Abstract: A package including an outer box and inner tray. The inner tray slidable into and out of the outer box. The outer box including a first tab, a second tab, and a lip. The first and second tabs movable toward an interior of the outer box when force is applied. The inner tray including a first flap and a second flap, the first and second flaps movable toward an interior of the inner tray when force is applied. When the inner tray is slid into the outer box and the first and second tabs are in a first position, the first and second flaps are engaged with the lip and the inner tray is locked to the outer box. When the first and second tabs are in a second position the first and second flaps are disengaged with the lip and the inner tray is slideable out of the outer box.

Abstract: Systems and methods for identifying one or more points of interest in pipes or drain lines are described. Examples of points of interest include blockages caused by debris in the pipe or drain line. The systems are incorporated into drain cleaning machines. Also described are drain cleaning machines utilizing the systems.

Abstract: A pressure bulkhead assembly for an aircraft includes an aft pressure bulkhead and a plurality of splice angles. The aft pressure bulkhead includes a bulkhead interface surface and aft-pressure-bulkhead holes, pre-drilled through the bulkhead interface surface. The plurality of splice angles is configured to be coupled to the aft pressure bulkhead. Each one of the plurality of splice angles includes a flange surface, configured to mate with the bulkhead interface surface. Each one of the plurality of splice angles also includes splice-angle holes, drilled through the flange surface. Each one of the plurality of splice angles further includes a splice surface, extending from the flange surface. With the splice-angle holes aligned with the aft-pressure-bulkhead holes, a plurality of splice surfaces forms a circumferential splice surface with an optimized shape.

Abstract: A method for making a pressure bulkhead assembly of an aircraft includes determining first locations and first orientations of a plurality of first holes, pre-drilled in an aft pressure bulkhead. The method also includes determining a first surface profile of a first interface surface of the aft pressure bulkhead and determining a second surface profile of a second interface surface of each one of a plurality of splice angles. The method also includes determining second locations and second orientations of a plurality of second holes to be drilled in each one of the plurality of splice angles corresponding to the plurality of first holes in the aft pressure bulkhead and drilling the plurality of second holes in each one of the plurality of splice angles at the second locations and second orientations.

Abstract: A method of making a pressure bulkhead assembly of an aircraft includes determining an optimized position of splice angles such that splice surfaces of the splice angles will form a circumferential splice surface of the pressure bulkhead assembly with an optimized shape. The method further includes performing a virtual fit between the plurality of splice angles, at the optimized position, and an aft pressure bulkhead. The method also includes determining splice-angle-hole positions of splice-angle holes to be drilled in each one of the splice angles such that the splice-angle holes will correspond to aft-pressure-bulkhead holes, pre-drilled in the aft pressure bulkhead. The method further includes drilling the splice-angle holes in each one of the splice angles at the splice-angle-hole positions. The method also includes joining each one of the splice angles with the aft pressure bulkhead such that the splice surfaces form the circumferential splice surface with the optimized shape.

Abstract: A method for dynamically scoring aspects of a data object includes receiving a first data object indicating and determining a first sum of a product of a first value and a first weight value plus a product of a second value and a second weight value and generating a first score based on a result of the first sum. The method also includes determining a second sum of a product of a third value and a third weight value plus a product of a fourth value and a fourth weight value and generating a second score based on a result of the second sum. The method also includes determining a first data object score for the first data object based on, at least, the first score, the second score, and a fifth value.

Abstract: A method includes identifying all possible data object combinations for at least some of a plurality of data objects and determining a total score value for each data object combination. The method also includes applying a mutation variable to a first set of data object combinations. The method also includes selecting at least two data object combinations of the first set of data object combinations after application of the mutation variable and identifying data objects that appear in each of the at least two data object combinations. The method also includes generating a second set of data object combinations using the data objects that appear in each of the at least two data object combinations and each possible combination of data objects that do not appear in at least one data object combination of the at least two data object combinations.

Abstract: A method of making a pressure bulkhead assembly of an aircraft includes determining an optimized position of splice angles such that splice surfaces of the splice angles will form a circumferential splice surface of the pressure bulkhead assembly with an optimized shape. The method further includes performing a virtual fit between the plurality of splice angles, at the optimized position, and an aft pressure bulkhead. The method also includes determining splice-angle-hole positions of splice-angle holes to be drilled in each one of the splice angles such that the splice-angle holes will correspond to aft-pressure-bulkhead holes, pre-drilled in the aft pressure bulkhead. The method further includes drilling the splice-angle holes in each one of the splice angles at the splice-angle-hole positions. The method also includes joining each one of the splice angles with the aft pressure bulkhead such that the splice surfaces form the circumferential splice surface with the optimized shape.

Abstract: A method for making a pressure bulkhead assembly of an aircraft includes determining first locations and first orientations of a plurality of first holes, pre-drilled in an aft pressure bulkhead. The method also includes determining a first surface profile of a first interface surface of the aft pressure bulkhead and determining a second surface profile of a second interface surface of each one of a plurality of splice angles. The method also includes determining second locations and second orientations of a plurality of second holes to be drilled in each one of the plurality of splice angles corresponding to the plurality of first holes in the aft pressure bulkhead and drilling the plurality of second holes in each one of the plurality of splice angles at the second locations and second orientations.

Abstract: A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structu

Abstract: A smart power center is for use in controlling DC power in mobile living quarters, such as an RV, and has switched outputs that are controlled using a mobile device, such as smartphone or tablet. The switched outputs connect DC power from a DC power source to an accessory, such as a light, fan, or motor. Some accessories, such as landing gear or slide-out rooms, require the polarity from the power source to be reversed for proper function. These are connected to reversing outputs which connect DC power from the DC power source in one orientation for one direction and a reversed orientation for the other direction. Smart override switches can be wired to the smart power center in the event the user desires to control the switched outputs without the mobile device.

Abstract: A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structu

Abstract: A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structu

Abstract: A system for measuring a flushness of a fastener in a surface includes a plurality of lights configured to illuminate the fastener and the surface. The system also includes a camera configured to capture a plurality of images of the fastener and the surface while the lights sequentially illuminate the fastener and the surface. The system also includes a computing system configured to determine a normal map of the fastener and the surface based at least partially upon the images, determine a depth map of the fastener and the surface based at least partially upon the normal map, and determine the flushness of the fastener with respect to the surface based at least partially upon the depth map.

Abstract: A system for measuring a flushness of a fastener in a surface includes a plurality of lights configured to illuminate the fastener and the surface. The system also includes a camera configured to capture a plurality of images of the fastener and the surface while the lights sequentially illuminate the fastener and the surface. The system also includes a computing system configured to determine a normal map of the fastener and the surface based at least partially upon the images, determine a depth map of the fastener and the surface based at least partially upon the normal map, and determine the flushness of the fastener with respect to the surface based at least partially upon the depth map.

Abstract: Methods for using predictive shimming to optimize part-to-part alignment. In accordance with one embodiment, the process uses measurement data acquired from mating surfaces and key features to virtually align two parts in a manner that optimizes the final orientation of the parts and determines the geometry of the shim needed to achieve this orientation during assembly.

Abstract: A system for inhibiting operation of a vehicle-based device while the vehicle is in motion includes a motion sensor, a timer, and a time delay override switch in communication with a control circuit. The control circuit selectively outputs one or more enable and/or inhibit signals based on the states of the motion sensor and timer. The time delay override switch can be actuated to place the timer into a timed out state from a timing state.

Abstract: Systems and methods are provided for placing non-destructive marks onto a part via an end effector of a robot. One embodiment is a system comprising an end effector of a robot. The end effector includes an extendable punch that places targets onto a part, and supports that hold a strip of reflective adhesive tape between the punch and the part. Extending the punch cuts out a target from the strip and applies an adhesive side of the target to the part, and retracting the punch leaves a reflective side of the target visible on the part.

Abstract: A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structu

Abstract: Systems and methods are provided for placing non-destructive marks onto a part via an end effector of a robot. One embodiment is a system comprising an end effector of a robot. The end effector includes an extendable punch that places targets onto a part, and supports that hold a strip of reflective adhesive tape between the punch and the part. Extending the punch cuts out a target from the strip and applies an adhesive side of the target to the part, and retracting the punch leaves a reflective side of the target visible on the part.