Abstract: The present invention is a security system for use with an ordinary bicycle. The Bicycle Security System of the present invention allows users: to leave their bicycle anywhere without the need to be tethered to an existing stationary support, eliminates the use of chaining systems that are easily cut off, comes equipped with a security system which offers a user peace of mind, and is easily locked and unlocked with a fob-lock system. The present invention employs a key-fob lock system which actuates a locking mechanism located on the down tube of a bicycle. A surface detection sensor attached to the handlebars of the bicycle is also employed to locate the bicycle in the event of theft.

Abstract: A method for controlling a drive for displacing a saddle into a travel or a mounting position, comprising measuring an acceleration and a lateral inclination of the two-wheeled vehicle continuously within a first time interval and a speed of the two-wheeled vehicle after the first time interval; carrying out a first acceleration comparison, which checks whether the acceleration is greater than a minimum positive acceleration, at least for a second time interval; carrying out a first speed comparison if the first acceleration comparison is positive, the first speed comparison checks whether the speed is higher than a minimum speed; displacing the saddle into the travel position if the first speed comparison is positive; and carrying out a second acceleration comparison if the first acceleration comparison is negative, the second acceleration comparison checks whether the acceleration is less than a minimum negative acceleration at least for a third time interval.

Abstract: Disclosed is a streamlined storage system for use with a motorcycle or other similar vehicle seat that does not detract from the riding experience, that is easy and convenient for the rider to access while riding, and that does not substantially increase the overall cost of the vehicle.

Abstract: An electric powered personal mobility vehicle that includes at least one front wheel and an electric motor that provides rotational force to a wheel of the vehicle. The electric motor is supported by the vehicle and is powered by a rechargeable battery that is also supported by the vehicle. The vehicle can also include swivel caster wheels each configured to rotate about a wheel axis.

Abstract: There is provided a front fork provided with a plurality of adjusters, while including a spring adjuster. In order to achieve the above object, in a front fork F according to the means for solving the problem of the present invention, a spring adjuster A is rotatably mounted on a position eccentric to a center O of a cap 4 as viewed in an axial direction and includes a screw portion 35 disposed in an outer periphery protruded into a fork main body 1, and a plate P in which the screw portion 35 of the spring adjuster A is screwed to change support positions of a suspension spring S is brought into contact with a case (tubular member) 14a at two points on both sides in a circumferential direction of the normal of the case 14a that passes a mounting center of the spring adjuster A. Accordingly, while being prevented from rotating, the plate P can be downsized and can be disposed so as not to interfere with first and second adjusters 5, 6.

Abstract: A bicycle operating device is basically provided with a main support body, a first operating member, a hydraulic brake operating unit, an additional operating unit and a second operating member. The main support body is configured to be attached to a handlebar. The first operating member is pivotally coupled to the main support body about a first pivot axis. The hydraulic brake operating unit is mounted to the main support body. The hydraulic brake operating unit has a piston operated in response to operation of the first operating member between a rest position to an operated position. The additional operating unit is mounted to the main support body. The second operating member is configured to actuate the additional operating unit.

Abstract: A saddle-ridden vehicle includes: a pair of frame members which are disposed on one side and on other side in a vehicle width direction so as to extend in a vehicle front-rear direction; an engine which is disposed between and supported by the pair of frame members; an air cleaner which cleans air for fuel combustion; a supercharger which compresses the air cleaned by the air cleaner; an intercooler which cools, using a cooling wind, the air compressed by the supercharger and supplies resulting air to the engine; and an exhaust wind duct which determines a discharge position or a discharge direction of the cooling wind discharged from the intercooler, and the exhaust wind duct is disposed above the engine on the one side in the vehicle width direction and extends to rear of the engine.

Abstract: A pin for a crown of a bicycle crankset that includes a mounting portion configured to be fixed to the crown, a chain engaging portion having a first face that faces towards said mounting portion for engaging a plate of a link of a bicycle chain, and a second face that faces the opposite way with respect to said mounting portion. The second face has at least one first surface portion inclined by a first angle smaller than 90° when measured in a longitudinal section plane of the pin.

Abstract: The invention relates to a multi-sprocket arrangement for installation on a rear-wheel hub and for engagement with a bicycle chain. The multi-sprocket arrangement includes at least ten adjacent sprockets with different numbers of teeth. In each case of the at least ten adjacent sprockets two adjacent sprockets of the sprockets are arranged with a defined spacing to one another. The defined spacing corresponds either to a smallest spacing or to a larger spacing.

Abstract: An automatic shifting device for a bicycle is disclosed. The device may include a shifting actuator to activate the gearshift mechanism, a computing unit connected to the shifting actuator, an operator control/display unit connected to the computing unit, an inclination angle sensor, and a velocity sensor. The operator control/display unit may receive a first input value of a gear speed of the gearshift mechanism for starting on a level underlying surface; a second input value of a velocity of the bicycle at which shifting into a maximum gear speed of the gearshift mechanism takes place on a level underlying surface; and a third input value of a velocity of the bicycle at which shifting into a maximum gear speed for this terrain inclination takes place on an underlying surface with a positive terrain inclination. An individualized shifting algorithm based on the input values may be stored in the computing unit.

Abstract: The present invention relates to a lashing bar of a composite material formed through filament winding to provide light weight and capacity to withstand high tensile loads, and a method of manufacturing the same. The invention comprises continuous fibers with high tensile strength wound around the core in the center and the exteriors of thimbles with holes and encased by a composite material, and metal parts provided in certain areas where loads are concentrated. Therefore, the invention offers the advantages of maximizing efficiency during transportation and installation by lowering the weight of lashing bars used for the lashing of containers.

Abstract: The method of supporting and lowering a subsea package load on an umbilical from the deck of an offshore service vessel to a subsea work location including providing a reel to store the umbilical on the deck which is not capable of sustaining the maximum load, providing a supporting tractor with dual chains which have multiple dogs mounted on skewed surfaces which amplify a spring load support against the umbilical for frictional support of the umbilical and therefore the subsea package.

Abstract: A container catching system, which is sea proof, includes a frame with a base on which a container is to be positioned, hinge pins secured to the frame above the base, and arms situated around the base, each arm having an abovementioned hinge pin. Arm portions situated above the hinge pin contact, in the unfolded state, a container to be lowered to guide the container towards the base, and arm portions situated below the hinge pin move outwards when they contact the container, thereby causing at least the top arm to engage the container.

Abstract: There is provided a fluid transfer system (100) and method in which a transfer manifold (150) is secured to a frame (120). The frame (120) is designed to engage with a coupling point (328) in a vessel, in order to support the manifold (150) in a desired position.

Abstract: An offshore floating structure such as a wind turbine includes a number of improvements. The floating structure can include a chain engaging system configured to prevent any lengthwise movement of a mooring chain. The floating structure can also include a mooring fixture pivotally coupled to the hull to prevent shock loads from being transmitted directly from the mooring line to the hull. The floating structure can also include installation aid structures that provide additional water plane area and/or buoyancy to the structure. The floating structure can also have a hull that is optimized for use as an offshore wind turbine.

Abstract: Proactive control of watercraft movement based on water surface features. A method obtains, from a plurality of floating sensors at least partially surrounding a watercraft in a body of water, information about movement of a surface of the body of water, the plurality of floating sensors being arranged in multiple sets, the floating sensors of each set of the multiple sets being interconnected by a respective tether extending from the watercraft. The method builds a surface model of the surface of the body of water based on the obtained information about movement of the surface, the surface model including indications of force and directional movement of features of the surface of the body of water, and determines, based on the surface model, at least one control maneuver for controlling movement of the watercraft.

Abstract: A watercraft lift includes a base that is configured to be attached to a fixed surface. The watercraft lift includes an extension that extends from the base. The extension includes a pair of arms and a pair of legs. Each leg is attached to, and extends away from, each arm. The extension is rotatable about the base between a lowered position and a raised position. Then in the lowered position, the extension is configured to receive a watercraft, and when in the raised positioned, the extension is configured to store the watercraft.

Abstract: Provided are underwater spectacles, including a spectacle holder, spectacle belts and an intelligent control system. The intelligent control system includes a warning device, a microprocessor and a plurality of radars. The plurality of radars are respectively disposed on the spectacle holder and the spectacle belts. Input ends of the microprocessor are respectively connected with the plurality of radars, and an output end of the microprocessor is connected with the warning device. The microprocessor acquires signals of the radars, determine obstacle information and/or danger avoiding information around the head of a user, and send the information to the warning device. The warning device receives and provides the user with the obstacle information and/or the danger avoiding information. A control method of the underwater spectacles is also provided.

Abstract: A method for cycling autonomous underwater vehicles (AUVs) that record seismic signals during a marine seismic survey. The method includes deploying plural current AUVs on the ocean bottom; recording the seismic signals during the marine seismic survey with plural current AUVs; releasing from an underwater base a new AUV to replace a corresponding current AUV from the plural current AUVs; recovering the current AUV; and continuing to record the seismic signals with the new AUV.

Abstract: A marine propeller composite blade an axially extending composite blade root including a dovetail wound in a partial spiral or helix around a centerline. Dovetail tapering down in width between clockwise and counter-clockwise dovetail sides of dovetail from dovetail bottom in a radially outwardly direction away from centerline. Marine propeller may include composite blade roots mounted in axially extending hub slots in a metallic hub, axially extending wedges disposed within the hub slots circumferentially between the blade roots and one of clockwise slot sides and counter-clockwise slot sides, and the wedges abutting the blade roots and the one of clockwise slot sides and counter-clockwise slot sides. Wedges and hub slots wound in a partial spiral or helix around a centerline. Radial retention means for radially retaining wedges in hub slots may include bolts engaging wedges and screwed into threaded holes in hub.

Abstract: A blade member includes a leading edge, a trailing edge, and a blade body extending therebetween. The blade member also includes a dovetail, a transition region, and a transition relief. The dovetail includes a dovetail chord line extending between an axially forward face of the dovetail and an axially aft face of the dovetail. The dovetail chord line has a dovetail chord length. The transition region is formed between the blade body and the dovetail. The blade body and the transition region form a blade body transition chord line at the interface of the blade body and the transition region which has a blade body transition chord length. The transition relief includes a geometric relief in at least one of a forward and an aft end of the transition region and the dovetail. The dovetail chord length is less than the blade body transition chord length.

Abstract: A propeller assembly is provided. The propeller assembly includes a central hub including a forward end, an aft end, and a hub body extending therebetween along an axis of rotation of the central hub. The propeller assembly further includes a first retention member including a first radial interference member, the first retention member coupled to the forward end of the central hub and a second retention member including a second radial interference member, the second retention member coupled to the aft end of the central hub. The propeller assembly also includes a fairing platform extending between the first retention member and the second retention member, wherein the fairing platform is retained by the first radial interference member and by the second radial interference member.

Abstract: An apparatus and system for a marine propeller assembly are provided. A forward retention member that may be used with the marine propeller assembly includes a planar base, a drive shaft engagement end opposite the planar base, and a conic body extending therebetween along a centerline normal to the planar base. The forward retention member also includes at least one protuberance extending radially away from a surface of the conic body, the protuberance extending axially from the planar base arcuately convergent to a predetermined point between the planar base and the drive shaft engagement end.

Abstract: A propeller assembly that includes a hub having an outer radial surface and a plurality of wedge retaining members removably coupled to the hub. The plurality of wedge retaining members are spaced circumferentially about the outer radial surface such that a dovetail slot is defined between adjacent wedge retaining members. The assembly also includes at least one propeller blade including a root portion having a dovetail profile. The root portion is coupled to the hub and positioned within the dovetail slot. The plurality of wedge retaining members are configured to restrict radial movement of the root portion within the dovetail slot.

Abstract: An apparatus and system for a marine propeller assembly are provided. An aft retention member that may be used with the marine propeller assembly includes a base, an opposing nose and a conic body extending therebetween along a centerline normal to the base. The aft retention member also includes at least one protuberance extending radially away from a surface of the conic body. The protuberance extends axially along a surface of the aft retention member from the base arcuately convergent to a predetermined point between the base and a tip of the nose.

Abstract: An apparatus and system for a propeller assembly are provided. In one aspect, marine propeller assembly includes a plurality of circumferentially-spaced blades that each include a dovetail having a radially inner surface. The marine propeller assembly also includes a hub including a plurality of circumferentially-spaced dovetail receiving portions configured to receive a corresponding dovetail of the plurality of blades. At least one gap is formed between the radially inner surface and at least a portion of the dovetail receiving portion.

Abstract: A tangential flow machine can be operated both as electric propulsion and as a generator, having a jacket housing which can have flow passing around it on an outer side, the profile of which is formed on a first front-side opening, and tapers to a second front side, on which a second front-side opening is formed. Between the two front-side openings, there extends a flow path along a main axis, and with an electrical machine, which on the jacket housing has a stator and a rotor that is supported so as to rotate within the stator. The rotor defines a free rotary axis and has a rotor ring and an arrangement of rotor blades which each extend from the rotor ring, radially to a free edge and the free edges of the rotor blades, in the projection direction parallel to the main axis, delimit a free circular surface. With this, provision is made that the rotor blades are formed by baffle plates, which extend in the direction of the main axis over the entire axial length of the rotor ring.

Abstract: A swimming propulsion device. The swimming propulsion device includes a fuselage at least one propulsor pivotally connected to the fuselage, and in some embodiments, at least one stabilizer affixed to the fuselage. The device also includes a swimmer connection mechanism removably attached to the fuselage by a locking mechanism whereby the swimmer connection mechanism connects a swimmer to the device, and a control mechanism installed within the propulsor. A method for efficient swimming is also disclosed.

Abstract: An outboard motor includes an engine, a supercharger that compresses air to be supplied to an air intake of the engine, and a cooler that cools the air compressed by the supercharger. The compressed air is cooled by spraying water obtained by condensing water vapor produced by combustion in the engine to the cooler.

Abstract: An atmospheric balloon descent system includes a system housing having a drogue chamber containing a drogue chute and a parachute chamber containing a parachute. The parachute coupled with the drogue chute with a drogue tether. A riser tether extends between a descent system end portion and a balloon system end portion, and the descent system end portion is coupled with the parachute. A drogue cover release is coupled between the riser tether and the drogue cover. The descent system transitions between riser deployment and parachute deployment configurations. In the riser deployment configuration the system housing is decoupled from the atmospheric balloon system and the riser tether is deployed between the system housing and the atmospheric balloon system. In the parachute deployment configuration the deployed riser tether opens the drogue chamber and deploys the drogue chute and the deployed drogue chute opens the parachute chamber and deploys the parachute.

Abstract: A moisture control apparatus for use with a structure within an aircraft fuselage, the structure including an upper surface, the apparatus comprising: a moisture absorbing layer including a moisture absorbing material, the layer including a leading edge, a trailing edge, side edges, an upper surface, and, a lower surface; and, a wicking layer disposed in fluid communication with the lower surface of the moisture absorbing layer, the wicking layer including a wicking layer leading edge, a wicking layer trailing edge and a wicking layer upper surface configured for capillary action of moisture from the wicking layer trailing edge towards the wicking layer leading edge, wherein the wicking layer leading edge is offset from the leading edge of the moisture absorbing layer such that an offset portion of the wicking layer is exposed to air to facilitate evaporation of the moisture.

Abstract: A moisture control apparatus for use with a structure within an aircraft, the structure including an upper surface, the moisture control apparatus comprising: a moisture absorbing layer including a moisture absorbing material, the layer including a leading edge, a trailing edge, side edges, an upper surface, and, a lower surface; and, a reverse-bevel defined along the leading edge of the layer, wherein the reverse-bevel and the upper surface of the structure define a gutter configured to retain moisture flowing along the upper surface of the structure.

Abstract: A compartment door of a galley within an internal cabin of a vehicle (such as an aircraft) includes a front panel having a front outer surface, and a footstep system secured to the front panel. The footstep system is moveable between a retracted position and an extended support position. The footstep system is vertically oriented in the retracted position. The footstep system outwardly extends and folds to provide a step surface in the extended support position.

Abstract: A foldable multi-rotor UAV includes: a fuselage; and a plurality of arms, wherein a first end of each of the arms is connected to a side face of the fuselage through a rotating mechanism; a motor and foldable blades connected to the motor are provided on a second end of each of the arms; each of the arms rotate relatively to the fuselage through the rotating mechanism; wherein the arms comprises a front arm and a rear arm; during a folded state, the rear arm upwardly rotates towards the fuselage for folding, in such a manner that the rear arm is contained at a lower portion of the side face of the fuselage; then the front arm upwardly rotates towards the fuselage for folding, in such a manner that the front arm is contained at an upper portion of the side face of the fuselage.

Abstract: The aircraft defines a lifting volume including at least part of the central body housing the transported payload. Said volume has a conventional aerodynamic profile along the longitudinal direction of the aircraft, with portions of wings projecting symmetrically and transversely at both sides thereof. From the longitudinal axis said wings at each side shows corresponding first sections with negative dihedral and forward swept until reaching corresponding inflexion points from which two distal second sections or tracts projects with positive dihedral and back swept until reaching the wingtips of the projected wingspan.

Abstract: Example apparatus and methods are disclosed herein for moving control surfaces on an aircraft wing to control airloads during a wing tip folding operation (from a folded position to an extended position or from an extended position to a folded position). An example method includes determining a position of a control surface on a wing of an aircraft. In the example method, the wing has a fixed wing portion and a wing tip moveably coupled to the fixed wing portion. The example method includes determining a change in the position of the control surface from a first position to second position for facilitating movement of the wing tip while the aircraft is not in flight. The example method also includes moving the control surface to the second position and moving the wing tip between an extended position and a folded position.

Abstract: A method and apparatus for controlling movement of an aircraft. An aerodynamic function desired for controlling the movement of the aircraft at a particular altitude is identified. The aerodynamic function identified is part of a group of aerodynamic functions used to control the movement of the aircraft at a number of different altitudes. A group of inflatable blades is filled with a fluid to a pressure that corresponds to the aerodynamic function. The group of inflatable blades at the pressure has a shape and a group of dimensions that provide the aerodynamic function.

Abstract: A method and system delay the laminar-to-turbulent transition of a supersonic or hypersonic boundary layer flow moving in a flow direction over a surface. For supersonic boundary layer flow, oblique first-mode instability waves present in the boundary layer and propagating at an oblique angle relative to the flow direction cause a laminar-to-turbulent transition in the boundary layer flow. These instability waves have a wavelength associated therewith in a direction perpendicular to the flow direction. Flow disruptors are used to generate modulations within the boundary layer flow wherein a wavelength of the modulations along the direction perpendicular to the flow direction is less than one-half of the wavelength of the instability waves.

Abstract: A brake system for an aircraft is provided according to various embodiments. The system may include a left pedal arrangement comprising a left pedal, a first left sensor to generate a first left signal in response to translation of the left pedal. The system also includes a right pedal arrangement comprising a right pedal, a first right sensor to generate a first right signal in response to translation of the right pedal. Normal brake control logic controls the brake system in response to a normal condition being set. The normal brake control logic commands a left brake based on the left signal, and a right brake based on the first right signal. Emergency brake control logic controls the brake system in response to an emergency condition being set. The emergency brake control logic commands a same force to the left and right brakes based the left and right signals.

Abstract: A system for controlling a parking brake system on an aircraft is provided. The system includes a switch interface comprising an enable switch and an activate switch. The parking brake system is configured to switch the state of a parking brake in response to the enable switch and the activate switch being engaged at the same time. A second switch interface also includes an enable switch and an activate switch with the parking brake system configured to switch the state of the parking brake system in response to the second enable switch and the second activate switch being engaged at the same time. The system may also be controlled from a remote and/or virtual location.

Abstract: A controller unit for an aircraft control system includes an interface that is electrically connectable to a controller slot of an electronics bay of the aircraft control system, a processor coupled to the interface, and a tangible non-transitory computer-readable medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform various operations. The various operations include identifying, by the processor, a first aircraft assembly in electrical communication with the controller slot of the electronics bay, identifying, by the processor, a first program code stored on the tangible non-transitory computer-readable medium corresponding to the first aircraft assembly, and selecting, by the processor, the first program code to control the first aircraft assembly.

Abstract: A helicopter silencing system incorporating two muffler assemblies mounted surrounding the body and propeller areas of the aircraft so as to reduce and dampen outputted sound to silence the aircraft. The cockpit contains, or otherwise being contained at a remote location, exists, a switch (pushbutton), for causing and initiating a response so that the two installed muffler assemblies discharge from the aircraft via electromechanical means. The construction of each muffler assembly comprises two installable pieces comprising multiple mufflers so shaped to formate around the majority of the helicopter body, extending upward at curvature or angular formations, surrounding portions of the propeller.

Abstract: An electric propulsion system includes a mast defining an axis of rotation. At least one yoke is rotatably mounted to the mast. A fairing assembly surrounds the at least one yoke. An electric motor includes a stator assembly associated with the fairing assembly and a rotor assembly associated with the yoke.

Abstract: A control horn arrangement includes a control horn body with an inboard end and an opposed outboard end. The control horn body defines a torque tube axis which extends between the inboard and outboard end of the control horn body. An inner flange and an outer flange are disposed on the outboard end of the control horn body. The inner flange and the outer flange extend about the torque tube axis and define between one another a receptacle to fix a torque tube to the outboard end of the control horn body.

Abstract: A lead-lag damper arranged inside a blade of a rotor of a rotary wing aircraft. The lead-lag damper (comprises an inner strength member provided with a cage in which a ball-joint connection is arranged, an outer strength member for securing to the blade, and an elastomer material member arranged between the two strength members. The two strength members and the elastomer material member extending beyond the zone around the cage so that the relative movements between two strength members resulting from the movements of the blade are damped by deformations of the elastomer material member, at least a portion of the lead-lag damper being designed to occupy a portion of the inside of the blade that is conventionally filled with foam.

Abstract: A technical object of the present invention is to provide an unmanned aerial vehicle capable of performing a position movement while maintaining posture stabilization. To this end, the unmanned aerial vehicle of the present invention includes: a main body unit; a plurality of propeller motors of which the rotational speed is adjusted by the main body unit; supports which extend from the main body unit in order to support the plurality of propeller motors; propellers which are axially coupled to the plurality of propeller motors and output thrust; and tilting units which tilt rotating shafts of the propellers with respect to the main body unit.

Abstract: A multicopter with angled rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a plurality of rotors. At least some of the rotors are disposed on opposite sides of the fuselage and each is oriented at a corresponding angle to a substantially horizontal plane of the aircraft, the angle being of a magnitude such that a plane of rotation of the rotor does not intersect at least a critical portion of the fuselage.

Abstract: Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.

Abstract: A method for selecting an operation mode of a mobile platform includes detecting a height grade of the mobile platform and selecting an operation mode of the mobile platform according to a result of the detecting.

Abstract: An unmanned aerial vehicle (UAV) with audio filtering components includes a background noise-producing component, a background microphone, and a noise emitter. The background noise-producing component is configured to produce a background noise. The background microphone is positioned within a proximity sufficiently close to collect interfering noise from the background noise producing component. The background microphone is configured to collect audio data including the background noise. The noise emitter is disposed within a proximity sufficiently close to the background noise-producing component to reduce the interfering noise. The noise emitter is configured to emit an audio signal having a reverse phase of the audio data collected by the background microphone.