Abstract: A blocking component for vehicle is used in a detection structure for vehicle including a bumper beam and a detection component. The bumper beam is mounted on a vehicle to maintain a bumper of the vehicle, and has a side end portion and an opening opened at the side end portion. The detection component is mounted at an inner side portion of the vehicle and located near the side end portion of the bumper beam. The blocking component for vehicle is mounted on the side end portion of the bumper beam to block the opening. The blocking component includes: an outer peripheral edge portion abutted against the outer peripheral edge of the side end portion; and a protruding portion extended from the opening into an inside of the bumper beam. At least a portion of the protruding portion is abutted against an inner wall surface of the side end portion.

Abstract: A vehicle door structure includes a door sash that includes an outer door sash, an inner door sash, and an auxiliary bracket. The outer door sash is provided on an outer side of the door sash in a vehicle width direction and forms a glass guide for a door window. The inner door sash is provided on an inner side of the door sash in the vehicle width direction and coupled to an inner side of the outer door sash in the vehicle width direction. The auxiliary bracket extends in a vehicle vertical direction on a rear portion of the door sash and is interposed and coupled between the outer door sash and the inner door sash. The auxiliary bracket is provided so as to cover a gap between the outer door sash and the inner door sash at an upper rear corner of the door sash.

Abstract: A headrest mounting assembly for mounting a headrest on a cross member of a seat back includes a mounting bracket having a centre portion, a first side portion and a second side portion. A first guide channel is provided for receiving a first headrest interconnecting member; and a second guide channel is provided for receiving a second headrest interconnecting member. The first and second guide channels are fastened to the centre portion of the mounting bracket. The first side portion is disposed outboard of the first guide channel on a first side of the mounting bracket; and the second side portion is disposed outboard of the second guide channel on a second side of the mounting bracket. The first and the second side portions are each configured to be fastened to the seat back outboard of the first and second guide channels respectively.

Abstract: The present invention relates to a body (2), at least one engine (3) that is located on the body (2) and generates the power required for flight, at least one air inlet (4) that is located as an opening on the body (2) and allows air intake from the atmosphere, at least one air duct (5) that is located on the air inlet (4) and transmits the air it takes from the air inlet (4) to the engine (3), at least one panel (6) that is located inside the air duct (5), to which the air contacts after passing through the air inlet (4), has radar absorbing properties and allows the air to absorb the electromagnetic waves that come into contact with its surfaces.

Abstract: An extending cargo restraint assembly for a cargo handling system mobile is provided. The extending cargo restraint assembly includes a base assembly, The base assembly includes a primary plunger and a secondary plunger. Responsive to be activated, the primary plunger is configured to extend in a first direction into an opening within a modular container thereby restraining the modular container in a second direction, the second direction being perpendicular to the first direction. Responsive to being activated, the secondary plunger is configured to extend in the second direction within the opening of the modular container thereby further restraining the modular container in the second direction.

Abstract: A rear side member is provided with a first bead that is set so as to be weaker than other portions of the rear side member. The first bead is set so as to induce deformation of the rear side member toward a vehicle width direction inner side and toward a lower side when a collision load is input from a rear cross member at a time of a rear collision of a vehicle, and when the collision load is input from the rear cross member at the time of a rear collision of the vehicle, the rear side member is deformed toward the vehicle width direction inner side, and is deformed toward the lower side, with the first bead as a starting point.

Abstract: A vehicle body 1 includes a center pillar 4 and a side sill 5. A front portion 5a and a rear portion 5b of the side sill 5 are restricted from moving inward in a width direction at a front restricting position X2F and a rear restricting position X2R, respectively. The center pillar 4 includes an overlapping portion 22 that covers an external surface of the side sill 5. A center position of the center pillar 4 is specified as X0, a front end position of the overlapping portion 22 from the center position X0 is specified as X1F, and a distance from the center position X0 to the front restricting position X2F is specified as L0. A distance from the center position X0 to the end portion position X1F is specified as L1. A ratio L1/L0 between the distances is 0.36?L1/L0?0.48.

Abstract: A front frame structure for an electric vehicle includes: front side frames extending in a front-rear direction of a vehicle body and disposed on both sides in a vehicle width direction of a motor room in a front portion of the vehicle body; impact absorbing members disposed at front ends of the front side frames; a bumper beam coupling the impact absorbing members; and a lower frame disposed in a lower portion of the motor room and having both sides supported by the front side frames. The front side frames are in extra spaces each defined with a side wall of the motor room and a side surface a power control unit. A frame-shaped rigid member is disposed in an extra space in a front of the motor room. The front side frames and the impact absorbing members are coupled respectively to rear and front surfaces of the rigid member.

Abstract: A vehicle window assembly and an assembly method therefor, and a vehicle. The vehicle window assembly includes an exterior decorative member, an encapsulation assembly, and a guide rail. The encapsulation assembly is disposed around a periphery of the exterior decorative member and wraps at least part of the periphery of the exterior decorative member. The encapsulation assembly has a first end and a second end in a direction of an edge S of the exterior decorative member, and the second end is far away from the first end. A limiting groove is defined at the first end of the encapsulation assembly. The guide rail has one end inserted into the limiting groove to limit the guide rail from moving. The guide rail is connected to the second end of the encapsulation assembly to fix the guide rail to the encapsulation assembly.

Abstract: The present invention provides a security partition having a quick release emergency release system for a vehicle comprising: a partition frame attached to a front partition panel and a release partition panel having a release partition pin interface, partition locking interfaces, and an emergency panel system having a panel, at least one handles, panel locking means, and quick release locking means; wherein in emergency conditions, the panel locking means and the quick release locking means are activated to quickly disengage the panel from the release partition to provide an emergency exit for the secured occupant area of the vehicle.

Abstract: The present disclosure relates to a method for fixing a flight vehicle during transportation and a MaaS providing method. A method for fixing a battery-driven flight vehicle during transportation that includes fixing the flight vehicle by connecting a predetermined portion of the flight vehicle and a moving body by a wire.

Abstract: An aerial drone system includes: a drone configured for flying, for being coupled with a user, and for operating autonomously at a separation distance from the user without supporting the user when the user is not fallen; and a control system operatively coupled with the drone and configured for: detecting a fall of the user; using the drone to arrest the fall of the user upon detecting the fall and to support the user in the air; and using the drone to fly the user to a platform.

Abstract: A bumper with a charging port which is closable by a cover that is, by way of a combined drive-and-guide device arranged in the bumper, movable between a closed position in which the charging port is covered by the cover and an open position in which the charging port is exposed by the cover. In order to simplify the manufacture of bumpers, the combined drive-and-guide device is fastened on the bumper to a unit fastening point of an individually customized adapter frame facing the combined drive-and-guide device.

Abstract: A portable headrest to be used with different seating accommodations. The headrest has a pillow adapted for a user to rest against. There is at least one restraining strap. The restraining strap has a pillow end and an attachment end, where the pillow end of the restraining strap is attached to the pillow. There is a connection device attached at each attachment end of the restraining straps. The connection device is adapted to attach the attachment end to a support forward of where the user is seated.

Abstract: A dual-axis adjustment device is provided. The adjustment device comprises a pivoting component configured to allow a top component of a furniture piece to rotate about a first axis with respect to a stand, and a lock component configured to allow the top component to slide relative to the stand along a second axis (BB?). The pivoting component and the lock component are arranged along a common axis (AA?), the first axis is a rotational axis, and the common axis (AA?) is co-axial with the first axis and perpendicular to the second axis (BB?). Further disclosed are a leg rest comprising a top component, a stand and a dual-axis adjustment device, and a method of manufacturing a dual-axis adjustment device.

Abstract: An assembly with a continuous structural element for aircraft and a fitting. The continuous structural element has an outer flange, an inner flange and a web between the flanges. The inner flange has at least one portion with a wavy shape such that the height of the web increases or decreases in that portion. The fitting has at least one through hole and is configured to fit the web at the portion of the inner flange with a wavy shape so that in an assembled state the fitting is joined to the web in such a way that the at least one through hole of the fitting is not covered by the web.

Abstract: A wind harness for a vehicle includes a low profile duct intake that extends along a roof and sides of a vehicle. At least one duct extends from the duct intake on each side of the vehicle. The ducts are positioned in the rear pillars directing air and through along the pillars. A wind turbine is positioned inside a body panel of the vehicle. The ducts have an exhaust nozzle directed at the turbine for delivering an air flow to rotate the turbine.

Abstract: A screen system for use in a window of a vehicle. The screen system includes a screen, a spool mounted to a leading edge of the screen, a housing configured to be mounted at a first edge of the window, and one or more bands that are operatively connected to the screen and configured to apply a biasing force to the screen. The screen is movable between a retracted position and an extended position. The retracted position includes the screen rolled onto the spool and with the screen and the spool positioned in the housing at the first edge of the window. The extended position includes the screen extending across the window.

Abstract: A wing assembly has a flexible cover which is movable between an extended position and a retracted position. In the extended position the flexible cover covers the leading edge of the wing assembly, thereby protecting the front of the wing assembly from impact by dirt or debris and preserving the smoothness of its surface. In the retracted position the flexible cover does not cover the leading edge of the wing assembly.

Abstract: A rotorcraft with a fuselage and a tail boom, comprising: a horizontal stabilizer mounted to the tail boom; rotor blades with rotor blade tips which form a virtual blade tip circle upon rotation around a rotor head; luminescent components provided on the rotor blade tips; and a blade tip illumination device comprising at least one light source integrated into the horizontal stabilizer and configured to emit a light beam toward the virtual blade tip circle for excitation of the luminescent components; wherein the luminescent components emit light in response to excitation via the emitted light beam, and wherein the emitted light forms during rotation of the rotor blade tips around the rotor head on the virtual blade tip circle a luminous ring.