Patent application number | Description | Published |
20140352132 | SYSTEM AND METHOD FOR MOUNTING UNDERCABINET VENTILATION HOOD - A ventilation hood is mounted to an underside of a cabinet, including a bottom panel and a lower support frame positioned above a cooking appliance, by first and second brackets secured below the cabinet at spaced positions aligned with outermost edge portions of the lower support frame and at least one fastener assembly secured to a front portion of the ventilation hood. Multiple embodiments are disclosed for the at least one fastener assembly, including tabs bent from a housing of the ventilation hood, feet threadably attached to the hood, mounting blocks including snap connectors, threaded fasteners, and pinned bolts. | 12-04-2014 |
20140352151 | SYSTEM AND METHOD FOR MOUNTING UNDERCABINET VENTILATION HOOD - A method for installing a ventilation hood to an underside of a wall cabinet including providing a ventilation hood having a housing, a removable utility structure with an aligning mechanism and at least one hanger stud. The removable utility structure is placed proximate the wall cabinet in at least one measuring position, wherein the aligning mechanism of the removable utility structure locates anchorage points of the ventilation hood. Hanger studs are secured in the anchorage points. The removable utility structure is secured to the housing in a structural position at least partially covering an electrical system of the ventilation hood. The housing is placed on the hanger studs to secure the ventilation hood proximate the wall cabinet. Electrical power is connected to the electrical system while the housing is secured on the hanger studs. The housing of the ventilation hood is then secured to the wall cabinet. | 12-04-2014 |
20150047198 | SYSTEM AND METHOD FOR MOUNTING UNDERCABINET VENTILATION HOOD - A ventilation hood is mounted to an underside of a cabinet by left and right support brackets each including a main body from which depend at least one support tab or hanger, as well as a locator tab. The main body is aligned on the cabinet, while the locator tab appropriately spaces the support bracket from an upstanding rear wall. Thereafter, the ventilation hood is positioned so the support tabs are received in slots formed in a top panel of the hood and, upon sliding the hood rearward, the hood rides upon ramped or tapered surfaces of the support tabs to position the hood against the cabinet while hanging the hood from the support tabs. Thereafter, the support tabs are bent to retain the ventilation hood in an operational position. Employing the distinct aligning, positioning and hanging structure enables a single person to readily mount the ventilation hood. | 02-19-2015 |
Patent application number | Description | Published |
20080319719 | METHODS AND SYSTEMS FOR DISPLAYING NETWORK INFORMATION - Methods and systems for displaying a network structure using force-directed layout are provided. The network includes a plurality of nodes, each node including an associated slack parameter having a value. The method including selecting a central time-directed axis, positioning each network node along the axis using the associated slack parameter value of the network node to determine a distance from the central time-directed axis, and applying force-directed computations to sets of concurrent nodes. | 12-25-2008 |
20090006293 | METHODS AND SYSTEMS FOR SCALABLE HIERARCHICAL FEED-FORWARD PROCESSES - Methods and systems for constructing a scalable feed-forward process are provided. The method includes identifying a plurality of segments of the process wherein the segments define a feed-forward network which is used to constrain the creation of more detailed segment components. The method also includes modeling each component by defining component outputs and determining component inputs that are combinable using the model to produce the defined output, ordering the components hierarchically based on the respective component outputs and inputs, determining segment inputs and outputs based on the component outputs and inputs, and ordering the segments hierarchically based on the respective segment outputs and inputs. | 01-01-2009 |
20140222487 | Total-Ordering In Process Planning - A method is provided that includes receiving process-related information describing a hierarchical process for production of a product. The process may include segments each of at least some of which include segment components. The method also includes determining an instance in which the segment components are total-ordered, which may include determining an instance in which the segments are total-ordered. For the total-ordered segments, the segment components may be partitioned by disjoint collections based upon earliest availability to produce earliest-available partitions, and separately based upon latest availability to produce latest-available partitions. Order flexibility may be identified for each segment component based upon membership in both earliest-available and latest-available partitions, and an instance in which each partition in both the earliest-available and latest-available partitions contains only one order-inflexible segment component may be determined. In this instance, the segment components may be total-ordered. | 08-07-2014 |
20140222492 | Alpha-Chain Constraints For Process Planning - A method is provided that includes receiving process-related information describing a process for production of a product, including a logical sequence of tasks to produce respective internal products of the process. The method also includes constructing a schedule for the process based on the process-related information, with the process schedule being for execution of at least some of the tasks each of which utilizes or requires inputs including temporally a last input. Construction of the process schedule includes separating each of at least some of the respective tasks into a closure portion that requires availability of the last input of its task before being initiated, and a distinct precursor portion capable of being initiated before the respective last input is available. The closure portions of the respective tasks may be temporally sequenced without intervening precursor portions, and the precursor portions may be prepended to respective, temporally-sequenced closure portions. | 08-07-2014 |
20140236651 | Display of Process-Plan Execution - A method is provided that includes receiving a plan model for a process including a plurality of tasks, and generating a layout including a network diagram that expresses the plan model. The method also includes simulating execution of the plan model, and dynamically updating the network diagram to reflect an actual task duration tracked for each task during the simulation. The network diagram includes along a time-directed axis, a plurality of task nodes that express respective tasks, with each task node being expressed as a first multi-dimensional shape having an outline with a dimension along the axis sized according to a task duration for a respective task. In the updated network diagram, then, each task node further includes a fill in the same first multi-dimensional shape as the respective outline but with a dimension along the axis sized according to the actual task duration of the respective task. | 08-21-2014 |
Patent application number | Description | Published |
20080226869 | METHODS OF JOINING STRUCTURES AND JOINTS FORMED THEREBY - A product including a first structure. A joint element is attached to the first structure. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive. | 09-18-2008 |
20090142130 | DOUBLE SHEAR JOINT FOR BONDING IN STRUCTURAL APPLICATIONS - Embodiments of methods and apparatus for providing a double shear joint for bonding in structural applications are disclosed. In one embodiment, a bonded composite joint includes a base having a foot configured to couple to a member, the base including a flange extending outward from the foot. The joint further includes a panel having a core configured between opposing skins, the skins having inner walls proximate the core, the skins extending outward beyond the core on at least one end of the panel to define a recess between the skins, the recess configured to receive the flange. A bonding agent is used to couple the flange to the inner walls of the panel. | 06-04-2009 |
20090208701 | JOINTS FORMED BY JOINING STRUCTURES - A joint is formed by joining two structures using a joint element. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. The joint element is attached to the first structure. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive. | 08-20-2009 |
20100230042 | Double Shear Joint For Bonding in Structural Applications - A bonded composite joint may include a base having a foot configured to couple to a member. The base may include a flange extending outward from the foot. The joint further may include a panel having a core positioned between opposing skins, where the skins have inner walls proximate the core and the skins extend outward beyond the core on at least one end of the panel to define a recess between the skins. The recess between the skins may receive the flange. A bonding agent may be used to couple the flange to the inner walls of the panel. | 09-16-2010 |
Patent application number | Description | Published |
20120180942 | Composite Sections for Aircraft Fuselages and Other Structures and Methods and Systems for Manufacturing Such Sections - Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure. | 07-19-2012 |
20130037217 | COMPOSITE SECTIONS FOR AIRCRAFT FUSELAGES AND OTHER STRUCTURES, AND METHODS AND SYSTEMS FOR MANUFACTURING SUCH SECTIONS - Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure. | 02-14-2013 |
20130040008 | Composite Sections for Aircraft Fuselages and Other Structures, and Methods and Systems for Manufacturing Such Sections - Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure. | 02-14-2013 |