Patent Application
20200339262
Aircraft galley structures may incorporate cart compartments and cart bays configured for temporary storage of galley carts (e.g., service carts, trolleys). Cart bays may be configured to store galley carts while minimizing the space they occupy, e.g., the inner dimensions of a cart bay may be as compact as possible. Galley carts may include wheels on casters mounted to their undersides, via which the galley carts may be inserted into their respective cart bays for secure storage (e.g., during taxi, takeoff and landing segments). The galley carts may similarly be removed from their bays for in-seat catering or food service, via which the carts may be transported along aircraft aisles and ultimately returned to their bays. The entry and exit of a galley cart into its cart bay may be guided by rubstrips or similar barriers on the walls of the cart bay.
The casters of the galley carts are designed to allow full 360-degree rotation by the cart wheels. When a galley cart is inserted into a cart bay, its caster wheels will all be oriented in the same direction, e.g., toward the back of the cart bay. When the galley cart is next removed from the cart bay, the initial reaction of the underside casters is to rotate the wheels 180 degrees to face the opposite direction. As the cart bay is too narrow to accommodate a full rotation, the result may be a caster or wheel rotation into the cart bay wall (or into a nearby rubstrip) at an angle associated with a binding or jamming of the wheel into the rubstrip. This binding or jamming action may significantly increase the force required to remove a galley cart from its cart bay. As multiple galley carts may be removed from, and reinserted into, their cart bays multiple times during the course of a normal flight, the cumulative additional force may vastly increase the workload for flight attendants and cabin crew. Further, random damage due to wheel binding or jamming may increase wear and tear on the sidewalls and rubstrips of the galley cart bays as well as the galley carts themselves.
A galley cart compartment is disclosed. In embodiments, the galley cart compartment includes an interior compartment (e.g., interior space) of an aircraft galley complex (galley structure, galley monument). The interior compartment includes left and right sidewalls and a floor, which may be the cabin floor. The interior compartment is capable of receiving a galley cart (e.g., trolley) insertable into, and removable from, the interior compartment along an axis of entry (e.g., parallel to the depth of the interior compartment). The galley cart has an outer housing with left and right sides and an underside, to which casters are pivotably or rotatably attached on the left and right sides. Each caster has a left and right (inside and outside) wheel, the two wheels separated by an interior wheel gap or space. Tracks extend along the cabin floor parallel to the axis of entry (e.g., from the front to the rear of the interior compartment), a left track and a right track positioned to engage respectively with the left-side and right-side casters. Each track includes a guide rail capable of partially extending into the wheel gap, preventing the caster wheels from laterally rotating when the galley cart is first removed from the interior compartment.
A galley cart wheel track system is also disclosed. In embodiments, the galley cart wheel track system includes a galley cart compartment (e.g., of a galley complex or galley monument) having two or more adjacent cart bays. Each cart bay is adjacent to a compartment wall (e.g., a compartment may include a left bay adjacent to the left inside wall and a right bay adjacent to the right inside wall). Each cart bay can accommodate a galley cart insertable into, and removable from, the cart bay along an axis of entry (e.g., parallel to the depth of the cart bay). Each galley cart has an outer housing including an outside face adjacent to the compartment wall, an inside wall opposite the outside wall, and an underside. Casters are attached to the underside of each galley cart on the inside and outside (e.g., the sides respectively closest to and farthest from the compartment wall), each caster having a left wheel and a right wheel separated by a wheel gap. Each cart bay includes a floor, which may be the galley floor, along with a track extends, parallel to the axis of entry and close to the compartment wall. The track includes a guide rail capable of extending into the wheel gaps of the set of casters closest to the compartment wall and preventing the casters from laterally rotating when the galley carts are removed from the cart bays.
This Summary is provided solely as an introduction to subject matter that is fully described in the Detailed Description and Drawings. The Summary should not be considered to describe essential features nor be used to determine the scope of the Claims. Moreover, it is to be understood that both the foregoing Summary and the following Detailed Description are example and explanatory only and are not necessarily restrictive of the subject matter claimed.
The detailed description is described with reference to the accompanying figures. The use of the same reference numbers in different instances in the description and the figures may indicate similar or identical items. Various embodiments or examples (“examples”) of the present disclosure are disclosed in the following detailed description and the accompanying drawings. The drawings are not necessarily to scale. In general, operations of disclosed processes may be performed in an arbitrary order, unless otherwise provided in the claims. In the drawings:
Before explaining one or more embodiments of the disclosure in detail, it is to be understood that the embodiments are not limited in their application to the details of construction and the arrangement of the components or steps or methodologies set forth in the following description or illustrated in the drawings. In the following detailed description of embodiments, numerous specific details may be set forth in order to provide a more thorough understanding of the disclosure. However, it will be apparent to one of ordinary skill in the art having the benefit of the instant disclosure that the embodiments disclosed herein may be practiced without some of these specific details. In other instances, well-known features may not be described in detail to avoid unnecessarily complicating the instant disclosure.
As used herein a letter following a reference numeral is intended to reference an embodiment of the feature or element that may be similar, but not necessarily identical, to a previously described element or feature bearing the same reference numeral (e.g., 1, 1a, 1b). Such shorthand notations are used for purposes of convenience only and should not be construed to limit the disclosure in any way unless expressly stated to the contrary.
Further, unless expressly stated to the contrary, “or” refers to an inclusive or and not to an exclusive or. For example, a condition A or B is satisfied by anyone of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present).
In addition, use of “a” or “an” may be employed to describe elements and components of embodiments disclosed herein. This is done merely for convenience and “a” and “an” are intended to include “one” or “at least one,” and the singular also includes the plural unless it is obvious that it is meant otherwise.
Finally, as used herein any reference to “one embodiment” or “some embodiments” means that a particular element, feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment disclosed herein. The appearances of the phrase “in some embodiments” in various places in the specification are not necessarily all referring to the same embodiment, and embodiments may include one or more of the features expressly described or inherently present herein, or any combination of sub-combination of two or more such features, along with any other features which may not necessarily be expressly described or inherently present in the instant disclosure.
A cart wheel track system for cart compartments (e.g., cart bays) is disclosed. The cart bays may be incorporated into aircraft galley configurations, e.g., galley structures, galley monuments, or structures otherwise mounted in an aircraft passenger cabin and incorporating cart bays. Guide rails on the floor of the cart bays prevent the cart wheels from rotating on removal from the bay, facilitating easy removal of the cart. Further, the guide rails may assist in the smooth return of the cart to its bay, preventing unnecessary impact with the compartment sidewalls or rubstrips attached thereto.
Referring to
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In embodiments, each track 110 may be set into the floor 134 of the galley cart compartment 100a (which floor may be the galley floor or the floor of the passenger cabin). The tracks 110 may be set into the floor 134 by bolting, fastening, adhering, or any other appropriate means for securing the guide rails to the floor in the desired alignment.
In embodiments, the tracks 110 may include guide rails 136 extending upward into the wheel gap 132 between the inside and outside wheels 126, 128 such that, when a crewmember initiates the removal of the galley cart 102a from the galley cart compartment 100a into which the galley cart is fully inserted (e.g., by pulling outward, substantially parallel to the axis of entry (122,
Referring to
In embodiments, the left cart bay 202 may be adjacent to a left compartment wall 206 of the galley cart compartment 100b while the right cart bay 204 is adjacent to a right compartment wall 208 of the galley cart compartment. The left and right cart bays 202, 204 may be separated by a central partition 210 which may assist in guiding the respective galley carts 102a-b into, and out of, their respective left and right cart bays (e.g., parallel to the axis of entry 122).
In embodiments, the left cart bay 202 may incorporate a left-side track 110a proximate to the left compartment wall 206 and positioned to engage with the wheel gaps 136 of the left-side casters 118 of the galley cart 102a. Similarly, the right cart bay 204 may incorporate a right-side track 110b proximate to the right compartment wall 208 and positioned to engage with the wheel gaps 132 of the right-side casters 120 of the galley cart 102b.
Referring to
In some embodiments, the left and right tracks 110a-b may extend along the cabin floor 134 of the galley cart compartment 100c for a sufficient length that the galley cart compartment 100c may accommodate, in front of the galley carts 102a-b, a second row of galley carts (102c). For example, the galley carts 102a-b may be inserted into the galley cart compartment 100c and guided along straight paths by the left and right tracks 110a-b and the central partition 210 to the rear of the galley cart compartment 100c. Flight attendants and cabin crew may then be able to insert the second galley cart 102c into the galley cart compartment 100c (e.g., guided by the left track 110a and central partition 210). In some embodiments, the galley cart compartment 100c may be equipped with any appropriate means of removing the galley carts 102a-b from the rear of the galley cart compartment once the galley cart 102c is removed.
Referring to
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In some embodiments, the mount 602 may be attached or mounted to the lower left rubstrip 108, and the rubstrip in turn mounted to the left compartment wall 206. In some embodiments, the left track 110a and the left rubstrip 108 may be incorporated into a single mount 602 attachable or mountable to the left compartment wall 206. In embodiments, the right track (110b,
It is to be understood that embodiments of the methods disclosed herein may include one or more of the steps described herein. Further, such steps may be carried out in any desired order and two or more of the steps may be carried out simultaneously with one another. Two or more of the steps disclosed herein may be combined in a single step, and in some embodiments, one or more of the steps may be carried out as two or more sub-steps. Further, other steps or sub-steps may be carried in addition to, or as substitutes to one or more of the steps disclosed herein.
Although inventive concepts have been described with reference to the embodiments illustrated in the attached drawing figures, equivalents may be employed and substitutions made herein without departing from the scope of the claims. Components illustrated and described herein are merely examples of a system/device and components that may be used to implement embodiments of the inventive concepts and may be replaced with other devices and components without departing from the scope of the claims. Furthermore, any dimensions, degrees, and/or numerical ranges provided herein are to be understood as non-limiting examples unless otherwise specified in the claims.
