) * | 1983-12-07 | 1985-06-14 | Martins Aderito | Device for locking inspection doors and trapdoors |
-
1986
- 1986-10-23 FR FR8614691A patent/FR2605671B1/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4365831A (en) * | 1980-04-04 | 1982-12-28 | Hartwell Corporation | Channel latch |
FR2556399A1 (en) * | 1983-12-07 | 1985-06-14 | Martins Aderito | Device for locking inspection doors and trapdoors |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1197619A1 (en) * | 2000-10-10 | 2002-04-17 | Hartwell Corporation | Blowout latch |
US6513841B1 (en) | 2000-10-10 | 2003-02-04 | Hartwell Corporation | Blowout latch |
CN109533273A (en) * | 2018-11-28 | 2019-03-29 | 中国特种飞行器研究所 | A kind of simple quick-release lid |
CN109533273B (en) * | 2018-11-28 | 2022-03-15 | 中国特种飞行器研究所 | Simple quick-release opening cover |
EP3882422A1 (en) | 2020-03-17 | 2021-09-22 | LISI Aerospace | Lock for panel of an aircraft |
FR3108353A1 (en) | 2020-03-17 | 2021-09-24 | Lisi Aerospace | Aircraft panel lock |
US11713104B2 (en) | 2020-03-17 | 2023-08-01 | Lisi Aerospace | Latch for aircraft panel |
Also Published As
Publication number | Publication date |
---|---|
FR2605671B1 (en) | 1995-04-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20060630 |
|
RN | Application for restoration | ||
D3 | Ip right revived |