Modular aircraft floor track adapter system
US-9481467-B2 · Nov 1, 2016 · US
US9663231B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9663231-B2 |
| Application number | US-201514816447-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 3, 2015 |
| Priority date | Aug 3, 2015 |
| Publication date | May 30, 2017 |
| Grant date | May 30, 2017 |
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A titanium seat track may include a track plate formed of one of cold and hot rolled titanium. The track plate may include a top surface and a bottom surface. The titanium seat track may also include a titanium U-shaped channel formed of cold worked titanium sheet. The titanium U-shaped channel may include a first side wall and a second side wall extending from a base and terminating in a first channel edge and a second channel edge, respectively. The first channel edge and the second channel edge may be continuously welded to the bottom surface of the seat track.
Opening claim text (preview).
What is claimed is: 1. A pre-weld seat track assembly, comprising: a track plate formed of one of cold and hot rolled titanium, the track plate including a top surface and a bottom surface, wherein the top surface is configured to retain seats, the bottom surface including spaced first and second plate joints, the first plate joint including a first plate lip and a first plate ridge, and the second plate joint including a second plate lip and a second plate ridge; and a titanium U-shaped channel formed of cold worked titanium sheet, the titanium U-shaped channel including a first side wall and a second side wall extending outwardly from a base and terminating in a first channel edge and a second channel edge, respectively; wherein the first channel edge and the second channel edge are configured to be received by the first plate joint and the second plate joint, respectively, so that the first plate ridge supports the first side wall and the second plate ridge supports the second side wall, the first plate ridge is sized to extend across a first interface between the first channel edge and the first plate lip, and the second plate ridge is sized to extend across a second interface between the second channel edge and the second plate lip. 2. The pre-weld seat track assembly of claim 1 , further including a plurality of saddle mounts, a first and a second mount joint extends from each saddle mount of the plurality of saddle mounts, the first mount joint includes a first mount ridge and a first mount lip and the second mount joint includes a second mount ridge and a second mount lip. 3. The pre-weld seat track assembly of claim 2 , wherein the channel further includes a plurality of saddle-shaped recesses, the first and the second mount joints of each saddle mount matingly received by and coupled to a selected one of the saddle-shaped recesses of the plurality of saddle-shaped recesses wherein the first and second mount ridges support the selected one of the saddle-shaped recesses, and the first and second mount lips are welded to the selected one of the saddle-shaped recesses. 4. The pre-weld seat track assembly of claim 1 , wherein the U-shaped channel includes a plurality of channel sections with each section being dimensioned to support a preselected load and to meet a required rigidity. 5. The pre-weld seat track assembly of claim 4 , wherein the plurality of channel sections include a forward channel section, an aft channel section, and a plurality of mid channel sections welded together such that the plurality of mid channel sections are disposed between the forward channel section and the aft channel section, the forward channel section includes a forward splice plate, and the aft channel section includes an aft splice plate. 6. The pre-weld seat track assembly of claim 5 , wherein the forward splice plate includes a first splice ridge and a first splice lip, the aft splice plate includes a second splice ridge and a second splice lip, the first splice ridge supports the forward channel section, the first splice lip is welded to the forward channel section, the second splice ridge supports the aft channel section, and the second splice lip is welded to the aft channel section. 7. The pre-weld seat track assembly of claim 1 , wherein the track plate includes a forward end and an aft end, the forward end includes a lug, the lug includes a protruding lip, the aft end includes a recessed lug, the recessed lug includes a recessed lip. 8. A method of fabricating a seat track, the method comprising: cold forming a titanium channel including a first side wall, a second side wall, and a base; one of stamping, laser cutting, water jet cutting, and machining the titanium channel to include a plurality of saddle-shaped recesses; roll forming a titanium track plate; machining the titanium track plate to include a first and a second plate joint, the first plate joint including a first plate ridge and a first plate lip, the second plate joint including a second plate ridge and a second plate lip; welding the first plate lip to the first side wall such that the first plate ridge supports the first side wall and contains excess heat and molten material of the first plate lip inside the first plate joint; welding the second plate lip to the second side wall such that the second plate ridge supports the second side wall and contains excess heat and molten material of the second plate lip inside the second plate joint; providing a plurality of saddle mounts with each saddle mount including a first and a second mount joint; and welding the first and the second mount joint of one of the saddle mounts of the plurality of saddle mounts to a respective saddle-shaped recess of the plurality of recesses. 9. The method of claim 8 , wherein the step of cold forming the channel includes one of cold roll forming the channel and cold break forming the channel. 10. The method of claim 8 , wherein the step of roll forming the track plate includes one of cold roll forming the track plate and hot roll forming the track plate. 11. The method of claim 8 , further including one of coining and stamping a plurality of stiffeners into the first side wall and the second side wall. 12. The method of claim 8 , further including one of stamping, laser cutting, water jet cutting, and machining a plurality of weight-reducing apertures into the base. 13. The method of claim 8 , further including drilling a plurality of mounting apertures into each saddle mount of the plurality of saddle mounts. 14. A method of reducing weight of a titanium seat track, the method comprising: cold forming a channel including a forward channel section, an aft channel section, and a plurality of mid channel sections; one of stamping and coining a plurality of stiffeners into the forward channel section, the aft channel section, and the plurality of mid channel sections; one of stamping, laser cutting, water jet cutting, and machining a plurality of weight-reducing apertures into the forward channel section, the aft channel section, and the plurality of mid channel sections; one of stamping, laser cutting, water jet cutting, and machining the channel to include a plurality of saddle-shaped recesses, the forward channel section to include a pair of forward ligaments, the aft channel section to include a pair of aft ligaments, and each mid channel section of the plurality of mid channel sections to include a first pair of mid ligaments and a second pair of mid ligaments; one of hot and cold roll forming a track plate; machining the track plate to include a first and a second plate joint, a recessed lug including a recessed lip, and a lug including a protruding lip, the first plate joint including a first plate ridge and a first plate lip, the second plate joint including a second plate ridge and a second plate lip; welding the first and the second plate lips to each of the forward channel section, the aft channel section, and the plurality of mid channel sections such that the first and the second plate ridges contain excess heat and molten material of the first and the second plate lips inside the first and the second plate joints, respectively; welding a forward splice plate to the forward channel section and a forward end the track plate; and welding an aft splice plate to the aft channel section and an aft end of the aft track plate. 15. The method of claim 14 , further including one of stamping, laser cutting, water jet cutting, and machining a plurality of saddle mounts such that each saddle mount includes a pair of mount joints including a mount ridge and a mount lip
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