Passenger seat

Abstract: A vehicle seat, such as an aircraft passenger seat, has a seat back (16) which is reclinable from a normal substantially vertical orientation, and a seat pan (28) which is tiltable between a normal substantially horizontal orientation and a tilted orientation in which its front edge is lower than its rear edge. The seat pan (28) has a rear portion (30) adjacent to the seat back (16) which is substantially horizontal when the main portion (32) of the seat pan is in its tilted orientation.

Description: This invention relates to a vehicle seat of the type having a seat back which is reclinable from a normal substantially vertical orientation, and a seat pan which is tiltable between a normal substantially horizontal orientation and a tilted orientation in which its front edge is lower than its rear edge. A seat of this type is disclosed in US-A-5058954. Because of the restricted pitch between successive rows of aircraft seats, it is not feasible to lower the seat back sufficiently for the aforesaid substantially continuous surface to be horizontal. When sleeping on a surface which slopes from head to foot there is a risk of a seat occupant tending to slip or wiggle down the slope while asleep. It is an object of the invention to provide a vehicle seat in which this disadvantage is reduced. According to the invention, the seat pan of a vehicle seat of the type described above has a rear portion adjacent to the seat back which is substantially horizontal when the main portion of the seat pan is in its tilted orientation. In one form of the invention, the orientation of the rear portion of the seat pan is permanently fixed in its substantially horizontal orientation and the main portion is pivotable relative to the rear portion. In another form of the invention, the rear portion of the seat pan is permanently fixed to the main portion and is stowed under the backrest when the main portion is horizontal. Embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings, in which: Figure 1 is perspective view of a sleeper seat, in accordance with a known aircraft passenger seat, in its upright orientation; Figure 2 is a perspective view of the sleeper seat shown in Figure 1 with its leg rest raised, its seat back inclined and its pan tilted; Figure 3 is a schematic longitudinal cross-sectional view of the seat shown in Figure 2; Figure 4 is a perspective view, similar to Figure 2, of an aircraft passenger seat in accordance a first embodiment of with the invention; Figure 5 is a schematic longitudinal cross-sectional view of the seat shown in Figure 4; Figure 6 is a schematic perspective view of an aircraft passenger seat in accordance a second embodiment of the invention, in its upright orientation; Figure 7 is a side view of the seat pan and the seat back of the seat shown in Figure 6; Figure 8 is a perspective view of the sleeper seat shown in Figure 6, with its leg rest raised, its seat back inclined and its pan tilted; Figure 9 is a side view of the seat pan and the seat back of the seat shown in Figure 8; Figure 10 is a schematic perspective view of the seat pan and the seat back of an aircraft passenger seat in accordance a third embodiment of the invention, with its leg rest raised, its seat back inclined and its seat pan tilted; and Figure 11 is a schematic perspective view, similar to Figure 10, of an aircraft passenger seat in accordance a fourth embodiment of the invention, with its leg rest raised, its seat back inclined and its seat pan tilted. Figure 1 shows a known aircraft seat. The seat comprises a base frame 10, whereby it may be secured in place in an aircraft. Armrests 12 and 14 are rigidly secured to the frame 10. A seat back 16 is pivotally secured to the frame 10 for angular movement about a horizontal transverse axis near its bottom edge between an upright orientation as shown in Figure 1 and a reclined orientation as shown in Figures 2 and 3. A seat pan 18 is also mounted on the frame 10 and has, secured to its front edge, a leg rest 20 which is movable between a stowed position, as shown in Figure 1, and a deployed position, as shown in Figures 2 and 3. The seat pan 18 is pivotally mounted for angular movement about a transverse axis near its rear edge between a generally horizontal orientation, as shown in Figure 1, and an inclined orientation, as shown in Figures 2 and 3. When the seat is in the reclined condition shown in Figures 2 and 3, there is a risk that the buttocks of a seat occupant 22 will slide down the inclined seat pan 18. To prevent this, it has been proposed to provide an upwardly projecting foot stop 24 on the outer end of the leg rest 20. This arrangement has two disadvantages. Firstly, unless the length of the leg rest 20 is adjustable, a seat occupant whose leg length differs from that of the occupant 22 shown in Figure 3 will not be able to position his torso correctly in relation to the seat back 16 when his feet are resting on the foot stop 24. Secondly, even for an occupant of the correct leg length, such as the occupant 22, there will be pressure on his feet and tension in his leg muscles while he is asleep. Figures 4 and 5 illustrate a seat in accordance with a first embodiment of the invention which is similar to the seat shown in Figures 1 to 3 in that it has a base frame 10, armrests 12 and 14, and a seat back 16. The mechanism for reclining the seat back 16 is conventional and is not described herein. The seat pan 28 is formed in two portions, namely a rear portion 30 which remains stationary in relation to base frame 10 and a main portion 32 which can pivot to an inclined position in which its front edge is lower than its rear edge. The two seat pan portions 30 and 32 are covered by a single bendable cushion 34. The leg rest 20 of Figures 1 to 3 is replaced by a leg rest 36 which does not have a foot stop similar to the foot stop 24. The length (in the longitudinal direction of the seat) of the rear portion 30 of the seat pan is preferably about half the length of the main portion 32. With this configuration, the buttocks of the occupant 20 can rest comfortably on the horizontal rear portion 30 when the seat is its reclined position as shown in Figures 4 and 5. Figures 6 to 9 illustrate an alternative aircraft passenger seat having a seat back 40 which is movable between an upright orientation as shown in Figures 6 and 7 and a reclined orientation as shown in Figure 9, in a similar manner to the seat back 16 of Figures 1 to 5. In Figures 6 to 9, the seat has a seat pan 42 comprising a main portion 44, together with a rear portion 46 which slopes downwardly and rearwardly relative to the main portion 44 and projects at least partially below the bottom of the seat back 40 when the seat is in its upright configuration, as shown in Figures 6 and 7. The seat pan 42 is supported at each side on laterally projecting front and rear guide pins 47 and 48 which engage in L-shaped guide slots 50 and 52 in each of the armrests 54 and 56. The outer cover of the arm rest 52 is omitted from Figures 7 and 9 so as to show the slot 50. When the seat is to be put into its reclined configuration, the seat back 40 is reclined as described above. The seat pan 42 slides forwardly to bring its front guide pins 47 into downwardly extending front end sections 58 and 60 of the slots 50 and 52. The rear portion 46 of the seat pan 42 is thus positioned in front of the bottom of the seat back 40 with its upper surface horizontal. The main portion 44 of the seat pan 42 is therefore in a downwardly sloping orientation, as shown in Figures 8 and 9. A leg rest 66 is deployed so as to form a continuation of the top surface of the main portion 44 of the seat pan. The buttocks of a seat occupant can then rest on the rear portion 46. Figure 10 illustrates a modification of the seat shown in Figures 6 and 9 in which the seat pan 42 is replaced by a seat pan 64 having a rear portion 66 with a concave upper surface in place of the flat upper surface of the rear portion 46 described previously. This further reduces the possibility of a seat occupant sliding down the seat when asleep. Figure 11 illustrates an alternative modification of the seat shown in Figure 6 to 9, with a seat pan 68 having a rear portion 70 with a flat upper surface which contains two recessed regions 72 and 74. As well as reducing the possibility of a seat occupant sliding down the seat when asleep, this relieves pressure on the under sides of the seat occupant's thighs at the junction between the top surface of the main portion 44 of the seat pan and the top surface of the rear portion 70. Although the invention is particularly applicable to aircraft passenger seats, it may also be applied to seats for land, marine and amphibious vehicles.

Claims: A vehicle seat having a seat back (16, 40) which is reclinable from a normal substantially vertical orientation, and a seat pan (28, 42, 68) which is tiltable between a normal substantially horizontal orientation and a tilted orientation in which its front edge is lower than its rear edge, characterised in that the seat pan (28, 42, 68) has a rear portion (30, 46, 70) adjacent to the seat back (16, 40) which is substantially horizontal when the main portion (32, 44) of the seat pan is in its tilted orientation. A vehicle seat according to claim 1, wherein the orientation of the rear portion (30) of the seat pan (28) is permanently fixed in its substantially horizontal orientation and the main portion (32) is pivotable relative to the rear portion (30). A vehicle seat according to claim 1, wherein the rear portion (46, 66, 70) of the seat pan (42, 64, 68) is permanently fixed to the main portion (44) and is stowed under the backrest (40) when the main portion (44) is horizontal. A vehicle seat according to claim 3, wherein the rear portion (66, 70) of the seat pan (64, 68) has a concave upper surface.

Inventors: MATSUMIYA JAMES A, MATSUMIYA, JAMES A.
Applicants: BRITAX AIRCRAFT INTERIORS UK L, BRITAX AIRCRAFT INTERIORS UK LIMITED
Application year: 1996
Main classification: B60N2
IPC codes: B60N2, A47C1, B64D11