Airplane seat with piston

Description

Field of the Invention

[0001] The present invention concerns an aircraft seat. More particularly, but not exclusively, this invention concerns an aircraft seat with cam followers. The invention also concerns cam followers.Background of the Invention

[0002] A cam follower is often used in aircraft seats in order to help manipulate the aircraft seat as it moves between various different positions. The cam follower may be attached to, for example, the seat back or the seat pan, and control the angle of the seat back and / or seat pan as they are moved forwards or backwards, for example between an upright or bed position. Significant loads may be experienced by the cam follower, leading to wear which results in restorative maintenance or replacement being required. A cam follower often has internal bearings which emit swarf, further adding to the wear of the cam follower.

[0003] EP 1 057 725 A2 discloses an aircraft seat, the aircraft seat comprising at least one moveable element, a cam follower arrangement associated with the moveable element, wherein the cam follower arrangement comprises a first cam follower and a second cam follower attached to a common bogie, the first cam follower and second cam follower having a common diameter.

[0004] The present invention seeks to mitigate the above-mentioned problems. Alternatively or additionally, the present invention seeks to provide an improved cam follower arrangement.Summary of the Invention

[0005] The present invention provides, according to a first aspect, an aircraft seat, the aircraft seat comprising at least one moveable element, a cam follower arrangement associated with the moveable element, wherein the cam follower arrangement comprises a first cam follower and second cam follower attached to a common bogie, the first cam follower and second cam follower comprise a common diameter and wherein the first cam follower and second cam follower are spaced apart no further than the common diameter.

[0006] Provision of a first cam follower and a second cam follower attached to a common bogie spreads the load experienced by each individual cam follower. As such, the wear on each individual cam follower is reduced. This reduction in wear may result in fewer maintenance tasks associated with the aircraft seat, and may make the aircraft seat more robust.

[0007] The moveable element may be a seat pan. The moveable element may be a seat back. The association of the cam follower with the moveable element may, for example, be a mechanical connection to a mounting point on the moveable element. The common bogie may be mechanically connected to the moveable element. The common bogie may be mechanically connected to the moveable element such that the common bogie is rotatable relative to the moveable element.

[0008] The cam followers may be arranged to follow a cam path. The cam path may form part of the aircraft seat chassis. The bogie may be rotatably connected to the moveable aircraft seat element.

[0009] According to a second aspect not defined by the appended claims there is also provided a cam follower arrangement, the cam follower arrangement comprising a first cam follower and a second cam follower attached to a common bogie. The bogie may comprise a connector allowing rotational connection of the bogie to a moveable element, for example part of an aircraft seat unit. The first cam follower and second cam follower may be identical in construction. The first cam follower and second cam follower comprise a common diameter. The first cam follower and second cam follower are attached to the common bogie such that they are spaced no further apart than the common diameter. The spacing referred to is the spacing from the closest points of the two external perimeters of the first cam follower and second cam follower. The first cam follower and second cam follower may be located immediately adjacent to one another. Locating the first cam follower and second cam follower close together may provide a cam follower arrangement that is capable of following cam follower paths with tighter curvature than if the cam followers are located far apart.

[0010] Embodiments of the present invention will now be described by way of example only with reference to the accompanying schematic drawings of which: Figure 1 shows a schematic view of an aircraft seat according to a first embodiment of the invention; Figures 2 and 3 show a section of the aircraft seat comprising a cam follower arrangement according to the first embodiment of the invention; and Figures 4 to 6 show the cam follower arrangement in different positions along a cam path. Detailed Description

[0011] Figure 1 shows an aircraft seat 10 comprising a seat back 12 and a seat pan 14. The seat back 12 and the seat pan 14 are pivotally connected to each other. The seat pan 14 is mounted to a first and second slide 16, the slides 16 located to either side of the aircraft seat 10. The slides 16 are mounted to a seat chassis 18. An actuator (not shown) is used to move the aircraft seat 10 between an upright position (for example, taxi, take off, and landing position - TTL) and a bed position. The aircraft seat 10 may also be moved into one or more seating positions between the upright position and bed position. The seat pan 14 includes a cam follower arrangement 20, with the cam follower arrangement 20 located within a cam path 22 provided by the seat chassis 18. The cam path 22 includes a curved section configured to cause the seat pan 14 to change angle as the seat pan is moved forwards and backwards by the slides 16.

[0012] Further detail can be seen in figure 2, where the cam follower arrangement 20 comprises a first cam follower 24 and a second cam follower 26, each mounted to a bogie 28. The bogie 28 is rotatably mounted to the seat pan 14. The rotational connection to the seat pan 14 allows the cam follower arrangement 20 to rotate as required when moving around the curved section of the cam path. Figure 3 shows the cam follower arrangement 20 in the curved section of the cam path 22. Figures 4 to 6 show how the rotation provided by the rotational connection of the bogie 28 to the seat pan 14 allows movement from the straight section of the cam path 22 to the curved section of the cam path 22.

[0013] Whilst the present invention has been described and illustrated with reference to particular embodiments, it will be appreciated by those of ordinary skill in the art that the invention lends itself to many different variations not specifically illustrated herein.

[0014] Where in the foregoing description, integers or elements are mentioned which have known, obvious or foreseeable equivalents, then such equivalents are herein incorporated as if individually set forth. Reference should be made to the claims for determining the true scope of the present invention. It will also be appreciated by the reader that integers or features of the invention that are described as preferable, advantageous, convenient or the like are optional and do not limit the scope of the independent claims. Moreover, it is to be understood that such optional integers or features, whilst of possible benefit in some embodiments of the invention, may not be desirable, and may therefore be absent, in other embodiments.

Claims

1. An aircraft seat (10), the aircraft seat comprising at least one moveable element (12, 14), a cam follower arrangement (20) associated with the moveable element, wherein the cam follower arrangement comprises a first cam follower (24) and a second cam follower (26) attached to a common bogie (28), the first cam follower and second cam follower having a common diameter, and wherein the first and second cam followers are spaced apart no further than the common diameter.

2. An aircraft seat as claimed in claim 1, wherein the moveable element is a seat pan (14).

3. An aircraft seat as claimed in claim 1, wherein the moveable element is a seat back (12).

4. An aircraft seat as claimed in claim 1, wherein the cam followers are arranged to follow a cam path (22), the cam path forming part of the aircraft seat chassis (18).

5. An aircraft seat as claimed in any preceding claim, wherein the bogie (28) is rotatably connected to the moveable aircraft seat element (12, 14).