The present invention provides an avionics tray assembly that includes a seal assembly and a tray detail. The seal assembly includes a metering plate detail, a plurality of tabs disposed along the metering plate detail, a plurality of location bosses disposed along the metering plate detail, and a f
The present invention provides an avionics tray assembly that includes a seal assembly and a tray detail. The seal assembly includes a metering plate detail, a plurality of tabs disposed along the metering plate detail, a plurality of location bosses disposed along the metering plate detail, and a flange extending from the metering plate detail, while the tray detail includes a plurality of index bosses and a horizontal surface, wherein the plurality of index bosses receive the plurality of location bosses, wherein the plurality of tabs secure the seal assembly to the tray detail, and wherein the flange secures the seal assembly to the horizontal surface.
대표청구항▼
1. An avionics tray assembly, comprising:a seal assembly, comprising:a metering plate detail;a plurality of tabs disposed along the metering plate detail;a plurality of location bosses disposed along the metering plate detail; anda flange extending from the metering plate detail; anda tray detail, c
1. An avionics tray assembly, comprising:a seal assembly, comprising:a metering plate detail;a plurality of tabs disposed along the metering plate detail;a plurality of location bosses disposed along the metering plate detail; anda flange extending from the metering plate detail; anda tray detail, comprising:a plurality of index bosses; anda horizontal surface;wherein the plurality of index bosses receive the plurality of location bosses;wherein the plurality of tabs secure the seal assembly to the tray detail; andwherein the flange secures the seal assembly to the horizontal surface. 2. The avionics tray assembly of claim 1, wherein the tray detail further comprises a recessed area located substantially in a center of the tray detail. 3. The avionics tray assembly of claim 2, wherein the recessed area further comprises a cutout, wherein the cutout receives the seal assembly. 4. The avionics tray assembly of claim 3, wherein the flange extends about 0.40 inches beyond the cutout. 5. The avionics tray assembly of claim 3, wherein the recessed area can be sunk to a minimum depth of about 0.05 inches. 6. The avionics tray assembly of claim 1, wherein the tray detail further comprises an internal radius that supports an area of transition between the horizontal surface and a vertical surface of the tray detail. 7. The avionics tray assembly of claim 6, wherein the internal radius comprises about 0.07 inches. 8. The avionics tray assembly of claim 1, wherein the seal assembly further comprises:a top portion; andan upper seal coupled to the top portion. 9. The avionics tray assembly of claim 8, wherein the upper seal can receive a line replaceable unit. 10. The avionics tray assembly of claim 1, wherein the seal assembly further comprises:a bottom portion; anda lower seal coupled to the bottom portion. 11. The avionics tray assembly of claim 1,wherein the tray detail further comprises a recessed area located substantially in a center of the tray detail;wherein the seal assembly further comprises:a bottom portion; anda lower seal coupled to the bottom portion; andwherein the lower seal can receive the recessed area. 12. An avionics tray assembly, comprising:a seal assembly, comprising:a metering plate detail;a plurality of tabs disposed along the metering plate detail;a plurality of location bosses disposed along the metering plate detail;a flange extending from the metering plate detail;a top portion;an upper seal coupled to the top portion;a bottom portion; anda lower seal coupled to the bottom portion; anda tray detail, comprising:a plurality of index bosses;a horizontal surface;at least one vertical surface;a recessed area; andan internal radius;wherein the internal radius supports an area of transition between the horizontal surface and the at least one vertical surface;wherein the recessed area further comprises a cutout; wherein the cutout receives the seal assembly;wherein the plurality of index bosses receive the plurality of location bosses;wherein the plurality of tabs secure the seal assembly to the tray detail; andwherein the flange secures the seal assembly to the horizontal surface. 13. The avionics tray assembly of claim 12, wherein the recessed area is located substantially in a center of the tray detail and wherein the recessed area is sunk to a minimum depth of about 0.05 inches. 14. The avionics tray assembly of claim 12, wherein the upper seal receives a line replaceable unit and wherein the lower seal receives the recessed area. 15. An avionics tray assembly, comprising:means for indexing a seal assembly of the tray assembly to a tray detail of the tray assembly;means for receiving the seal assembly, wherein the means for receiving is a cutout within a recessed area of the tray detail;means for supporting a line replaceable unit by the seal assembly; wherein the means for indexing, the means for receiving, and the means for supporting improve an alignment and engagement of the line replaceable unit with the tra y assembly; andwherein the means for indexing comprise a plurality of index bosses and a plurality of attachment tabs, wherein the plurality of index bosses receive a plurality of location bosses. 16. The avionics tray assembly of claim 15, wherein the means for supporting comprise a metering plate detail and a flange extending from the metering plate detail.
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이 특허에 인용된 특허 (10)
Whitson Frederick A. (Oconomowoc WI) Assef Carlos (Oak Creek WI), Avionic instrument tray cooling system.
Whitson Frederick A. (Oconomowoc WI) Siebert William K. (West Bend WI) Raihala Kenneth B. (Racine WI), Filter for mounting on an avionic line replaceable unit.
Dantin, Benoit; Senac, Serge; Guirado, Bernard; Pedoussaut, Philippe; Carrere, Sylvain, Support rack for at least one item of aircraft electronics, corresponding support device and aircraft.
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