Seat track assembly with elongate carbon-fiber reinforced polymer flange

A seat track assembly is disclosed. The seat track assembly includes an elongate titanium crown, an elongate carbon-fiber reinforced polymer (CFRP) flange, and an elongate CFRP base. The elongate titanium crown is configured to removably secure a plurality of seats to the seat track assembly. The elongate CFRP flange is configured to support the elongate titanium crown. The elongate CFRP base has a top, two sidewalls extending vertically from opposing sides of the top, and two bottom flanges each extending laterally outward from a corresponding sidewall of the two sidewalls. A fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other.

FIELD

The disclosure relates generally to a seat track assembly, and more specifically to a seat track assembly that is separable into a collection of sub-components that are mechanically fastened together to form the seat track assembly.

BACKGROUND

Monolithic seat tracks in passenger floor structures of aircraft or other vehicles are prone to corrosion and physical degradation over time. Physical degradation usually occurs in a crown of the seat track, where seats and other monuments attach to the seat track. In some cases, physical degradation can occur in a flange of the seat track that supports floor panels that reside in between neighboring seat tracks. In one example, a method of repairing a monolithic seat track that has physically degraded requires the entire seat track to be removed and replaced with a new seat track even though only a portion of the seat track is physically degraded. Such a repair process destroys the previous alignment to adjacent seat tracks for Waterline (WL), Station (STA), and Buttline (BL) axes of the aircraft. Collectively re-aligning a plurality of seat tracks in all three axes upon installing a new seat track as part of a repair process is exceedingly time consuming.

SUMMARY

A seat track assembly is disclosed. The seat track assembly includes an elongate titanium crown, an elongate carbon-fiber reinforced polymer (CFRP) flange, and an elongate CFRP base. The elongate titanium crown is configured to removably secure a plurality of seats to the seat track assembly. The elongate CFRP flange is configured to support the elongate titanium crown. The elongate CFRP base has a top configured to support the elongate CFRP flange, two sidewalls extending vertically from opposing sides of the top, and two bottom flanges each extending laterally outward from a corresponding sidewall of the two sidewalls. A fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other. The fastener is removeable from the aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other.

DETAILED DESCRIPTION

The present description is directed to a seat track assembly having improved corrosion resistance, while also being easier to repair or replace, and lighter in weight and lower in cost relative to other monolithic seat track assemblies. The herein-described seat track assembly reduces the time needed to effect repairs by separating the seat track structure into a collection of sub-components including an elongate titanium crown, an elongate carbon-fiber reinforced polymer (CFRP) flange, and an elongate CFRP base. The elongate titanium crown is configured to removably secure a plurality of seats to the seat track assembly. The elongate CFRP flange is configured to support the titanium crown. The elongate CFRP flange is further configured to support a floor panel positioned between neighboring seat track assemblies.

A fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other. The fastener is removeable from the aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other.

By forming the elongate crown from titanium, the elongate crown has improved degradation and corrosion characteristics relative to a crown formed from materials such as steel or aluminum. Further, by forming the elongate flange and the elongate base from CFRP, the elongate flange and the elongate base have improved degradation and corrosion characteristics relative to corresponding sub-components formed from aluminum or other materials. Also, by forming these sub-components from CFRP, the sub-components are less expensive to produce relative to corresponding sub-components formed from titanium. The elongate crown is formed from titanium while the elongate flange and the elongate base need not be formed from titanium and instead are formed from CFRP, because the elongate crown is exposed to more frequent sources of degradation. For example, passenger and crew exposure, and/or the process of installing and uninstalling seats into a seat track, can be sources of degradation that are resisted by the superior material strength properties of titanium. Since the other sub-components are less exposed to such sources of degradation, CFRP can provide suitably high degradation and corrosion characteristics while being less expensive and lighter weight than titanium. Moreover, using CFRP instead of titanium allows for fasteners to be installed in the seat track assembly without requiring fay sealing and/or wetting lubricant during install.

FIG.1shows an illustrative aircraft100including a fuselage102. The fuselage102includes an interior cabin section104, illustrated with increased detail in the call out. The interior cabin section104includes a plurality of passenger seats106arranged in rows oriented perpendicular to a longitudinal axis108of the fuselage102. Each row of passenger seats106is mechanically fastened to two or more seat track assemblies110, which are typically oriented coaxially with the longitudinal axis108of the fuselage102. The seat track assemblies110provide a structural frame that anchors the passenger seats106to the fuselage102. An aircraft floor panel112is installed in between a pair of seat track assemblies110. The aircraft floor panel112provides a structural floor to support passengers, luggage, and other equipment within the interior cabin section104.

The aircraft100is provided as a non-limiting example of a vehicle in which the seat track assemblies110may be used. The seat track assemblies110may be used in any suitable type of vehicle to provide improved corrosion resistance, while also being easier to repair or replace, and lighter in weight and lower in cost relative to other monolithic seat assemblies.

FIG.2shows an example embodiment of a portion of a floor support structure200of an aircraft including a plurality of seat track assemblies202supported by a plurality of floor support beams204. The seat track assemblies202are mounted on top of the floor support beams204via a plurality of shear clips206. A plurality of floor stanchions208mechanically couple the plurality of floor support beams204to a plurality of fuselage support frames210. In particular, a representative seat track assembly202′ is mounted on top of a representative floor support beam204′. Note that the use of (′) and (″) indicate individual representative instances of a plurality of a particular component. For example, representative seat track assembly202′ is representative of the plurality of seat track assemblies202included in the floor support structure200. A representative shear clip206′ mechanically fastens the representative seat track assembly202′ to the representative floor support beam204′. A pair of representative floor stanchions208′ and208″ are mechanically coupled to opposing ends of the representative floor support beam204′. The pair of representative floor stanchions208′ and208″ are mechanically coupled to a representative fuselage support frame210′.

Each of the plurality of seat track assemblies202may be arranged in the same manner as the representative seat track assembly202′ to form the floor support structure200. The plurality of seat track assemblies202are aligned relative to each other in terms of Waterline (WL), Station (STA), and Buttline (BL) axes of the aircraft.

The representative seat track assembly202′ includes a collection of sub-components that can be mechanically separated from each other in case the need arises to replace or repair a particular sub-component. For example, an elongate titanium crown (e.g., the elongate titanium crown302shown inFIGS.3-4) is configured to be removable from the representative seat track assembly202′ without destroying the overall alignment of the representative seat track assembly202′ in any of the Waterline, Station, and Buttline axes. In particular, the other sub-components of the representative seat track assembly202′ can remain in place in the floor support structure200even when the elongate titanium crown is removed.

FIGS.3-4show an example embodiment of a portion of a seat track assembly300. For example, the seat track assembly300may be representative of any of the plurality of seat track assemblies202shown inFIG.2.FIG.3shows a top view of a partial length of the seat track assembly300.FIG.4shows a cross-section view of the seat track assembly300.

The seat track assembly300includes an elongate titanium crown302configured to removably secure a plurality of seats (not shown) to the seat track assembly300. The elongate titanium crown302forms a plurality of holes304that are configured to receive a plurality of fasteners, such as a fastener305. In some cases, a fastener may be inserted into one of the plurality of holes304to mechanically fasten the different sub-components of the seat track assembly to each other. In some cases, a fastener may be inserted into one of the plurality of holes304to mechanically fasten a seat to the seat track assembly300. The plurality of holes304formed in the elongate titanium crown302allows for secure attachment of a seat, with flexibility to move a seat quickly and simply by removing the corresponding fasteners and aligning the seat with a different set of holes in the elongate titanium crown302.

The material strength characteristics of the elongate titanium crown302are suitable to reduce or prevent degradation over time due to absorbing various forces applied by seats or other components fastened to the elongate titanium crown302during operation. The material strength characteristics of titanium are greater than other more corrodible materials typically used to form a crown, such as aluminum. Further, titanium has material characteristics that are suitable to reduce or prevent corrosion over long-term operation. Additionally, titanium has a higher strength per weight ratio relative to other materials having similar material strength characteristics, which contributes to an overall weight reduction of an aircraft in which the seat track assembly300is installed.

The seat track assembly300includes an elongate carbon-fiber reinforced polymer (CFRP) flange306that is configured to support the elongate titanium crown302. The elongate CFRP flange306has a width that is greater than a width of the elongate titanium crown302. The elongate CFRP flange306includes projections310and312that extend outward laterally beyond sides314and316of the elongate titanium crown302. The projections310and312are configured to support floor panels318and320that span between corresponding projections of neighboring seat track assemblies (not shown). The projections310and312may have a width that is suitable to support the floor panels318and320.

In some embodiments, the elongate CFRP flange306is flat—that is, the flange has a planar upper surface—to support the floor panels318and320. In other embodiments, the elongate CFRP flange306, or a portion thereof, has anon-flat surface (e.g., concave or convex cross-section) that supports the floor panels318and320. In some embodiments, the elongate CFRP flange306has a surface that varies along the length of the seat track assembly300. For example, the elongate CFRP flange306may include a sequence of features (e.g., posts, holes, scallops) that interfaces with a cooperating sequence of features of the floor panels318and320that allow for the floor panels318and320to interlock between neighboring seat track assemblies. In some embodiments, the elongate titanium crown302may include a sequence of features that interface with a cooperating sequence of features of the floor panels318and320.

Somewhat similarly, although the portion of the elongate CFRP flange that supports the elongate titanium crown is also shown inFIG.4to be flat, some embodiments may include a non-flat portion (e.g., a concave or convex cross-section) and/or may include surface features (e.g. nubs, grooves, detents, and so forth), such as to mate or align with a correspondingly shaped surface or complementary surface features provided on the elongate titanium crown, for example to facilitate alignment of the components prior to being fastened together.

The elongate CFRP flange306forms a plurality of holes322that are configured to receive a plurality of fasteners, such as the fastener305. The plurality of holes322in the elongate CFRP flange306are configured to align with the plurality of holes304formed in the elongate titanium crown302. In some embodiments, the plurality of holes304formed in the elongate titanium crown302and the plurality of holes322formed in the elongate CFRP flange306may have a same diameter.

The seat track assembly300includes an elongate CFRP base324having a top326configured to support the elongate CFRP flange306. The elongate CFRP base324further includes two sidewalls328and330extending vertically from opposing sides of the top326, and two bottom flanges332and334each extending laterally outward from a corresponding sidewall of the two sidewalls328and330. As used here, vertically can mean substantially vertically (e.g., within +/−10 degrees) such that sidewalls328and330are not necessarily parallel; and horizontally can mean substantially horizontally (e.g., within +/−22.5 degrees). In general, any shape that provides suitable structural properties is within the scope of this disclosure.

Also, although the surfaces of the elongate CFRP flange and that of the elongate CFRP base that contact each other when the components are fastened together are shown inFIG.4to be flat, as noted above, these surfaces or portions thereof may be non-flat (e.g., concave or convex), and/or include corresponding surface features, to facilitate alignment of the components prior to being fastened together.

In some embodiments, one or more of the bottom flanges332and334of the elongate CFRP base324include stiffening return flanges338that project upward from outer edges of the bottom flanges. In the illustrated embodiment, the bottom flange334includes a stiffening return flange338. The stiffening return flanges338may be included in the elongate CFRP base324in scenarios where the elongate CFRP base324has greater operational weight requirements. For example, stiffening return flanges338may be included in the elongate CFRP base324when the seat track assembly300is used in a floor support structure of a cargo aircraft and the seat track assembly300has to support the weight of cargo that may be greater than the weight of passengers.

The elongate CFRP base324forms a plurality of holes336that are configured to receive a plurality of fasteners, such as the fastener305. The plurality of holes336formed in the elongate CFRP base324are configured to align with the plurality of holes304formed in the elongate titanium crown302and the plurality of holes322formed in the elongate CFRP flange306. In some embodiments, the plurality of holes304formed in the elongate titanium crown302, the plurality of holes322formed in the elongate CFRP flange306, and the plurality of holes336formed in the elongate CFRP base324may have a same diameter.

In one example of an embodiment in which one or more of the components of the assembly is shaped and/or includes surface features to facilitate alignment in assembly, at least some of the holes may be configured to provide such alignment. In such an example, at least some of the plurality of holes322in the elongate CFRP flange306, and/or at least some of the plurality of holes336in the elongate CFRP base324are configured to partially protrude from the surface of the component, such as to partially nest within a corresponding hole in another component.

The fastener305is insertable through aligned holes304,322,336defined by the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324to mechanically fasten the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324to each other. Further, the fastener305is removeable from the aligned holes304,322,336to allow for the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324to be mechanically separated from each other.

The aligned holes304,322,336defined by the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324form a first set of aligned holes336that correspond to the fastener305. Further, the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324form a plurality of sets of aligned holes336,336′,336″, . . . The plurality of sets of aligned holes336,336′,336″, . . . are longitudinally spaced apart along the seat track assembly300.

A plurality of fasteners (not shown) are insertable through the plurality of sets of aligned holes336,336′,336″, . . . to mechanically fasten the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324to each other. The plurality of fasteners are removeable from the plurality of sets of aligned holes336,336′,336″, . . . to allow for the elongate titanium crown302, the elongate CFRP flange306, and the elongate CFRP base324to be mechanically separated from each other.

By allowing the individual sub-components of the seat track assembly300to be separable from each other, the individual sub-components of the seat track assembly300can be removed and/or replaced while preserving a prior alignment (that is, without requiring re-alignment) of the seat track assembly300within the floor support structure of the aircraft with respect to the Waterline (WL), Station (STA), and Buttline (BL) axes of the aircraft. In this way, the seat track assembly300facilitates quick and easy maintenance and/or repairs relative to a monolithic seat track assembly that must be arduously realigned when being replaced and/or repaired.

The elongate CFRP flange306and the elongate CFRP base324are formed from CFRP material, which has a higher strength-to-weight ratio and stiffness (rigidity) relative to steel, aluminum, and other materials typically used in a monolithic seat track assembly. The CFRP material may include a binding polymer that provides suitable material strength and stiffness characteristics to support the floor panels318and320as well as additional weight requirements (e.g., seats, passengers, cargo) of the aircraft. In some examples, the CFRP flange306may be formed using a binding polymer that includes a thermoset resin, such as epoxy. In some examples, other thermoset or thermoplastic polymers may be used. Additionally, the CFRP material can be easily curved/folded to form the curved corners of the elongate CFRP base324. Forming such curved corners for a base made from metal may be substantially more complex and time consuming relative to CFRP material.

A seat track assembly can be configured to mount to a plurality of floor support beams differently in different embodiments. In some embodiments, a seat track assembly can be configured to mount on top of a plurality of floor support beams such that the seat track assembly passes above the plurality of floor support beams.FIGS.5-6show an example embodiment of a seat track assembly500that is configured to mount on top of a plurality of floor support beams510. For example, the seat track assembly500can be representative of the seat track assembly300shown inFIGS.3-4. The seat track assembly500comprises an elongate titanium crown502, an elongate CFRP flange504, and an elongate CFRP base506. The seat track assembly500further comprises a plurality of shear clips508corresponding to a plurality of floor support beams510. Each of the plurality of shear clips508is configured to mechanically fasten the elongate CFRP base506of the seat track assembly500to a corresponding floor support beam510.

In some embodiments, the plurality of shear clips508comprise titanium. Shear clips comprising titanium reduces the likelihood of the shear clips corroding relative to shear clips comprising materials such as steel or even aluminum. Further, titanium sheer clips eliminate the need for fay seal and wet installation of fasteners. In other embodiments, the plurality of shear clips508comprise CFRP. Shear clips comprising CFRP provide high strength-to-weight characteristics while being lower in cost and complexity to manufacture than titanium. In still other embodiments, the plurality of shear clips508may comprise another material having suitably high strength-to-weight and/or corrosion-resistive characteristics.

A representative shear clip508′ of the plurality of shear clips508comprises a backplate512and two sidewalls514,516. An exterior width (W1) of the representative shear clip508′ is slightly less than an interior width (W2) between sidewalls518,520of the elongate CFRP base506, so that the representative shear clip508′ is able to fit within the elongate CFRP base506. Each of the sidewalls518,520of elongate CFRP base506form holes522,524,526,528that are configured to receive base fasteners530,532,534,536. Correspondingly, each of the sidewalls514,516of the representative shear clip508′ form holes538,540,542,544that are configured to receive the base fasteners530,532,534,536. The holes538,540,542,544formed in the representative shear clip508′ are configured to align with the holes522,524,526,528formed in the elongate CFRP base506when the representative shear clip508′ is fit within the elongate CFRP base506. In the illustrated embodiment, two base fasteners are used to mechanically fasten each sidewall of the representative shear clip508′ to the elongate CFRP base506to prevent the representative shear clip508′ from rotating relative to the elongate CFRP base506. A different number of base fasteners can be used.

The representative shear clip508′ is configured to mechanically fasten to a representative floor support beam510′ via a plurality of beam fasteners (e.g., representative beam fastener546′ shown inFIG.6). In particular, the backplate512forms a plurality of holes (e.g., representative hole548′ shown inFIG.6) each configured to receive a corresponding beam fastener (e.g., representative beam fastener546′). The plurality of beam fasteners546are configured to mechanically fasten the representative shear clip508′ to the representative floor support beam510′. The representative shear clip508′ is mechanically fastened to the representative floor support beam510′ via two or more beam fasteners to prevent the representative shear clip508′ from rotating relative to the representative floor support beam510′.

In the illustrated embodiment, the plurality of beam fasteners546are oriented perpendicular to the plurality of base fasteners530,532,534,536to maintain alignment of the seat track assembly500in all three axes (i.e., STA, BL, WL axes) when the seat track assembly500is mechanically fastened to the plurality of floor support beams510.

In the illustrated embodiment, the representative shear clip508′ is configured to mechanically fasten the elongate CFRP base506to the representative floor support beam510′, such that two bottom flanges550,552of the elongate CFRP base506are positioned above the representative floor support beam510′. In some embodiments, the bottom flanges550,552can rest on a top554of the representative floor support beam510′. In other embodiments, there may be a gap between the bottom flanges550,552and the top554of the representative floor support beam510′. Such clearance may depend on the design requirements of the floor support structure of the aircraft. The illustrated embodiment of the seat track assembly that is positioned entirely over the tops of the plurality of floor support beams facilitates straightforward alignment since each of the plurality of floor support beams is continuous. However, such a seat track assembly has an increased overall height relative to a seat track assembly that at least partially fits between adjacent floor support beams.

In some embodiments, a seat track assembly can be configured to at least partially fit between adjacent floor support beams.FIGS.7-9show an example embodiment of a seat track assembly700that is configured to at least partially fit between adjacent floor support beams of a plurality of floor support beams702. For example, the seat track assembly700can be representative of the seat track assembly300shown inFIGS.3-4. The seat track assembly700comprises an elongate titanium crown704, an elongate CFRP flange706, and a plurality of discrete elongate CFRP base sections708.

In the illustrated embodiment, the elongate titanium crown704and the elongate CFRP flange706are both configured to span across tops of the plurality of floor support beams702. Each of the plurality of discrete elongate CFRP base sections708is configured to fit between adjacent floor support beams of the plurality of floor support beams702. The plurality of discrete elongate CFRP base sections708is configured to fasten to the plurality of floor support beams702via a plurality of shear clips710. For example, a representative discrete elongate CFRP base section708′ is configured to fit between representative adjacent floor support beams702′ and702″. A first end712of the representative discrete elongate CFRP base section708′ is fastened to the first representative floor support beam702′ via a first shear clip710′ at a first intersection714and a second end716of the representative discrete elongate CFRP base section708′ is fastened to the second representative floor support beam702″ via a second shear clip710″ at a second intersection718.

FIG.8shows a top view of the intersection714of the seat track assembly700shown inFIG.7, andFIG.9shows a bottom view of the intersection714of the seat track assembly700shown inFIG.7. In the illustrated embodiment, the first shear clip710′ mechanically fastens to a corresponding sidewall800of the representative discrete elongate CFRP base section708′ via base fasteners802and804. Further, the first shear clip710′ mechanically fastens to a corresponding sidewall806of the representative floor support beam702′ via support fasteners808and810. Any suitable type of fasteners can be used to mechanically fasten the first shear clip710′ to the corresponding sidewall800of the representative discrete elongate CFRP base section708′ and the corresponding sidewall806of the representative floor support beam702′. For example, the fasteners may be screws, bolts, rivets, or another type of fastener.

In the illustrated embodiment, the first shear clip710′ is configured to maintain the representative discrete elongate CFRP base section708′ in alignment with the representative floor support beam702′ by bracketing the representative discrete elongate CFRP base section708′. In particular, the first shear clip710′ comprises exterior bracket walls (e.g., exterior bracket wall812) that fasten to corresponding exterior sidewalls of the representative discrete elongate CFRP base section708′ (e.g., exterior sidewall800). The first shear clip710′ further comprises interior bracket walls (e.g., interior bracket wall814shown inFIG.9) that fasten to interior sidewalls (e.g., interior sidewall900shown inFIG.9) of the representative discrete elongate CFRP base section708′. The shear clip710′ is provided as a non-limiting example. The shear clip may take any suitable form to mechanically fasten the representative discrete elongate CFRP base section708′ to the representative floor support beam702′.

In some embodiments, the seat track assembly700comprises a plurality of splice fittings720. Each splice fitting720is configured to mechanically fasten two adjacent discrete elongate CFRP base sections to each other as well as to an intervening floor support section. As shown inFIGS.8-9, a representative splice fitting720′ is mechanically fastened to a bottom flange818of the representative discrete elongate CFRP base section708′, a bottom flange820of an adjacent discrete elongate CFRP base section822, and the representative floor support beam702′ via a plurality of base flange fasteners824. The plurality of splice fittings720may comprise any suitable material. In some embodiments, the plurality of splice fittings720comprise CFRP. In other embodiments, the plurality of splice fittings720comprise titanium. The plurality of splice fittings may be used to increase the overall rigidity of the seat track assembly700, since the elongate CFRP base is divided into discrete sections in this embodiment.

In some embodiments, the elongate CFRP flange706is configured to mechanically fasten to each of the plurality of floor support beams702via a plurality of flange fasteners. In particular, the elongate CFRP flange706comprises a plurality of protrusions that extend laterally over the tops of the plurality of floor support beams702. As shown inFIGS.8-9, the elongate CFRP flange706comprises a representative protrusion826that forms holes828configured to receive flange fasteners830. The representative floor support beam702′ forms corresponding holes832configured to align with the holes828formed in the representative protrusion826of the elongate CFRP flange706. The flange fasteners830are insertable through the holes828and832to mechanically fasten the elongate CFRP flange706to the representative floor support beam702′.

In the illustrated embodiment, the elongate titanium crown704and the elongate CFRP flange706are continuous, and the elongate CFRP base is segmented into a plurality of discrete sections708. Each discrete CFRP base section708fits between adjacent floor support beams702spanned by the elongate titanium crown704and the elongate CFRP flange706. The elongate CFRP flange706rests directly on the tops of the plurality of floor support beams702and is mechanically fastened to the plurality of floor support beams to provide suitable alignment strength. Each CFRP base section708mechanically fastened to adjacent floor support beams702via shear clips710to maintain moment continuity. In this embodiment, the elongate titanium crown704and the elongate CFRP flange706are lowered down relative to the position of corresponding sub-components of the seat track assembly500shown inFIG.5. Such an arrangement allows the seat track assembly700to be recessed mostly between the floor support beams to lower the overall height of the floor support structure of the aircraft. Such a height reduction can allow for an overall height reduction of the fuselage cross-section for drag reduction and improved aircraft flight performance and/or accommodate a taller cabin.

The herein-described seat track assembly comprises materials (i.e., titanium and CFRP) that reduce or eliminate the problem of corrosion. Further, such materials do not require fay surface sealant or corrosion inhibiting compound for installation. The CFRP components are shaped in such a manner that they can be produced using a variety of resin/fiber systems, including thermoset and thermoplastic materials as desired. Furthermore, the seat track assembly is separable into sub-components in a manner that allows for the elongate titanium crown and the elongate CFRP flange to be removeable for repair or replacement without causing the seat track assembly to fall out of alignment with a floor support structure in which the seat track assembly is aligned. In particular, the elongate CFRP base remains attached to the floor support beams and in WL, BL, and STA alignments. Because this joint remains intact during crown and flange removal, the aligned holes in the crown, flange, and base allows the crown and flange to be re-aligned in the WL, BL, and STA alignments without the need for tooling when those sub-components are re-installed in seat track assembly. In this way, the original factory alignment can be maintained for the life of the aircraft. Although the seat track assembly is described in the context of being used in an aircraft, the seat track assembly can be used in any suitable vehicle to provide the features and benefits described above.

In an example, a seat track assembly, comprises an elongate titanium crown configured to removably secure a plurality of seats to the seat track assembly, an elongate carbon-fiber reinforced polymer (CFRP) flange configured to support the elongate titanium crown, and an elongate CFRP base having a top configured to support the elongate CFRP flange, two sidewalls extending vertically from opposing sides of the top, and two bottom flanges each extending laterally outward from a corresponding sidewall of the two sidewalls, wherein a fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other, and wherein the fastener is removeable from the aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other. In this example and/or other examples, the elongate CFRP flange may include projections that extend outward laterally beyond sides of the elongate titanium crown, and the projections may be configured to support floor panels that span between corresponding projections of neighboring seat track assemblies. In this example and/or other examples, the bottom flanges of the elongate CFRP base may include stiffening return flanges that project upward from outer edges of the bottom flanges. In this example and/or other examples, the seat track assembly may further comprise a plurality of shear clips corresponding to a plurality of floor support beams, each of the plurality of shear clips being configured to mechanically fasten the elongate CFRP base to a corresponding floor support beam. In this example and/or other examples, the plurality of shear clips may be at least one of titanium or CFRP. In this example and/or other examples, the seat track assembly further comprises a plurality of floor stanchions configured to mechanically couple the plurality of floor support beams to a fuselage structure. In this example and/or other examples, the elongate CFRP base may be configured to span the plurality of floor support beams, and each of the plurality of shear clips may be configured to mechanically fasten the elongate CFRP base to the corresponding floor support beam such that the two bottom flanges of the elongate CFRP base are positioned above the plurality of floor support beams. In this example and/or other examples, each of the plurality of shear clips may be configured to fit between the two sidewalls of the elongate CFRP base, and each of the plurality of shear clips may be configured to mechanically fasten to each of the two sidewalls via a plurality of base fasteners. In this example and/or other examples, each of the plurality of shear clips may be configured to mechanically fasten to the corresponding floor support beam via a plurality of beam fasteners, and the plurality of base fasteners may be oriented perpendicular to the plurality of beam fasteners in the seat track assembly. In this example and/or other examples, the elongate CFRP base may be configured to fit between a pair of adjacent floor support beams of the plurality of floor support beams, and each of the plurality of shear clips may mechanically fasten to a corresponding sidewall of the elongate CFRP base and a corresponding sidewall of an adjacent floor support beam. In this example and/or other examples, the elongate titanium crown and the elongate CFRP flange may be both configured to span across tops of the plurality of floor support beams. In this example and/or other examples, the elongate CFRP flange may be mechanically fastened to the pair of adjacent floor support beams via a plurality of flange fasteners. In this example and/or other examples, the seat track may further comprise a splice fitting mechanically fastened to a bottom flange of the elongate CFRP base, an adjacent bottom flange of an adjacent elongate CFRP base, and a floor support beam that is mechanically fastened to the elongate CFRP base and the adjacent elongate CFRP base. In this example and/or other examples, the aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base may form a first set of aligned holes, the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base may form a plurality of sets of aligned holes including the first set, the plurality of sets of aligned holes may be longitudinally spaced apart along the seat track assembly, a plurality of fasteners may be insertable through the plurality of sets of aligned holes to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other, and the plurality of fasteners may be removeable from the plurality of sets of aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other.

In another example, a seat track assembly, comprises an elongate titanium crown configured to removably secure a plurality of seats to the seat track assembly, an elongate CFRP flange configured to support the elongate titanium crown, an elongate CFRP base having a top configured to support the elongate CFRP flange, two sidewalls extending vertically from opposing sides of the top, and two bottom flanges each extending laterally outward from a corresponding sidewall of the two sidewalls, wherein the elongate CFRP base is configured to span a plurality of floor support beams, and a plurality of shear clips corresponding to the plurality of floor support beams, each of the plurality of shear clips being configured to mechanically fasten the elongate CFRP base to the corresponding floor support beam, such that the two bottom flanges of the elongate CFRP base are positioned above the plurality of floor support beams, wherein a fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other, and wherein the fastener is removeable from the aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other. In this example and/or other examples, each of the plurality of shear clips may be configured to fit between the two sidewalls of the elongate CFRP base, and each of the plurality of shear clips may be configured to mechanically fasten to each of the two sidewalls via a plurality of base fasteners. In this example and/or other examples, each of the plurality of shear clips may be configured to mechanically fasten to the corresponding floor support beam via a plurality of beam fasteners, and the plurality of base fasteners may be oriented perpendicular to the plurality of beam fasteners in the seat track assembly.

In yet another example, a seat track assembly, comprises an elongate titanium crown configured to removably secure a plurality of seats to the seat track assembly, an elongate CFRP flange configured to support the elongate titanium crown, an elongate CFRP base having a top configured to support the elongate CFRP flange, two sidewalls extending vertically from opposing sides of the top, and two bottom flanges each extending laterally outward from a corresponding sidewall of the two sidewalls, wherein the elongate CFRP base is configured to fit between a pair of adjacent floor support beams, and a plurality of shear clips, each of the plurality of shear clips being configured to mechanically fasten to a corresponding sidewall of the elongate CFRP base and a corresponding sidewall of an adjacent floor support beam, wherein a fastener is insertable through aligned holes defined by the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to mechanically fasten the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to each other, and wherein the fastener is removeable from the aligned holes to allow for the elongate titanium crown, the elongate CFRP flange, and the elongate CFRP base to be mechanically separated from each other. In this example and/or other examples, the elongate titanium crown and the elongate CFRP flange may both configured to span across tops of the pair of adjacent floor support beams. In this example and/or other examples, the elongate CFRP flange may be mechanically fastened to the pair of adjacent floor support beams via a plurality of flange fasteners.

The present disclosure includes all novel and non-obvious combinations and subcombinations of the various features and techniques disclosed herein. The various features and techniques disclosed herein are not necessarily required of all examples of the present disclosure. Furthermore, the various features and techniques disclosed herein may define patentable subject matter apart from the disclosed examples and may find utility in other implementations not expressly disclosed herein.