Beverage service on an aircraft is usually accomplished by attendants who wheel beverage carts down the aisles of the plane, providing drinks to those passengers that request them. The challenge with most beverage carts used in today's aircraft is that these units are quite heavy and mobile, and in the event of turbulence or other aircraft movement these units can shift or even begin moving if not properly constrained, leading to a danger risk. Also, storing these carts when not in use requires that they be securely stationed, but easily and quickly released when needed. Accordingly, these carts are provided with immobilization systems that attempt to keep the beverage carts stationary when not in use but is easily disengaged when the cart needs to be released for serving the passengers.
In order to retain a catering cart within a commercial aircraft during normal service and in emergency conditions, carts are normally equipped with retraining devices commonly known as “turn buttons” that are deployed to secure the carts in place. The turn buttons are levers or handles that are rotated downward, causing the cart to engage with a lower surface of a work deck beam. However, turn buttons have inherent drawbacks in their design.
One disadvantage concerns the current trend towards the “air over” method of cart chilling that requires the cart bays to have doors. This means that the turn buttons have to be placed either on the outside of the doors or inside the doors. If placed outside the doors, there is a resultant increase in the depth of the galley when the carts are stored in the galley, and the turn buttons are visible to the observer, leading to a poor aesthetic appearance of the cart. There are also issues with ergonomics in having the turn button outside the doors. Alternatively, the turn buttons can be located on the inside of the bay doors, but this also leads to a resultant increase in the depth of a galley, and an increase in the work deck height. There are also potential cold bridge issues through the doors themselves, i.e., thermal losses resulting from conduction via the turn buttons. In this case, the doors are not normally used for retention (with the possible exception of cart kick-up loads), although additional door latching is required to secure the doors themselves.
To release the carts, both turn buttons need to be stowed which requires the use of both hands or a repeated single action, and there is no simultaneous “close-lock” operation available with this design in an emergency.
The present invention is a paddle latch that is integrated into an aircraft beverage cart bay door that acts as a brake actuator to secure the cart and its contents. The paddle latch comprises an actuator such as a paddle that rotates or pivots on a spindle and is coupled to an actuation fork. The actuation fork is connected to an articulating link that engages and moves a latch block. Movement of the paddle downward from its extended position to a vertical orientation rotates the fork upward, which in turn drives the link that extends the block. The latch features a manual release and can either be manually closed, or have the option of an automatic deadlock operation that results in a “close-lock” feature.
Other features and advantages of the present invention will become more apparent from the following detailed description of the preferred embodiments in conjunction with the accompanying drawings, which illustrate, by way of example, the operation of the invention.
In the galley of an aircraft, the bays that house the beverage carts are latched for convenience and safety. The present invention is a paddle latch assembly that is integrated into an aircraft beverage cart bay door 20 that also serves as a brake actuator to secure the cart and its contents. The paddle latch 10 comprises an actuator such as a paddle 22 that rotates or pivots on a spindle 24 as shown in
To open a secured latch 10, the paddle 22 is lifted to the open position (
In an alternative embodiment, the latch 10 is spring loaded to provide an automatic release of the latch block 30 on closure. This involves a spring that is compressed when the paddle is lifted (or placing a spring in tension) to positively lock the latch block in the withdrawn position. A toggle lock or similar device can be used to release the latch, and the movement of the latch block downward on closure of the door would release the toggle lock. This release would allow the latch blocks to be returned to the secure position by the spring, and the paddle itself would re-set automatically.
The present invention allows both latches 10 to be opened simultaneously with one hand and eliminates the need for a separate door handle (See
The latches 10 can be positioned centrally on the door, or offset to the side opposite the hinge. One benefit of the present invention is that the latch system may be integrated into the composite door 20, and is therefore isolated from the cold interior of a chilled compartment to eliminate the possibility of a thermal bridge (i.e., heat transfer resulting in thermal losses). Also, as the latch block receiver requirements are far less substantial, the work deck beam 34 can be removed and replaced with a composite structure within the lower forward section of the work deck. A composite structure is cheaper and lighter than the type of deck beams presently used.
Because the paddles 22 control a pair of latch blocks 32, the present invention allows one handed operation of both primary and secondary latches 10 simultaneously.
In addition, the latch can be manually operated or have a secure automatic deadlock action when engaged. Another advantage of the present invention is that the latch 10 is designed to be mounted with the cart bay door 20 as the means of cart retention, eliminating a work deck beam with a resulting saving in weight and elimination of the opportunity for a thermal bridge. The resulting bay door is both safer and more esthetically pleasing while eliminating many of the drawbacks of prior designs. Further, the present invention can be used on all types of narrow or wide bodied commercial aircraft monuments both for new and existing airplane types or variants.
While the foregoing description is intended to be illustrative, it should not be read as limiting the invention to any particular embodiment or embodiments depicted in the figures or described herein. Rather, one of ordinary skill in the art would understand and appreciate that various modifications are available and the present invention is intended to include all such modifications as would be understood and appreciated by the person of ordinary skill in the art.
This application claims priority from U.S. application No. 61/617,507, filed Mar. 29, 2012, the contents of which are fully incorporated herein by reference.
Number | Date | Country | |
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61617507 | Mar 2012 | US |