Abstract: Disclosed are multi-ply tissue products comprising a non-crosslinked binder that are durable and dispersible. The products generally have a Slosh time less than 2 minutes, such as less than about 60 seconds, such as less than about 45 seconds. Surprisingly, the foregoing Slosh times are achieved despite the tissue products having relatively high cross-machine direction (CD) wet tensile strength, such as greater than about 100 g/3?. Typically, increasing wet tensile strength, particularly wet CD tensile strength, negatively effects dispersability and increases Slosh time. Despite this trend, the present invention surprisingly provides a tissue product having a relatively high degree of wet strength and good dispersability.

Abstract: The creped multi-ply tissue products are durable, smooth and have low levels of Slough. In certain instances, the creped multi-ply tissue products are produced using a creping composition comprising a non-crosslinked latex polymer. The creped multi-ply tissue products may have a geometric mean tensile (GMT) from about 700 to about 1,500 g/3?, a basis weight from about 45 to about 60 gsm and a Slough less than about 2.00 mg, such as from about 0.10 to about 2.00 mg. The inventive tissue products also have good durability, such as a Durability Index from about 10.0 to about 20.0, smooth surfaces, such as a TS750 value from about 15.0 to 40.0 and low stiffness, such as a Stiffness Index less than about 10.0.

Abstract: A hygienic slow feeding bowl includes a container and a set of dividers disposed within said container. Each divider incorporates conic spikes extending away from one or two side surfaces of the divider. The side surfaces are flat or curved. The divider also includes a set of fasteners for attaching the divider to an inner wall of the container. The spaces between the dividers are adapted to receive pet food. The pet food rests on the bottom surface of the inner wall. The dividers can be removably attached to the inner wall. The container also includes a base and an outer wall extending upward from the base. The outer wall can be slanted or straight upward. The inner wall and the outer wall merge at a top edge forming a top opening of the cavity enclosed by the inner wall.

Abstract: Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a non-responsive component detector to determine a position difference between a first position of a first control surface of an aircraft and a second position of a second control surface of the aircraft, the first position lagging the second position, and a command generator, in response to determining that the position difference satisfies a threshold, the command generator is to cease movement of the second control surface at the second position, attempt to move the first control surface to the second position, and cease movement of the first control surface when moved to the second position.

Abstract: A hygienic slow feeding bowl includes a container and a set of dividers disposed within said container. Each divider incorporates conic spikes extending away from one or two side surfaces of the divider. The side surfaces are flat or curved. The divider also includes a set of fasteners for attaching the divider to an inner wall of the container. The spaces between the dividers are adapted to receive pet food. The pet food rests on the bottom surface of the inner wall. The dividers can be removably attached to the inner wall. The container also includes a base and an outer wall extending upward from the base. The outer wall can be slanted or straight upward. The inner wall and the outer wall merge at a top edge forming a top opening of the cavity enclosed by the inner wall.

Abstract: A hygienic pulling waste collector includes a frame with a leg, two frame arms coupled to the leg, a frame handle coupled to the leg, a rod coupled to the two frame arms, and two claws rotatably coupled to the rod and also attached to the two frame arms. The collector also includes a puller assembly having a puller handle, a puller frame, two puller arms coupled to the puller frame and attached to the two claws, and a spring coupled to the puller frame and the rod. The collector further includes a first locking member mounted to the leg, and a second locking member unevenly mounted to the rod. The puller frame is adapted to move inside the cavity disposed the leg. The first and second locking members each include a cover made of flexible material and incorporate a through cut.

Abstract: A method and apparatus for positioning a control surface. A desired position for the control surface associated with an aerodynamic aircraft structure is identified. The control surface is moved to the desired position using an electronically controlled rotary actuator system located inside of the aerodynamic aircraft structure, wherein a shape of the aerodynamic aircraft structure with the electronically controlled rotary actuator system has a desired aerodynamic performance.

Abstract: A waste collector comprises a handle assembly, a receptacle, a lid pivotally attached to the receptacle, a yoke operatively coupled to a shaft of the handle assembly, and a set of locking members. The yoke is pivotally attached to the receptacle. The lid incorporates a guiding channel for receiving the shaft. The receptacle incorporates a downward lip. A subset of the locking members is attached to walls of the receptacle and another subset of the locking members is attached to the yoke. Each locking member incorporates a set of through cuts. The set of through cuts creates a corresponding set of leaves. Each leave within the set is flexible and adapted to extend away from the corresponding locking member when a force is applied. When the force is released, the leaf intends to retain its original form.

Abstract: Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a non-responsive component detector to determine a position difference between a first position of a first control surface of an aircraft and a second position of a second control surface of the aircraft, the first position lagging the second position, and a command generator, in response to determining that the position difference satisfies a threshold, the command generator is to cease movement of the second control surface at the second position, attempt to move the first control surface to the second position, and cease movement of the first control surface when moved to the second position.

Abstract: A waste collector comprises a handle assembly, a receptacle, a lid pivotally attached to the receptacle, a yoke operatively coupled to a shaft of the handle assembly, and a set of locking members. The yoke is pivotally attached to the receptacle. The lid incorporates a guiding channel for receiving the shaft. The receptacle incorporates a downward lip. A subset of the locking members is attached to walls of the receptacle and another subset of the locking members is attached to the yoke. Each locking member incorporates a set of through cuts. The set of through cuts creates a corresponding set of leaves. Each leave within the set is flexible and adapted to extend away from the corresponding locking member when a force is applied. When the force is released, the leaf intends to retain its original form.

Abstract: Methods and apparatus for controlling aircraft flight control surfaces are disclosed. An example apparatus includes a flight control surface controller to move a control surface of an aircraft to a target position via at least one of a first actuator or a second actuator associated with the control surface based on a command input received by the flight control surface controller. The flight control surface controller to: obtain a flight characteristic of the aircraft; compare the flight characteristic to a flight characteristic threshold; in response to a first comparison result, cause the first actuator to move the control surface to the target position based on the command input without moving the second actuator; and in response to a second comparison result, cause the first actuator and the second actuator to move the control surface to the target position based on the command input.

Abstract: Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a collection engine to obtain first monitoring information corresponding to a first set of control surfaces of an aircraft, the first set including a first control surface on a first side of the aircraft and a second control surface on a second side of the aircraft, the second side opposite the first, and obtain second monitoring information corresponding to a second set of control surfaces of the aircraft, the second set including a third control surface on the first side and a fourth control surface on the second side.

Abstract: Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a collection engine to obtain first monitoring information corresponding to a first set of control surfaces of an aircraft, the first set including a first control surface on a first side of the aircraft and a second control surface on a second side of the aircraft, the second side opposite the first, and obtain second monitoring information corresponding to a second set of control surfaces of the aircraft, the second set including a third control surface on the first side and a fourth control surface on the second side.

Abstract: Methods and apparatus for controlling aircraft flight control surfaces are disclosed. An example apparatus includes a flight control surface controller to move a control surface of an aircraft to a target position via at least one of a first actuator or a second actuator associated with the control surface based on a command input received by the flight control surface controller. The flight control surface controller to: obtain a flight characteristic of the aircraft; compare the flight characteristic to a flight characteristic threshold; in response to a first comparison result, cause the first actuator to move the control surface to the target position based on the command input without moving the second actuator; and in response to a second comparison result, cause the first actuator and the second actuator to move the control surface to the target position based on the command input.

Abstract: A dust mop assembly is disclosed. The dust mop includes a mop head that comprises a top surface and a bottom surface. The bottom surface includes a dust gathering assembly, such as a reusable dust gathering pad or a plurality of dust gathering yarns. A deflector is coupled to the front of the mop head using any acceptable means. The deflector keeps dust and debris from being thrown over the dust mop while in use.

Abstract: A brush assembly comprises a top surface and a bottom surface. The bottom surface comprises a plurality of bristles extending substantially downward. The top surface includes a fitting to which a handle can be coupled as well as a wash port that can be coupled to a standard hose connection port. The wash port allows a user to easily wash the bottom of the brush head including the bristles.

Abstract: A lobby pan comprises a receptacle having a substantially flat bottom wall of a generally rectangular shape, a rear wall extending transversely from the bottom wall and having a first height, a front wall extending transversely from the bottom wall in substantially the same direction as the rear wall and having a second height that is less than the first height, and a pair of side walls that extend in the same direction as the rear wall and are connected to the rear wall and the front wall so as to form a continuous edge that defines an aperture into the receptacle. The front wall and rear wall are separated by a suitable distance, as are the side walls. In addition, a wash port is disposed on the exterior of the lobby pan so as to enable the interior of the receptacle to be easily washed.

Abstract: A method and apparatus for positioning a control surface. A desired position for the control surface associated with an aerodynamic aircraft structure is identified. The control surface is moved to the desired position using an electronically controlled rotary actuator system located inside of the aerodynamic aircraft structure, wherein a shape of the aerodynamic aircraft structure with the electronically controlled rotary actuator system has a desired aerodynamic performance.

Abstract: A system and methods for alleviating an anomaly in a structure are presented. At least one anomaly detector structural member is embedded in the structure. A measurement signal is sent to the anomaly detector structural member and a feedback signal is received from the anomaly detector structural member in response to the measurement signal. A difference between the measurement signal and the feedback signal is calculated to determine a change in the structure, and at least one non-optimal event is identified in real-time if the change exceeds an event threshold.

Abstract: A toy play set with multiple modes and a housing for a touchscreen portable electronic device includes a support structure, a first movable portion defining a housing configured to receive a portable electronic device, and a second movable portion. The first and second movable portions are rotatably coupled to the support structure and movable between a first configuration and a second configuration. In the first configuration, the first movable portion is in an upright orientation and in the second configuration the first movable portion is in a flat orientation. The portable electronic device is configured to provide different game modes depending at least upon the orientation of the first movable portion and the detection of certain toy objects thereon.