CA2627696C - Pivoting luggage rack intended for an aircraft cabin - Google Patents
Pivoting luggage rack intended for an aircraft cabin Download PDFInfo
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- CA2627696C CA2627696C CA2627696A CA2627696A CA2627696C CA 2627696 C CA2627696 C CA 2627696C CA 2627696 A CA2627696 A CA 2627696A CA 2627696 A CA2627696 A CA 2627696A CA 2627696 C CA2627696 C CA 2627696C
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- compartment
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- pivoting
- aircraft cabin
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- 238000000151 deposition Methods 0.000 claims description 5
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Step Arrangements And Article Storage (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
The invention relates to a bin for luggage (2), comprising a compartment having a lower external face (8), an upper face (12), an open face for accessing the compartment and a base (10). The inventive bin is mounted such that it can pivot about a pivot axis (4) between an open position in which the open face of the compartment can be accessed and in which the rear part (26) of the lower external face (8) is concealed and a closed position in which the open face of the compartment is retracted and in which the rear part (26) of the lower external face (8) is visible. The aforementioned rear part (26) takes the form of a cylinder having generatrices (34, 36) that are essentially parallel to the pivot axis (4) of the bin. Moreover, the distance (R1, R2) from the pivot axis (4) to the generatrices (R1, R2) increases from the base (10) of the compartment towards the open face of same.
Description
Pivoting luggage rack intended for an aircraft cabin This invention relates to a luggage rack intended for an aircraft cabin.
The sphere of this invention is the transport of passengers in an aircraft.
During a trip, the travelers' luggage is placed in the holds of the aircraft, while lighter luggage can accompany the travelers in the aircraft cabin. In this cabin, storage spaces are provided for this luggage, also referred to as hand luggage.
More often than not, these storage spaces are arranged in the upper portion of the aircraft cabin, beneath the ceiling of this cabin and above the seats intended to accommodate the passengers.
There are two major types of storage space for luggage such as described previously. On the one hand there are luggage bins and on the other hand luggage racks. A luggage bin is a compartment fixed in relation to the aircraft cabin, and a door, generally pivoting, allows the opening and closing of access to the luggage compartment. A luggage rack, for its part, also has a compartment intended to accommodate luggage and comprising an access.
Here this compartment is a compartment movable between a first extended position in which access to the compartment is open, allowing the insertion and removal of luggage, and a position retracted inside the ceiling of the aircraft cabin, in which access to the compartment is closed.
The current trend, dictated by the airline companies, is to increase the volume of storage space for hand luggage inside aircraft cabins. However, the volume inside an aircraft cabin is limited. It therefore is advisable to make the most of the available space inside a given cabin. Moreover, as regards the luggage racks and bins, their dimensions are limited inasmuch as the standards provide that these storage spaces, in open or dosed position, must not hinder the movement of passengers in the aisles of the aircraft cabin.
This invention then has as a purpose to provide a luggage rack that, for a given length (measured longitudinally in the aircraft cabin), makes possible a greater volume of storage space for luggage than the known racks of the prior art.
To this end, it proposes a rack for luggage, intended in particular for an aircraft cabin, comprising a compartment having a lower outer face, an upper face, an open face, arranged between the lower outer face and the upper face,
The sphere of this invention is the transport of passengers in an aircraft.
During a trip, the travelers' luggage is placed in the holds of the aircraft, while lighter luggage can accompany the travelers in the aircraft cabin. In this cabin, storage spaces are provided for this luggage, also referred to as hand luggage.
More often than not, these storage spaces are arranged in the upper portion of the aircraft cabin, beneath the ceiling of this cabin and above the seats intended to accommodate the passengers.
There are two major types of storage space for luggage such as described previously. On the one hand there are luggage bins and on the other hand luggage racks. A luggage bin is a compartment fixed in relation to the aircraft cabin, and a door, generally pivoting, allows the opening and closing of access to the luggage compartment. A luggage rack, for its part, also has a compartment intended to accommodate luggage and comprising an access.
Here this compartment is a compartment movable between a first extended position in which access to the compartment is open, allowing the insertion and removal of luggage, and a position retracted inside the ceiling of the aircraft cabin, in which access to the compartment is closed.
The current trend, dictated by the airline companies, is to increase the volume of storage space for hand luggage inside aircraft cabins. However, the volume inside an aircraft cabin is limited. It therefore is advisable to make the most of the available space inside a given cabin. Moreover, as regards the luggage racks and bins, their dimensions are limited inasmuch as the standards provide that these storage spaces, in open or dosed position, must not hinder the movement of passengers in the aisles of the aircraft cabin.
This invention then has as a purpose to provide a luggage rack that, for a given length (measured longitudinally in the aircraft cabin), makes possible a greater volume of storage space for luggage than the known racks of the prior art.
To this end, it proposes a rack for luggage, intended in particular for an aircraft cabin, comprising a compartment having a lower outer face, an upper face, an open face, arranged between the lower outer face and the upper face,
2 and allowing access to the compartment for the depositing and removal of luggage or similar items inside same, as well as a back, opposite the open face of the compartment, this rack being mounted pivoting around an axis of pivoting and being movable around this axis between an open position in which the open face of the compartment is accessible from the cabin and in which a rear portion of the lower outer face is concealed, and a closed position in which the open face of the compartment is retracted and in which the said rear portion of the lower outer face is visible.
According to the invention, the said rear portion, concealed when the rack is open, has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and the distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the latter.
By cylindrical surface there is to be understood here a surface that can be generated by the movement of a straight line always retaining the same orientation. Such a surface therefore is the juxtaposition of parallel lines, referred to as generatrices, and arranged one next to the other.
A rack according to the invention therefore does not have circular cylindrical form near the back thereof, but a form reminiscent of a spiral.
This new form makes it possible to enlarge the interior volume of the luggage rack without having to encroach on the space set aside for the movement of passengers in the aircraft cabin.
In a rack for luggage according to the invention, an appreciable gain in volume is obtained when the distance from the axis of pivoting to the generatrices varies from one end to the other of the said rear portion by a value ranging from 5 to 20 cm, preferably from 10 to 15 cm.
For the interior layout of a rack for luggage according to the invention, the compartment advantageously comprises a lower inner face forming a floor in this compartment; the lower inner face of the compartment is substantially plane adjacent the open face; the lower inner face of the compartment rises up near the back, and a groove, the concavity of which is directed toward the upper face of the compartment, is formed in the junction zone between the raised portion of the
According to the invention, the said rear portion, concealed when the rack is open, has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and the distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the latter.
By cylindrical surface there is to be understood here a surface that can be generated by the movement of a straight line always retaining the same orientation. Such a surface therefore is the juxtaposition of parallel lines, referred to as generatrices, and arranged one next to the other.
A rack according to the invention therefore does not have circular cylindrical form near the back thereof, but a form reminiscent of a spiral.
This new form makes it possible to enlarge the interior volume of the luggage rack without having to encroach on the space set aside for the movement of passengers in the aircraft cabin.
In a rack for luggage according to the invention, an appreciable gain in volume is obtained when the distance from the axis of pivoting to the generatrices varies from one end to the other of the said rear portion by a value ranging from 5 to 20 cm, preferably from 10 to 15 cm.
For the interior layout of a rack for luggage according to the invention, the compartment advantageously comprises a lower inner face forming a floor in this compartment; the lower inner face of the compartment is substantially plane adjacent the open face; the lower inner face of the compartment rises up near the back, and a groove, the concavity of which is directed toward the upper face of the compartment, is formed in the junction zone between the raised portion of the
3 lower face and the back. This interior layout of the luggage rack makes it possible in particular to accommodate a suitcase not down flat on the lower inner face of the compartment intended to accommodate luggage, but diagonally in this compartment.
In such a rack, for a better retention of a suitcase, or of another piece of luggage, it can be provided that the free edge of the lower inner face of the compartment situated adjacent the open face for access to the compartment has a rim projecting from the lower inner face of the compartment toward the upper face of the latter.
Accordingly, in one aspect, the present invention provides a baggage rack for an aircraft cabin, the rack comprising: a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and wherein a distance from the axis of pivoting to the generatrices continuously increases from an intersection of the lower outer face and the back of the compartment to the open face of the compartment.
In a further aspect, the present invention provides a baggage rack for an aircraft cabin, the rack comprising: a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face, and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, 3a wherein said axis of pivoting is fixed relative to said compartment as said compartment pivots from said open position to said closed position, wherein said rear portion has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and wherein a distance from the axis of pivoting to the generatrices continuously increases from an intersection of the lower outer face and the back of the compartment to the open face of the compartment.
This invention also relates to an aircraft cabin, characterized in that it comprises at least one rack for luggage such as described above.
In such an aircraft cabin, an air vent extending along the rear portion of the lower outer face of a luggage rack can be provided, and this air vent has a movable flap at its outlet, for example. In this way, the outlet surface of the air vent can remain constant by making the position of the flap dependent on that of the luggage rack. In an advantageous embodiment, for it is quite simple to implement, the movable flap has a pivoting strip, extending under the junction between the rear portion of the lower outer face and the back of the compartment, when the rack is closed, and the pivoting strip is mounted, for example, pivoting around a longitudinal axis substantially parallel to the axis of pivoting of the corresponding luggage rack A movable flap such as described above can have spacing shims adjacent the luggage rack, and prestressing means then can be provided in order to keep the spacing shims bearing against the rear portion of the lower outer face of the luggage rack. It thus is possible, in simple manner, to ensure a constant air slit width. When the pivoting strip is mounted pivoting around a longitudinal axis substantially parallel to the axis of pivoting of the corresponding luggage rack, the prestressing means comprise, for example, a spring integrated into the pivoting shaft of the pivoting strip. For example, a spring can be provided at each bearing of the axis of pivoting of the pivoting strip.
Accordingly, in one aspect, the present invention provides an aircraft cabin, comprising: at least one baggage rack, each baggage rack including a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment; and a movable flap including a pivoting strip extending under a joining portion between the rear portion of the lower outer face and the back of the compartment when the at least one baggage rack is closed, wherein said rack is 3b pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, wherein a distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the compartment, and wherein the pivoting strip is pivotably mounted around a longitudinal axis substantially parallel to the axis of pivoting of the at least one baggage rack.
This invention also relates to an aircraft, characterized in that it comprises a cabin such as described above.
In such a rack, for a better retention of a suitcase, or of another piece of luggage, it can be provided that the free edge of the lower inner face of the compartment situated adjacent the open face for access to the compartment has a rim projecting from the lower inner face of the compartment toward the upper face of the latter.
Accordingly, in one aspect, the present invention provides a baggage rack for an aircraft cabin, the rack comprising: a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and wherein a distance from the axis of pivoting to the generatrices continuously increases from an intersection of the lower outer face and the back of the compartment to the open face of the compartment.
In a further aspect, the present invention provides a baggage rack for an aircraft cabin, the rack comprising: a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face, and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, 3a wherein said axis of pivoting is fixed relative to said compartment as said compartment pivots from said open position to said closed position, wherein said rear portion has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, and wherein a distance from the axis of pivoting to the generatrices continuously increases from an intersection of the lower outer face and the back of the compartment to the open face of the compartment.
This invention also relates to an aircraft cabin, characterized in that it comprises at least one rack for luggage such as described above.
In such an aircraft cabin, an air vent extending along the rear portion of the lower outer face of a luggage rack can be provided, and this air vent has a movable flap at its outlet, for example. In this way, the outlet surface of the air vent can remain constant by making the position of the flap dependent on that of the luggage rack. In an advantageous embodiment, for it is quite simple to implement, the movable flap has a pivoting strip, extending under the junction between the rear portion of the lower outer face and the back of the compartment, when the rack is closed, and the pivoting strip is mounted, for example, pivoting around a longitudinal axis substantially parallel to the axis of pivoting of the corresponding luggage rack A movable flap such as described above can have spacing shims adjacent the luggage rack, and prestressing means then can be provided in order to keep the spacing shims bearing against the rear portion of the lower outer face of the luggage rack. It thus is possible, in simple manner, to ensure a constant air slit width. When the pivoting strip is mounted pivoting around a longitudinal axis substantially parallel to the axis of pivoting of the corresponding luggage rack, the prestressing means comprise, for example, a spring integrated into the pivoting shaft of the pivoting strip. For example, a spring can be provided at each bearing of the axis of pivoting of the pivoting strip.
Accordingly, in one aspect, the present invention provides an aircraft cabin, comprising: at least one baggage rack, each baggage rack including a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment; and a movable flap including a pivoting strip extending under a joining portion between the rear portion of the lower outer face and the back of the compartment when the at least one baggage rack is closed, wherein said rack is 3b pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, wherein a distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the compartment, and wherein the pivoting strip is pivotably mounted around a longitudinal axis substantially parallel to the axis of pivoting of the at least one baggage rack.
This invention also relates to an aircraft, characterized in that it comprises a cabin such as described above.
4 Details and advantages of this invention will emerge more clearly from the description that follows, presented with reference to the attached schematic drawings on which:
Figure us a schematic view of a rack according to the invention in closed position, while Figure 2 shows this rack schematically in open position.
The luggage rack 2 depicted in the drawings is a rack mounted pivoting around an axis of pivoting 4. Here it is a luggage rack 2 mounted in an aircraft cabin. This rack is mounted in the upper portion of this cabin, above the passenger seats, not depicted. The axis of pivoting 4 is a longitudinal axis in relation to the aircraft cabin. The ceiling 6 of this cabin is recognizable on the drawings.
The luggage rack 2 comprises a lower outer face 8, a back 10, an upper face 12 and lateral walls 14. The overall shape of this rack is substantially parallelepipedal with a rounded lower face. The face opposite the back 10 is a completely open face.
On Figure 1, the luggage rack 2 is depicted in its closed position. It then is retracted in the ceiling 6 of the aircraft cabin. Inside this ceiling, a fixed flap 16 comes to close the open face of the luggage rack, opposite the back 10 of the luggage rack. This fixed flap 16 takes, for example, as depicted in the drawings, the form of a circular cylindrical section, the axis of which corresponds to the axis of pivoting 4.
For esthetic reasons, streamlining 18 is provided at the connection between the ceiling and the luggage rack. In closed position of the latter, the streamlining completely conceals the fixed flap 16 from the sight of the passengers occupying the aircraft cabin. This streamlining 18, in the closed position of the luggage rack, extends the lower outer face 8 of this luggage rack 2 toward the ceiling.
Beneath the luggage rack 2, the outer lower face 8 is extended by a lateral wall 20 of the aircraft cabin. Usually, at the junction between the luggage rack and the lateral wall 20 of the cabin there is an air vent through which air generally is sent into the cabin. In this embodiment according to the invention, this air vent comprises a movable flap 22 at its outlet.
Figure 2 depicts the luggage rack in its open position. In order to go from the closed position depicted on Figure 1 to the open position of Figure 2, the luggage rack 2 pivots downward around its axis of pivoting 4. In this position, the fixed flap 16 no longer covers the open face of the rack and this open face is completely clear. A passenger then can place a suitcase 24 inside the rack or remove it therefrom.
The lower outer face 8 of the luggage rack 2 has an area situated adjacent the back 10, referred to as rear portion 26, that is visible from the inside of the aircraft cabin when the luggage rack 2 is in its closed position (Figure 1) and that is concealed by the movable flap 22 and the lateral wall 20 of the cabin when the luggage rack 2 is in its open position.
The rear portion 26 of the lower outer face 8 has a cylindrical form. Such a surface is a surface that can be generated by the movement of a straight line, also referred to as generatrix, always retaining the same direction. Such a surface therefore is a succession of straight lines, referred to as generatrices, all parallel and arranged one next to the other. The rear portion 26 has the form of a cylindrical surface the generatrices of which are parallel to the axis of pivoting 4 and such that the distance from a generatrix to the axis of pivoting 4 increases from the back 10 of the luggage rack 2 toward the open front face of the latter.
When the luggage rack opens and closes, the movable flap 22 remains bearing against the lower outer face 8 of the luggage rack. This movable flap comprises a profiled strip 28 extending parallel to the axis of pivoting 4, as well as spacing shims 30 that make it possible to ensure a constant air outlet slit width is kept for the air vent, thus maintaining the same flow of air whether the luggage rack 2 is in open or closed (or intermediate) position.
The profiled strip 28 (and therefore also the movable flap 22) is mounted pivoting around a second axis of pivoting 32 parallel to the axis of pivoting 4 of the luggage rack 2. This second axis of pivoting 32 is borne by the lateral wall 20 of the aircraft cabin. It comprises prestressing means, not depicted, keeping the movable flap 22 always supported by way of spacing shims 30 on the rear portion = CA 02627696 2008-05-15 26 of the lower outer face 8 of the luggage rack 2. These prestressing means can comprise, for example, a spring associated with each bearing of the second axis of pivoting 32 so as to exert a return couple on the movable flap 22.
By way of example, there are considered on the one hand, a first generatrix 34 of the rear portion 26 corresponding to the generatrix on which the spacing shims 30 rest when the luggage rack 2 is in its open position, and on the other hand, a second generatrix 36 of the rear portion 26 corresponding to the generatrix on which the spacing shims 30 rest when the luggage rack is in its closed position. The first generatrix 34 is apart from the axis of pivoting 4 of the luggage rack 2 by a distance R1, while the second generatrix is apart from this axis of pivoting 4 by a distance R2. According to the invention, R2> R1. The value R2-R1 ranges, for example, between 5 and 20 cm, preferably between 10 and 15 cm.
With such a luggage rack, it is clearly evident that the volume of the luggage rack 2 is increased by maintaining the same depth, that is, the distance separating the back 10 from the open face of the luggage compartment.
In order to better take advantage of the increased inside volume of the luggage rack 2, a layout of the interior of the compartment accommodating a suitcase 24 is proposed.
A floor is arranged in the compartment intended to accommodate the luggage. This floor forms the lower inner face 38 of the luggage rack 2. This lower inner face 38 has a plane portion 40 adjacent the open face of the rack.
This plane portion 40 extends, for example, over 60 to 85% of the surface of the lower inner face 38. In the embodiment depicted in the drawings, it extends over approximately 70% of the depth of the luggage rack. Then, on approaching the back 10 of the luggage rack 2, the lower inner face 38 has a raised portion 42 directed toward the upper face 12. Thus, on the attached Figures corresponding substantially to a cross section, the lower inner face 38 of the luggage rack 2 has an angulate form.
The free end of the raised portion 42 has a groove 44. The latter therefore is in the immediate vicinity of the back 10. This groove 44 is of circular cylindrical form. Its concavity is directed toward the upper face 12 of the luggage rack 2. This groove 44 is of a size suitable for accommodating a wheel 46 of a suitcase 24. Thus the radius of curvature of the groove 44 is, for example, on the order of 3 to 10 cm.
At the present time, a very great majority of suitcases have wheels 46.
The placement of a suitcase 24 with wheels 46 then is performed in the following manner. The luggage rack 2 is set in its open position depicted on Figure 2.
The suitcase 24 then is positioned so that these wheels 46 are introduced first inside the luggage rack 2 and come to roll over the plane portion 40 of the lower inner face 38 of the luggage rack 2. On approaching the back 10 of the luggage rack, the raised portion 42 of the lower inner face 38 guides the wheels 46 toward the groove 44. The suitcase 24 then is in place in the luggage rack 2. For the comfort of the passenger, the raised portion 40 rises up gradually from the plane portion 40 to the groove 44, so that the suitcase 24 reaches the groove 44 smoothly and without jolts. This loading process is natural for the passenger who prefers to position the handle of his item of luggage (generally opposite the wheels thereof) on the accessible side of the rack.
Once in place in the respective compartment, the wheels 46 of the suitcase 24 are approximately 5 to 30 cm above the level of the plane portion of the lower inner face 38. The suitcase 24 then is held in this rack thanks to the cooperation of the wheels 46 and the groove 44.
The plane portion 40 of the lower inner face 38 of the luggage rack 2 preferably is substantially horizontal when the luggage rack 2 is in its open position. The aircraft here is considered to be down on the ground. In this case, the floor of the aircraft cabin is itself substantially horizontal. Thus, in relation to the aircraft cabin, it may be considered that the plane portion 40 of the lower inner face 38 of the luggage rack 2 is substantially parallel to the floor (and/or to the ceiling) of the aircraft cabin when the luggage rack is in open position.
In order to better hold the suitcase 24 inside the luggage rack 2, it also is provided to equip the free edge of the lower inner face 38 situated adjacent the open face of the luggage rack 2 with a profiled rail 48 forming a slight projection above the plane portion 40 of the lower inner face 38 of the luggage rack 2.
This profiled rail 48 thus forms a barrier for any object situated on the lower inner face 38 of the luggage rack 2. In order to avoid damaging the luggage or other objects in place in the luggage rack 2, and especially in order to avoid any injury to the passengers using the luggage rack 2, the profiled rail has a somewhat rounded form.
An embodiment of a luggage rack in which only one profiled rail would be used to hold a suitcase diagonally in the compartment without having a lower inner face having a plane portion and a raised portion is conceivable here. Of course, a rack according to the invention also possibly does not comprise a profiled retaining rail.
Such an embodiment of a luggage rack makes it possible to accommodate luggage of a larger size. In relation to a luggage rack of the state of the art, the fact of arranging in the luggage rack 2 a floor such as described above makes possible a saving of the order of 3" (or approximately 7 to 8 cm) in space occupied crosswise. It should be mentioned here that the luggage racks in an aircraft cabin, even in open position, must not hinder the movement of passengers passing along the aisles provided for this purpose. The luggage racks therefore must not project beyond the cabin seats, above the passage aisles.
Thanks to the space saving achieved, on the one hand through the special shape of the lower outer face of the rack and on the other hand through means making it possible to position a suitcase not down flat but diagonally in the storage compartment, it becomes possible to place a suitcase 24 of a size greater than that of a suitcase corresponding to the maximum size generally accepted by the airline companies in the aircraft cabin (usually referred to as "traveler pro") crosswise in the luggage rack 2, while in the racks of the prior art, storage for such suitcases had to be implemented longitudinally. The space saving is very appreciable. With a rack of the prior art, the space sufficing to accommodate four suitcases of traveler pro size, or even larger, in a rack according to the invention, can scarcely accommodate two suitcases of traveler pro size.
The volume 50 existing between the lower inner face 38 of the luggage rack 2 according to the invention and the suitcase 24 is not a wasted space¨quite =
the reverse. A passenger could take advantage of this volume to store therein, in complete safety, various small-sized objects and in particular a jacket or similar item. Since this volume 50 is well defined, the objects that are placed there also are held there.
This invention is not restricted to the preferred embodiment described above by way of non-limitative example. It also relates to all the variations within the capability of the individual skilled in the art, in the context of the claims below.
Figure us a schematic view of a rack according to the invention in closed position, while Figure 2 shows this rack schematically in open position.
The luggage rack 2 depicted in the drawings is a rack mounted pivoting around an axis of pivoting 4. Here it is a luggage rack 2 mounted in an aircraft cabin. This rack is mounted in the upper portion of this cabin, above the passenger seats, not depicted. The axis of pivoting 4 is a longitudinal axis in relation to the aircraft cabin. The ceiling 6 of this cabin is recognizable on the drawings.
The luggage rack 2 comprises a lower outer face 8, a back 10, an upper face 12 and lateral walls 14. The overall shape of this rack is substantially parallelepipedal with a rounded lower face. The face opposite the back 10 is a completely open face.
On Figure 1, the luggage rack 2 is depicted in its closed position. It then is retracted in the ceiling 6 of the aircraft cabin. Inside this ceiling, a fixed flap 16 comes to close the open face of the luggage rack, opposite the back 10 of the luggage rack. This fixed flap 16 takes, for example, as depicted in the drawings, the form of a circular cylindrical section, the axis of which corresponds to the axis of pivoting 4.
For esthetic reasons, streamlining 18 is provided at the connection between the ceiling and the luggage rack. In closed position of the latter, the streamlining completely conceals the fixed flap 16 from the sight of the passengers occupying the aircraft cabin. This streamlining 18, in the closed position of the luggage rack, extends the lower outer face 8 of this luggage rack 2 toward the ceiling.
Beneath the luggage rack 2, the outer lower face 8 is extended by a lateral wall 20 of the aircraft cabin. Usually, at the junction between the luggage rack and the lateral wall 20 of the cabin there is an air vent through which air generally is sent into the cabin. In this embodiment according to the invention, this air vent comprises a movable flap 22 at its outlet.
Figure 2 depicts the luggage rack in its open position. In order to go from the closed position depicted on Figure 1 to the open position of Figure 2, the luggage rack 2 pivots downward around its axis of pivoting 4. In this position, the fixed flap 16 no longer covers the open face of the rack and this open face is completely clear. A passenger then can place a suitcase 24 inside the rack or remove it therefrom.
The lower outer face 8 of the luggage rack 2 has an area situated adjacent the back 10, referred to as rear portion 26, that is visible from the inside of the aircraft cabin when the luggage rack 2 is in its closed position (Figure 1) and that is concealed by the movable flap 22 and the lateral wall 20 of the cabin when the luggage rack 2 is in its open position.
The rear portion 26 of the lower outer face 8 has a cylindrical form. Such a surface is a surface that can be generated by the movement of a straight line, also referred to as generatrix, always retaining the same direction. Such a surface therefore is a succession of straight lines, referred to as generatrices, all parallel and arranged one next to the other. The rear portion 26 has the form of a cylindrical surface the generatrices of which are parallel to the axis of pivoting 4 and such that the distance from a generatrix to the axis of pivoting 4 increases from the back 10 of the luggage rack 2 toward the open front face of the latter.
When the luggage rack opens and closes, the movable flap 22 remains bearing against the lower outer face 8 of the luggage rack. This movable flap comprises a profiled strip 28 extending parallel to the axis of pivoting 4, as well as spacing shims 30 that make it possible to ensure a constant air outlet slit width is kept for the air vent, thus maintaining the same flow of air whether the luggage rack 2 is in open or closed (or intermediate) position.
The profiled strip 28 (and therefore also the movable flap 22) is mounted pivoting around a second axis of pivoting 32 parallel to the axis of pivoting 4 of the luggage rack 2. This second axis of pivoting 32 is borne by the lateral wall 20 of the aircraft cabin. It comprises prestressing means, not depicted, keeping the movable flap 22 always supported by way of spacing shims 30 on the rear portion = CA 02627696 2008-05-15 26 of the lower outer face 8 of the luggage rack 2. These prestressing means can comprise, for example, a spring associated with each bearing of the second axis of pivoting 32 so as to exert a return couple on the movable flap 22.
By way of example, there are considered on the one hand, a first generatrix 34 of the rear portion 26 corresponding to the generatrix on which the spacing shims 30 rest when the luggage rack 2 is in its open position, and on the other hand, a second generatrix 36 of the rear portion 26 corresponding to the generatrix on which the spacing shims 30 rest when the luggage rack is in its closed position. The first generatrix 34 is apart from the axis of pivoting 4 of the luggage rack 2 by a distance R1, while the second generatrix is apart from this axis of pivoting 4 by a distance R2. According to the invention, R2> R1. The value R2-R1 ranges, for example, between 5 and 20 cm, preferably between 10 and 15 cm.
With such a luggage rack, it is clearly evident that the volume of the luggage rack 2 is increased by maintaining the same depth, that is, the distance separating the back 10 from the open face of the luggage compartment.
In order to better take advantage of the increased inside volume of the luggage rack 2, a layout of the interior of the compartment accommodating a suitcase 24 is proposed.
A floor is arranged in the compartment intended to accommodate the luggage. This floor forms the lower inner face 38 of the luggage rack 2. This lower inner face 38 has a plane portion 40 adjacent the open face of the rack.
This plane portion 40 extends, for example, over 60 to 85% of the surface of the lower inner face 38. In the embodiment depicted in the drawings, it extends over approximately 70% of the depth of the luggage rack. Then, on approaching the back 10 of the luggage rack 2, the lower inner face 38 has a raised portion 42 directed toward the upper face 12. Thus, on the attached Figures corresponding substantially to a cross section, the lower inner face 38 of the luggage rack 2 has an angulate form.
The free end of the raised portion 42 has a groove 44. The latter therefore is in the immediate vicinity of the back 10. This groove 44 is of circular cylindrical form. Its concavity is directed toward the upper face 12 of the luggage rack 2. This groove 44 is of a size suitable for accommodating a wheel 46 of a suitcase 24. Thus the radius of curvature of the groove 44 is, for example, on the order of 3 to 10 cm.
At the present time, a very great majority of suitcases have wheels 46.
The placement of a suitcase 24 with wheels 46 then is performed in the following manner. The luggage rack 2 is set in its open position depicted on Figure 2.
The suitcase 24 then is positioned so that these wheels 46 are introduced first inside the luggage rack 2 and come to roll over the plane portion 40 of the lower inner face 38 of the luggage rack 2. On approaching the back 10 of the luggage rack, the raised portion 42 of the lower inner face 38 guides the wheels 46 toward the groove 44. The suitcase 24 then is in place in the luggage rack 2. For the comfort of the passenger, the raised portion 40 rises up gradually from the plane portion 40 to the groove 44, so that the suitcase 24 reaches the groove 44 smoothly and without jolts. This loading process is natural for the passenger who prefers to position the handle of his item of luggage (generally opposite the wheels thereof) on the accessible side of the rack.
Once in place in the respective compartment, the wheels 46 of the suitcase 24 are approximately 5 to 30 cm above the level of the plane portion of the lower inner face 38. The suitcase 24 then is held in this rack thanks to the cooperation of the wheels 46 and the groove 44.
The plane portion 40 of the lower inner face 38 of the luggage rack 2 preferably is substantially horizontal when the luggage rack 2 is in its open position. The aircraft here is considered to be down on the ground. In this case, the floor of the aircraft cabin is itself substantially horizontal. Thus, in relation to the aircraft cabin, it may be considered that the plane portion 40 of the lower inner face 38 of the luggage rack 2 is substantially parallel to the floor (and/or to the ceiling) of the aircraft cabin when the luggage rack is in open position.
In order to better hold the suitcase 24 inside the luggage rack 2, it also is provided to equip the free edge of the lower inner face 38 situated adjacent the open face of the luggage rack 2 with a profiled rail 48 forming a slight projection above the plane portion 40 of the lower inner face 38 of the luggage rack 2.
This profiled rail 48 thus forms a barrier for any object situated on the lower inner face 38 of the luggage rack 2. In order to avoid damaging the luggage or other objects in place in the luggage rack 2, and especially in order to avoid any injury to the passengers using the luggage rack 2, the profiled rail has a somewhat rounded form.
An embodiment of a luggage rack in which only one profiled rail would be used to hold a suitcase diagonally in the compartment without having a lower inner face having a plane portion and a raised portion is conceivable here. Of course, a rack according to the invention also possibly does not comprise a profiled retaining rail.
Such an embodiment of a luggage rack makes it possible to accommodate luggage of a larger size. In relation to a luggage rack of the state of the art, the fact of arranging in the luggage rack 2 a floor such as described above makes possible a saving of the order of 3" (or approximately 7 to 8 cm) in space occupied crosswise. It should be mentioned here that the luggage racks in an aircraft cabin, even in open position, must not hinder the movement of passengers passing along the aisles provided for this purpose. The luggage racks therefore must not project beyond the cabin seats, above the passage aisles.
Thanks to the space saving achieved, on the one hand through the special shape of the lower outer face of the rack and on the other hand through means making it possible to position a suitcase not down flat but diagonally in the storage compartment, it becomes possible to place a suitcase 24 of a size greater than that of a suitcase corresponding to the maximum size generally accepted by the airline companies in the aircraft cabin (usually referred to as "traveler pro") crosswise in the luggage rack 2, while in the racks of the prior art, storage for such suitcases had to be implemented longitudinally. The space saving is very appreciable. With a rack of the prior art, the space sufficing to accommodate four suitcases of traveler pro size, or even larger, in a rack according to the invention, can scarcely accommodate two suitcases of traveler pro size.
The volume 50 existing between the lower inner face 38 of the luggage rack 2 according to the invention and the suitcase 24 is not a wasted space¨quite =
the reverse. A passenger could take advantage of this volume to store therein, in complete safety, various small-sized objects and in particular a jacket or similar item. Since this volume 50 is well defined, the objects that are placed there also are held there.
This invention is not restricted to the preferred embodiment described above by way of non-limitative example. It also relates to all the variations within the capability of the individual skilled in the art, in the context of the claims below.
Claims (4)
1. An aircraft cabin, comprising:
at least one baggage rack, each baggage rack including a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment; and a movable flap including a pivoting strip extending under a joining portion between the rear portion of the lower outer face and the back of the compartment when the at least one baggage rack is closed, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, wherein a distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the compartment, and wherein the pivoting strip is pivotably mounted around a longitudinal axis substantially parallel to the axis of pivoting of the at least one baggage rack.
at least one baggage rack, each baggage rack including a compartment having a lower outer face, an upper face, an open face arranged between the lower outer face and the upper face and allowing access to the compartment for depositing and removal of at least a baggage, and a back positioned opposite to the open face of the compartment; and a movable flap including a pivoting strip extending under a joining portion between the rear portion of the lower outer face and the back of the compartment when the at least one baggage rack is closed, wherein said rack is pivotably mounted around an axis of pivoting and pivots around said axis between an open position in which the open face of the compartment is accessible from the aircraft cabin and in which a rear portion of the lower outer face is concealed by a wall of the aircraft cabin, and a closed position in which the open face of the compartment is inaccessible from the aircraft cabin and in which the rear portion of the lower outer face is not concealed by the wall of the aircraft cabin, wherein said rear portion of the lower outer face has a cylindrical form comprising generatrices substantially parallel to the axis of pivoting of the rack, wherein a distance from the axis of pivoting to the generatrices increases from the back of the compartment toward the open face of the compartment, and wherein the pivoting strip is pivotably mounted around a longitudinal axis substantially parallel to the axis of pivoting of the at least one baggage rack.
2. The aircraft cabin according to claim 1, wherein the movable flap has spacing shims on a side of the at least one baggage rack.
3. The aircraft cabin according to claim 2, wherein the pivoting strip is pivotably mounted around a longitudinal axis substantially parallel to the axis of pivoting of the at least one baggage rack.
4. An aircraft comprising the cabin according to any one of claims 1, 2 or 3.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0511028A FR2892703B1 (en) | 2005-10-28 | 2005-10-28 | SWIVEL LUGGAGE BINK FOR AN AIRCRAFT CABIN |
| FR0511028 | 2005-10-28 | ||
| PCT/FR2006/002380 WO2007048916A1 (en) | 2005-10-28 | 2006-10-24 | Pivoting luggage bin for an aircraft cabin |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2627696A1 CA2627696A1 (en) | 2007-05-03 |
| CA2627696C true CA2627696C (en) | 2015-06-16 |
Family
ID=36888726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2627696A Active CA2627696C (en) | 2005-10-28 | 2006-10-24 | Pivoting luggage rack intended for an aircraft cabin |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP1948509B1 (en) |
| JP (1) | JP2009513432A (en) |
| CN (1) | CN101296845B (en) |
| BR (1) | BRPI0619301A2 (en) |
| CA (1) | CA2627696C (en) |
| FR (1) | FR2892703B1 (en) |
| RU (1) | RU2415783C2 (en) |
| WO (1) | WO2007048916A1 (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007030330B4 (en) * | 2007-06-29 | 2010-07-22 | Airbus Deutschland Gmbh | Swiveling implement carrier in combination with modified luggage rack |
| DE102008049639A1 (en) | 2008-09-30 | 2010-04-08 | Airbus Deutschland Gmbh | Load Path Optimized Swiveling Luggage Rack (Hatrack) |
| DE102008051240B3 (en) | 2008-10-10 | 2010-09-30 | Airbus Deutschland Gmbh | Device for receiving luggage in a passenger cabin of an aircraft |
| US10029794B2 (en) | 2012-02-14 | 2018-07-24 | C&D Zodiac, Inc. | Outboard rotating pivot bin assembly |
| JP6483799B2 (en) * | 2014-07-10 | 2019-03-13 | シーアンドディー ゾディアック，インコーポレイティド | Rotary shelf assembly |
| EP3339172B1 (en) | 2016-12-21 | 2022-12-07 | Airbus Defence and Space GmbH | Luggage storage system, aircraft and method for its operation |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4275942A (en) * | 1978-12-26 | 1981-06-30 | The Boeing Company | Stowage bin mechanism |
| DE3741164C1 (en) * | 1987-12-04 | 1989-07-20 | Airbus Gmbh | Luggage rack for vehicles, in particular airplanes |
| US5456529A (en) * | 1993-12-30 | 1995-10-10 | The Boeing Company | Powered overhead stowage bin |
| US5823472A (en) * | 1996-06-04 | 1998-10-20 | Fuselage Engineering Services Ltd. | Stowage compartment construction particularly for aircraft |
| US6527325B2 (en) * | 2001-01-30 | 2003-03-04 | Britax Health Tecna Inc. | Pull-down stowage bin restraint |
| AT413812B (en) * | 2001-10-17 | 2006-06-15 | Fischer Adv Components Gmbh | SUSPENSION DEVICE FOR SLEEVABLE BIN STORAGE TANKS |
| JP4046554B2 (en) * | 2002-06-12 | 2008-02-13 | 嘉信 香取 | Airplane baggage storage |
| US20050064174A1 (en) * | 2003-09-18 | 2005-03-24 | The Boeing Company | Reaction injection molded members and method of forming |
-
2005
- 2005-10-28 FR FR0511028A patent/FR2892703B1/en not_active Expired - Fee Related
-
2006
- 2006-10-24 BR BRPI0619301-3A patent/BRPI0619301A2/en not_active IP Right Cessation
- 2006-10-24 CN CN2006800396835A patent/CN101296845B/en active Active
- 2006-10-24 JP JP2008537136A patent/JP2009513432A/en active Pending
- 2006-10-24 RU RU2008121232/11A patent/RU2415783C2/en not_active IP Right Cessation
- 2006-10-24 EP EP06830996.2A patent/EP1948509B1/en active Active
- 2006-10-24 WO PCT/FR2006/002380 patent/WO2007048916A1/en active Application Filing
- 2006-10-24 CA CA2627696A patent/CA2627696C/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2008121232A (en) | 2009-12-10 |
| EP1948509B1 (en) | 2019-06-26 |
| WO2007048916A1 (en) | 2007-05-03 |
| CN101296845B (en) | 2010-08-18 |
| RU2415783C2 (en) | 2011-04-10 |
| EP1948509A1 (en) | 2008-07-30 |
| CA2627696A1 (en) | 2007-05-03 |
| JP2009513432A (en) | 2009-04-02 |
| CN101296845A (en) | 2008-10-29 |
| FR2892703B1 (en) | 2008-02-01 |
| FR2892703A1 (en) | 2007-05-04 |
| BRPI0619301A2 (en) | 2011-09-27 |
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| Date | Code | Title | Description |
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| EEER | Examination request |