CN101495371A - Baggage bin and associated door intended in particular for an aircraft - Google Patents

Baggage bin and associated door intended in particular for an aircraft Download PDF

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Publication number
CN101495371A
CN101495371A CNA200780028274XA CN200780028274A CN101495371A CN 101495371 A CN101495371 A CN 101495371A CN A200780028274X A CNA200780028274X A CN A200780028274XA CN 200780028274 A CN200780028274 A CN 200780028274A CN 101495371 A CN101495371 A CN 101495371A
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CN
China
Prior art keywords
compartment
door
baggage rack
pivotal axis
open surface
Prior art date
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Granted
Application number
CNA200780028274XA
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Chinese (zh)
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CN101495371B (en
Inventor
T-M·博克
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Airbus SAS
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Airbus SAS
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Filing date
Publication date
Application filed by Airbus SAS filed Critical Airbus SAS
Priority claimed from PCT/FR2007/001270 external-priority patent/WO2008012427A1/en
Publication of CN101495371A publication Critical patent/CN101495371A/en
Application granted granted Critical
Publication of CN101495371B publication Critical patent/CN101495371B/en
Expired - Fee Related legal-status Critical Current
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R5/00Compartments within vehicle body primarily intended or sufficiently spacious for trunks, suit-cases, or the like
    • B60R5/003Luggage racks, e.g. for busses
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B61RAILWAYS
    • B61DBODY DETAILS OR KINDS OF RAILWAY VEHICLES
    • B61D37/00Other furniture or furnishings
    • B61D37/003Other furniture or furnishings luggage rack and umbrella-stand for rail vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/003Stowage devices for passengers' personal luggage

Abstract

A rack comprises a compartment which has an open face for inserting and removing luggage, a lower face (8) and an end wall (10) opposite the open face. This compartment is mounted such that it can pivot about a fixed pivot axis (4) between an open position in which the open face of the compartment is accessible, and a closed position in which the open face of the compartment is retracted. It also comprises a door (18) that is pivot-mounted in such a way that this door (18) impedes access to the open face when the compartment is in the closed position and allows free access to this face when the compartment is open. Connecting means (22) connect the door (18) and the compartment of the luggage rack in such a way that the pivoting movement of the compartment causes the door (18) to pivot.

Description

Be used in particular for the baggage container and the relevant door of aerocraft
Technical field
[01] the present invention relates to be particularly useful for the baggage container of aerocraft and the door of being correlated with.
[02] the field of the invention is a conveying people in aerocraft.In travelling, tourist's luggage is placed in the cargo hold of aerocraft, and lighter luggage can be placed in the main cabin of aerocraft with the tourist.In this main cabin, for the light luggage that is called hand-baggage again is provided with the incorporating section.These incorporating sections are usually located at the top of aircraft cabin, below the top board in main cabin and be used to admit above passenger's the seat tool.
Background technology
[03] the luggage incorporating section of existence two big classes in the aerocraft.The baggage container of one side known fixed, the baggage rack of known pivot on the other hand.Here the incorporating section with the fixing compartment of relative aircraft cabin and door is called baggage container, described door generally pivots, and leads to the gangway of luggage compartment thereby allow to open and close.As for baggage rack, it also comprises the compartment of being furnished with the gangway that allows to put into and take out luggage.Here this compartment is and to receive that the top board in-to-in of aircraft cabin takes in compartment movable between the position at first extended position, and at first extended position, the gangway of leading to compartment is open, and is takeing in the position, and the gangway of leading to compartment is closed.
[04] in this two classes incorporating section, there is considerable restraint in aesthetic.In fact, compartment is fixed on the one hand, and its shape is forced in aircraft cabin.On the other hand, the top board shape is restricted, so as can be when movable compartment should to be closed as the closure member of movable compartment.
Summary of the invention
[05] thereby the objective of the invention is to: the luggage incorporating section in the aircraft cabin is provided, and it allows for determines that the designer wishes that the shape in the aircraft interior space of giving reserves the space of freely bringing into play.
[06] for this reason, the present invention proposes baggage rack, and it is particularly useful for aircraft cabin, and this baggage rack comprises compartment, and described compartment comprises: open surface, and it allows to lead to described compartment luggage or similar articles are put into compartment or take out from compartment; Be used to admit the lower surface of luggage; And the bottom relative with the open surface of described compartment, this compartment is installed between release position and off position pivotally around fixing pivotal axis, and in described release position, the user can be near the open surface of described compartment, and at described off position, the open surface of described compartment is packed up.
[07] according to the present invention, such baggage rack comprises door in addition, described hingen changes to be installed, thus when described compartment is in the closed position the open surface of the approaching described compartment of this prevention, and when described compartment is in the release position this permission freedom near this open surface; And link connects the compartment of described door and described baggage rack, make the pivoting action of described compartment drive described hingen commentaries on classics, and/or the pivoting action of door driving compartment pivots.
[08] therefore, two parts are that compartment and pivoted door all are movable in baggage rack.Can in the shaped design in baggage rack and space, baggage rack place, have bigger degree of freedom like this.In fact, Men shape in the off position of baggage rack and main cabin (or other) arrange that desirable shape matches.Because this is movable, it can be in and take in the position then, thereby allows to enter in the compartment of baggage rack.
[09] in a favourable embodiment, in the release position of compartment, the relative horizontal direction of lower surface is in the lopsidedness of open surface 0 ° to 10 ° angle for example, with the convenient luggage that takes out, and at the off position of compartment, the relative horizontal direction of lower surface is at the lopsidedness of compartment bottom.Therefore, at off position, the luggage that places in compartment is tending towards whereabouts compartment bottom naturally by gravity, so the compartment bottom is as block piece.
[10] for the ease of the motion of baggage rack compartment, the bottom and the open surface of the relative compartment of pivotal axis of compartment are placed in the middle substantially.
[11] preferred implementation of the present invention proposes: the lower surface of compartment comprises outer casing, and pivoted door is in the extension of this outer casing at the off position of compartment.Therefore outer casing can make the shape of baggage rack adapt to the shape of space outerpace.In this embodiment, the pivotal axis of door is advantageously parallel with the pivotal axis of compartment, and the pivotal axis of door is preferably at the reveal relative with the outer casing of compartment lower surface.This configuration can make two movable members have simple relative motion.Can consider that also pivoted door is in the extension of compartment upper surface in the compartment release position.
[12] one embodiments are arranged to: described link comprises rod member, and described rod member connects described door and described compartment and transmitting movement.The advantage of this embodiment is that its enforcement is simple, reliable and low-cost.In this embodiment, described rod member can have: the first arm, and it is being fixed near pivotal axis of described door on the described door; And second arm, it is installed in the end relative with described door of described the first arm on the one hand and is installed between the described compartment by pivot connector on the other hand.Also can consider to have the commutation machinery of other type attaching parts or have mechanism more than two arms.All these depend on the motion of wishing realization.The objective of the invention is to also have the vpg connection of luggage compartment to give very big degree of freedom,, can consider many modification of the bindiny mechanism between these two parts especially in order to adapt to these difformities in the shape of pivoted door.
[13] for simpler mechanism is arranged, realize that preferably bonded assembly bindiny mechanism can make between compartment and the door: compartment and door pivot in the same direction during motion.
[14] the invention still further relates to the aircraft cabin that comprises top board, it is characterized in that, this main cabin comprises at least one above-mentioned baggage rack, and the door of installing that pivots is integrated in the top board of main cabin.
[15] the present invention also relates to an aerocraft at last, it is characterized in that, this aerocraft comprises at least one above-mentioned baggage rack and/or main cabin.
Description of drawings
[16] description by carrying out below with reference to schematic figures, details of the present invention and advantage will more clearly embody, and accompanying drawing is as follows:
[17] Fig. 1 is the schematic cross section of baggage rack according to the invention of aircraft cabin and the partial cross section scheme drawing that also has aircraft cabin, and baggage rack is in off position;
[18] Fig. 2 schemes accordingly with Fig. 1, but the baggage rack that mediates is shown; And
[19] Fig. 3 represents this baggage rack in the closed position with similar diagram.
The specific embodiment
[20] accompanying drawing represents to be pivoted on pivotal axis 4 baggage rack 2 on every side.Here relate to the baggage rack 2 that is installed in the aircraft cabin.This baggage rack is installed in top, main cabin and is being used to admit on passenger's the seat tool.Pivotal axis 4 is that relative aircraft cabin is axle longitudinally.See that as knowing among the figure this relative main cabin is fixed.Can see the top board 6 in this main cabin among the figure.
[21] baggage rack comprises the compartment that is used to admit luggage.This compartment has outer lower surface 8, bottom 10, upper surface 12 and sidewall 14.The shape of this compartment is parallelepiped substantially.Lower surface 8 is externally covered by case 16, and this case is slightly rounded to form the outside face of projection.The face relative with bottom 10 is complete open surface.
[22] baggage rack shown in Figure 1 is in its off position.This moment, baggage rack took in the top board 6 of aircraft cabin.Case 16 is as the component part of this top board shape.Thereby also can see door 18 in the extension of case 16, and door 18 also is connected with top board 6.Represented as different figure, this 18 pivots.In illustrated embodiment, the pivotal axis 4 that the pivotal axis 20 of door is parallel to the compartment of baggage rack 2 extends.Shown in preferred implementation in be also noted that this pivotal axis 20 is in the place, junction surface of pivoted door 18 and top board 6, promptly at the reveal relative with baggage rack compartment and baggage rack case 16.
[23] pivotal axis 4 of baggage rack compartment is vertical with the sidewall 14 of this compartment, and pivotal axis 4 is in the center of preceding open surface, bottom 10, lower surface 8 and upper surface 12 substantially.Therefore in this preferred implementation, this pivotal axis is equidistant substantially apart from open surface and bottom 10, and similarly, this pivotal axis is also equidistant substantially apart from lower surface 8 and upper surface 12.
Here notice that [24] at the off position of compartment, the lower surface 8 of compartment tilts to bottom 10.Therefore because gravity, be arranged in compartment and be tending towards keeping off on the bottom 10 that leans against compartment by the luggage that is put on the lower surface 8.Therefore, luggage is tending towards remaining in the compartment and can drop out from compartment through the open surface of compartment.
[25] compartment is connected by rod member 22 with pivoted door 18.This rod member has the first arm 24 and second arm 26.
[26] the first arm 24 is fixed on the pivoted door 18.In a preferred embodiment, the first arm extends perpendicular to the pivotal axis 20 of pivoted door 18, and is in the same plane with this pivotal axis 20.In addition, still for this preferred implementation, the first arm 24 is vertical substantially with pivoted door 18.
[27] second arm 26 of rod member 22 makes the compartment of baggage rack 2 be connected with the first arm 24.Second arm is connected with the sidewall 14 of compartment by pivot connector 28.Can consider other connection mode of rod member 22 and compartment.For example, pivot connector 28 comprises axle and bearing.This axle can connect together with second arm 26, and this bearing can link to each other with sidewall 14, perhaps implements conversely.Being connected also between second arm 26 and the first arm 24 realizes by the pivot connector that for example is hinge 30 forms.Pivot connector 28 is on the sidewall 14 near the intersection point of bottom 10 and upper wall 12.
[28] unique rod member 22 has only been described in the description of carrying out above.Certainly each sidewall 14 can be correlated such rod member.As already noted, the rod member of connection pivoted door and baggage rack compartment can be mounted on compartment and pivoted door in different loci.Can by other parts beyond the rod member for example train of gears guarantee being connected between compartment and the pivoted door.Although said method is admissible, its cost is higher.Also can consider other connecting device.
[29] compartment of Fig. 1-3 expression baggage rack 2 and three relative positions of pivoted door 18.As has been described, Fig. 1 represents to be in the baggage rack of its off position.In order to open baggage rack 2, the passenger catches the handle (not shown) near the case 16 that for example is hidden in lower surface 8 pivoted door 18.The passenger drives the compartment of baggage rack 2 then, and it is pivoted with the fixing pivotal axis 4 of simple rotational motion around it.This rotational motion passes to pivoted door 18 by rod member 22.Thereby pivoted door 18 is pivoted along the direction identical with the compartment of baggage rack 2.Under the situation also shown in the figure in the embodiment shown, when opening baggage rack 2, compartment and pivoted door 18 are rotated along clockwise direction.Rod member 22 is given pivoted door 18 Motion Transmission of compartment on a pivotal orientation, so same on another pivotal orientation.
Midway location when [30] Fig. 2 opens baggage rack 2 as example shown.In Fig. 3, baggage rack 2 is in its release position.In this release position, the open surface of the compartment of baggage rack 2 can touch from the inside of aircraft cabin fully.Pivoted door 18 is received top board 6 inside in main cabin, and no longer forms the obstacle in the compartment that leads to baggage rack 2.In this release position, the free end of pivoted door 18 arrives the last seamed edge of compartment opening.This moment, pivoted door 18 was in the extension of upper surface 12 substantially.The lower surface 8 of compartment tilts towards open surface now.Degree of dip for example is about 8 °.This degree of dip allows conveniently luggage to be fetched into beyond the compartment when baggage rack is opened, and luggage can wholely not drop.It also can make the passenger can see compartment inside better in the release position of baggage rack 2.
[31] advantage with the pivot compartment that combines with pivoted door is: the shape for the top board 6 that will give aircraft cabin has very big degree of freedom.The shape that provides as example in the accompanying drawing is a complete uncommon shape in the aircraft known.Certainly also can consider other shape.For example can have the pivoted door that is basically parallel to the compartment bottom at the off position of baggage rack.The designer also can consider many other shapes.
[32] the present invention also has (particularly owing to use fixing pivotal axis) such advantage: do not compare with the orthodox method of using during luggage is taken in and can bring fringe cost.The cost of baggage rack according to the invention is similar to the cost of the baggage rack of prior art.
[33] preferred implementation of describing as non-limiting example above the present invention is not limited to.The invention still further relates to those skilled in the art's enforcement modification within the scope of the following claims.

Claims (12)

1. baggage rack (2), it is particularly useful for aircraft cabin, and this baggage rack comprises compartment, and described compartment comprises: open surface, it allows to lead to described compartment luggage or similar articles are put into compartment or take out from compartment; Be used to admit the lower surface (8) of luggage; And the bottom (10) relative with the open surface of described compartment, this compartment is installed between release position and off position pivotally around fixing pivotal axis (4), in described release position, the user can be near the open surface of described compartment, and at described off position, the open surface of described compartment is packed up
It is characterized in that, this baggage rack comprises door (18) in addition, described hingen changes to be installed, thereby this door (18) prevention is near the open surface of described compartment when described compartment is in the closed position, and this door (18) allows free near this open surface when described compartment is in the release position; And link (22) connects the compartment of described door (18) and described baggage rack, make the pivoting action of described compartment drive described door (18) pivot, and/or vice versa.
2. baggage rack as claimed in claim 1, it is characterized in that, release position at described compartment, the relative horizontal direction of described lower surface (8) is at the lopsidedness of described open surface, with the convenient luggage that takes out, and at the off position of described compartment, described lower surface (8) relatively horizontal direction at the bottom (10) of described compartment lopsidedness.
3. baggage rack as claimed in claim 2 is characterized in that, in the release position, described lower surface (8) relatively horizontal direction tilts one between 0 ° to 10 ° angle.
4. as each described baggage rack in the claim 1 to 3, it is characterized in that the open surface of described relatively bottom of the pivotal axis of described compartment (4) (10) and described compartment is placed in the middle substantially.
5. as each described baggage rack in the claim 1 to 4, it is characterized in that the lower surface of described compartment (8) comprises outer casing (16); And at the off position of described compartment, described pivoted door (18) is in the extension of this outer casing (16).
6. baggage rack as claimed in claim 5 is characterized in that, the pivotal axis (20) of described door (18) is parallel with the pivotal axis (4) of described compartment; And this pivotal axis (20) is in door (18) side relative with the outer casing (16) of the lower surface (8) of described compartment.
7. as each described baggage rack in the claim 1 to 6, it is characterized in that in the release position of described compartment, described pivoted door (18) is in the extension of upper surface (12) of described compartment substantially.
8. as each described baggage rack in the claim 1 to 7, it is characterized in that described link comprises rod member (22), described rod member connects described door (18) and described compartment and transmitting movement.
9. baggage rack as claimed in claim 8 is characterized in that, described rod member (22) has: the first arm (24), and it is being fixed near pivotal axis (20) of described door (18) on the described door (18); And second arm (26), its be installed on the one hand described the first arm (24) the end relative with described door (18), be installed between the described compartment by pivot connector (28) on the other hand.
10. as each described baggage rack in the claim 1 to 9, it is characterized in that, realize that the described link of bonded assembly (22) is such between described compartment and described door (18): described compartment and described door (18) pivot in the same direction during motion.
11. aircraft cabin, it comprises top board, it is characterized in that, described aircraft cabin comprises at least one as each described baggage rack (2) in the claim 1 to 9; And the door of installing (18) that pivots is integrated in the top board (6) in described main cabin.
12. aerocraft is characterized in that, described aerocraft comprises at least one as each described baggage rack (2) in the claim 1 to 9.
CN200780028274XA 2006-07-24 2007-07-24 Baggage bin and associated door intended in particular for an aircraft Expired - Fee Related CN101495371B (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FR0606735 2006-07-24
FR0606735A FR2903963B1 (en) 2006-07-24 2006-07-24 LUGGAGE BOX AND ASSOCIATED DOOR, IN PARTICULAR FOR AN AIRCRAFT
US84407506P 2006-09-13 2006-09-13
US60/844,075 2006-09-13
PCT/FR2007/001270 WO2008012427A1 (en) 2006-07-24 2007-07-24 Luggage locker and associated door which are intended in particular for an aircraft

Publications (2)

Publication Number Publication Date
CN101495371A true CN101495371A (en) 2009-07-29
CN101495371B CN101495371B (en) 2012-04-18

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CN200780028274XA Expired - Fee Related CN101495371B (en) 2006-07-24 2007-07-24 Baggage bin and associated door intended in particular for an aircraft

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CN (1) CN101495371B (en)
FR (1) FR2903963B1 (en)
RU (1) RU2435708C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105188477A (en) * 2013-04-05 2015-12-23 B/E航空公司 Overhead equipment stowage pod for an aircraft interior

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007059686A1 (en) 2007-12-12 2009-06-18 Airbus Deutschland Gmbh Storage compartment arrangement
US9327834B2 (en) * 2013-10-04 2016-05-03 Embraer S.A. Overhead bin system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4275942A (en) * 1978-12-26 1981-06-30 The Boeing Company Stowage bin mechanism
DE4209037C2 (en) * 1992-03-20 1994-06-23 Deutsche Aerospace Airbus Device for carrying luggage in airplanes
US5228763A (en) * 1992-03-30 1993-07-20 Lawrence Gingold Extendable storage element
US5456529A (en) * 1993-12-30 1995-10-10 The Boeing Company Powered overhead stowage bin
DE4425869C2 (en) * 1994-07-21 1996-05-30 Daimler Benz Aerospace Airbus Overhead luggage rack, in particular for a passenger aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105188477A (en) * 2013-04-05 2015-12-23 B/E航空公司 Overhead equipment stowage pod for an aircraft interior
CN105188477B (en) * 2013-04-05 2018-01-09 B/E航空公司 The top arrangement storage gondola of aircraft interior

Also Published As

Publication number Publication date
RU2009106056A (en) 2010-08-27
CN101495371B (en) 2012-04-18
FR2903963B1 (en) 2009-04-03
FR2903963A1 (en) 2008-01-25
RU2435708C2 (en) 2011-12-10

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