A track fitting for securing a seat pedestal of an aircraft seat to a floor of an aircraft may comprise a strut and a lock assembly. The strut may include an aft section configured to attach to an aft foot of the seat pedestal, a forward section configured to attach to a forward foot of the seat pedestal, and a central section extending between the aft section and the forward section. The lock assembly may be located proximate the aft section of the strut.

An integrable seat leg for an original equipment manufacturer seat, including a vertical member, including a front end and a rear end, a first side surface and a second side surface, a top surface and a bottom surface, one or more engaging members extending from the bottom surface, and one or more through-bores arranged proximate the top surface to secure the integrable seat leg to the seat, wherein the one or more engaging members are operatively arranged to engage one or more respective apertures in track.

A vehicle seating assembly includes a frame rail having a rear catcher pin. A seat frame slidably engages the rear catcher pin at a lateral support. A head of the catcher pin is vertically offset from the seat frame in a static condition. During an impact condition, the seat frame deflects upward and engages the head of the catcher pin to define a dynamic structure condition.

A plinth attachment system for attachment to at least one track includes: a first plate having a first side configured for mounting to a longitudinally extending track, and a first mounting feature for mounting a first structure; and a second plate having a first side configured for mounting to the track, and a second mounting feature for mounting a second structure. When mounted on the track, at least one interlinking feature of the first side of the first plate and at least one interlinking feature of the first side of the second plate interlock at the track, and, the first mounting feature and second mounting feature are aligned at essentially equivalent longitudinal positions.

Embodiments of the present invention provide systems and methods for installing seats in a passenger vehicle using seat tracks and seat fittings. The seat track fittings may include a sleeve (22) with a cylindrical threaded opening (24), a double effect post (26) with an external lower thread (28) and an internal threaded portion (36). The external lower thread is configured to cooperate with the cylindrical threaded opening of the sleeve. The seat track fitting also has a track stud (38) with a lower flange (46) that is configured to cooperate with a seat track (10) and an upper external thread (42) configured to cooperate with the internal threaded portion of the double effect post. The double effect post external lower thread and the track stud external thread have inverse hands, such that rotation of the double effect post tightens the post and the track stud simultaneously.

A seat rail system for a vehicle includes an upper rail and a stationary lower rail attached to a floor structure. The upper rail is attached to a vehicle seat and is movable relative to the lower rail. The upper rail comprises first and second side sections with a cavity between the side sections. The lower rail includes first and second lateral side elements respectively connected to the first and second side sections. An elongated load member is attached to the lower rail, where an upper part of which extends into the cavity. A lower part of the load member is connected to the floor structure. The first lateral side element blocks lateral movement of the first side section and the second lateral side element blocks lateral movement of the second side section upon deformation of the upper rail in a vehicle impact event.

Track fitting assembly having a base frame (12) comprising a pivot shaft (44) arranged so that the pivot shaft substantially aligns with an upper surface of a track when the base frame is coupled to the track and at least one pivotable insert (14) pivotally coupled to the pivot shaft.

A vehicle seat includes a back frame, a side frame, and a slider. The side frame includes a first frame member configured to couple the back frame and the slider, a second frame member disposed on one side of the first frame member in a seat width direction and configured to couple the back frame and the first frame member, and a third frame member disposed on the other side of the first frame member in the seat width direction and configured to couple the slider and the first frame member. The side frame is provided such that the first frame member, the second frame member and the third frame member are arranged in the seat width direction at least in a portion between the back frame and the slider.

A seat track fitting assembly can include a seat track having a channel sized and shaped to removably, coupleably receive a seat track fitting, which seat track fitting can include a central flange having a lug aperture which is sized and shaped to be coupleable to a payload component, and at least a pair of shear pads, with each one of the shear pads protruding outwardly from opposing sides of the central flange and including a shear flange, and a tensile flange, wherein the tensile flange and the shear flange are integrally formed with the central flange. Related methods are also provided.

A seat assembly for an aircraft is disclosed. The seat assembly includes a seat frame, a track and a track lock assembly slidably connecting the seat frame to the track. The track lock assembly includes a track foot body configured for sliding translation within the track, a pin member having a first end configured for threaded engagement with the track foot body and a second end, and a plunger configured for sliding engagement with the pin member between the first end and the second end and for locking engagement with the track lock assembly.