This system is locked in place on the rails unless the flight attendant applies an appropriate downwards force to release the brake. If the flight attendant releases this downwards force the system will lock—similar to a dead mans brake.
The pivoting section hinge contains an up biased spring loading. This avoids the inadvertent dropping of the pivoting section should the closed position locking mechanism fail. It also allows flight attendants to lower the pivoting section safely and assist them closing this section too. In the event of severe turbulence the up-biased spring loading will be able to close the pivoting section to the up and locked position under it owns momentum. A lower position detent on the hinge will overcome the up spring bias when the pivoting section is lowered below an appropriate angle—depending on device size and application.
To lower the system a draw cord is used. This draw cord allows shorter flight attendants to reach the system while the aforementioned spring bias permits safe lowering of the pivoting section to the serving and moving positions. The use of a draw cord minimizes injuries that a hard lever could cause.
The draw cord would also activate the up and locked position latch or locking mechanism. If inadvertently operated the draw cord would not lower the pivoting section as the up-biased spring loading would hold the pivoting section in place—to lower the pivoting section would require concerted effort on the draw cord.
The meals would be stored on the pivoting section at an angle that minimized leaking of any liquids/juices from meals. The angle to which the pivoting section is lowered to is aircraft application dependant. The meals would sit horizontal when the pivoting section was lowered to the serving position. As the pivoting section is raised to the closed position the tray upon which the meals sit would remain fixed with respect to their mounted angle on the pivoting section and the meals would therefore also tilt from the horizontal position to an angle greater and horizontal but not exceeding 60 degrees.
A fluid drainage groove/spillage skirt runs would line the outer and lower rim of the pivoting section to capture and channel any liquid to a sump/bilge in the lower portion of the pivoting section. This would reduce the difficulty flight attendants currently have dispensing liquids during turbulence. These fluids are stored in an integral lower bilge for later cleaning if required.
The pivoting section would curve up on the edges in a concave manner to assist in food tray/drink security and prevent lateral food tray movement, this would also be integral to the spillage skirt. When closed this bathtub design would be able to secure extensive liquid spillage.
Other options to prevent lateral food tray movement when opened to the serving position would be through use of raised edges on each food tray or a cord running the length of the pivoting section on either side of the food trays.
The extreme lower end of the pivoting section would be a level serving and food preparation platform. This section could also mount a garbage bag underneath it to instantly separate food and other garbage from the trays as they are collected—a process currently not able to be completed on an airline wheeled cart.
A lifting flap or sliding flap in this platform would allow direct access to the top of the garbage bag through the base of the food preparation platform. This would allow for access to a large garbage bag at all phases of food/beverage delivery and collection without reducing space for food, beverages and utensils.
The level preparation area would house the handle used to move the system along the aisle.
When in the serving position the system is locked on the rails/tracks, the range of movement from the level, locked serving position to the lower moving position would be slight and dependant on aircraft and pivoting section size. The intention is to allow the preparation area to hold open beverages whilst the flight attendant moves the system along the aisle. The minor downwards force would release the brake and permit device travel without tilting so far down as to allow beverages to slide off the tray.
The food supporting trays house the airline meals, snacks or beverages. These supporting trays remain with the pivoting section and should not be confused with the trays given to the passenger. The supporting trays hold the passengers food tray. The supporting trays are held at a fixed angle so that they are horizontal when the pivoting section is lowered to the serving position. Upon delivery of the passenger meal of drink the supporting trays could be slid down an integral set of side rails to stack all trays at the lower end of the pivoting section. This requirement would be application dependant and would require two side rails running the length of the pivoting section and housing the small hinges of the food support trays. The trays could be held in place by a gravity lock or detent which would require the supporting tray to be lifted in order to slide it down to the lower end of the pivoting section.
The size and strength of the main pivot/hinge would minimize lateral movement—resulting in very little travel of the lower pivoting section sideways (towards the left and right side of the aisle). Much less lateral movement than current food carts.
If required a rubber seal on the pivoting section would reduce odor/aroma escaping from the stored meals.
One possible configuration includes power supplied to the invention through the rails to allow for an oven heating element. This would allow meals to be cooked overhead and free up valuable galley space current taken up by ovens.
Another variation of the design includes all design parameters claimed but mounts the pivoting section offset from the center aisle overhead the passenger baggage compartments. This variation allows all the same benefits of the center aisle design but utilizes the frame structure already in place above passenger luggage compartments in many aircraft. This variation would lower at an angle to the center aisle with a curved or angle arm to avoid passenger's heads. This variation is particularly suited to smaller domestic aircraft designed to serve beverages and snacks only. FOG 10 highlights this design.
If cooling was required the invention could be stored in a suitable position to engage ducting from the aircraft's air conditioning to keep beverages cool without requiring addition aircraft power.
Another embodiment of the invention shown in
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows:
Number | Date | Country | |
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60852117 | Oct 2006 | US |