Abstract: A boat comprising a wake shaping system comprising starboard and port wake shaping devices located aft of the transom. Each wake shaping device is operable to move between a first, non-deployed position behind the transom and a second, deployed position extending outside the side of the hull or below the transom. When the starboard wake shaping device is in the deployed position, a port wakesurf wake is created. When the port of the wake shaping device is in the deployed position, a starboard wakesurf wake is created. When neither wake shaping device is deployed, a symmetrical wakeboard wake is created.

Abstract: A jet boat includes a cockpit arranged in a central portion of the jet boat on a boat body centerline, a bulwark provided along a circumference of a deck, and a platform fixed to a stern. In the bulwark, the upper surface of a rear bulwark between the platform and the cockpit is located above the upper surface of a foot space and below the seating surface of a seat.

Abstract: A method and structure for mooring seaworthy craft against boat landings is disclosed. The structure comprises a fender (4) with a layer of compressible material having an exposed surface, mounted on the craft. Anchor points (12) are secured at laterally spaced locations on the craft, as are two draw mechanisms (14), one associated with each anchor point (12). A tie (10) is provided for extending from each anchor point (12) to its associated draw mechanism (14), and each mechanism is operable to draw its respective tie from an anchor point around a pylon thereby urging the fender (4) against both pylons. In the mooring process, the craft is first steered to the boat landing to engage the fender (4) against the pylons (6), and the ties (10) are withdrawn from each draw mechanism (14) and taken around one of the pylons. Each tie is then attached to an anchor point (12) on the craft, and the mechanisms (14) are activated to draw the ties (10) around the pylons to urge the fender (4) against them.

Abstract: A cylindrical receiver has an upper region with female screw threads, a lower region, and a centrally located washer. A cylindrical sleeve has an upper end with male screw threads threadedly coupled to the female screw threads of the receiver. A cylindrical passageway is formed between the receiver and the sleeve. A cylindrical stake is slidably received in the sleeve. A tether line couples the stake to a movable patch whereby when the movable patch is coupled to a fixed patch, the stake will be in a raised orientation and whereby when a user separates the movable patch from the fixed patch, the weight of the stake will lower the stake into a lower orientation into a sandy or rocky bottom.

Abstract: Device, system and method for protecting towed marine survey equipment from line entanglement are provided. A cutter device has a mounting mechanism configured to fixedly attach at a predetermined position along a cable used for towing, and one or more cutting structures. The cutting structures are attached to and extend away from the mounting mechanism, being configured to cut lines that get caught by the cutting structures or slide along the cable to the predetermined position.

Abstract: A pop up storage system for a boat having an opening formed in a deck includes a cabinet beneath the opening in the deck. A drawer is mounted for vertical sliding movement into and out of the cabinet and defines a storage compartment movable between an open position and a closed position. A motion assistance arrangement extends between the cabinet and the drawer, and is configured for assisting in movement of the drawer relative to the cabinet between a raised position and a lowered position.

Abstract: A buoyant element includes an elongate buoyant body that defines: (i) a major side; (ii) a minor side that is parallel to the major side; (iii) axial ends connecting the major and minor sides at an angle of substantially 45° from the orthogonal spanning the major and minor sides; and (iv) means for connecting adjacent buoyant elements together. The length of the major side is twice the length of the minor side.

Abstract: An offshore drilling vessel includes a main deck, a moonpool a firing line hoist system having a tower, a BOP transport system and a pivotally supported U-shaped working deck. The U-shaped working deck can be pivoted between an active position, in which it extends in a substantially horizontal direction such that it covers a portion of the moonpool, and a non-active position, in which it extends in a substantially vertical direction such that it provides room for a BOP to be moved by the BOP transport system from a storage position adjacent the moonpool into a launch position above the moonpool, in which launch position the BOP is located between the tower and the working deck.

Abstract: An offshore floating support apparatus includes an underwater base, an anchor unit and a plurality of supporting units. The anchor unit is connected to the underwater base and is adapted to be attached to a water bed. The supporting units are connected to and surround the underwater base. Each of the supporting units has a support member that defines a receiving space for receiving water therein and that has a valve component operable to establish fluid communication between the receiving space and external environment for adjusting quantity of water received in the support member.

Abstract: A pontoon cleaning assembly for cleaning floats on a pontoon boat includes a handle that may be manipulated. A scrubbing unit is movably coupled to the handle. The scrubbing unit may scrub a float on a pontoon boat while the pontoon boat is floating.

Abstract: A pitch angle indicator system indicates a pitch angle of blades of a propeller of a marine propulsion unit. A mechanical link couples at least one of the blades to a first end of a first rod. An indicator is coupled to a second end of the first rod. The mechanical link is configured to convert a change in the pitch angle into a rotation of the first rod about its longitudinal axis. The indicator is configured to provide an indication of the amount of rotation of the first rod about the longitudinal axis.

Abstract: An assembly for a retractable thruster suitable for attachment to the hull of a maritime vessel. The assembly comprises a thruster accommodating structure from which the thruster may be deployed into and retracted from the water. The thruster accommodating structure is provided with a drive assembly that suspends the thruster and further comprises a thruster deploying and retracting device, a thruster rotating device, a motor assembly, and a switching device. The same drive assembly is used for deploying, retracting, and rotating the thruster.

Abstract: A propeller position changing device which is capable of changing position according to cruise conditions of a vessel of a floating type.

Abstract: A human driven water propulsion apparatus includes a propeller and a human powered drive coupled to the propeller for driving the propeller. The propeller and human powered drive are connected to and supported by a chassis. Foot pedals are slidably engaged with the helical drive shafts. The helical drive shafts are connected to the propeller through one-way clutches and a gear train such that the propeller is driven by the helical drive shafts when driven by the pedals. In a watercraft application, the chassis is rotatably mounted for rotation between a first position where the propeller is faced in a forward direction and a second position where the propeller is faced in a rearward direction. In a swimmer application, a seat is attached to the chassis by a seat post and straps secure the seat to a user.

Abstract: There is provided an identification number setting apparatus of a plurality of outboard motors attached to a ship body. A plurality of engine control modules are provided in the plurality of outboard motors. A keyless controller is configured to perform an authentication process for keyless control between the keyless controller and the plurality of engine control modules. During initial registration of authentication information for the authentication process, the keyless controller sets identification numbers in the plurality of engine control modules.

Abstract: The inventive technology described herein generally relates to the field of power transmission, more particularly power transmission through a mechanical drive system. More specifically, in certain embodiments the inventive technology includes methods and apparatus for a variable coupler drive utilizing, in one embodiment a dynamic drive-ratio gearing system to transmit a drive input for application with a variety of output uses. In a preferred embodiment, such a variable coupler drive may be used to transmit a rotational drive input to a drive shaft to power, for example, a variety of commercial and industrial applications, and may be particularity suited to power rotational propeller based propulsion systems.

Abstract: A noise abatement system for an aircraft landing gear is provided. The system may have a retention member and a covering member. In this regard, the system may be configured to block the airflow through a structural void to abate noise. Moreover, the system may be shaped to diminish aerodynamic drag.

Abstract: An aircraft landing gear including: a sprung arm mounted to a main pivot and carrying one or more wheels; leaf springs; a transfer arm attached to each of the leaf springs; and a swinging link with a first end which is pivotally coupled to the sprung arm via a first swinging link pivot and a second end which is pivotally coupled to the transfer arm via a second swinging link pivot. The leaf springs are arranged to provide a resilient biasing force via the transfer arm and the swinging link which opposes rotation of the sprung arm about the main pivot. Each leaf spring only absorbs a portion of the landing loads, so load and stress levels in each individual spring are lower. The swinging link enables the leaf springs to be positioned remotely from the sprung arm, in a suitable position to optimize the use of space and distribute loads efficiently into the airframe.

Abstract: A rotor arm assembly for use in a rotor craft rotor hub system includes a pitch shaft and a plurality of discrete bearings coupled to the pitch shaft. The plurality of bearings are elastomeric bearings configured to facilitate movement of the rotor arm assembly about a plurality of degrees of freedom. A respective one of the plurality of bearings is configured to accommodate a single degree of freedom.

Abstract: A method of assisting a pilot in order to minimize the risks of an aircraft rolling over on the ground, the aircraft having a main rotor and a yaw movement control rotor (4), together with lateral cyclic pitch control means for the main rotor and yaw movement control means for the yaw movement control rotor. At least one measurement is taken relating to left forces exerted on a left side undercarriage and to right forces exerted on a right side undercarriage in order to evaluate asymmetry, if any, between the left and right forces, and then a recommended position (26) is determined for at least one of the yaw and lateral cyclic pitch control means in order to make the left and right forces more symmetrical. Each recommended position is displayed on a display unit.

Abstract: A set of swashplates having a non-rotary swashplate and a rotary swashplate. The set includes drive means constraining the rotary swashplate and the rotor mast in rotation about the axis of rotation. The drive means are provided with a drive arm driving the rotary swashplate in rotation about the axis of rotation by plane connection means including a fork, the drive arm extending in elevation from a first end to a second end that is fastened to the rotor mast, the first portion being held captive laterally between two lateral branches of the fork, the fork being hinged to the rotary swashplate by movement means giving the rotary swashplate a degree of freedom to move in rotation about a radial direction of the rotary swashplate relative to the fork.

Abstract: The present invention relates to an automatic system suitable for reducing the speed of rotation of one or more suspended loads, preferably where said rotation is originated by the flow tube located downstream preferably of the blades of the helicopter whereto said loads are attached, or by any other cause, and whose mechanical operation is based on the use of at least one aerodynamic surface, which automatically positions so as to exert, through the actual interaction with this flow tube, an aerodynamic moment, with respect to the center of mass of these suspended loads, appropriately contrary to said speed of rotation, so as to determine the slowing and therefore the progressive stabilization thereof. The automation of this deceleration is obtained through the use of a cycle of automatic control which is based primarily on the interaction, obtained with a processor, between an element responsive to said speed of rotation and an actuator capable of rotating said aerodynamic surface.

Abstract: A medical block associated with a couchette for a patient to lie on. The block includes: a water supply; a power supply; a stop region for at least one trolley; at least one trolley located in the stop region and including drawers containing medical equipment; and an access flap corresponding to each trolley, provided with a locking mechanism and enabling the drawers of the trolley to be accessed.

Abstract: The invention relates to a reading lamp for installation in a cabin trim element (4) of a vehicle, in particular of an aircraft, comprising an installation frame (1) having a ring element (2), a lamp housing (7) having a mating support surface (8), and a clamping ring (9) wherein the clamping ring (9) is connected to the installation frame (1) by means of tension spring elements (10), such that the lamp housing (7) is forced against the support surface (6) of the inner surface of the ring element (2) by means of the clamping ring (9) and may be moved with respect to the installation frame (1) in the manner of a ball and socket joint.

Abstract: The vehicle seat back according to the invention includes a textile assembly (30) having at least one embrittled linear zone (32, 32A, 32B) able to tear during an impact of the head of a passenger located on the seat behind the seat back considered, so as to enable rocking of this passenger's head to be continued and, at the same time, to be slowed down. Application to aircraft seats.

Abstract: A passenger cabin of an aircraft includes a seat arrangement that includes a number of seat assemblies. The seat assemblies include a seat structure having a seat backrest forming a backrest surface the and a seat cushion element forming a seat surface, and a passenger space partition, which spatially partitions a passenger space of the seat and which at least partially surrounds the seat structure and leaves open an access to the seat structure. The seat cushion element is moveable between a comfort position, in which the seat cushion element projects further into the access in order to provide a larger seat surface, and an access position in which the seat cushion element does not project as far or does not project at all into the access in order to make possible a wider access.

Abstract: An air compressing system is provided that includes a compressor configured to compressor air. An engine is operatively connected to the compressor. Further, an infinitely variable transmission is operatively connected between the engine and the compressor. A first shaft operatively connects the engine to the infinitely variable transmission and is configured to rotate at a first speed and a second shaft operatively connects the infinitely variable transmission to the compressor and is configured to rotate at a second speed.

Abstract: A method of controlling solar panels in a solar propelled aircraft which has a wing having solar cell modules mounted therein. The solar propelled aircraft includes: first solar cell modules which are positioned in a main wing or a tail wing of the aircraft and receive solar energy directly from the sun; second solar cell modules which are positioned in a main wing or a tail wing of the aircraft and supplied with directed energy from the earth; and rotating shafts which rotate the first solar cell modules and the second solar cell modules so that the first solar cell modules and the second solar cell modules correspond to each other in both directions. The first solar cell module at the upper surface obtains solar energy from the sun, and the second solar cell module at the lower surface obtains directed energy transferred from the earth.

Abstract: An aircraft monitoring system includes multiple wireless aircraft sensors and multiple meta sensors mounted on-board an aircraft. Each wireless aircraft sensor is configured to sense an aircraft parameter. Each meta sensor is associated with an aircraft sensor and is configured to determine a location or orientation on the aircraft of the aircraft sensor. A data acquisition system mounted on-board the aircraft and connected to the multiple aircraft sensors and the multiple meta sensors can perform aircraft monitoring operations based on the sensed aircraft parameters and on a location or orientation of the aircraft sensors.

Abstract: Various embodiments of the present invention provide a system and method for notifying a flight crew of a fire condition in a cargo container of an aircraft. For instance, particular embodiments involve installing at least one notification device on a cargo container that is in communication with at least one of a fire-detection system or a fire-suppression system for the cargo container. In these particular embodiments, the notification device is configured to emit energy when the fire-detection system detects the fire condition in the cargo container or the fire-suppression system activates as a result of the fire condition. Further, particular embodiments of the invention involve installing at least one detector positioned to detect the energy emitted by the notification device. In these particular embodiments, the detector is configured to send a signal to notify the flight crew of the fire condition after detecting the energy emitted by the notification device.

Abstract: A method and system for generating an alert report on board an aircraft, comprising an on-board acquiring module configured to acquire data relating to the aircraft, the data originating from sensors and/or equipment installed in the aircraft. An on-board processing module is configured to detect possible anomalies by automatically partitioning the data into a set of homogeneous groups, each anomaly being revealed by a corresponding datum belonging to no homogeneous group. An on-board alert-emitting module is configured to emit an alert report on each detection of an anomaly. An on-board transmitting module is configured to transmit the alert report to the ground and in real-time.

Abstract: An aerial sensor system is disclosed. The system includes an aerial vehicle, a camera, and a sensor mounting assembly coupled to the aerial vehicle and to the camera. The sensor mounting assembly permits the camera to be positioned radially outwardly from the aerial vehicle in all spherical positions.

Abstract: A barrel assembly for a composite structure includes a barrel of composite material, a first end ring, and a mid support. The barrel of composite material has a first end, an interior surface and an outer surface, and the first end ring is removably attached to the first end. The first end ring has a perimeter that is substantially congruent with the first end, and is configured to maintain a shape of the barrel. The mid support is removably disposed within the barrel, and has a plurality of spokes extending outwardly from a central hub to contact the interior surface, to maintain a shape of the barrel.

Abstract: A satellite system includes a so-called carrier satellite and a so-called piggyback satellite, each one having an Earth face. The piggyback satellite is attached to the carrier satellite by fastening elements that can be released on command. The piggyback satellite includes propulsion elements suitable for maintaining same in orbit, and the carrier satellite includes propulsion elements for performing a change of orbit of the satellite system including the carrier satellite and the piggyback satellite. The piggyback satellite is attached to the Earth face of the carrier satellite in such a way that the Earth face of the piggyback satellite is essentially perpendicular to the Earth face of the carrier satellite.

Abstract: A deployable structure comprises: a mount comprising a first point and a second point opposite and a third point, a storage reel able to rotate about an axis Z, a tape spring able to switch from a configuration in which it is wound about the axis Z in the storage reel into a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the first and second points forming a double support with the tape spring to keep the tape spring in the deployed configuration. The third point is able to form a simple support with the tape spring, the storage reel is able to move with respect to the third point and the storage reel is pressed against the third point to guide the deployment of the tape spring.

Abstract: A modular device for a spacecraft includes a propulsion system having a tank, a plenum, and a manifold, wherein the propulsion system is integrally formed with a structural frame of the spacecraft. A method of manufacturing the modular device is also discussed, the method including utilizing an additive manufacturing process to construct the propulsion system.

Abstract: A fuel-free spacecraft propelling system having an open-ended outer cylinder of a propelling device and an atomic oxygen collecting device is disclosed. The latter is arranged at the forwardly-propelled front end of the outer cylinder and is hermetically connected with an RF generating device and an ion cyclotron wave heating device through a magnetic confinement device. A spiral wave discharge oxygen plasma inlet and a spiral wave discharge oxygen plasma outlet in the ion cyclotron wave heating device are respectively provided with another magnetic confinement device. The propulsion of the invention does not need to carry the propellant, which greatly reduces the launch costs, and enables a spacecraft to advantageously have an increased orbit life over existing spacecraft systems.

Abstract: Systems, methods, and apparatus for dual port ring compatible satellites are disclosed. In one or more embodiments, a method for removably attaching at least one spacecraft to a payload attach ring on a launch vehicle involves attaching a strongback of each of the spacecrafts to two respective payload ports of the payload attach ring on the launch vehicle. In one or more embodiments, the strongback of each of the spacecrafts is attached to each of the two respective payload ports via a respective beam mounted to a respective port adaptor plate. The method further involves separating the strongback of each of the spacecrafts from the two respective payload ports of the payload attach ring on the launch vehicle by using at least one mechanical actuator on each of the beams.

Abstract: A method for filling and closing pharmaceutical objects disposed in parallel rows in nests includes removing the objects from the nests at an inlet of a conveying device in a removal station and placing the objects into the conveying device. In the conveying device, the objects are fed in succession to a first weighing station and weighed, to filling station and filled and to a second weighing station and again weighed and to a closing station and/or crimping station and closed. After closing, the objects are removed from the conveying section. In every case, pre-sterilized objects are processed in an aseptic manner.

Abstract: Aqueous compositions contain hydrochloric acid at a concentration between 8 wt % and 28 wt % inclusive. The amino acid; hydrochloric acid mole ratio may be between 0.2 and 1.5. Sufficient water is present to dissolve the hydrochloric acid and the amino acid. Such compositions have utility as retarders for acid compositions employed in the stimulation of subterranean formations. Slowing the reaction between the acid and formation helps maximize formation permeability and productivity.

Abstract: A method of filling by weight containers having respective bottoms standing on a conveyor, including the steps of: grasping each container in order to separate it from the conveyor and to bring it up to a substance dispenser spout; weighing the container while it is held separated from the conveyor under the dispenser spout and while simultaneously filling it in order to reach a desired weight; and putting the container back onto the conveyor. In addition, an installation for performing the above method is provided.

Abstract: A manual check valve for use when priming a fluid supply for a spray gun includes an orifice that opens from the fluid supply into a storage chamber, the storage chamber captures any fluid that is expelled from the fluid supply during priming, and the storage chamber is sealed with a closure. Sealing the storage chamber traps any expelled fluid in the storage chamber and prevents any of the expelled fluid from leaking onto another surface, which keeps the priming operation clean.

Abstract: A pallet wrapping platform comprises a lower frame, a pallet supporting table, constraining means interposed between the frame and the table, being designed to allow the frame and table to move by rotating relative to one another, a driving unit and transmission means for transmitting the motion from the driving unit to the table. The table comprises an upper flat disk and at least one lower ring gear, fixed to the disk and designed to interact with the motion transmission means, in such a way that the total thickness of the platform is less than at least 24 millimeters.

Abstract: A method for laying multiple conductors in a container may be provided. The method may comprise receiving the multiple conductors at a monitoring station; receiving the multiple conductors at a drive; and receiving the multiple conductors at the container.

Abstract: A robotic material handling apparatus comprises a packing head using vacuum to lift bottles, and a robot arm including two four-bar linkages. The four-bar linkages include a tubular structural member forming a rigid link with an internal passageway extending along the robot arm. A vacuum source is connected by hoses to the internal passageways and to the packing head as a way in integrating the vacuum lines into the robot arm. The packing head has bottle-lifting stations using vacuum to lift bottles, each including a seal shaped to sealingly engage a shoulder on the bottle. A vacuum source is connected to the seal for suctionally gripping the bottle using the shoulder to lift the bottle, regardless of whether a bottle cap is present or is missing.

Abstract: An apparatus for packaging dosed quantities of solid drug portions includes multiple storage containers and dosing elements for storing and dispensing first dosed quantities of drug portions, multiple moving collecting containers for collecting and outputting drug portions to a packaging station, and fall tubes for guiding the drug portions dispensed by the dosing elements to the collecting containers. An ancillary dosing station has multiple buffer receptacles for storing and delivering second dosed quantities of drug portions to the collecting containers. A conveyor moves the collecting containers between multiple locations along a predetermined path. A controller controls closure members of the buffer receptacles depending on the positions of the moving collecting containers so that drug portions temporarily held in the buffer receptacles are output to selected collecting containers.

Abstract: A stretched and foamed plastic formed body forming, in at least a portion thereof, a foamed region which incorporates foamed cells therein, wherein the foamed cells have a flat shape with a maximum thickness of not more than 30 ?m and an average aspect ratio of not less than 4 as viewed in cross section of the formed body perpendicular to a direction in which the formed body is stretched to a maximum degree, and a non-foamed plastic skin layer having no foamed cell distributed therein is formed on the outer surface of the foamed region. The formed body is, further, blended with a non-lustrous pigment as the coloring agent, which is different from a lustrous pigment such as flaky pigment, and exhibits a metal color over the foamed region thereof. The foamed formed body exhibiting a metal color and, specifically, a gold color or a silver color is thus provided without using any expensive lustrous pigment such as metal powder pigment or flaky pigment.

Abstract: A method of making a preassembled display with automatic stackable supports (PDASS) is described. A PDASS may include two or more blanks (for example pieces of corrugated paperboard) that are joined together, for example to initially form a knocked down flat (KDF). The PDASS may include an insert formed from a single blank, where the single insert blank, when the whole display is erected, automatically erects and provides asymmetric supports that form at opposing corners of the outer blank.

Abstract: The present invention provides a blank for forming a tray for dispensing eye shields. The present invention also provides a tray. The tray is made from the single blank of material. In another embodiment, the present invention provides an eye shield and frame dispenser including a carton, a frame insert and a shield insert. The carton and inserts are made from a single blank of material.

Abstract: A method and system for identifying product is disclosed. A product identifier having product identifying information for one of a plurality of consumable products is provided. The product identifier is selected for a consumable product. The product identifier is displayed at or near a location on a dispensing system, or where access to the consumable product is provided. The system uses a product identifier having product and/or brand information for one or more consumable products. A window is provided in a body of a dispenser or other member of a dispensing system for viewing the product identifier associated with the consumable product therein.