Abstract: A bicycle assembly comprises a saddle adjustment assembly, the saddle adjustment assembly comprising an adjustable height saddle post, the adjustable height saddle post comprising first and second slidably coupled supports; a saddle post locking mechanism that selectively restricts sliding of the second support relative to the first support; and a saddle angle adjustment mechanism configured to couple to a bicycle saddle to enable rotation of the bicycle saddle between a first predetermined position and a second predetermined position, wherein, when the saddle post locking mechanism is in an unlocked configuration, the saddle angle adjustment mechanism enables rotation of the bicycle saddle between the first and second predetermined positions, and wherein, when the saddle post locking mechanism is in a locked configuration, the saddle angle adjustment mechanism maintains the bicycle saddle in one of the first and second predetermined positions.

Abstract: A fast combination structure for a bicycle rear shelf and luggage bag, includes a rear shelf and a luggage bag; the rear shelf has a connection device, shelf body and adjustment unit, where the rear shelf is coupled to a bicycle seat tube through the connection device, and the self body is configured with a slide groove and perforated slot; the adjustment unit has an adjustment element, latching unit and pull rod, where the adjustment element is configured with an accommodation groove in which the latching unit is installed, the pull rod is passed through the accommodation groove and connected to the latching unit, and a return spring is positioned therebetween; the lower side of the luggage bag has a slide device having slide wings and a plurality of buckling holes each allowing the latching unit to be inserted in to fix the luggage bag.

Abstract: A motorcycle cargo storage system is disclosed having a lid that is translatable and rotatable relative to a compartment body to permit for the lid to be fully cleared of the access opening of the cargo storage system. The system may further include a securing system that selectively holds the lid of the cargo storage system in a closed position relative to the compartment body.

Abstract: A protective case for a handheld electronic device is provided. The protective case can include a removable mounting system comprised of an interlocking member and a plurality of mounting bases. The protective case may further include a non-slip member to prevent the device from slipping on a surface and a magnet for attaching the device to a magnetic surface.

Abstract: A side mirror for a straddle vehicle includes: a mirror stay including a base end portion attached to a vehicle body of a motorcycle (straddle vehicle); and a mirror portion including a mirror and provided at a tip end portion of the mirror stay. The mirror stay includes a first stay portion and a second stay portion which branch from the base end portion to extend toward the tip end portion.

Abstract: The field of the invention relates to bicycle systems, especially to bicycle systems adapted for use with smartphones, to smartphones configured for use with bicycle systems, and to methods and to computer software for use with such bicycle systems or smartphones, and to servers configured to communicate with such bicycle systems or smartphones. According to a first aspect of the invention, there is provided a bicycle system including a bicycle, the bicycle system including a processor integral to the bicycle, the bicycle system further including a battery integral to the bicycle, wherein the processor is powerable by the battery, the bicycle system including a smartphone holder configurable to receive a smartphone and to connect the smartphone to the processor, wherein in use the smartphone holder is attachable to, and detachable from, the smartphone.

Abstract: A folding, personal vehicle includes a frame having a foot deck, a front wheel, a bracket, and a handle. The bracket is pivotally connected to the frame and has a bottom position and a top position. The handle is connected to the bracket and is positioned at least partially elevationally above the foot deck of the frame when the bracket is in the top position and is positioned at least partially elevationally below the foot deck of the frame when the bracket is in the bottom position. A folding mechanism for a personal vehicle includes a bracket with a first bracket profile and a second bracket profile. The first bracket profile engages a rear side of a bottom rod when the bracket is in a top position. The second bracket profile engages a front side of the bottom rod when the bracket is in a bottom position.

Abstract: A component mounting structure of a vehicle comprises a frame assembly having a recess which is recessed in a predetermined direction; an intermediate section accommodated in the recess and removably fastened to the frame assembly; and a mounting member used to mount a first adjacent component adjacent to the frame assembly to the frame assembly, and the mounting member includes a connection element connected to the intermediate section in an inner space of the recess and a support element which is continuous with the connection element and supports the first adjacent component in a state in which the connection element is exposed outside through an opening of the recess.

Abstract: A quick release assembly for attaching handlebars to a vehicle is disclosed. The assembly is a cam assembly that in a first position engages the handlebars of a vehicle in an operational position and when said cam assembly is in a second position disengages the handlebars to permit easy storage of the vehicle in a minimum of space. The quick release assembly permits a tool free assembly of a vehicle with a handlebar, such as, for example, a bicycle.

Abstract: A bicycle operating device comprises a base member, a user interface member, an electrical switch, and a transmitting structure. The user interface member is movably mounted to the base member to move relative to the base member in a first direction. The electrical switch is mounted to the base member. The transmitting structure is provided between the user interface member and the electrical switch to transmit a first movement of the user interface member in the first direction to the electrical switch in a second direction different from the first direction.

Abstract: A suspension device includes a pair of suspensions each containing at least one of a damping mechanism and a suspension spring. A tubular body-side member is on a vehicle body side. A tubular wheel-side member is on a vehicle wheel side and coupled to the body-side member, and moves relative to the body-side member in an axial direction. A hollow cylindrical cylinder is inside of the body-side member and the wheel-side member and includes a weak portion in the axial direction on an outer side. A rod member is inside of the body-side member and the wheel-side member and moves relatively in the axial direction in accordance with movement of the body-side member and the wheel-side member. A first defining member secured to an end portion of the rod member and in contact with the cylinder movably in the axial direction of the cylinder defines space in the cylinder.

Abstract: A straddle-type vehicle includes a steering stem, a top bridge, a first front fork, a second front fork, a front wheel braking unit, an ABS modulator, a supporter, and a brake pipe. The front wheel braking unit is provided at the first front fork. The ABS modulator is disposed rearward with respect to the top bridge. The supporter is provided at the second front fork forward with respect to the top bridge. The brake pipe extends from the ABS modulator to the front wheel braking unit through the supporter. The brake pipe between the ABS modulator and the supporter passes through a space between the head pipe and the second front fork below the top bridge. The brake pipe between the supporter and the front wheel braking unit passes through a position higher than the top bridge to be connected to the front wheel braking unit.

Abstract: A bicycle pedal, including a pedal body rotationally connected to a spindle assembly suitable to be coupled to a pedal crank, the pedal body having a central portion including a cylindrical seat in which the spindle assembly is inserted and rotatably supported. The pedal includes a plurality of spacers, inserted along the spindle assembly and/or inside the cylindrical seat, suitable to be relocated in order to modify the Q-factor of the pedal.

Abstract: A bicycle has a main frame, a rear suspension having a spring and guiding a wheel along a prescribed path and an electric drive mounted on the main frame. A driving pinion thereof being is disposed coaxial to the shaft of a bottom bracket, and at least one driven pinion is disposed coaxial to the rear wheel and operationally connected to the driving pinion of the electric drive by a chain. A chain segment transmitting torque from the driving to the driven pinions is guided by a chain deflector. A distance between where the chain segment engages the driven pinion and the point of the chain deflector about which the chain is substantially pivoted when the wheel is deflected changes so slightly that the crank arms of the bottom bracket rotate by a maximum permissible angle relative to a non-deflected position of the wheel when the spring is deflected.

Abstract: A first sprocket includes a first opening having a first diameter smaller than a radially outer diameter of a sprocket support portion of a bicycle rear hub assembly. A lock member includes a main body, a male thread portion, and a radial projection. The main body has a first axial end configured to pass through the first opening and a second axial end opposite to the first axial end in an axial direction. The male thread portion is provided to the first axial end and configured to engage with a female thread portion of the bicycle rear hub assembly in a state where a bicycle rear sprocket assembly is mounted to the bicycle rear hub assembly. The radial projection extends radially outwardly from the second axial end to restrict axial displacement of the first sprocket with respect to the sprocket support portion in the state.

Abstract: A bicycle front sprocket comprises a sprocket body and at least one sprocket tooth. The sprocket body includes a crank arm mounting portion including a first mounting axial surface facing toward an axial bicycle-center plane in an axial direction in a state where the bicycle front sprocket is mounted to the bicycle frame. The at least one sprocket tooth has a first chain-engagement axial surface facing toward the axial bicycle-center plane in the axial direction in a state where the bicycle front sprocket is mounted to the bicycle frame. The first chain-engagement axial surface is offset from the first mounting axial surface toward the axial bicycle-center plane in the axial direction. An axial distance is defined from the first mounting axial surface to the first chain-engagement axial surface in the axial direction and is equal to or larger than 6 mm.

Abstract: A multiple-sprocket arrangement for mounting on a rear wheel axle of a bicycle includes a receiving body designed for mounting on the rear wheel axle, and a sprocket assembly. The sprocket assembly includes a first sprocket, the inner diameter of which is greater than an outer diameter of the receiving body and which is connected to the receiving body. The sprocket assembly further includes at least one second sprocket, the inner diameter of which is smaller than an outer diameter of the receiving body and which is designed in an unsupported manner and connected to the receiving body in a torque-transmitting manner by means of the first sprocket. The first sprocket and the at least one second sprocket may be of a one-piece construction.

Abstract: The invention provides a wireless control system for a bicycle, including at least one actuator having at least a pressed state and a released state, and a control unit configured to generate a first control signal responsive to the pressed state and a second control signal responsive to the released state, and to transmit the first control signal and the second control signal to at least one bicycle component.

Abstract: Two watercraft are connected together using a hinge system. A knuckle in one watercraft is placed in a corresponding space therefore in a second watercraft. Similarly, a buttress in the second watercraft is placed in a corresponding space in the first watercraft. An axle is placed within the buttresses as well as within the knuckle to attach the hinge device to attach the two watercraft together. This axle is also attached to a rear transom and to a forward bow connector. A second axle adds further rigidity to the system as it attached through a first watercraft passageway to both the transom and to the bow connector.

Abstract: A cleat includes two cams (36) comprising mutually opposed convex surfaces rotatable about parallel axes which extend vertically in a rope-trapping position of the cleat, to bring the arcuate surfaces together and apart. The cams (36) are urged towards each other to trap a rope (66) therebetween. Each cam is also mounted to a horizontal cylinder (2) for rotation about an axis of the cylinder, in order to allow the rope (66) to rotate the arcuate surfaces by pulling in a line above this horizontal axis and to free the rope.

Abstract: A method for offshore floating petroleum production, storage and offloading comprising receiving hydrocarbons from at least one of an FPSO, production risers, or wellhead on the seabed by a floating hull; processing received hydrocarbons forming hydrocarbon product in the floating hull; storing the hydrocarbon product in the floating hull; and offloading the stored hydrocarbon product. The floating hull contains a hull plan view that is circular and wherein the floating hull has a bottom surface, a top deck surface, at least three connected sections, joined in series and symmetrically configured about a vertical axis with the connected sections extending downwardly from the top deck surface toward the bottom surface. The at least three connected sections contain an upper cylindrical portion, a lower conical section, a cylindrical neck section, and a set of fins secured to the hull configured to provide hydrodynamic performance through linear and quadratic damping.

Abstract: The invention relates to a method for producing a vessel hull (1) for use as a hull of an FPSO or FSO, comprising producing a vessel hull with a stern portion (2), a bow portion (3) and a central portion (4), arranging a deck (6) on the hull, for supporting processing modules, arranging hydrocarbon storage tanks inside the hull, providing the hull with an anchoring connection arrangement (7), characterized by arranging process module reinforcements (8) in the deck for supporting the hydrocarbon process modules, providing both longitudinal hull sides with mooring line connection reinforcements (9) at or near the bow portion, arranging riser connection reinforcements (10, 14) on one or more longitudinal hull sides, in between the mooring line connection reinforcements in longitudinal direction, for a riser balcony (28, 29), and providing the bow portion with turret reinforcements (11, 12).

Abstract: A platform (1) for the landing of an aircraft on a boat (B), comprising at least one lower base (2) fixed on the boat (B), and at least one upper base (21), fixed on an aircraft landing footboard (3), wherein a plurality of first curved tubular sections (4), parallel one to each other, are welded inside the frame of the lower base (2), while a plurality of second curved tubular sections (5), parallel one to each other and placed orthogonally with respect to said first tubular sections (4), are welded inside the frame of the upper base (21); said tubular sections (4, 5) are bounded together by means of sliding shaped structures, which are driven through actuating and control means.

Abstract: A body board for use by a rider in water includes a buoyant board body defined as having a top rider surface opposite a bottom submerged surface, a front half opposite a rear half, a left half opposite a right half and a board centerline. The board centerline extends from the front section half to the rear section half separating the left half from the right half. A left side riser is disposed on the top rider surface located in the left half and rear half, the left side riser extending above the top rider surface and configured to abut a rider's left rib cage and/or left hip. A right side riser is disposed on the top rider surface located in the right half and rear half, the right side riser extending above the top rider surface and configured to abut a rider's right rib cage and/or right hip.

Abstract: Wakeboat ballast pump systems and methods are provided to monitor the operational condition and parameters of wakeboat ballast components. Systems and methods for sensing and measurement are provided to detect parameters associated with wakeboat ballast pumps and compartments, including systems and methods that can economically retrofit into existing wakeboat ballast systems. Systems and methods are also provided to enable automated action based on various operational conditions and parameters to improve the safety, automation, performance, convenience, and marketing advantage of wakeboat ballast pumps.

Abstract: The practice of this invention enables saving a life. A passive distress alert for distressed vessel in water is provided. The self-activating alert is positioned on or near hull bottom zone and distress message is at least partially presented, without human or mechanical, electronic or other trigger, when vessel is keel over or in other overturned positioned and can indicate relative percent keel over. The alert reflects natural and artificial light and/or has components which are fluorescent, with or without special black light, either at day or night to present a distress message to a detector. Detector can be an aided or unaided human eye, camera, bar code reader, or other alphabetic or numerical character or symbol electronic recognition device. Distress message can be SOS, MOB, HELP, CQD, R&R, MAYDAY and other local or universal distress messages or combinations thereof or special distress alert comprising bars, dots, dashes and other symbols.

Abstract: Methods and systems for detecting and locating a man overboard situation. In particular, the methods and systems detect a point of loss of a man overboard situation and allow for the ship to coordinate back to the point of loss.

Abstract: A dry suit having detachable or permanent zippered compression flaps. The compression flaps can be disposed over the front or the back of a dry suit. The compression flaps are used to gather and hide excess dry suit materials and dry zipper ends under the compression flaps. The compression flaps form a tunnel around the wearer under which a kayak spray skirt or a kite boarding/surfboarding harness can be worn.

Abstract: A system for subsea operation is described, comprising a free swimming, submersible garage and docking station (10,10?), and also an associated free swimming ROV (50), where the garage and docking station (10,10?) comprises a framework (14) arranged to function as a garage (40) or docking (40?) for the free swimming ROV (50), and where the submersible garage and docking station (10,10?) comprises at least equipment in the form of several thrusters (16,18) for operation in the vertical and horizontal directions, respectively, units and a steering system for positioning in the water, and also a winch (12) connected to said ROV (50) via a cable (34) for the transfer of electricity and signals.

Abstract: An underwater robotic vehicle development system for building underwater robotic vehicles (URVs), including a pressure vessel system, modular chassis elements, a propulsion system and compatible buoyancy modules. The pressure vessel system uses standardized, interchangeable modules to allow for ease of modification of the URV and accommodation of different internal and external components such as sensors and computer systems. The system also includes standard, reconfigurable connections of the pressure vessel to the modular chassis system. A standardized, modular propulsion system includes a magnetic clutch, and a magnetic sleeve used to power the URV on or off.

Abstract: Boat rowing apparatus including a framework having spaced horizontal flotation members disposed outside the boat sides and extending into the body of water supporting the boat. A plurality of spaced paddle members are pivotally mounted on the flotation members to propel the boat when the framework is moved back and forth by a rower.

Abstract: The present application relates generally to a control arrangement for controlling at least two azimuthing propulsion units of a ship. The control arrangement comprises a crash stop activation member for activating a crash stop procedure, after which the crash stop procedure is executed in which the orientation and propulsion speed of the azimuthing propulsion units are controlled until the propagation speed of the ship has at least been reduced from the moment when the crash stop procedure was activated.

Abstract: A wedge frame for an aircraft that provides tailstrike angle enhancement. The wedge frame has converging, non-parallel faceplanes that tilt a rear portion of the aircraft fuselage upward in order to prevent or reduce risk of the tail of the aircraft striking the ground during takeoff and landing. A method to prevent or reduce risk of the rear portion of an aircraft from striking the ground during takeoff and landing by using a wedge frame having converging, non-parallel faceplanes to tilt upward the rear portion of the aircraft.

Abstract: Systems and methods are provided for enhanced water capture systems for aircraft interiors. One embodiment is a strip that is formed from a water-absorbent material for retaining moisture. The strip is adhered to an interior surface of an aircraft at a location proximate to an entry point for water into a cabin of the aircraft, and the strip comprises holes within the water-absorbent material that are staggered with respect to each other.

Abstract: A method of supplying hydraulic power via a zonal hydraulic system to an aircraft having a plurality of operating phases includes determining a current operating phase of the aircraft and setting a power limit (e.g., a pressure set point and/or flow limitation) for at least one hydraulic power unit based on the current operating phase. The hydraulic system includes a plurality of hydraulic zones. Each of the hydraulic zones includes a local controller, a hydraulic power unit controlled by the local controller, and at least one actuator powered by the hydraulic power unit. Energy savings may be realized by altering the pressure set point for and/or limiting the flow to hydraulic systems in inactive and/or less active zones. The zonal hydraulic system may be reconfigured for safety based on sensed failures and/or during emergency or alternate power conditions with limited available power. Duty cycles for multiple electric motor driven pumps of the system may be balanced.

Abstract: A compact electromechanical decoupler device is operatively connected between a manual control device of an aircraft and an electromechanical actuator that controls the flight modes of the aircraft. The electromechanical decoupler device is operable to decouple the operative connection between the manual control device and the electromechanical actuator with the absence of power supplied to the electromechanical decoupler device. The electromechanical decoupler device can recouple the operative connection between the manual control device and the electromechanical actuator on resupply of power to the electromechanical decoupler device and on manually achieving proper rotational alignment or indexing between the mechanical control device and the electromechanical actuator.

Abstract: A method of controlling a magnitude of a sonic boom caused by off-design-condition operation of a supersonic aircraft at supersonic speeds includes, but is not limited to the step of operating the supersonic aircraft at supersonic speeds and at an off-design-condition. The supersonic aircraft has a pair of swept wings having a plurality of composite plies oriented at an angle such that an axis of greatest stiffness is non-parallel with respect to a rear spar of each wing of the pair of swept wings. The method further includes, but is not limited to the step of reducing wing twist caused by operation of the supersonic aircraft at supersonic speeds at the off-design condition with the composite plies. The method still further includes, but is not limited to, minimizing the magnitude of the sonic boom through reduction of wing twist.

Abstract: An apparatus and method using an interference body to shape a sonic boom signature is provided herein. The interference body can be installed on various control surfaces, including a vertical control surface. The interference body can be sized and positioned to create a desired amount of interference with expansion wave s generated by one or more components of an aircraft. In one configuration, the interference body can be operative to reduce the sonic boom formed by an aircraft operating at or above supersonic speeds.

Abstract: A pneumatic taxi system of an aircraft with a rotary non-turbine air motor for driving a wheel, of an aircraft landing gear, with compressed air.

Abstract: A drive system for rotating a wheel of an aircraft landing gear is disclosed including a motor operable to rotate a drive pinion via a drive path; and a driven gear adapted to be attached to the wheel so as to be capable of rotating the wheel. The drive system has a drive configuration in which the drive pinion is capable of meshing with the driven gear to permit the motor to drive the driven gear via the drive path. The drive path includes a first compensating gear mounted on a common drive shaft with the drive pinion so as to be capable of rotating in tandem with the drive pinion, and a second compensating gear which is meshed with the first compensating gear.

Abstract: An interior length of a confined space is inspected by autonomously flying an unmanned aerial vehicle having a sensor pod. The sensor pod can be tethered to the unmanned aerial vehicle and lowered into the confined space from above perhaps by an electromechanical hoist. An altitude or heading of the sensor pod can be measured. The confined space can be the flue of a chimney.

Abstract: In accordance with an embodiment of the present invention, a method of operating a rotorcraft includes operating the rotorcraft in a heading control mode that includes activating a yaw channel path of a heading controller and deactivating a roll channel path of the heading controller when a speed of the rotorcraft is less than a first speed threshold or a heading error is less than a heading error threshold, and activating the roll channel path of the heading controller and deactivating the yaw channel path of the heading controller when the speed of the rotorcraft is greater than a second speed threshold and the heading error is not less than the heading error threshold.

Abstract: A system and method for efficiently maneuvering a multirotor drone having a control system, an electrical power source, a plurality of rotor assemblies each having a rotor boom, a rotor mast, at least one rotor blade, a rotor assembly adjustment apparatus, a plurality of electric motors, wherein each electric motor is connected to a rotor boom positioned in a substantially horizontal direction and drives a rotor mast positioned in a substantially vertical direction and connected to at least one rotor blade, with the position of said rotor boom automatically adjustable in a substantially horizontal direction by the adjustment apparatus and the control system.

Abstract: An unmanned flying device including a body, a first blade and at least a second blade, and a coupling assembly for coupling the first blade and the at least second blade to the body. Both the first blade and the at least second blade are rotateable about the body and are deployable away from the body via rotation of the first and the at least second blades about the body. The coupling assembly urges the collapsing of the first blade and the at least second blade towards the body.

Abstract: An unmanned aerial vehicle includes a plurality of arm units, each having a rotary wing, a motor, and an arm main body and detachably coupled to a main body; the main body having a plurality of receptacles for coupling to the arm units; and a battery unit detachably coupled to the main body to be exposed to outside, in which at least a part of the battery unit is exposed to outside when the battery unit is coupled to the main body.

Abstract: A passenger service system includes a seat, a first sensor associated with the seat that senses a position of the seat and generates a first signal, a second sensor associated with the seat that senses the presence of a passenger in the seat and generates a second signal, a first light source disposed at a predetermined location with respect to the seat, where the first light source generates light, a third sensor associated with the first light source that senses at least a position of at least one hand of the passenger and generate a third signal, and a controller that receives the first signal, a first light signal that controls at least one parameter associated with the light including at least one of an intensity, a color, a projected pattern, projected pattern location, or a width.

Abstract: A lavatory arrangement for a vehicle cabin comprises a lavatory housing defining an inner space having an entrance opening, a floor and a first lateral delimitation, a toilet arranged adjacent to the first lateral delimitation, having a front end and a back end and defining a first plane spanned by a longitudinal direction of the toilet and a first axis vertical to the floor, a wash table arranged at the first lateral delimitation. The wash table has a horizontal surface and a lining arrangement extending from the horizontal surface in the direction to the floor, thereby creating a wash table lining surface, the lining arrangement comprises an indentation in a region facing to the toilet, in which indentation the lining arrangement is indented in a direction facing away from the first plane.

Abstract: A modular lavatory monument assembly configured to be positioned in the interior of an aircraft. The modular lavatory monument assembly includes first, second, third and fourth walls that cooperate to form an outer shell that defines a lavatory interior. The fourth wall includes an alcove extending outwardly therefrom. The assembly also includes a sink module positioned in the alcove, a mirror module positioned above the sink module in the alcove, and a door positioned on one of the second or third walls.

Abstract: The present invention relates to an assembly (1) of seats (2?, 3?, 2?, 3?) for airplanes, said assembly (1) comprising at least two rows (4?, 4?) of pairs of adjacent seats (2?, 3?; 2?, 3?), each seat (2?; 3?; 2?; 3?) comprising one seatback (5), one sitting portion (6), and an element (7) for the support of the lower limbs, each seat (2?; 3?; 2?; 3?) being configured in order to make a reclining movement along a respective recline axis (r2?; r3?; r2?; r3?) between a sitting position, wherein at least said seatback (5) and said sitting portion (6) cooperate in order to form a sitting element, and an extended position, wherein said seatback (5), said sitting portion (6) and said element (7) cooperate in order to form a bed surface, and vice versa, each seat (2?; 3?; 2?; 3?) being tilted in respect to the adjacent seat (3?; 2?; 3?; 2?) of a first angle (??; ??) obtained by the intersection of the respective recline axis (r2?, r3?; r2?, r3?) in a convergence point (A?; A?) arranged rearward said pair of adjacent

Abstract: A passenger seat 100 for an aircraft, including a seat bottom frame 210, a backrest frame 220 and a headrest frame 230 that constitute a reclining assembly, which are supported by a spreader 170 and pipes 130 and 132 fastened to a floor by seat track fittings 110, the pipes 130 and 132 passing through left and right legs 120. A direct-acting-type damper 300 is attached to the backrest frame 230, and an extension member 400 is attached to the headrest frame 230, whereby a structural design is provided in which the reclining assembly, the direct-acting-type damper and the extension member can be easily replaced.