Abstract: The present disclosure relates to an animal ball. The animal ball includes a hollow sphere having a first half and a second half mate-able with said first half. The first half includes a first wall and a first rim and the second half also a second wall and a second rim. In addition, the animal ball includes a mating fastener including a first fastening portion and a second fastening portion. The first fastening portion is connected to the first wall and the second fastening portion is connected to the second wall and the first fastening portion is spaced from the first and second walls.

Abstract: A method and apparatus comprising a frame, a first linking system connected to the frame, and a second linking system connected to the frame. The frame may be configured to be connected to a support structure for an engine of an aircraft. The first linking system may be configured to be connected to a fan case in the engine. The second linking system is configured to be connected to an engine core case in the engine.

Abstract: Apparatus for control of vegetation having at least a part within a body of water such as a lake which includes a generally planar surface and a plurality of Ultra Violet Light-C (UV-C) light sources capable of producing UV-C light at substantially a wave length of 254 nm, the sources being disposed on the generally planar surface. The method for control of vegetation includes providing a generally planar surface, providing the plurality of UV-C light sources capable of producing UV-C light at substantially a wave length of 254 nm and positioning the sources on the generally planar surface, and positioning the generally planar member with the UV-C light sources within 12 inches of vegetation to be controlled, and exposing the vegetation to be controlled to the UV-C light sources for a finite period of time.

Abstract: The present invention is a variable geometry lighter-than-air (LTA) aircraft that is adapted to morph its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.

Abstract: An unmanned aerial vehicle (UAV) that can operate both as a conventional multicopter with no wing attached, or, it can operate as a winged multicopter. The detachable wing design used in the invention provides versatility without compromising performance; the wing attachment receptacles add no weight to the wingless multicopter configuration because they also function as the leg receptacles. In one embodiment, the base multicopter configuration is a quad-copter with four propeller drives. Four tubular receptacles, two forward and two aft, provide attachment points for the vertical struts of a detachable rectangular shaped wing, these vertical struts also function as the legs of the multicopter. The wing is fabricated using lightweight struts and rip stop nylon fabric which can be easily folded into a compact shape using quick release pins. In another embodiment, the wing is fabricated using a foam core.

Abstract: A glove has a separate finger section, a separate palm section, and a separate thumb section. The glove has a plurality of separate substrate sheets. Each substrate sheet has top and bottom surfaces. The separate finger section and the separate thumb section and the separate palm section adhesively receive and support at least one substrate sheet. A plurality of sticks are attached to each substrate sheet. A plurality of hooks are attached to each substrate sheet. The sticks are arched and the hooks are in an inverted J-shaped configuration.

Abstract: The present invention relates to a wing for an aircraft. The wing includes a main wing section extending from an inboard end to an outboard end along a lateral axis of the wing, the inboard end for connecting the main wing section to the aircraft. The wing also includes a wing tip having a proximal end and a distal end, the wing tip being rotatably mounted at the proximal end to the outboard end of the main wing section and arranged to freely rotate about a wing tip rotational center with respect to the main wing section.

Abstract: A plant watering device includes a first body portion, a second body portion having a chamber therein and connected to the bottom of the first body portion, a third body portion set on the top outer wall of the first body portion, and a water supplying tube which is inserted into one side of the third body portion, extending downwards along one side of the first and second body portions to the bottom of the second body portion and upwards along the opposite side of the second and first body portions, and out of the third body portion at the opposite side. Water is provided by the water supplying tube through a hole into the bottom of the chamber and its pressure is regulated using a micropore material block or a water-absorbent rod in the chamber, and a soft water-permeable disc at the bottom of the first body portion.

Abstract: Apparatus and method for joining composite structures of aircrafts are disclosed. An example apparatus includes an inboard composite wing panel having a first end portion configured to be coupled to upper and lower inboard fittings composed of a metallic material and an outboard composite wing panel having a first end portion configured to be coupled to upper and lower outboard fittings composed of a metallic material. A side of body rib has a plate shaped first end portion composed of a metallic material. A fuselage frame is configured to be joined at one end of the upper inboard fitting, and the upper and lower inboard fittings and the upper and lower outboard fittings are coupled to the side of body rib at the plate shaped first end portion.

Abstract: The foot snare triggering device of the present invention is designed to be used with a foot snare, and comprises a trigger plate assembly, having a tension adjustment means which allows the trigger plate assembly to pivotally yield to vertical pressure. A trigger mechanism has a trigger end set within said plate assembly and is attached to an extension mechanism providing a tandem extension spring configuration attached to a pair of pulleys, and a snare attachment port located within the trigger mechanism for releasably securing a foot snare by moving longitudinally when the trigger mechanism is engaged by pressure to said plate assembly allowing a foot snare to be released from the snare attachment port after triggering said device. A pan, pivotally connected to the plate underside distal to the pan tension adjustment means, has a trigger mount to engagingly receive the trigger mechanism.

Abstract: An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event between the drogue and probe. A positive coupling signal may serve to trigger a hose reel actuator to take up slack in the hose 16.

Abstract: A fishing lure having an internal cavity for containing a hook and a weight attached to the hook such that the weight is coupled to the hook closer to a throat of the hook than to a line receiving portion of the hook. The combined hook and weight resist being pulled through a shank containing region of lure. The weight may be positioned in a midsection of the lure enabling the lure to maintain a relatively level attitude in the water while being pulled through the water.

Abstract: A winglet attach fitting may include a wing attachment portion, an upper winglet attachment portion, and a lower winglet attachment portion. The upper winglet attachment portion may be coupled to the wing attachment portion and may be configured to support an upper winglet. The lower winglet attachment portion may be coupled to the wing attachment portion and may be configured to support a lower winglet. The wing attachment portion may be removably attachable to a wing tip using fasteners.

Abstract: A wing fold system may move a second portion of a wing with respect to a first portion of the wing between flight position 301 and folded position 303. A first link may rotate in response to actuating an actuator. A second link may move in response to rotating of the first link. The second portion of the wing may move in response to moving the second link and the second portion may move with respect to the first portion of the wing. One of the first portion and the second portion may be a fixed portion of the wing and the other of the first portion and the second portion may be a wingtip of the wing.

Abstract: A sinker or float that releasably clamps around a line, such as a fishing line, including two members shaped to define a channel for the line when in a closed position. A locking means is provided to releasably lock the two members in the closed position. Each of the members has at least a portion of high or low density material to provide a sinking or floating effect. A jacket may be provided that retains the high or low density material therein. The jacket may also include a hinge portion such that the two members can be hingedly opened and closed.

Abstract: An aircraft wing system for differentially adjusting a first deployable lift device and a second deployable lift device on a wing during take-off and landing, the system having a controller, which is programmed to determine desired positions for the first and second deployable lift devices, based on a desired position signal, and to activate high and low horsepower motors to move the first deployable lift devices to desired positions. The system has a controller which determines an adjustment amount for each motor, based on the system architecture.

Abstract: A method for attenuating aerodynamic noise from a landing gear may include researching a start point of a shear layer as a flow field characteristic of a region in the vicinity of an original shape of the landing gear, and adding a plate-shaped object in the vicinity of the start point, changing the start point to an edge portion of the plate-shaped object to make the shear layer farther from the original shape. Another method for attenuating aerodynamic noise from a landing gear may include researching a static pressure and an airflow velocity in a region in the vicinity of the landing gear as a flow field characteristic of the region, and adding a plate-shaped object covering a surface of the landing gear which is different from a surface facing an upstream side in an airflow direction, increasing the static pressure in the region to reduce the airflow velocity.

Abstract: The present invention is a fishing lure connector that traps a portion of fishing line inside a threaded male/female connection between a pole side base and a lure side base.

Abstract: A system for reducing a stopping distance of an aircraft may include an edge control system configured to control a leading edge device mounted to a wing of an aircraft. The edge control system may be configured to automatically command extension of the leading edge device from a first position to a second position in response to deployment of a spoiler if a ground speed of the aircraft is greater than a threshold ground speed.

Abstract: The present invention relates to a shot applicator device and, more particularly, to an automatic shot applicator device including a housing with a shot storage/delivery chamber, a tip structured to deliver the shot into tubing attached to various fishing tackle/equipment including fishing rigs, line, hooks, leaders, fly fishing tippet, and/or inserting directly into lures and baits, thereby changing the density (add or decrease weight) of the fishing tackle/equipment, and a mechanism structured to apply a force to the shot thrusting it through the tip and into such material.