[go: up one dir, main page]

WO2010004030A2 - Compartiment à bagages pour aéronef de passagers - Google Patents

Compartiment à bagages pour aéronef de passagers Download PDF

Info

Publication number
WO2010004030A2
WO2010004030A2 PCT/EP2009/058827 EP2009058827W WO2010004030A2 WO 2010004030 A2 WO2010004030 A2 WO 2010004030A2 EP 2009058827 W EP2009058827 W EP 2009058827W WO 2010004030 A2 WO2010004030 A2 WO 2010004030A2
Authority
WO
WIPO (PCT)
Prior art keywords
handle
base plate
luggage rack
connecting elements
elements
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.)
Ceased
Application number
PCT/EP2009/058827
Other languages
German (de)
English (en)
Other versions
WO2010004030A9 (fr
WO2010004030A3 (fr
Inventor
Gottfried Steiner
Thomas Krivec
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.)
Dipl Ing Gottfried Steiner Ingenieurbuero fur Kunststofftechnik
Original Assignee
Dipl Ing Gottfried Steiner Ingenieurbuero fur Kunststofftechnik
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 Dipl Ing Gottfried Steiner Ingenieurbuero fur Kunststofftechnik filed Critical Dipl Ing Gottfried Steiner Ingenieurbuero fur Kunststofftechnik
Publication of WO2010004030A2 publication Critical patent/WO2010004030A2/fr
Publication of WO2010004030A3 publication Critical patent/WO2010004030A3/fr
Publication of WO2010004030A9 publication Critical patent/WO2010004030A9/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/003—Stowage devices for passengers' personal luggage
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B53/00—Operation or control of locks by mechanical transmissions, e.g. from a distance
    • E05B53/003—Operation or control of locks by mechanical transmissions, e.g. from a distance flexible
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B41/00—Locks with visible indication as to whether the lock is locked or unlocked
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B63/00—Locks or fastenings with special structural characteristics
    • E05B63/14—Arrangement of several locks or locks with several bolts, e.g. arranged one behind the other
    • E05B63/143—Arrangement of several locks, e.g. in parallel or series, on one or more wings

Definitions

  • the invention relates to a luggage rack with a device for locking in the closed position and a mechanism for opening with an externally operable handle.
  • the luggage rack may be a hinged, a chute having luggage rack or a fixed luggage rack with a rotatably mounted lid.
  • luggage racks In the aviation sector, two fundamentally different embodiments of luggage racks are known. These are, on the one hand, pivotable or lowerable luggage racks, on the other hand, fixed luggage racks with a laterally openable lid are used today in passenger aircraft. Of particular importance for these
  • Luggage carrier operators - passengers or cabin crew - is a fast, reliable and effortless opening and closing.
  • opening and closing and when operating the handle of this and the directly associated with him and interacting parts are heavily stressed.
  • it often happens that the handle and possibly also the externally visible parts of the actuating mechanism are damaged during assembly of the luggage rack.
  • the invention is therefore based on the object, the visible parts of the
  • Opening mechanism on one on the inside of the chute or the lid fixed base plate is arranged and connected to the handle via detachable plug / snap connections, wherein the handle is received by a cover, which in turn is via releasable plug / snap connections with the base plate in combination.
  • the parts visible on the outside of the luggage installation, the handle and the covering element, can be easily exchanged as a result of their detachable connection as required.
  • the arrangement of the handle and the cover allows, with the same design of the functional components of the opening mechanism or the
  • Base plate to customize the design of the handle and the cover.
  • releasable connecting elements are screwed, plugged or snap-in connections.
  • Such fasteners can run durable and reliable in both metal and plastic and operate comfortably.
  • the base plate can be carried out particularly advantageously in hybrid construction.
  • Fiber composite material manufactured.
  • This blank is overmoulded directly in an injection molding machine with a suitable thermoplastic material.
  • the required functional elements such as snap connections or plug-in elements are molded directly onto the inserted base plate.
  • the operative connection to the opening mechanism of the luggage tray is advantageously carried out such that releasable connecting elements connect the handle with a release lever of the opening mechanism, which release lever is pivotally or displaceably mounted on the base plate.
  • the operative connection of the release lever to the locking devices of the luggage rack provides that the release lever functional elements such as tension members or driving elements are attached, which are connected to the locking devices, such that pivoting of the trigger lever by pressing the handle train to the tension members and a Unlocking the locking devices causes.
  • an optical, acoustic or electronic signal element is arranged on the handle, which is imperceptible from the outside in the rest position of the handle. If the handle can not be completely closed when the locking devices of the luggage rack are not properly closed, this is clearly indicated by the signal element.
  • the signal element can be designed as a simple color bar with red color, which gives a visual indication.
  • Alternative design variants are, for example, constantly illuminated or flashing signal lights, acoustic warning signal transmitters or corresponding sensors and signal transmitters which centrally confirm uncontrolled luggage racks.
  • 1 is an overall view of a lowerable luggage compartment
  • 3 to 9 are views of components of an operating mechanism
  • Fig. 6 and Fig. 7 are views of a cover and design element and Fig. 8 and Fig. 9 components of the actuating mechanism.
  • Fig. 1 shows a pivoting luggage rack 1 for a passenger cabin of an aircraft in the form of a stowage of the cabin luggage provided around a pivot axis indicated in this figure 2 pivoted, one-piece running chute 1 b with a body with side walls 1a and a cabin facing the lower part 1 c, at which the center of the passenger or flight personnel for opening and closing the luggage rack 1 provided handle 3 is arranged.
  • On each side wall 1 a is a catch lock 4 is fixed, wherein the two catch locks 4 are simultaneously by means of the handle 3 to not shown holding elements in a releasable manner latched.
  • FIG. 2 shows a luggage rack 5 fixedly mounted on the aircraft structure for a passenger cabin of an aircraft with a cover 6 for closing off the area for stowing the cabin luggage.
  • the lid is mounted by means of hinges 7 on the upper side of the luggage rack 5.
  • a handle 3 for actuating the triggering device 9 for opening and closing the luggage rack 1 and a not shown in detail catching lock, wherein the catch lock by means of
  • Handle 3 is attached to the luggage rack mounted holding elements 10 in a detachable manner can be latched.
  • the triggering device for opening the lid and the actual catch lock are integrated directly into an assembly.
  • Locking locks 4 When the handle 3 is omitted when the luggage rack 1 is open, the catching locks 4 take their starting positions in a manner not shown.
  • the locking device To open the luggage rack 5 by hand, the locking device is unlocked via the handle 3. When omitting the handle 3 when the luggage rack 1 is open, the locking device assumes its starting position in a manner not shown.
  • a base plate 12 is fixed, in particular glued or screwed.
  • Fig. 3 shows the inner side 12a, which is associated with the lower part 1c (Fig. 1), Fig. 4 the
  • FIGS. 5 and 6 show the inside of the cover 19 with four suspension lugs 24 and four plug-in elements 26.
  • the ends of the snap hooks 16a can be latched into openings 24a of the suspension lugs 24, the plug-in elements 26 can be clipped into the latching elements 16b. Since plug and clip connections are known in the art and can be carried out in various ways, a detailed description of the components 16a, 16b, 24 and 26 is omitted.
  • Fig. 4 also shows on the outside of the base plate 12 formed, arranged in two pairs bearing plates 12c and two bearing blocks 12d.
  • Fig. 8 shows the base plate 12 with attached cover 19.
  • a side arm 13b of an approximately U-shaped release lever 13 is rotatably mounted on a bolt 14.
  • the two mutually parallel arms 13b are centrally connected to each other via a transverse web 13a and extended beyond the transverse web 13a as profiles 13c, which merge into about 90 ° bent end portions 13d, which are pluggable through openings 19a of the cover 19.
  • the end portions 13d are provided with resilient snap elements, not shown in the figures, which can be latched into latching elements 17 of the control element (see FIG. 5) designed as a handle 3. In this way, the connection between the handle 3, which fits into a recess 19b of the cover 19 (Fig. 7), is made.
  • a signal bar 18 is mounted, which in a striking color, in particular red, can be colored.
  • the base plate 12 is designed in hybrid construction.
  • the flat portion of the base plate 12 is made of a fiber composite material in machining.
  • the functional elements such as bearing plates 12c, bearing blocks 12d, snap hooks 16a and 16a latching elements in a corresponding thermoplastic material, formed by overmolding in an injection molding machine.
  • a helical spring 15 is arranged on the bolt 14, which is supported at one end in a stationary manner, for example on the base plate 12, and at the other end against a stop part 13e formed on the arm 12b of the trigger lever 13.
  • the springs 15 therefore act on the Release lever 13 in the opening direction, against the closing force in the safety locks. 4
  • each cable 1 1 is fixed in a clamping part 25 which is formed in the region of the bending point of the profile 13 c of the release lever 13.
  • the end portion of each cable 1 1 is guided over a bearing on the associated bearing block 12 d roller 20 in a clamping element 21, which is attached to the profile 13 c of the release lever 13.
  • a clamping screw 22 allows adjusting or changing the effective rope length.
  • the handle 3 is grasped by hand and moved slightly away from the lower part 1c of the luggage rack.
  • the trigger lever 13 connected to the handle 3 is slightly pivoted.
  • the cables 11 are pulled and the two safety locks 4 are released. If the system is not properly closed, for example due to a misalignment in one of the catch locks 4, this misalignment is transmitted via the tension cables 11 to the release lever 13 and thus to the handle 3, which can not be completely closed.
  • the signal bar 18 visible in this case indicates an improper closing.
  • the invention is not limited to the illustrated embodiment.
  • ropes as tension or actuators tie rods are provided, the attachment in the catch and the release lever is to be carried out accordingly.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

L'invention concerne un compartiment à bagages (1) pivotant ou pouvant être monté de manière fixe, ce compartiment à bagages présentant un dispositif permettant de le verrouiller en position fermée et un mécanisme pour l'ouvrir au moyen d'une poignée (3) actionnable de l'extérieur. L'objectif de l'invention est de permettre un remplacement simple et rapide des pièces visibles si celles-ci sont endommagées ou cassées. À cet effet, le mécanisme d'ouverture est disposé sur une plaque de base (12) et relié à la poignée (3) par des éléments de liaison démontables, la poignée (3) étant logée dans un élément de recouvrement (19) qui est lui-même relié à la plaque de base (12) par des éléments de liaison démontables.
PCT/EP2009/058827 2008-07-11 2009-07-10 Compartiment à bagages pour aéronef de passagers Ceased WO2010004030A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT10872008A AT506980B1 (de) 2008-07-11 2008-07-11 Gepäckablage für ein passagierflugzeug
ATA1087/2008 2008-07-11

Publications (3)

Publication Number Publication Date
WO2010004030A2 true WO2010004030A2 (fr) 2010-01-14
WO2010004030A3 WO2010004030A3 (fr) 2010-05-14
WO2010004030A9 WO2010004030A9 (fr) 2010-07-01

Family

ID=41353878

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/058827 Ceased WO2010004030A2 (fr) 2008-07-11 2009-07-10 Compartiment à bagages pour aéronef de passagers

Country Status (2)

Country Link
AT (1) AT506980B1 (fr)
WO (1) WO2010004030A2 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011070072A1 (fr) * 2009-12-09 2011-06-16 Sfs Intec Holding Ag Mécanisme de verrouillage pour un boîtier et serrure adaptée à ce mécanisme
WO2018075766A1 (fr) * 2016-10-21 2018-04-26 Southco, Inc. Verrou de poubelle
JP2019196170A (ja) * 2013-02-13 2019-11-14 シーアンドディー ゾディアック，インコーポレイティド 回転式棚アセンブリ
EP4112462A1 (fr) * 2021-07-01 2023-01-04 BSP2019 Aeronáutica S.L. Système de sécurité pour compartiments à bagages à main d'aéronef

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4637642A (en) * 1983-12-16 1987-01-20 The Boeing Company Stowage bin latch assembly
US5785788A (en) * 1992-02-20 1998-07-28 Fischer Advanced Composite Components Gmbh Process for manufacturing a stowage container for use in an aircraft
US5823472A (en) * 1996-06-04 1998-10-20 Fuselage Engineering Services Ltd. Stowage compartment construction particularly for aircraft
DE20017674U1 (de) * 2000-10-14 2000-12-28 Schwarz Verbindungs-Systeme GmbH, 75382 Althengstett Lösbare mechanische Verriegelungsanordnung zwischen einem schwenkbaren Deckel und einem Behälter, vorzugsweise einem Gepäckfach
US7234666B2 (en) * 2005-03-02 2007-06-26 The Boeing Company Pivoting storage bin and method of making
US7302150B2 (en) * 2006-04-27 2007-11-27 The Boeing Company Illuminated latch indicator assembly

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011070072A1 (fr) * 2009-12-09 2011-06-16 Sfs Intec Holding Ag Mécanisme de verrouillage pour un boîtier et serrure adaptée à ce mécanisme
US8939473B2 (en) 2009-12-09 2015-01-27 Sfs Intec Holding Ag Locking mechanism for a housing and lock suitable therefor
JP2019196170A (ja) * 2013-02-13 2019-11-14 シーアンドディー ゾディアック，インコーポレイティド 回転式棚アセンブリ
JP2021079944A (ja) * 2013-02-13 2021-05-27 サフラン キャビン インコーポレイティド 回転式棚アセンブリ
JP7114761B2 (ja) 2013-02-13 2022-08-08 サフラン キャビン インコーポレイティド 回転式棚アセンブリ
WO2018075766A1 (fr) * 2016-10-21 2018-04-26 Southco, Inc. Verrou de poubelle
US11585130B2 (en) 2016-10-21 2023-02-21 Southco, Inc. Bin latch
EP4112462A1 (fr) * 2021-07-01 2023-01-04 BSP2019 Aeronáutica S.L. Système de sécurité pour compartiments à bagages à main d'aéronef

Also Published As

Publication number Publication date
WO2010004030A9 (fr) 2010-07-01
AT506980A1 (de) 2010-01-15
AT506980B1 (de) 2010-07-15
WO2010004030A3 (fr) 2010-05-14

Similar Documents

Publication Publication Date Title
EP2363323B1 (fr) Support de charges avec un support fonctionnel
EP0754130A1 (fr) Dispositif de verrouillage servant a assujettir de maniere amovible le toit d'un vehicule a une partie fixe de la carrosserie
EP0437711B1 (fr) Dispositif de sécurité pour panneaux pivotants de véhicule automobile, notamment pour capot de moteur
EP1524152B1 (fr) Volet pour coffre
EP2690050A1 (fr) Cabine élévatrice avec fenêtre d'entretien
DE102013222955A1 (de) Doppelte Haubenverriegelungsanordnung
AT506980B1 (de) Gepäckablage für ein passagierflugzeug
EP2157006B1 (fr) Passerelle pour un passage d'intercirculation entre deux véhicules articulés, par exemple d'un tramway
WO2009086897A2 (fr) Auxiliaire de montage et procédé de montage
AT506979B1 (de) Gepäckablage für ein passagierflugzeug
EP0606547B1 (fr) Mécanisme de verrouillage pour le dispositif de déplacement longitudinal d'un siège de véhicule
AT410536B (de) Aufhängevorrichtung für absenkbare gepäckablagebehälter
EP2526009B1 (fr) Système de verrouillage
DE102017204494B4 (de) Schiebedachsystem für ein Kraftfahrzeug
DE102012004999A1 (de) Kraftfahrzeuganhängevorrichtung
DE202012100259U1 (de) Handbremshebel
DE102010026764A1 (de) Betätigungseinrichtung für eine Verriegelungsvorrichtung eines Kraftwagens
DE102005009204B3 (de) Betätigungsanordnung zum Entsichern der Motorhaube eines Kraftwagens
DE2632890C2 (de) Ortsfeste Kupplungsvorrichtung einer Unterflurschleppkettenföderanlage
DE102013011172B3 (de) Schwenkklappe zum Verschließen eines Ablagefachs eines Fahrzeugs
EP1847447B1 (fr) Ranche pour l'ouverture de chargement d'une construction automobile
CH662317A5 (de) Dachtraeger fuer kraftfahrzeuge.
DE102004039370B4 (de) Fahrzeugsitz, insbesondere für ein Kraftfahrzeug
DE102010021897A1 (de) Gestängeklappenanordnung für ein Cabriolet
EP3750772B1 (fr) Tête d'attelage, en particulier pour un véhicule ferroviaire

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 09780435

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 09780435

Country of ref document: EP

Kind code of ref document: A2