Abstract: A modular unmanned aerial vehicle (UAV) having a fuselage, a nose cone, a left wing piece, a right wing piece, and a tail section. The tail section and nose cone each join to the fuselage through mating bulkhead structures that provide quick connection capability while being readily separated so as to enable the UAV to break apart at these connection points and thereby absorb or dissipate impact upon landing. The UAV is capable of rapid assembly in the field for two-man launch and data retrieval, as well as quick disassembly into these five component parts for transport and storage in a highly compact transport case that can be carried as a backpack.

Abstract: A pot cover that is comprised of detachable components and which can be used in combination with any conventional garden pot or any other suitable container, for purposes of facilitating the propagation of seedlings or seed germination, and which also resembles a novel animalian figure appearing to be living in the pot. The sections (02) and (04) of the pot cover connect together via clips (06) or other conventional connecting device to enable the sections to be easily connected and disconnected from each other and from the pot as required. The user would fill a pot with soil medium, and add seeds and water. Then connect the sections of the pot cover together, and then insert the connected sections of the pot cover into the upper rim of the pot, so that the pot cover sits securely on top of the pot, with the outside bottom edge (08) and (09) of the pot cover abutting the inner top rim of the pot.

Abstract: This invention relates to the design of a Modular Aerospace Plane (MAP) comprising a forward fuselage section, a main wing section, a tail section and wing attachments. Various sections can be integrated to offer a variety of aircraft characteristics, performance and missions. This modular design offers a new method of aircraft fabrication, maintenance, repair and ground handling to reduce costs for the manufacturers, owners and operators. The forward fuselage and tail sections may utilize a parachute device whereby these sections can separate in an emergency and safely lower the occupants to the ground.

Abstract: An improved seating apparatus for an aircraft comprising: a seat assembly and a positive lock device for securing the seat assembly to the aircraft. In the preferred embodiment, the positive lock device comprises: an adjustable force applicator for selectively applying force, a track fitting for insertion into an aircraft seat track, a rigid force bearer having a top region and for transferring force to an aircraft seat track, and a lock plate biased toward the applicator head. Also, in the preferred embodiment, the seat assembly includes a seat leg.

Abstract: A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways. In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.

Abstract: This invention is a servo mounting system, which allows a servo with a rotating output shaft to directly power an aircraft control surface. A specially designed servo mount securely positions the servo with the central axis of its rotational output shaft on, and axially aligned with, the hinge line of the control surface it drives. The servo shaft and servo body are directly connected to the airframe and control surface, thereby conserving rotational motion while driving control movement. Electronic means are then used to control the neutral point and the limit of travel of the servo. The system eliminates lost motion without generating adverse linear loads within the drive assembly.

Abstract: A device for feeding poultry kept in a barn, comprises at least one food supply tube (1) which is held above the floor of the barn such as to be able to be lowered or raised, with a series of branch openings, each provided with a dish device (2) hanging on the supply tube, comprising a dropping tube extending from the branch opening and a feeding dish (4) arranged below, the dropping tube with a spoked arrangement of lattice bars (5) forming the cup of the dish. The dropping tube comprises an inner cylinder (7) leading off from the branch opening and an outer cylinder (8) surrounding the inner cylinder, from which the dish hangs by means of the lattice bars, such as to be placed on the floor of the barn in the lowered state of the food supply tube. The outer cylinder runs on the inner cylinder such as to rotate, be raised or lowered and at least one stop is provided for limiting the raising and lowering stoke.

Abstract: Flaps, for example leading edge flaps and/or trailing edge flaps of an aircraft wing, are driven and adjusted by respective drive units. Drive shafts of neighboring flaps are coupled to each other by a differential gear. The differential gear is thus coupled to a main drive shaft which is driven by a main drive unit. Additionally, the differential gear is coupled to a secondary drive unit. The main drive power and the secondary drive power and thus the respective flap motions are super-imposable on each other, which permits operating the flaps independently of each other or in synchronism with each other.

Abstract: The invention concerns a device designed to be used in horse riding, consisting of a pivoting base provided with female fixing means so as to be secured to the rider's foot through a male fixing means attached on the sole of his shoes. The use of a single stirrup branch enables rapid release of the foot outwards. Said branch includes damping means so as to absorb part of the forces exerted on the stirrup by the rider's weight and thus avoid accidental release of the attachment. The automatic stirrup provides greater safety in case the rider falls by preventing the foot from being jammed through the use of a single branch prevents the rider from losing his stirrups as a result of the horse's sudden movements or loss of balance through the fixing means and dampens the rider's movements, particularly when jumping over an obstacle through its damper.

Abstract: Tethering stakes of the nature intended to be pounded flush with or below ground level. Certain of the tethering stakes include a cap on the pounding end which is adapted for ease of placement and release of a tethering line. Accordingly, the tethering line can be removed from the stake when it is to be pounded into the ground and then engaged with the stake only when tethering is desired. Certain of the embodiments include caps having uniquely shaped apertures for securing the tethering line. Another includes an aperture in communication with an aperture in the stake such that a lead cable or the like may be moved out of the way when the stake is pounded into the ground and may be fully received within the stake when tethering is not desired. Another embodiment employs a coupler passing through an aperture directly beneath the pounding surface to facilitate ease of attachment and removal of the tethering line.

Abstract: In a hog production plant the hogs are divided into a series of separate pens within the hog plant based generally on weight such that the lightest hogs closest to the initial weight are arranged in the first pen when the arrive and the heaviest hogs closest to the final market weight are arranged in the last pen. Each pen includes a sorting scale arranged to receive a hog therein and to weigh the hog for selection of one of two outlet paths leading to the next pen of the series or, in respect of the last pen, to a discharge location.

Abstract: A housing structure that includes a transparent opening in one wall thereof, the opening being covered with a transparent material such as PLEXIGLAS®. This opening allows a user to view the interior of the structure and ascertain the welfare of any animals within or check for pests without opening the birdhouse and risk frightening or harming the animals. In addition, the housing structure may also include a light within such that a user can illuminate the interior thereof. This allows the user to inspect the interior of the structure when it is too dark to do so without the help of an artificial light source. Moreover, the structure may include a removable roof or side wall for easy access to the interior of the birdhouse for the purpose of cleaning and the like, or access ports that may be used to access the structure without opening.

Abstract: A method and apparatus are disclosed for treating fuel to temporarily reduce its combustibility, and thereafter restore its combustibility. As used in an aircraft, the method comprises the following steps: (a) treating aircraft engine fuel to substantially reduce its combustibility in open air; (b) carrying the treated fuel in a fuel tank of an aircraft; (c) increasing the combustibility of a portion of the treated fuel, as needed by the aircraft engine; and (d) supplying the increased restored combustibility fuel to the aircraft engine. Using this method, the preponderance of the fuel on board the aircraft is maintained at low combustibility for safety.

Abstract: A bark control device (10) for deterring a dog from barking. The bark control device (10) includes a housing (12) carried by the dog, the housing having a vibration dampening surface (13) covering at least a portion of the exterior of the housing (12). The device (10) also includes a bark detection mechanism (18), a stimulus delivery system (26) for delivering a stimulus to the dog to dissuade the dog from barking, and circuitry (22, 24) for activating the stimulus delivery system (26) in response to the detection by the bark detection mechanism (18) of a bark by the dog. The vibration dampening surface (13) of the housing (12) inhibits the delivery of false correction stimuli to the dog as the result of vibrations emanating from a source other than a bark by the dog.

Abstract: A “wing in ground effect” aerial vehicle includes a wing mounted on a fuselage, and two cycloidal propulsion units for providing lift, thrust and longitudinal control. Additional lift is provided by a lighter-than-air gas such as helium contained in the fuselage. Operationally, the two cycloidal propulsion units and the volume of lighter-than-air gas are concertedly regulated to achieve “wing in ground effect” flight. Importantly, the two cycloidal propulsion units may operate in one of several modes, to include a curtate mode, a prolate mode, and a fixed-wing mode. Additionally, the vehicle may hover. Also, a thruster unit is mounted on the fuselage for providing forward thrust in combination with, or in lieu of, the two cycloidal propulsion units.

Abstract: A flexible electric bandage protector for use on a bandage or an animal. The protector comprising a flexible thin battery and a conductive layer disposed on one side of the battery. The conductive layer is in the form of two sets of conductive traces, the conductive traces not being conductively connected to each until touched by the mouth of the animal and wherein the battery has sufficient voltage to cause discomfort to the animal.

Abstract: A UAV capture system is disclosed. In the illustrative embodiment, the UAV capture system is coupled to the deck of a sea-faring vessel. The UAV capture system includes a single arresting line that is supported by a stanchion. In the illustrative embodiment, the stanchion is disposed on a rotatable boom.

Abstract: A fluid-structure interactive analysis is performed while n types of wing structure models are caused to flap in accordance with a prescribed model of flapping manner. Based on an analysis, data 1, data 2, . . . data n of physical values related to fluid behavior and physical values related to structural behavior are calculated. Among data 1, data 2, . . . data n, a data having a prescribed parameter such as the lift force optimized is extracted. A prototype of a wing portion is formed, which has such a structure that is specified by various parameter values of the numerical model of wing structure corresponding to the extracted data. A driving unit 905 drives the prototype of the wing portion in a manner of flapping that is represented by the flapping motion model equivalent to the manner of flapping of an insect. At this time, the wing has a stiffness that is suitable for flapping flight so that prescribed parameters come to have optimal values.

Abstract: Controllable refueling drogues and associated systems and methods are disclosed. A system in accordance with one embodiment includes a fuel delivery device having a deployable portion configured to be deployed overboard an aircraft during aerial refueling. The deployable portion can include at least a portion of a flexible fuel line, a drogue coupled to the flexible fuel line, and an actuatable device operatively coupled to at least one of the drogue and the fuel line. The deployable portion can further include a guidance system that is operatively coupled to the actuatable device and that includes instructions to direct the operation of the actuatable device and move the drogue during flight.

Abstract: A reentry vehicle includes a nose section, a modular section comprised of two or more connected modules, a flared section. The nose section is connected to a first end of the modular section, and the flared section is positioned proximate a second end of the modular cylindrical section.