EP2010430A1 - Ensemble de sieges de vehicule - Google Patents

Ensemble de sieges de vehicule

Info

Publication number
EP2010430A1
EP2010430A1 EP07732327A EP07732327A EP2010430A1 EP 2010430 A1 EP2010430 A1 EP 2010430A1 EP 07732327 A EP07732327 A EP 07732327A EP 07732327 A EP07732327 A EP 07732327A EP 2010430 A1 EP2010430 A1 EP 2010430A1
Authority
EP
European Patent Office
Prior art keywords
seat
backrest
assembly
pan
seat pan
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.)
Withdrawn
Application number
EP07732327A
Other languages
German (de)
English (en)
Inventor
Joe Ferry
Steve Blakeney Ridgway
Nathan David Sparshott
Tom Zackery Lloyd
Luke Neil Pearson
Paul Owens
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Virgin Atlantic Airways Ltd
Original Assignee
Virgin Atlantic Airways Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GB0606991A external-priority patent/GB0606991D0/en
Priority claimed from GB0619056A external-priority patent/GB0619056D0/en
Application filed by Virgin Atlantic Airways Ltd filed Critical Virgin Atlantic Airways Ltd
Publication of EP2010430A1 publication Critical patent/EP2010430A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/04—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable
    • B60N2/10—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable tiltable
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0696—Means for fastening seats to floors, e.g. to floor rails
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/04—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable
    • B60N2/12—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable slidable and tiltable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/20—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being tiltable, e.g. to permit easy access
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/22—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/22—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable
    • B60N2/2209—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable by longitudinal displacement of the cushion, e.g. back-rest hinged on the bottom to the cushion and linked on the top to the vehicle frame
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/22—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable
    • B60N2/2222—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable the back-rest having two or more parts
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/062—Belts or other passenger restraint means for passenger seats
    • B64D11/06205—Arrangements of airbags
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0627—Seats combined with storage means
    • B64D11/0636—Personal storage means or waste disposal bags
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
    • B64D11/064—Adjustable inclination or position of seats
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
    • B64D11/0644—Adjustable arm rests
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0646—Seats characterised by special features of stationary arms, foot or head rests
    • 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
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0647—Seats characterised by special upholstery or cushioning features
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Definitions

  • This invention relates to a vehicle seat assembly, and in particular to vehicle seats to be arranged in rows of such seats in a vehicle such as an aircraft, and a support structure therefor.
  • the distance between rows of seats in an aircraft, or the seat pitch, has an impact on how many passengers may be accommodated in the aircraft cabin, and is therefore of great importance to airlines. Rows of seats are placed as close together as possible taking into account passenger comfort. The seats are sometimes also required to have an upright position and a reclined position to allow the passenger to rest.
  • rows of the seats are commonly supported by transverse support struts under the seat pan at the front and rear thereof.
  • the seat legs are slidably mounted on the struts, with an upright leg portion under the rear of the seat pan which tends to interfere with the foot space of the passenger behind.
  • a vehicle seat assembly comprising a vehicle seat and support structure, which seats may be arranged in rows with an optimal seat pitch.
  • a support structure for supporting a plurality of seats side by side in a vehicle, the structure comprising at least a first elongate support strut for extending laterally of the seats, at least one seat leg assembly mounted to the strut, the leg assembly comprising: a foot portion arranged to be adjacent the floor of the vehicle for attaching the structure thereto; a seat support portion arranged to be adjacent the underside of the seat for attachment to the seat; and an intermediate portion extending between the seat support portion and the foot portion; wherein, in use, the support strut(s) and the intermediate portion of the or each leg assembly are arranged to be positioned under the front part only of each seat.
  • the foot portion is preferably elongate, extending in the fore-and-aft direction, so as to be attachable to a floor rail such as is commonly provided in aircraft.
  • the intermediate portion and support strut(s) may for example be arranged to be positioned under the front half of the seat pan.
  • the profile of the supporting legs of the seats can be very low (ie close to the floor) except at the front of the seat, so a passenger sitting behind may rest their feet under the seat with minimal interference from the support structure.
  • This is preferably achieved by providing two support struts both under the front part of the seat pan, one adjacent the foot portion of the leg assembly, and the other adjacent the seat support portion.
  • the lower strut may be positioned rearwardly of the upper strut, to allow heel room or stowage space for the passenger in the seat.
  • the leg assemblies may comprise first and second leg elements: the first element comprising the foot portion, and an upwardly extending portion mounted to the first and second support struts and forming part of the intermediate portion of the leg assembly; and the second element comprising the seat support portion, and a downwardly extending portion mounted to the first and second support struts and forming a further part of the intermediate portion of the leg assembly.
  • the second element may be in the form of a side plate or hanger bracket extending along the edge of each seat, and may be journalled to the seat pan and at least the lower part of the backrest.
  • the seat pan and backrest may be movably connected to the hanger bracket, for example by means of cooperating sliders and runners, for allowing reclining movement of the seat.
  • the seat may be fixed in position in relation to the support structure.
  • each seat is disposed between a pair of second leg elements. These elements are therefore separated by the width of a seat. Since the floor rails of aircraft are generally in fixed positions, the lateral positions of the first leg elements are determined by the rail positions. Therefore the first and second elements of the leg assemblies may be adjacent one another, or may be laterally spaced, depending on the seat width.
  • the invention also provides a seat assembly comprising such a support structure and at least one seat supported thereon, in which the seat comprises a seat pan and a backrest, and in which the rear of the seat pan and the rear of the backrest adjacent the seat pan have corresponding convex shapes when viewed from behind. This is made possible because there is no support strut at the rear of the seat pan, as was required by prior art structures. For example, the side edges of the base of the backrest and the sides of the rear edge of the seat pan may be curved in the direction towards the front of the seat. This allows more knee-room for the passenger behind at the sides of the seat back.
  • the invention also provides a seat assembly comprising a support structure and a plurality of seats supported side by side thereon, the seats each comprising a seat pan and a backrest, the support structure comprising an elongate laterally extending support strut and at least one leg assembly mounted to the strut, in which the rear edge of the seat pan and the lower edge of the backrest are curved forwardly at the sides thereof, and in which the support strut is disposed forwardly of at least a part of the rear edge of the seat pan, such that a recess is formed at the sides of each seat to accommodate the knees of a passenger sitting behind.
  • the support strut is positioned forwardly of the majority of or the whole of the rear edge of the seat pan in a position corresponding to the upright position of the seat.
  • the support strut may be just forward of the end of the curve of the rear edge, where the side edge of adjacent seat pans meets. This position is preferably around at least 5 inches, and most preferably around 7 inches forward of the rearmost part of the backrest. There may be a further support strut further towards the front of the seat pan.
  • the invention provides a seat assembly for arranging in rows of such seat assemblies in a vehicle, the seat assembly comprising a seat pan, a backrest, and a supporting structure for supporting the seat pan and backrest on the floor of the vehicle, the backrest being tiltable in relation to the supporting structure between a first upright position and a second reclined position about a pivot location on the supporting structure which is positioned above the base of the backrest.
  • the pivot location is at a height at least approximately equal to the knee height of a passenger in the seat.
  • the problem of encroaching on the passenger's leg room is alleviated, since the part of the backrest at the height of the legs moves forwardly, further away from the passenger behind.
  • the high pivot minimises the intrusion of the backrest into the aft passenger space, in particular the passenger's head space.
  • a storage pocket for use by the passenger may also be included on the front of the leg assembly; that is, behind the passengers legs. This further reduces interference with passengers knee-room by the backrest of the seat in front.
  • the seat includes means for locking the seat pan and backrest in selected relative positions, and comprising a manual actuating member for the locking means which is positioned beneath the front of the seat pan.
  • a manual actuating member for the locking means which is positioned beneath the front of the seat pan.
  • this may be a lever which the passenger activates by lifting it towards the seat to release the seat for movement.
  • This arrangement avoids the need to provide a recline actuator in the armrest, as is conventional for aircraft seats.
  • the armrest may therefore be of a simpler and less bulky construction.
  • This invention also provides a seat assembly comprising a plurality of seats arranged side by side, the seats each having a backrest and an armrest pivotable between a substantially upright stowed position and a substantially horizontal use position, the pivot location being positioned forwardly of the backrest, or the backrest pivot.
  • the armrest may be mounted on a flange extending forwardly from between the backrests. With this arrangement, the armrest can be stowed to lie substantially flat against the backrest or adjacent backrests. Since the armrest and backrest are arranged such that the armrest abuts the backrest in the stowed position thereof, the armrest may not extend behind the backrest. This eliminates the need for retaining tabs which are commonly provided on the sides of conventional backrests. Furthermore, it is easier to disassemble the armrest, for example for maintenance, since the pivot is accessible without dismantling the seat.
  • the armrest is shorter than conventional armrests; for example one third to one-half of the usual length.
  • the armrest is less intrusive in the passenger space, and alleviates the problem of restricted leg movement for larger passengers which can occur with conventional armrests.
  • the invention also comprises a seat assembly comprising a seat pan and backrest, the seat being movable between upright and reclined positions of the seat, by tilting movement of the seat pan and the backrest, in which the tilting movement of seat pan causes the front of the seat pan to move relatively upwardly, and the tilting movement of the backrest causes the top of the backrest to move relatively backwardly, and in which the angle of tilting travel of the backrest is equal to approximately 3.2 times the angle of tilting travel of the seat pan.
  • a flange may be provided on the rear edge thereof which extends upwardly for covering any gap between the seat pan and the backrest.
  • the backrest may comprise a shaped rigid frame member and a shaped cushion member, the cushion member being applied to the front side only of the rigid frame member.
  • the frame member may be profiled to form the required backrest shape, and the cushion may have a simple thin profile.
  • the shape of this rigid frame member is thus preferably an 'S' curve, corresponding to the natural curve of the spine.
  • This arrangement provides a seat of a less bulky construction.
  • the seat pan may include a moveable element, movement of which causes adjustment of the thickness of the seat pan at a front portion thereof relative to the thickness of the seat pan at a rear portion thereof.
  • the passenger may effectively adjust the height of the lumbar support of the seat, for enhanced comfort.
  • the passenger may also adjust the relative height at which the lower part of the thigh, or knee, is supported such that the legs may adopt an optimal position. For example a larger passenger may lower the knee height to place their legs comfortably. Conveniently, this may be done by the seat pan cushion including an airbag at the rear, and optionally also one at the front, which may be inflated or deflated by the passenger.
  • resilient member such as a spring biased pivotal plate in the front of the seat, which biases it upwardly and pivots downwardly under the weight of a passenger's legs.
  • Figure 1 is a perspective view from in front of a seat assembly comprising a pair of seats according to one embodiment of the present invention
  • Figure 2 is a perspective view from behind of the seat assembly shown in Figure 1;
  • Figure 3 is a rear view from below of the support structure of the seat assembly;
  • Figure 4 is a side view of the seat assembly of Figure 1 showing upright and reclined positions of the seat;
  • Figure 5 is a partial side view of two rows of such seat assemblies with a person sitting in the rear row;
  • Figure 6 is a partial side view of the seat assembly showing the arm rest in different positions
  • Figure 7 is a partial cross-sectional side view of the seat assembly showing airbags in the seat pan.
  • Figures 8a to 8c are a series of side views of a first element of a leg assembly according to various embodiments of the invention.
  • Figure 9 is a side view of the second element of the leg assembly of the seat of Figure 1;
  • Figure 10 is a perspective view from behind of a seat assembly according to another embodiment of the invention.
  • Figure 11 is a further rear view from below of a support structure according to the invention.
  • Figure 12 is a perspective view from in front of a seat assembly comprising a row of seats according to another embodiment of the invention.
  • Figure 13 is a schematic side view showing an example of the dimensions of the seat assemblies with the support structure of Figures 1 to 9 and Figure 12 overlaid;
  • Figure 14 is a perspective view from behind of the seat assembly of Figure 12;
  • FIG 15 is a schematic plan view of the seat pan of a seat according to the invention also showing a seat pan in the row behind.
  • the seat assembly comprises a pair of seats each including a seat pan 2 and a back rest 4, and a supporting structure 6 for supporting the seats on the vehicle floor. Aircraft seats are commonly mounted on rails extending fore and aft of the aircraft cabin floor (not shown).
  • the support structure 6 includes a pair of leg assemblies 8.
  • the leg assemblies 8 are substantially 'L' shaped, each including a first element 9 with a foot portion 10 having an elongate shape for attachment to the floor rail of an aircraft in a known manner. The elongate and substantially flat shape of the foot portion 10 reduces intrusion into the passenger foot space.
  • the foot portion 10 has a depth of about 60 mm.
  • the depth is about 90 mm, allowing a weight reduction as compared with the profile of Figure 8a of about 0.28 kg. If the depth is about 150 mm, as shown in Figure 8c, the weight of the first portion may be reduced by about 0.52 kg compared to that of Figure 8a.
  • a preferred profile has a depth of about 100 mm.
  • an upwardly extending portion 11 of the first element 9 extends from the front end thereof to form part of an upright intermediate portion of the leg assembly, which is positioned under the front part of the seat pan 2.
  • a downwardly extending part 14 of a second element 12 forms a further part of the upright intermediate portion of the leg assembly.
  • the second element 12 is in the form of a side plate or hanger bracket.
  • the bracket 12 is generally of an elongate 'S' shape, having a middle part 15 extending along the side edge of the seat pan and an upper part 17 extending along the side edge of the lower part of the backrest, with a corner 19 therebetween.
  • the middle and upper parts 15, 17 form a seat support portion of the bracket 12.
  • the bracket 12 is journalled to the seat pan and backrest to allow reclining movement of the seat, as will be described below.
  • the leg assemblies 8 are mounted to upper and lower laterally extending support struts 16, 18.
  • the upper strut 18 extends through upper mounting apertures 20 of each leg element 9, 12, respectively and the lower strut 16 extends through lower mounting apertures 22 thereof.
  • the lower mounting aperture 22 of the first element 9 is adjacent the foot portion 10, and in the second element 12 it is adjacent the distal end of the downwardly extending part 14.
  • the upper mounting apertures 20 are adjacent the seat support portion of the hanger bracket 12 at the underside of the seat pan, and adjacent the top end of the upwardly extending portion 11 of the first element 9. With this arrangement, the lower support strut 16 may be positioned a little rearwardly of the upper strut 18. This has the advantage of allowing more heel room to the passenger in the seat.
  • a storage pocket 50 may be mounted to the front of the leg assemblies (see Figure 4). This has the advantage of negating the need for a pocket on the seat back in front of the passenger, as is commonly provided in aircraft, which interferes with knee room.
  • the aperture 22 for the lower strut 16 is positioned about 205 mm below the aperture 20 for the upper strut 18, and the forward-most part of the lower aperture 22 is about 19.5 mm behind the forward- most part of the upper aperture 20.
  • the rear edge may be convex in shape, and the lower edge of the backrest may have a corresponding convex shape.
  • a recess 3 is formed at each side of the rear of each seat for accommodating the aft passenger knees.
  • the brackets 12 extend along the edges of the seats both between the seats and at each end of the rows. At the end of each row the bracket 12 may be covered by a protective panel 30 having a peripheral bump strip 3. Also, a baggage bar 52 may extend from the corner 19 of the bracket 12 between the seat pan and backrest to the end of the downwardly extending portion 14, to retain any passenger baggage. An alternative position for the baggage bar would be for the upright portion to be inclined towards the corner of the bracket adjacent the upper support strut 18, as shown in Figure 10.
  • the seat assembly thus far described is suitable either as a fixed seat or as a reclinable seat.
  • a recline mechanism is shown.
  • the upper end of each bracket 12 terminates adjacent a pivot location 32.
  • the backrest 4 of each seat is mounted between two brackets 12 so as to be reclinable about the pivot location 32.
  • This location is positioned above the vehicle floor at a height intended substantially to coincide with or be just above the height of the knee 33 of a passenger 34 sitting in the seat with their feet resting on the floor (see also Figure 4).
  • the 95 centile middle of knee height of the adult population is about 542 mm, and thus the pivot height may be about 561 mm, but may be somewhat lower or higher.
  • the backrest pivots about a fixed point 32, but it may alternatively tilt about a pivot path in a similar manner to the seat pan, as described below.
  • the pivot location as defined above corresponds to the position where the backrest substantially moves neither forwardly nor rearwardly.
  • the pivot location may be positioned forwardly of the location on a seat with a conventional flat backrest.
  • the seat may be reclined by actuation of a lever 36 mounted underneath the front part of the seat pan 2.
  • the seat pan 2 is mounted to the brackets 12 such that, upon reclining movement of the backrest 4, the seat pan 2 translates forwardly and tilts such that the front edge 38 moves upwardly slightly whilst the rear edge 40 moves downwardly.
  • This may be achieved by a slider and runner arrangement, for example by machining the guide path 41 or runner for a slider (not shown) mounted to the edge of the seat pan 2, into the brackets 12, as shown in Figure 3.
  • the angle of tilt ⁇ of the backrest is approximately 3.2 times the angle of tilt ⁇ of the seat pan. This provides a comfortable 'cradled' position for the passenger.
  • the seat pan 2 is additionally supported towards the front by a support ring 45 mounted on the upper strut 18 and bolted to the underside of the seat pan 2.
  • a support ring 45 mounted on the upper strut 18 and bolted to the underside of the seat pan 2.
  • An example of an alternative mechanism is shown in Figure 11.
  • a cable connected to release member 71 of a gas strut 72 unlocks the mechanism. If the passenger in the seat applies backward force to the backrest, the backrest tilts and the rear edge of the seat pan 2 is pushed forwardly by the lower end of the backrest moving forwards.
  • the seat pan 2 movement is guided by a guide path 41 in the brackets 12 as already described in relation to Figure 3.
  • a further guide member or cam 78 towards the front of the seat pan 2 helps to guide the front of the seat pan 2 upwardly throughout the recline movement.
  • the cam 78 is fixed to a bracket 80 on the lower side of the seat pan 2.
  • the cam 78 is caused to rotate on a fixed bar 82, pushing the bracket 80 upwardly.
  • the lever 36 is released, the mechanism is locked in position.
  • the seat pan 2 is connected to a pair of levers 74, 75, which in turn are connected to the gas strut 72.
  • a spring 76 on the gas strut 72 urges the seat pan 2 back to the non-reclined position via the cam 74 when the actuator 36 once again is activated.
  • each seat is a table arm 46 extending backwardly such that each pair of arms 46 carries therebetween a table 48 at the other end thereof behind the seat (see Figure 2).
  • the aft passenger may grip the table and pull it down into a substantially horizontal position for use.
  • There may also be a screen 49 and a handset 51 having a coiled cord 53 provided on the upper part of the rear of each backrest for the use of the passenger sitting behind.
  • a thin literature pocket for example formed of a flat sheet of material, may also be provided on the lower part 47 the rear of the backrest, for example to contain a safety card. This may for example be a piece of netting attached to the backrest at the sides and base.
  • a further storage pocket 50 for passenger use may be mounted to the front of the leg assemblies.
  • a life vest is also stored under the seat.
  • each bracket 12 includes forwardly angled flange 42 mounting an armrest 44.
  • the armrest is pivotally mounted on the flange 42 for movement between a substantially horizontal position for use, and a stowed position substantially parallel to the adjacent backrest, whether the backrest is in the upright or the reclined position.
  • the armrest pivot point 43 (see Figure 9) is positioned forwardly of the backrest 4. This allows the armrest to be fully stowed, lying against the backrest, to allow passengers to move in and out of the seats. Since the armrest is not required to carry operating members such as a recline button, it may be of a simple construction and therefore less bulky. It may also be mounted by a simple pivot which is separate from the rest of the seat assembly and may easily be accessed. This armrest arrangement is suitable for a reclinable or non-reclinable seat.
  • the armrest Since the armrest lies against the backrest, it is prevented from extending behind it, and thus with reclinable seats, when the backrest moves from a relined to an upright position with the armrest stowed (ie parallel to the backrest), it will also push the armrest into an upright position. Thus there is no need for a tab extending from the backrest to abut with the armrest and prevent it extending behind the seat back, as is common in prior seat assemblies.
  • the seat back 4 and seat pan 2 each comprise rigid frame members 58 and 56 (not shown) respectively onto which corresponding shaped cushions 60, 62 and 64 are attached to form seat, back and head rest cushions respectively on the passenger bearing surfaces.
  • the cushions may be attached with hook and loop or other such fasteners.
  • the backrest member is a rigid member which is shaped to provide the required ergonomic seat back profile. It therefore forms an 'S' curve corresponding to the natural curvature of the spine. Furthermore, the backrest member itself may be thin; for example not substantially exceeding about 30mm in thickness. Furthermore it is visually aesthetic, so that no cladding is required. Therefore the back and head rest cushions 62, 64 may be provided to the front side only of the backrest frame member, and can be of a simple thin profile, being less bulky than conventional seat cushion cover members. For example, the cushions may not substantially exceed 30mm or even 20mm in thickness. Other attachment means for the cushioning may be used, such as a thin fabric skirt wrapping around the seat back 4. Alternatively a thin cushioning layer may continue over the back surface of the backrest member 58.
  • the seat cushion 60 may include a pair of airbags 66, 68 mounted within the cushion at the front part and further to the rear respectively.
  • the passenger may be provided with an actuator of a known type (not shown) for inflating or deflating each airbag.
  • they may be direct access airbags, which inflate upon actuation when passenger weight is removed, and may deflate upon actuation when weight is applied.
  • a spring plate member may be provided in the front part of the seat to bias it upwardly, and be movable downwardly when pushed by the weight of the passenger's legs.
  • the passenger may thus adjust the height of the rear of the seat relative to the backrest, such that the position of the lumber support area of the backrest can be adjusted to suit the passenger.
  • the angle of tilt of the seat part may also be adjusted using the airbags 66, 68. Therefore a smaller passenger may lower the seat pan height and remove pressure under the thighs by deflating the airbags, and a taller passenger may more easily straighten the legs by creating an angled seat pan which is still supportive. This feature also facilitates reclining the seat pitch, since optimal leg position may be achieved by both short and tall passengers.
  • a footrest 70 is mounted adjacent the lower strut 10 for pivotable movement between a stowed position under the seat pan 2, and a use position as shown.
  • the structure comprises two support struts 84, 86 positioned one at the front and the other further rearwardly of the underside of the seat pan 2.
  • the seat leg assembly comprises an elongate foot portion 88 for attaching to the aircraft floor rails.
  • the seat pan 2 and backrest 4 are similar to those shown in Figures 1 to 9, and a seat support portion or bracket 90 supports the seat in a similar manner whilst being somewhat modified in shape.
  • the intermediate leg portion comprises a forward upright member 92, extending from the front strut 84 to the front of the foot 88, and a rear member 94 extending from the rear strut 86 to the rear of the foot 88.
  • the rear member 94 is curved inwardly towards the front strut 84 to reduce interference with passenger foot space.
  • An arm 96 connects the front and rear leg portions together.
  • the headrest cushions 98 in this example also each include an auxiliary cushion 99 for added comfort.
  • the rear strut 86 is positioned adjacent and forwardly of the majority of the rear edge of the seat pan, so as still to provide a recess 95 at the sides of each seat for the aft passenger knees.
  • the rear strut 86 may be positioned forwardly of the whole of the rear edge of the seat pan.
  • Figure 13 the relative positions of various parts of the seat are shown by way of example, all of which are taken from the front foot attachment point 100.
  • the drawing shows a first support structure 112 correspond to that of Figure 1, and overlays a second support structure 114 corresponding to that of Figure 12.
  • the lumber region 102 of the backrest 2 is forward of the upper back region 104 (the two "bends' of the 1 S' curve) by a distance 108 which may be about 5 inches in the upright position.
  • the height 110 of the backrest pivot from the floor is about 22.44 inches.
  • the rear strut 86 of the second support structure 114 is sufficiently forward, by a distance 116, of the rear edge 106 of the seat pan 2 not to interfere significantly with the curved edges.
  • this distance is about 6.77 inches.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Seats For Vehicles (AREA)
  • Chairs For Special Purposes, Such As Reclining Chairs (AREA)

Abstract

La présente invention concerne un ensemble de siège de véhicule destinés à être disposés en rangées, tel que dans un aéronef, présentant une structure compacte pour permettre un pas minimal. Les pieds de sièges (8) présente une forme compacte avec des entretoises de support (16) orientées vers l'avant du siège, les sièges sont convexes ou en forme de 'baquet', la manette d'actionnement d'inclinaison et la poche de rangement sont disposées sous la partie avant du siège, les pivots de dossier (4) à hauteur des genoux pour le mouvement d'inclinaison, et le dossier est ergonomique, comprenant des coussins (62) fixés uniquement côté passager.
EP07732327A 2006-04-06 2007-04-05 Ensemble de sieges de vehicule Withdrawn EP2010430A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0606991A GB0606991D0 (en) 2006-04-06 2006-04-06 Vehicle seat assembly
GB0619056A GB0619056D0 (en) 2006-09-27 2006-09-27 Vehicle seat assembly
PCT/GB2007/001283 WO2007128978A1 (fr) 2006-04-06 2007-04-05 Ensemble de sièges de véhicule

Publications (1)

Publication Number Publication Date
EP2010430A1 true EP2010430A1 (fr) 2009-01-07

Family

ID=38091031

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07732327A Withdrawn EP2010430A1 (fr) 2006-04-06 2007-04-05 Ensemble de sieges de vehicule

Country Status (7)

Country Link
EP (1) EP2010430A1 (fr)
JP (1) JP2009532158A (fr)
AU (1) AU2007246912A1 (fr)
CA (1) CA2652584A1 (fr)
GB (1) GB2437164A (fr)
WO (1) WO2007128978A1 (fr)
ZA (1) ZA200809438B (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SG173164A1 (en) 2009-01-30 2011-08-29 Air New Zealand Ltd Seating arrangement, seat unit, tray table and seating system
GB2469180B8 (en) 2009-03-23 2016-06-08 Air New Zealand Ltd Vehicle seating arrangement
USD665182S1 (en) 2010-01-14 2012-08-14 Air New Zealand Limited Aircraft seat unit
WO2012078499A2 (fr) * 2010-12-07 2012-06-14 Weber Aircraft Llc Ensemble d'affichage
JP5956134B2 (ja) * 2011-10-21 2016-07-27 株式会社岡村製作所 椅子の肘掛け装置
DE102013005859A1 (de) 2013-04-08 2014-10-09 Zim Flugsitz Gmbh "Fluggastsitz mit einem Gestell"
JP6185172B2 (ja) * 2013-11-12 2017-08-23 ビーイー・エアロスペース・インコーポレーテッドＢ／Ｅ Ａｅｒｏｓｐａｃｅ， Ｉｎｃ． 地上走行、離陸および着陸時にフルフラット位置にできる航空機座席
DE102014101441A1 (de) * 2014-02-05 2015-08-06 Airbus Operations Gmbh Passagiersitz für ein Luftfahrzeug
EP3154818A2 (fr) 2014-06-10 2017-04-19 Zodiac Seats US LLC Sièges passagers de conception ergonomique monocoques et semi-monocoques
DE102014119596A1 (de) * 2014-12-23 2016-06-23 Recaro Aircraft Seating Gmbh & Co. Kg Sitzvorrichtung mit Abstützelement
DE102014119611A1 (de) * 2014-12-23 2016-06-23 Recaro Aircraft Seating Gmbh & Co. Kg Sitzvorrichtung
EP3362358B1 (fr) 2015-10-14 2021-04-28 Safran Seats USA LLC Siège passager comprenant un dossier net
DE102015122830A1 (de) * 2015-12-23 2017-06-29 Recaro Aircraft Seating Gmbh & Co. Kg Flugzeugsitzvorrichtung
EP3600970B1 (fr) 2017-03-24 2022-07-13 Safran Passenger Innovations, LLC Unité d'affichage interne pivotante à écran fixe
US10858108B2 (en) 2017-09-13 2020-12-08 Safran Seats Usa Llc Aisle access side facing seat
DE102018111209A1 (de) * 2018-05-09 2019-11-14 Recaro Aircraft Seating Gmbh & Co. Kg Flugzeugsitzvorrichtung
EP3647195A1 (fr) * 2018-10-31 2020-05-06 Safran Seats USA LLC Siège tourné vers l'accès à l'allée
US11845557B2 (en) * 2022-03-29 2023-12-19 B/E Aerospace, Inc. Springless dress cover and lower closeout system for passenger seat

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2629425A (en) * 1946-06-18 1953-02-24 Boeing Co Berthable chair
FR2318759A1 (fr) * 1975-07-22 1977-02-18 Air France Siege articule destine aux vehicules de transport et plus particulierement aux aeronefs
BR7701091A (pt) * 1976-02-23 1977-10-18 Paulisch Kg Assentos para veiculos,em particular para onibus
FR2442742A1 (fr) * 1978-11-13 1980-06-27 Chardon Max Siege notamment pour vehicules de transports en commun
US5133587A (en) * 1989-11-20 1992-07-28 Hadden Jr James R Seat
US5636898A (en) * 1994-04-15 1997-06-10 Burns Aerospace Corporation Seat with recline linkage
GB2292676B (en) * 1994-09-02 1998-01-21 Flight Equip & Eng Reclinable seat for passenger-carrying vehicles
DE4432874B4 (de) * 1994-09-15 2006-07-06 Grammer Ag Sitz für Eisenbahnwagen oder Straßenbahnwagen
ES2121516B1 (es) * 1995-06-12 1999-05-16 Asientos Esteban S L Asiento para vehiculos, perfeccionado.
GB2390806A (en) * 2000-05-06 2004-01-21 Seymour Powell Ltd Aeroplane seat with inflatable section
US6672661B2 (en) * 2001-11-21 2004-01-06 B E Aerospace, Inc. Passenger seat, passenger seat leg module and method
US6899397B2 (en) * 2002-11-27 2005-05-31 Be Aerospace, Inc. Aircraft passenger seat with forward arm rest pivot
US6802568B1 (en) * 2003-04-28 2004-10-12 Be Aerospace, Inc. Segmented beam aircraft passenger seat
US7066551B2 (en) * 2003-04-28 2006-06-27 Be Aerospace, Inc. Curved beam aircraft passenger seat
US20050127740A1 (en) * 2003-12-15 2005-06-16 Be Aerospace, Inc. Vehicle seating with integral passenger seat restraints
US20060006704A1 (en) * 2003-12-15 2006-01-12 Be Aerospace, Inc. Vehicle seating with storage feature
DE102005009419A1 (de) * 2005-03-02 2006-09-07 Recaro Aircraft Seating Gmbh & Co. Kg Sitz

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2007128978A1 *

Also Published As

Publication number Publication date
GB0706812D0 (en) 2007-05-16
WO2007128978A1 (fr) 2007-11-15
CA2652584A1 (fr) 2007-11-15
AU2007246912A1 (en) 2007-11-15
GB2437164A (en) 2007-10-17
ZA200809438B (en) 2012-02-29
JP2009532158A (ja) 2009-09-10

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