Abstract: A connectable dolly having a platform with an upper surface, a peripheral edge and a bottom surface, a plurality of caster wheels extends from the bottom surface and are attached thereto, and a connector element is mounted to the platform proximal the peripheral edge and is moveable from a stored position to a deployed position, the connector element having a proximal end and a distal end, the distal end having an engaging member dimensioned for removably connecting the connectable dolly to a second dolly.

Abstract: A steering system for a motor vehicle includes a steering handle for manual actuation of the steering system, at least one steerable motor vehicle wheel which can be mechanically coupled to the steering handle, and a steering column which is rotatable about a steering-system axis and has an input shaft connected fixedly to the steering handle and an output shaft connected to the at least one steerable motor vehicle wheel for rotation therewith. A steering-system-blocking element is connected fixedly to a body of the motor vehicle. A locking device can either enable or block a relative rotation between the input shaft and the body-mounted steering-system-blocking element. A coupling device can either enable or block a relative rotation between the input shaft and the output shaft.

Abstract: A connector assembly body has: on an end surface on an opposite side to an output side of a motor; a large-current connector of a power supply system, with large-current connector being disposed in the same direction as the motor output shaft; a small-current connector of a signal system, with the small-current connector being disposed in the same direction as the motor output shaft; and a component mounting section including at least one of a capacitor and a coil, and the large-current connector, the small-current connector and the component mounting section are disposed separately in respective regions.

Abstract: A system for actively damping a power steering system includes a damping activation module that generates a damping activation signal based on a motor velocity signal, a t-bar torque signal, and a final motor command; a command calculation module that generates a calculated command based on the motor velocity signal and a vehicle speed signal; and a damping calculation module that generates a damping command based on the damping activation signal and the calculated command, the damping command reduces a motor velocity of a motor of the power steering system to mitigate a rack disturbance.

Abstract: A vehicle steering device includes: a target-steered-angle setting unit configured to set a left target steered angle that is a target value of the steered angle of a left steered wheel and a right target steered angle that is a target value of the steered angle of a right steered wheel; left motor controllers configured to control a left steering motor based on a left-steered-angle deviation that is a difference between the left steered angle and the left target steered angle; right motor controllers configured to control a right steering motor based on a right-steered-angle deviation that is a difference between the right steered angle and the right target steered angle; and an abnormality determination unit configured to determine that an abnormality has occurred when an absolute value of difference between the left-steered-angle deviation and the right-steered-angle deviation is equal to or larger than a first threshold.

Abstract: Provided is a steering control device that more appropriately performs a limiting function for a controlled variable having an abnormal value even if a plurality of kinds of state quantities that are used for steering control include a state quantity that does not meet a required level of reliability. The range of variation in first assist controlled variable calculated by using steering torque, a steering torque differential value, and a steering velocity, namely state quantities for which the required level of reliability is ensured, is limited by final limiting values calculated based on first to third limit maps. The range of variation in compensation amount calculated by using a steering angle, namely a state quantity for which the required level of reliability is not ensured, is limited by predetermined upper and lower limits. A variation in compensation amount per unit time is limited by a predetermined variation limiting value.

Abstract: A steering control system is disclosed for use with a machine. The steering control system may have left and right motors, at least one input device configured to generate first and second signals indicative of desired speed and desired steering, a left speed sensor configured to generate a third signal, and a right speed sensor configured to generate a fourth signal. The steering control system may further have a controller configured to determine a difference between desired and actual steering based on the second, third, and fourth signals, to determine a steering command change that should be implemented based on the difference, and to determine a gain based on the second signal. The controller may also be configured to adjust the steering command change as a function of the gain, and to selectively apply the adjusted steering command change to one of the left and right motors.

Abstract: A vehicle includes steering devices configured to change a travel state of the vehicle between a normal travel mode and a special travel mode by steering right and left wheels in right and left opposite directions; a display device; and a processor configured to calculate an angle difference between the angle of each of the right and left wheels in either one of the normal travel mode and the special travel mode, and the current angle of each of the right and left wheels, which have been steered by the steering devices. The processor is further configured to display, on the display device, information necessary for a driver to steer the right and left wheels based on the angle difference.

Abstract: When an object detected by a lane marking/object detection section has been determined to be an object present in an adjacent lane change target lane or in the vicinity of the adjacent lane, lane change control is performed to reduce a predetermined maximum lateral acceleration Aymax? or maximum lateral velocity Vymax? according to the lane width Lob of the adjacent lane.

Abstract: An upper wheel fairing assembly for increasing the propulsive efficiency of a wheeled vehicle having wheels otherwise exposed to headwinds, comprising a deflector panel or skirt panel assembly mounted upstream in front of a wheel set, extending downward to not lower than the axle level, and arranged to deflect headwinds from impinging upon the high drag-inducing mechanically advantaged upper wheel surfaces downward onto the low drag-inducing mechanically disadvantaged lower wheel surfaces.

Abstract: A system is configured to control aerodynamics of a vehicle. The vehicle includes a vehicle body arranged along a longitudinal axis with a first vehicle body end configured to face incident ambient airflow. The system includes an aerodynamic-aid element mounted to the vehicle body and configured to generate a downforce thereon via controlling the incident ambient airflow. The system also includes an adjustable flap arranged at the aerodynamic-aid element. The adjustable flap is configured to shift relative to the aerodynamic-aid element and thereby control movement of the incident ambient airflow relative to the aerodynamic-aid element. The system additionally includes a mechanism configured to vary position of the adjustable flap relative to the aerodynamic-aid element and thereby vary a magnitude of downforce generated by the aerodynamic-aid element.

Abstract: The present invention relates to a wheel air gap for a motor vehicle of which according to the invention at least one section of the wheel air gap open air comprises a sound-absorbing material.

Abstract: The present invention is directed to modifications to driving flexible tracks, typically of the type used on small excavators and tractors. The present invention provides a second outer sprocket arrangement to engage with outer guard teeth on the track, these being present on a number of proprietary flexible track arrangements to act as an antifouling measure.

Abstract: An elastic crawler includes an endless elastic body; cores that each include a core body and a pair of protrusions; lugs, on the outer circumferential side of the elastic body, each disposed so as to avoid a crawler circumferential direction area corresponding to at least a portion of the core in the crawler circumferential direction; and grooves, on the crawler inner circumferential surface, each positioned outward in the crawler width direction from the pair of protrusions in a crawler circumferential direction area corresponding to the core, each of the grooves being recessed relative to crawler inner circumferential surface portions adjacent to the groove on both sides in the crawler circumferential direction.

Abstract: The present disclosure provides a method of manufacturing a hybrid side sill for an automobile. The method includes a step for forming a pultruded profile part including a continuous fiber reinforced thermoplastic polymer, which has a heat deflection temperature of at least 200° C., and a step for attaching a terminal part made of steel to an end portion of the pultruded profile part.

Abstract: The invention is a utility belt used to alert vehicles and pedestrians to the presence of a cyclist through a built-in LED lighting device. Another function of the safety utility belt is to alert vehicles and pedestrians of the direction the cyclist intends to turn by the use of built-in LED turn signal indicators. The utility belt is composed of a shock resistant, water resistant, silicone rubber belt. The electronics associated with this belt are encased within the silicon rubber belt to protect the electronics from shock and weather conditions. The cyclist has complete control over the brightness and alternating frequency or speed of the warning lights. This allows the cyclist to adjust to various traffic conditions. The cyclist can control whether the LED warning lights will be flashing or non-flashing. This adjustment allows the cyclist to use the non-flashing lights when cycling with other cyclists, therefore not interfering with the vision of other cyclists.

Abstract: A light device includes a light engine. A plurality of petals extends radially outward from the light engine. A trim is disposed over the petals and light engine. An installation card is disposed between the trim and the petals and includes an elongated opening. A strap extends through the elongated opening of the installation card. A light-emitting diode is connected to the light engine. A support component is formed on a surface of the petals. The strap includes a hook surface and a loop surface opposite the hook surface. The installation card includes a second elongated opening formed near an edge of the installation card and a third opening formed in a central region of the installation card. A plurality of straps includes a width of the straps being less than a width of the elongated opening. The plurality of straps includes a zip tie.

Abstract: The present invention provides a generator for a bicycle which can be applied to a rim of all kinds of bicycle wheels, comprising: a rotating body 30 which is arranged to be adjacent to or to make contact with the rim 10, wherein eddy current induction magnet 35 is installed along an outer circumferential surface of the rotating body 30; a rotation shaft 62 whose one side end part is fixed at a center of the rotating body 30; and a generation unit 60 which is arranged at the other side end part of the rotation shaft 62, wherein at least a portion of the outer circumferential surface of the rotating body 30 is arranged farther outside than an outer circumferential surface of the eddy current induction magnet 35.

Abstract: A device for providing improved safety in using a side stand for parking the two wheeled vehicle is disclosed

Abstract: A bicycle component fixing structure includes at least one bracket including at least one connecting portion and at least one fixing portion. The connecting portion is connected to the bicycle component. The fixing portion extends from the connecting portion and is fixed with respect to an outer peripheral surface of a cylindrical portion having an open end. The fixing portion includes at least one inner surface that opposes an outer peripheral surface of the cylindrical portion, and at least one outer surface that faces in the opposite direction from the inner surface. The fixing portion is fixed to the outer peripheral surface of the cylindrical portion by a pressing force that acts on the outer surface. The bracket fixes the bicycle component to the open end of the cylindrical portion, in a state in which the fixing portion is fixed to the outer peripheral surface of the cylindrical portion.

Abstract: A communication system comprises a distance calculator configured to sense objects approaching from the rear and or sides of a moving body. Particularly, the communication system is able to indicate that an object may be too close and/or approaching the moving body at an unsafe speed and/or an unsafe closure rate. In response the communication system is able to generate a response. For example, in some embodiments, the response is an external indicator that the object is too close and/or approaching the moving body. Alternatively, or in conjunction, the communication system is able to generate a warning to the moving body that an object is approaching. The warning is able to alert the moving body that the object is in the area and/or may be approaching the moving body.

Abstract: The disclosure discloses a device for detecting a driving mode of a self-balancing vehicle including: a detecting system comprising at least one detecting mechanism (102) each of which (102) is installed at each detecting point under a pedal (101) of the electric self-balancing vehicle and is used for detecting whether the pedal (101) deforms at a corresponding detecting point and sending the detection result to the controller; and the controller for judging whether the pedal (101) deforms according to the detection result sent by each detecting mechanism (102) and then determining current driving mode of the electric self-balancing vehicle. The driving mode includes a manned mode and an unmanned mode. The disclosure also discloses a method for detecting a driving mode of a self-balancing vehicle. The disclosure can prevent the electric self-balancing vehicle from entering an action state caused by a misoperation of the driver and eliminate potential dangers.

Abstract: A bicycle rear wheel suspension systems. In one aspect, a bicycle rear wheel suspension system is provided comprising a bicycle rear wheel suspension system comprising a frame comprising a bottom bracket and a first chain stay, the system further comprising a rear wheel comprising an axle, and a first linkage member pivotally connected with respect to the first chain stay at a first main pivot point, the first linkage member extending rearwardly to bridge the main pivot point and the axle, wherein the main pivot point is in a position higher than the bottom bracket, and closer to the axle than it is to the bottom bracket, and wherein at least the first linkage member further comprises a pivotable connection point for a shock absorbing mechanism bridging this connection point and a portion of a remainder of the frame. Further, a bicycle comprising the rear wheel suspension system is provided.

Abstract: A method and device for operating an electric bicycle that has an electric motor and a transmission with at least two gears is provided. The method includes ascertaining a current pedal frequency that is generated by a user of the electric bicycle and checking whether the ascertained current pedal frequency lies within a specified pedal frequency interval. The method also includes ascertaining a current travel speed of the electric bicycle, ascertaining at least two transmission gears within the specified pedal frequency interval depending on the ascertained travel speed, and ascertaining a respective output of the electric motor for each of the ascertained at least two gears. The method also includes ascertaining the lowest ascertained output of the electric motor by comparing the two ascertained outputs of the electric motor, and ascertaining the transmission gear for which the lowest output was ascertained.

Abstract: An electrically assisted bicycle includes a motor controller that calculates a command value which determines a magnitude of an assisting torque based on at least an output of a pedal torque detector. The motor controller switches between a first control and a second control, in which a time required for the assisting torque to change to meet a change in the pedal torque is shorter and the amount of change in the assisting torque to meet a change in the pedal torque is greater than in the first control.

Abstract: An electrically assisted bicycle includes an electric motor which applies a walk-push assisting torque to a rear wheel of the bicycle when a rider propels the bicycle by pushing it while walking, and a motor controller configured or programmed to execute a first mode in which the electric motor applies no torque to the rear wheel, a second mode in which the electric motor applies to the rear wheel a stay assisting torque which causes the electrically assisted bicycle to stay in a position where the rider wants to stay, and a third mode in which the electric motor applies the walk-push assisting torque to the rear wheel, wherein the first mode, the second mode, and the third mode are able to be selected by using an operator able to be operated by the rider.

Abstract: An integrated power module is provided, which may include a power port, battery, controller, motor, and a connection element. The power port may include a first positive electrode terminal, second positive electrode terminal, and a negative electrode terminal. The positive electrode of the battery may be electrically coupled to one end of the first positive electrode terminal. The negative electrode of the controller may be electrically coupled to the negative electrode of the battery and one end of the negative electrode terminal; the positive electrode of the controller may be electrically coupled to one end of the second positive electrode terminal. The motor may be electrically coupled to the output of the controller. The connection element may include a single circuit; the other end of the first positive electrode terminal may be electrically coupled to the other end of the second positive electrode terminal via the single circuit.

Abstract: A bicycle drive unit has a transmission and a motor that transmits torque to the transmission. The transmission includes first and second input side rotating bodies, first and second output side rotating bodies, an output unit and a switching mechanism. The first and second output side rotating bodies are coupled to the first and second input side rotating bodies, respectively. The switching mechanism switches between a first state in which rotation of the first input side rotating body is transmitted to the output unit, and a second state in which rotation of the second input side rotating body is transmitted to the output unit. Only torque of the motor is transmitted from the first and second input side rotating bodies to the output unit, while torque outputted from the output unit merges with a manual drive force in a drive force transmission path from the output unit to a wheel.

Abstract: A bicycle drive unit has a planetary gear mechanism, a switching mechanism, a motor and a housing. The planetary gear mechanism includes an input body, an output body and a plurality of transmission paths having different transmission ratios between the input body and the output body. The switching mechanism is configured to switch between the plurality of transmission paths. The motor is configured to transmit rotational force to the input body. The housing rotatably supports a crankshaft and on which are provided the planetary gear mechanism, the switching mechanism and the motor. A manual drive force that is input to the crankshaft joins with a rotational force that is output from the output body of the planetary gear mechanism in a transmission path of a driving force from the output body of the planetary gear mechanism to a wheel.

Abstract: A hull for low drag boats has, from bow to stern, a deep V-shaped keel (10) whose dead-rise angle decreases up to a flattened bottom (30) in the stern, and sides (20) comprising side chines (200) protruding downward from the flattened bottom that is not inclined upwards.

Abstract: A universal hydrofoil comprises a hydrofoil assembly, a universal mount assembly and a plurality of lateral connectors. The hydrofoil assembly has a longitudinal axis and includes a centerfoil having first and second longitudinal ends. A foil assembly is disposed at the centerfoil second end and includes a fuselage, a wing at a fuselage first end and a tail at a fuselage second end. The universal mount assembly comprises a base having first and second mounting surfaces. The second mounting surface defines a mounting interface configured to reversibly mate with the centerfoil first end. Lateral supports having a pair of arms projecting from a central beam are selectively engageable with the base. The lateral connectors are adjustably secured within the lateral channel and configured to engage a structural feature of a craft.

Abstract: An onboard lift for lifting a boat such as a pontoon boat includes legs that have one end pivotally attached to a bottom substantially horizontal surface of a boat deck. The legs are typically continuous substantially imperforate tubes throughout essentially the entire length. The lower ends of the legs carry support feet or pads. One end of an actuator attaches to an outer side of one of the tubular legs and another end of the actuator is attached to a bottom substantially horizontal bottom surface of the boat deck. The actuators are manipulated to pivot each of the legs between a retracted or stowed position where the legs are substantially parallel to the bottom substantially horizontal surface of the boat deck and a working or lifting position where a pad or foot engages the bottom of the body of water and as the legs are further pivoted downwardly, the boat is lifted upward and out of the water.

Abstract: A cover system for pontoon boats is provided. The cover system facilitates the expeditious covering of a pontoon boat. The cover system includes a plurality of support bows that are laterally extendable across a pontoon boat deck and attachable to the railing of a superstructure thereof. A cover is affixed to a tubular roller that is configured to extend and retract the cover over the plurality of support bows. Support arms disposed at ends of the tubular roller include brackets for mounting the tubular roller onto the superstructure of a pontoon boat and supporting the cover on a side thereof. A handle is attached to the cover for enabling a user to manually extend the cover over the plurality of support bows. The tubular roller is operably coupled to an actuator that is configured to rotate the roller and retract the cover.

Abstract: A boat lift with hydraulically or mechanically actuated arms which self-installs a fitted three-dimensional boat cover on a powerboat. The control logic of the system allows for cover operation only when the lift is raised. A spring-tensioned roller keeps the cover tight and self-rolls the cover on the roller when the actuated arms are pivoted forward. The roller is hidden behind the boat in ‘cover-on’ position. A slip clutch prevents the torsion spring from being over tightened. The forward position of the roller is adjusted by adjusting the hydraulic cylinder length. The rearward position of the roller is adjusted by limiting the retracted position of the hydraulic cylinder. A non-hydraulic embodiment actuates the cover when the lift is operated.

Abstract: A frame for a top of a boat in accordance with the present invention can be moved into an deployed position with the aid of a biasing member such that the manual effort required is minimized. When the frame is in the deployed position a locking member may be engaged to hold the frame and top in the deployed position. When the locking member is disengaged, the frame may be manually collapsed into a stowed position in a controlled and safe manner.

Abstract: A hull support structure of a liquefied gas tank has a foundation deck disposed around a liquefied gas tank; a skirt which supports the liquefied gas tank on the foundation deck; an inner bottom plate extending in a hull length direction, at a location that is below the liquefied gas tank; and a pair of bilge hopper plates each of which is provided between the foundation deck and corresponding one of both end portions of the inner bottom plate, wherein a plate connection section at which each of the pair of bilge hopper plates is connected to the foundation deck is disposed outward in a hull width direction, relative to a skirt connection section at which the skirt is connected to the foundation deck.

Abstract: A buoyancy compensator jacket for scuba diving includes an inflatable and deflatable bladder; a backplate part, to which the bladder and elements fastening at least one breathing gas cylinder are attached; and at least one pair of shoulder straps for securing it to the torso of a user and at least one ventral securing strap or ventral closure of the jacket. The jacket further includes a sternal securing element composed of at least one sternal or chest strap, which has at least one costal connection element distinct from the pair of shoulder straps and connecting the sternal strap to the backplate part.

Abstract: A bionic pectoral fin propelling device based on a planetary gear train, including a frame, a power source (1), a propelling part (2), left and right maneuvering parts (3), a fixed support plate (4), a movable support plate (5), a left pectoral fin (6), a right pectoral fin (7), a fish body (8), and a tail fin (9). The fixed support plate (4) and the movable support plate (5) are installed on the frame parallel to each other; the fixed support plate (4) is located in front of the movable support plate (5); and the left and right maneuvering parts (3) are located between the fixed support plate (4) and the movable support plate (5). The present invention solves the problem that the two pectoral fins are not synchronized, realizes variable speed propelling and left/right maneuvering, facilitates increasing the bearing capacity of the propelling device, and is particularly suitable in limited space applications.

Abstract: A method for decelerating a watercraft is disclosed. The watercraft has a reverse gate and a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least a stowed position and a deceleration position. The method includes: receiving, in a control unit, a deceleration signal from a deceleration device position sensor, the deceleration signal being indicative of an actuated position of a deceleration device; controlling, by the control unit, an operation of the reverse gate actuator based at least in part on the actuated position of the deceleration device; and moving the reverse gate from the stowed position to the deceleration position with the reverse gate actuator, the reverse gate actuator being controlled such that a speed of rotation of the reverse gate depends at least in part on the actuated position of the deceleration device.

Abstract: An aircraft includes a wing and a wing box. The wing is joined to the wing box at a side of body joint. The wing and the wing box each includes lower skin and a plurality of stringers on the skin. Ends of at least some of the stringers at the side of body joint have a web cutout and a base that is spanwise tapered to a knife edge at the skin.

Abstract: An aircraft body and a method of making an aircraft body are provided. In one embodiment, an aircraft body may be molded from a single layer of carbon fiber stock, producing curved sections of single layer molded carbon fiber by molding pliable carbon fiber stock, and heat curing the carbon fiber stock to form a rigid, molded wing section.

Abstract: An aircraft (5) including a wing (7) having a wing tip device (1) configurable between: a flight configuration and a ground configuration in which the span of the wing (7) is reduced. The aircraft (5) further includes a lock (13) for locking the wing tip device (1) in the flight configuration, and an actuator (3) for unlocking the lock (13) and for subsequently actuating the wing tip device (1) to the ground configuration. The actuator (3) is a two-stage hydraulic actuator, including a first hydraulic actuator stage (21) arranged to unlock the lock and a second hydraulic actuator stage (23) arranged to actuate the wing tip device (1) to the ground configuration. The first and second hydraulic actuator stages (21, 23) are arranged in series such that the second actuator stage (23) is unable to receive a hydraulic input feed until the first actuator stage (21) unlocks the lock (13).

Abstract: An aircraft including a wing 10 having a fixed wing 12 and a swing wing tip device 14 pivotably mounted about a pivot 16 at the tip of the fixed wing, wherein the swing wing tip device 14 is configurable between a flight configuration for use during flight and a ground configuration for use during ground-based operations, where the span of the aircraft wing is reduced. The swing wing tip device 14 includes a receiving portion 48 arranged such that in the ground configuration, portions of the upper wing skin and lower wing skin of the fixed wing which are exposed in the flight configuration are at least partially received within the receiving portion 48 of the swing wing 14.

Abstract: A folding wing comprises a fixed section, a folding section, and a latch system for latching the folding section to the fixed section. The latch system includes a plurality of latch pins, and a corresponding plurality of non-backdriveable mechanical actuators for extending the latch pins to engage the folding section.

Abstract: A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.

Abstract: An airfoil includes a proximal end and a distal end opposite the proximal end. The airfoil also includes a distal portion extending adjacent the distal end and an edge extending between the proximal end and the distal end. The airfoil further includes a surface extending between the proximal end and the distal end. The edge and the surface define a sweep and a cahedral through the distal portion and at least a portion of the intermediate portion.

Abstract: In some embodiments, an airfoil comprises a proximal end; a distal end opposite said proximal end; a distal portion extending adjacent said distal end; an edge extending between said proximal end and said distal end; and a surface extending between said proximal end and said distal end, said edge and said surface defining a sweep and a cahedral through said distal portion, wherein the distal portion extends over an acoustically active portion of the airfoil.

Abstract: An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes multiple controllable airflow modification devices coupled thereto. By virtue of having multiple controllable airflow modification devices, the wing extension is capable of adjusting control surfaces of the multiple controllable airflow modification devices in response to in-flight conditions, to reduce wing loads, improve wing fatigue characteristics, increase range, reduce torsional loads, alleviate flutter, and/or increase efficiency.

Abstract: Actuating system for an aircraft comprising: an electromechanical actuator (25) comprising a non-volatile memory (60) wherein stored data (61) including configuration data (62) specific to the electromechanical actuator is stored; a control unit (22) using the configuration data to implement a servo-control loop, the output signal of which is a digital signal controlling the electric motor of the electromechanical actuator; at least one digital transmission channel (50) connecting the control unit and the electromechanical actuator.

Abstract: A device including a profiled member conformed to constitute an edge portion of an aircraft aerodynamic profile. The device includes a blower chamber to be pressurized and an air ejector nozzle making it possible to provide fluidic communication between the blower chamber and an external surface of the profiled member, the profiled member, the blower chamber and the nozzle forming an assembly to be mounted in one piece on the aerodynamic profile to constitute a trailing edge thereof. The blower chamber and the nozzle are formed directly in the profiled member, the profiled member, the blower chamber and the air ejector nozzle being formed in one piece.