Aircraft waste bin extractor
09567084 ยท 2017-02-14
Assignee
Inventors
Cpc classification
B65F1/1426
PERFORMING OPERATIONS; TRANSPORTING
B65F1/1468
PERFORMING OPERATIONS; TRANSPORTING
Y02T50/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
Abstract
An aircraft galley waste bin extraction unit is disclosed having a first compartment formed by a plurality of walls that conform with walls of the waste bin, an extraction chamber adjoining the first compartment and sharing a common wall, and a platform within the common wall including a hinged bottom edge that allows the platform to pivot into a horizontal position against a rest on an extraction chamber side wall, the deploying of the platform forming a window through which the waste bin can pass through from the first compartment to the extraction chamber. The unit preferably also includes retractable ramp extendable from the platform to a ground surface to guide the waste bin from the extraction unit to the ground.
Claims
1. An aircraft galley waste bin extraction unit comprising: a non-rectangular waste bin; a first compartment having a plurality of walls that conform with the non-rectangular waste bin; an extraction chamber adjoining the first compartment and sharing a common wall with the first compartment, and further including a side wall opposite the common wall and including a retractable projection; a platform within the common wall and pivoting about a lower edge from a vertical position to a horizontal position against the retractable projection, and a ramp extendable from the platform to a position outside of the extraction chamber.
2. The aircraft galley waste bin extraction unit of claim 1, wherein the ramp comprises a pair of rails that extend from within the platform.
3. The aircraft galley waste bin extraction unit of claim 2, wherein the ramp includes an upturned distal end when extended from the platform to stop the waste bin.
4. The aircraft galley waste bin extraction unit of claim 1, wherein the common wall includes tabs to retain the platform in the vertical position.
5. The aircraft galley waste bin extraction unit of claim 1, wherein the first compartment includes a ramp for directing the waste bin away from the common wall.
6. The aircraft galley waste bin extraction unit of claim 1, further comprising casters on a bottom surface of the non-rectangular waste bin that allow the bin to roll along a smooth horizontal surface.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
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(11) The compartment 24 includes a fifth wall 32 adjacent to the bin's main wall 12a that is also part of a larger secondary structure, namely an extraction chamber for extracting the bin 10. The wall 32 is formed with a draw bridge type swinging platform 50 that extends downward from the wall 32 as shown in
(12) When the platform 50 is lowered, the void in the wall 32 forms a window through which the bin 10 can pass through. The width of the window is sufficient to accommodate the waste bin 10 plus a few inches on each side. The fifth wall 32 can also include tabs 86 that maintain the platform in a vertical orientation, and can be rotated away from the platform to release the platform 50 so that it can rotate to its horizontal position. Other securing mechanisms can also be used to prevent the platform 50 from inadvertently dropping into the extraction compartment. To support the platform 50 and the bin 10, the side wall 62 of the extraction compartment may include supports 64 that can extend out of the wall, or alternative a ledge or dowel affixed to the side wall 62 will work to help stabilize the platform 50 and prevent it from bowing or dipping when the heavy bin 10 is transferred thereto.
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(14) The present invention can be modified in a number of ways, and one of ordinary skill in the art would readily understand and appreciate various modifications within the scope of the present invention. Thus, the scope of the present invention should not be limited to any depiction or description herein, but rather the scope of the invention should include all such modifications and alternate embodiments. Accordingly, the invention is limited only by the words of the appended claims, using the common and ordinary meanings of the words therein.