# US 7,607,613 B2 · Payload support track interface and fitting > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 7,607,613 B2 - Document ID: US7607613B2 - Status: Granted - Kind: B2 - Application number: 12/172,849 - Filed: 2008-07-14 - Published: 2008-11-13 - Granted: 2009-10-27 - Earliest claimed: 2004-03-29 - Assignees: The Boeing Company - Inventors: Walter Forrest Frantz; Martin R. Grether; Raymond R. Reed; Douglas W. Hackett - Web page: https://patentgrep.com/patent/US7607613B2 ## CPC - B64D 11/0696: {Means for fastening seats to floors, e.g. to floor rails} - B64C 1/20: specially adapted for freight - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - B64C: AEROPLANES; HELICOPTERS ## Abstract Apparatus for coupling a payload to a support track are disclosed. In one embodiment, a seat track configured for use with an interface assembly includes at least one elongated support. The seat track also includes an engagement member coupled to the elongated support and having a plurality of coupling apertures disposed therethrough. Each coupling aperture may be configured to receive at least one of a clamp arm and a fastener of the interface assembly and further configured to be engaged with the at least one of the clamp arm and the fastener in an unsecured position. The clamp arm may be extractable from the coupling aperture in a first position and may not be extractable from the coupling aperture in a second position. ## Claims ### Claim 1 A seat track configured for use with an interface assembly, the seat track comprising: at least one elongated support; and an engagement member coupled to the elongated support and having a plurality of coupling apertures disposed therethrough, each coupling aperture being configured to receive at least one of a clamp arm and a fastener of the interface assembly and further configured to engage with the at least one of the clamp arm and the fastener in an unsecured position where the clamp arm is extractable from a corresponding coupling aperture, and in a secured position where the clamp arm is fixed firmly with the corresponding coupling aperture, wherein the clamp arm clampably engages a portion of the engagement member disposed between two or more of the coupling apertures when the corresponding coupling aperture is engaged with the at least one of the clamp arm and the fastener in the secured position, and wherein the clamp arm engages an underside of the engagement member and extends longitudinally along the engagement member spanning across at least two coupling apertures of the engagement member when the corresponding coupling aperture is engaged with the at least one of the clamp arm and the fastener in the secured position. ### Claim 2 (depends on 1) The seat track of claim 1, wherein the at least one elongated support includes a channel member having an upper surface located between or over structure that takes a form of at least one of “C”-shaped members, “J”-shaped members, “I”-shaped members, hat shaped members, and box shaped members. ### Claim 3 (depends on 1) The seat track of claim 1, wherein the at least one elongated support includes a raised plateau portion centrally disposed between a pair of outwardly-extending flange portions, the raised plateau portion being coupled to the engagement member. ### Claim 4 (depends on 1) The seat track of claim 1, wherein at least one of the coupling apertures includes an enlarged first portion and at least one relatively smaller end portion. ### Claim 5 A payload support assembly, comprising: a component having at least one support member; an interface assembly coupled to the support member; a floor assembly including at least one floor panel and at least one seat track, the seat track including: at least one elongated support; and an engagement member coupled to the elongated support and having a plurality of coupling apertures disposed therethrough, the plurality of coupling apertures configured to engage with two clamp arms of the interface assembly in an unsecured position where the clamp arms are extractable from a corresponding coupling aperture, and the plurality of coupling apertures configured to engage with the two clamp arms and to engage therebetween with a lug of the interface assembly in a secured position where the clamp arms and the lug are firmly fixed to the corresponding coupling aperture, wherein the two clamp arms extend longitudinally along the engagement member and span across at least two coupling apertures of the engagement member when the plurality of coupling apertures are in the secured position. ### Claim 6 (depends on 5) The assembly of claim 5, wherein the at least one elongated support includes: a first channel member having a first upper surface; and a second channel member approximately parallel to and spaced apart from the first channel member, the second channel member having a second upper surface approximately co-planar with the first upper surface, wherein the engagement member is coupled between the first and second channel members proximate the first and second upper surfaces. ### Claim 7 (depends on 5) The assembly of claim 5, wherein the at least one elongated support includes a raised plateau portion centrally disposed between a pair of outwardly-extending flange portions, the raised plateau portion being coupled to the engagement member. ### Claim 8 (depends on 5) The assembly of claim 5, wherein at least one of the plurality of coupling apertures includes an enlarged first portion and at least one relatively smaller end portion. ### Claim 9 (depends on 5) The assembly of claim 5, wherein the interface assembly includes: a base engaged with a first surface of the engagement member, the two or more clamp arms projecting outwardly therefrom; and a support arm coupled to the base and coupled to the support member of the component. ### Claim 10 An aircraft, comprising: a fuselage operatively coupled to an airframe; a propulsion system operatively coupled to the airframe; a component having at least one support member; an interface assembly coupled to the support member; a floor assembly including at least one floor panel and at least one seat track, the seat track including: at least one elongated support; and an engagement member coupled to the elongated support and having a plurality of coupling apertures disposed therethrough, each coupling aperture configured to receive two clamp arms of the interface assembly and further configured to engage with the two clamp arms in an unsecured position where the two clamp arms are extractable from an associated coupling aperture, and in a secured position where the two clamp arms are fixed firmly to the associated coupling aperture, wherein the two clamp arms engage an underside of the engagement member and extend longitudinally along the engagement member to span across at least two coupling apertures of the engagement member when the corresponding coupling apertures are engaged with the two clamp arms in the secured position. ### Claim 11 (depends on 10) The aircraft of claim 10, wherein the at least one elongated support includes: a first channel member having a first upper surface; and a second channel member approximately parallel to and spaced apart from the first channel member, the second channel member having a second upper surface approximately co-planar with the first upper surface, wherein the engagement member is coupled between the first and second channel members proximate the first and second upper surfaces. ### Claim 12 (depends on 10) The aircraft of claim 10, wherein the at least one elongated support includes a raised plateau portion centrally disposed between a pair of outwardly-extending flange portions, the raised plateau portion coupleable with the engagement member. ### Claim 13 (depends on 10) The aircraft of claim 10, wherein at least one of the coupling apertures includes an enlarged first portion and at least one relatively smaller end portion. ### Claim 14 (depends on 10) The aircraft of claim 10, wherein the interface assembly includes: a base engaged with a first surface of the engagement member, the two clamp arms of the interface assembly projecting outwardly therefrom; a support arm coupled to the base and coupled to the support member of the component; and at least one lug member operatively coupled to the base and moveable between in the unsecured position and the secured position. ### Claim 15 (depends on 10) The aircraft of claim 10, wherein the component includes a seat member. ### Claim 16 (depends on 10) The aircraft of claim 10, wherein the component includes a partition. ### Claim 17 (depends on 10) The aircraft of claim 10, wherein each clamp arm of the two clamp arms is “L” shaped.