CN101495371B - 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 PDFInfo
- Publication number
- CN101495371B CN101495371B CN200780028274XA CN200780028274A CN101495371B CN 101495371 B CN101495371 B CN 101495371B CN 200780028274X A CN200780028274X A CN 200780028274XA CN 200780028274 A CN200780028274 A CN 200780028274A CN 101495371 B CN101495371 B CN 101495371B
- Authority
- CN
- China
- Prior art keywords
- compartment
- door
- baggage rack
- pivotal axis
- pivot
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000033001 locomotion Effects 0.000 claims abstract description 11
- 230000005484 gravity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R5/00—Compartments within vehicle body primarily intended or sufficiently spacious for trunks, suit-cases, or the like
- B60R5/003—Luggage racks, e.g. for busses
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B61—RAILWAYS
- B61D—BODY DETAILS OR KINDS OF RAILWAY VEHICLES
- B61D37/00—Other furniture or furnishings
- B61D37/003—Other furniture or furnishings luggage rack and umbrella-stand for rail vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hinges (AREA)
- Vehicle Step Arrangements And Article Storage (AREA)
- Cabinets, Racks, Or The Like Of Rigid Construction (AREA)
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
Technical field
The present invention relates to be particularly useful for the baggage container and the relevant door of aerocraft.
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 with the seat tool that is used to admit the passenger above.
Background technology
There is two big types luggage incorporating section in the aerocraft.The baggage container of one side known fixed, the baggage rack of known pivot on the other hand.Here call baggage container to the incorporating section with the fixing compartment of relative aircraft cabin and door, said 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.
In these two types of incorporating sections, there is considerable restraint in aesthetic.In fact, compartment is fixed on the one hand, and forces its shape 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
Thereby the objective of the invention is to: the luggage incorporating section in the aircraft cabin is provided, and its shape that allows for the aircraft interior space of confirming that the designer hopes to give is reserved the space of freely bringing into play.
For this reason, the present invention proposes baggage rack, and it is particularly useful for aircraft cabin, and this baggage rack comprises compartment, and said compartment comprises: open surface, and it allows to lead to said compartment to put into compartment to luggage or similar articles or to take out from compartment; Be used to admit the lower surface of luggage; And the bottom relative with the open surface of said compartment; This compartment is installed between release position and off position around fixing pivotal axis pivotally, and in said release position, the user can be near the open surface of said compartment; And at said off position, the open surface of said compartment is packed up.
According to the present invention, such baggage rack comprises door in addition, and said hingen changes to be installed, thus when said compartment is in the closed position the open surface of the approaching said compartment of this prevention, and when said compartment is in the release position this permission freedom near this open surface; And link connects the compartment of said door and said baggage rack, make the pivoting action of said compartment drive said hingen commentaries on classics, and/or the pivoting action of door driving compartment pivots.
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, (or other) desirable shape of layout matches the shape of door in the off position of baggage rack and main cabin.Because this is movable, it can be in and take in the position then, thereby allows to enter in the compartment of baggage rack.
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 through gravity, so the compartment bottom is as block piece.
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 basically.
A 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 the shape adaptation of baggage rack in 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.
One embodiment is arranged to: said link comprises rod member, and said rod member connects said door and said compartment and transmitting movement.The advantage of this embodiment is that its enforcement is simple, reliable and low-cost.In this embodiment, said rod member can have: the first arm, and it is being fixed near pivotal axis of said door on the said door; And second arm, it is installed in the relative end of door said the first arm and said on the one hand and is installed between the said compartment through pivot connector on the other hand.Also can consider to have the switching-over machinery of other type attaching parts or have mechanism more than two arms.All these depend on the motion of hoping 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.
For simpler mechanism is arranged, realize that preferably bonded assembly bindiny mechanism can make between compartment and the door: compartment pivots with door in the same direction during motion.
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.
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
Through the following description of carrying out with reference to schematic figures, details of the present invention and advantage will more clearly embody, and accompanying drawing is following:
Fig. 1 is schematic cross section and the partial cross section scheme drawing that also has aircraft cabin of the baggage rack according to the invention of aircraft cabin, and baggage rack is in off position;
Fig. 2 schemes with Fig. 1 accordingly, but the baggage rack that mediates is shown; And
Fig. 3 representes this baggage rack in the closed position with similar diagram.
The specific embodiment
Accompanying drawing representes 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 fixes.Can see the top board 6 in this main cabin among the figure.
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 basically.Lower surface 8 is externally covered by case 16, and this case is slightly rounded to form protruding outside face.With bottom 10 relative faces are complete open surfaces.
Be in its off position at baggage rack shown in Fig. 1.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 the door 18 in the extension of case 16, and door 18 also is connected with top board 6.Figure as different is represented, and 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.
The 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 basically.Therefore in this preferred implementation, this pivotal axis is apart from open surface and bottom 10 basic equidistance, and likewise, this pivotal axis is also apart from lower surface 8 and upper surface 12 basic equidistance.
Here notice that 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 from compartment, drop out through the open surface of compartment.
Compartment is connected through rod member 22 with pivoted door 18.This rod member has the first arm 24 and second arm 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 basically with pivoted door 18.
The compartment of Fig. 1-3 expression baggage rack 2 and three relative positions of pivoted door 18.As described, Fig. 1 representes 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 pivoted door 18, is hidden in lower surface 8.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 through rod member 22.Thereby the pivoted door 18 edges direction identical with the compartment of baggage rack 2 pivots.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 Fig. 2 representes to open baggage rack 2 as an example.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 basically.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 better that in the release position of baggage rack 2 compartment is inner.
Advantage with the pivot compartment that combines with pivoted door is: the shape for the top board that will give aircraft cabin 6 has very big degree of freedom.The shape that provides as an 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.
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 with the cost of the baggage rack of prior art.
The preferred implementation of describing as non-limiting example above the present invention is not limited to.The invention still further relates to the enforcement modification of those skilled in the art in the scope of following claim.
Claims (12)
1. baggage rack (2), it is used for aircraft cabin, and this baggage rack comprises compartment, and said compartment comprises: open surface, it allows to lead to said compartment to put into luggage compartment and to take out from compartment; Be used to admit the lower surface (8) of luggage; And the bottom (10) relative with the open surface of said compartment; This compartment is installed between release position and off position around fixing pivotal axis (4) pivotally; In said release position, the open surface of the approaching said compartment of user's ability, and at said off position; The open surface of said compartment is packed up
It is characterized in that; This baggage rack comprises door (18) in addition; Said hingen changes to be installed, thereby this door (18) stops the open surface near said compartment when said compartment is in the closed position, and this door (18) allows free near this open surface when said compartment is in the release position; And link connects the compartment of said (18) and said baggage rack, make the pivoting action of said compartment drive said door (18) pivot, and/or the pivoting action of said door drives said compartment pivot.
2. baggage rack as claimed in claim 1; It is characterized in that; In the release position of said compartment, the relative horizontal direction of said lower surface (8) is at the lopsidedness of said open surface, with the convenient luggage that takes out; And at the off position of said compartment, said lower surface (8) relatively horizontal direction in the bottom (10) of said compartment lopsidedness.
3. baggage rack as claimed in claim 2 is characterized in that, in the release position, said lower surface (8) relatively inclined one between 0 ° to 10 ° angle.
4. like each described baggage rack in the claim 1 to 3, it is characterized in that the open surface of said relatively bottom of the pivotal axis of said compartment (4) (10) and said compartment is placed in the middle basically.
5. like each described baggage rack in the claim 1 to 3, it is characterized in that the lower surface of said compartment (8) comprises outer casing (16); And at the off position of said compartment, the said door (18) of pivot 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 said door (18) is parallel with the pivotal axis (4) of said compartment; And, this pivotal axis (20) of said door with relative door (18) side of outer casing (16) of the lower surface (8) of said compartment.
7. like each described baggage rack in the claim 1 to 3, it is characterized in that in the release position of said compartment, the said door (18) of pivot is in the extension of upper surface (12) of said compartment basically.
8. like each described baggage rack in the claim 1 to 3, it is characterized in that said link comprises rod member (22), said rod member connects said door (18) and said compartment and transmitting movement.
9. baggage rack as claimed in claim 8 is characterized in that, said rod member (22) has: the first arm (24), and it is being fixed near pivotal axis (20) of said door (18) on the said door (18); And second arm (26), said second arm makes the compartment of said baggage rack (2) be connected with said the first arm (24), and said second arm is connected with the sidewall (14) of said compartment through pivot connector (28).
10. like each described baggage rack in the claim 1 to 3, it is characterized in that, between said compartment and said door (18), realize that the said link of bonded assembly is such: said compartment and said door (18) pivot on equidirectional during motion.
11. aircraft cabin, it comprises top board, it is characterized in that, said aircraft cabin comprises at least one like 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 said main cabin.
12. aerocraft is characterized in that, said aerocraft comprises at least one like each described baggage rack (2) in the claim 1 to 9.
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0606735A FR2903963B1 (en) | 2006-07-24 | 2006-07-24 | LUGGAGE BOX AND ASSOCIATED DOOR, IN PARTICULAR FOR AN AIRCRAFT |
| FR0606735 | 2006-07-24 | ||
| 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 CN101495371A (en) | 2009-07-29 |
| CN101495371B true CN101495371B (en) | 2012-04-18 |
Family
ID=37763925
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200780028274XA Expired - Fee Related CN101495371B (en) | 2006-07-24 | 2007-07-24 | Baggage bin and associated door intended in particular for an aircraft |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN101495371B (en) |
| FR (1) | FR2903963B1 (en) |
| RU (1) | RU2435708C2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007059686A1 (en) | 2007-12-12 | 2009-06-18 | Airbus Deutschland Gmbh | Storage compartment arrangement |
| CN105188477B (en) * | 2013-04-05 | 2018-01-09 | B/E航空公司 | The top arrangement storage gondola of aircraft interior |
| US9327834B2 (en) * | 2013-10-04 | 2016-05-03 | Embraer S.A. | Overhead bin system |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5228763A (en) * | 1992-03-30 | 1993-07-20 | Lawrence Gingold | Extendable storage element |
| US5441218A (en) * | 1992-03-20 | 1995-08-15 | Deutsche Aerospace Airbus Gmbh | Overhead luggage compartment system for passenger aircraft |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4275942A (en) * | 1978-12-26 | 1981-06-30 | The Boeing Company | Stowage bin mechanism |
| 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 |
-
2006
- 2006-07-24 FR FR0606735A patent/FR2903963B1/en not_active Expired - Fee Related
-
2007
- 2007-07-24 CN CN200780028274XA patent/CN101495371B/en not_active Expired - Fee Related
- 2007-07-24 RU RU2009106056/11A patent/RU2435708C2/en not_active IP Right Cessation
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5441218A (en) * | 1992-03-20 | 1995-08-15 | Deutsche Aerospace Airbus Gmbh | Overhead luggage compartment system for passenger aircraft |
| US5228763A (en) * | 1992-03-30 | 1993-07-20 | Lawrence Gingold | Extendable storage element |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101495371A (en) | 2009-07-29 |
| RU2009106056A (en) | 2010-08-27 |
| FR2903963A1 (en) | 2008-01-25 |
| FR2903963B1 (en) | 2009-04-03 |
| RU2435708C2 (en) | 2011-12-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120418 Termination date: 20210724 |