A constant velocity universal joint includes outer and inner joint members that transmit torque while allowing angular displacement via balls, a power transmission shaft connected to the inner joint member in a torque transmittable manner, and a detachable mechanism between the inner joint member and the power transmission shaft to detach the power transmission shaft from the inner joint member. The detachable mechanism includes a cylindrical member externally fit onto the power transmission shaft, spheres movable in a radial direction in the cylindrical member, and an annular member movable in an axial direction on an outer periphery of the cylindrical member. Locking claws are provided at an end of an inner joint member side of the annular member, and a locking groove is provided at an end of an annular member side of the inner joint member. The locking claws are fitted into the locking groove.

Rattling of a vehicle-mounted equipment supported by a bracket is restricted. The attaching structure 1 for vehicle-mounted equipment has a housing 20 of vehicle-mounted equipment; an engagement arm 40 provided in the housing 20; a bracket 10 fixed to a vehicle body; and an engagement hole 13 formed in the bracket 10 to be engaged with the engagement arm 40, the engagement arm 40 is formed with a predetermined width along with one side edge 131 of the engagement hole 13 and is capable of being displaced in an engagement direction (the longitudinal direction of the center line Lm) to the engaged portion 135 formed on one side edge 131 of the engagement hole 131, the engagement arm 40 inserted into the engagement hole 13 being elastically engaged with the engaged portion 135 of the engagement hole 13 to attach the housing 20 of vehicle-mounted equipment to the bracket 10, wherein engagement members 50 and 50 are provided independently of the engagement arm 40 on both sides of the engagement arm 40 in the width direction thereof to be capable of being displaced in the width direction (the radial direction of the center line Lm), elastically engaging the engagement members 50 and 50 with the other side edges 133 and 134 of the engagement hole 13.

The disclosed technology includes a control wire clamp for securing a control member, such as a control wire, in place. The default state of the control wire clamp may be a clamped state. The control wire clamp may be placed in an unclamped state by applying force to a clamp handle.

To develop a conventional coupling for transmitting a driving force.

A coupling member is provided with a supporting portion for movable supporting a driving force receiving portion for receiving a driving force.

A locking spanner assembly for an aircraft is disclosed. A clasp can be secured to an anchor by urging the clasp onto the anchor. The anchor contacts a trigger which opens a gate assembly to release a locking member which locks to the anchor. A lever arm allows for release which resets the clasp.

A clip (2) for fitting between a first component (6) and a second component (4) in a building structure, the clip including a first member (8), a second member (10) and a connecting portion (12) connecting the first member (8) to the second member (10); the first member (8), the second member (10) and the connecting portion (12) forming a space (38) in which a portion of a leg (18) of the second component (4) is adapted to reside; the first member (8) and the second member (10) adapted for engagement with the portion of the leg (18) of the second component (4).

A ramp assembly comprises a support defining each of a vertical axis and a horizontal axis, a ramp being coupled to the support and being configured to support an passenger thereon. An optional actuator mechanism may be coupled to at least one of the support, the ramp, a power source and a controller, the actuator mechanism configured, in a response to a control signal from the controller or in a response to a manual force, to rotate the ramp about the vertical axis between a stowed position and a deployed position or rotate the ramp about the horizontal axis between the deployed position and a ground engaging position. The actuator may comprise a motor with a gearbox and two gears to rotate the ramp about the vertical axis. The actuator may comprise a linear actuator to rotate the ramp about the horizontal axis.

A tool for inserting or removing a tang-free wire thread insert is described, the entraining blade of which is manually fastenable and replaceable within the axial recess of the spindle body by means of a latching connection. In addition to the secure removal of wire thread inserts, this tool construction also ensures a quick replacement of worn entraining blades of the tool. Furthermore, a production method for such a tool is described.

The invention relates to a fuel dispensing unit comprising a fuel conduit comprising an external annular bead, and a locking member comprising inwardly extending resilient tongues and the being arranged to retain the fuel conduit in a locked position and receive the fuel conduit in an open position, wherein the external annular bead of the fuel conduit is arranged to put the locking member in the open position when receiving.

A respiratory mask system is provided. The respiratory mask system has a patient interface that is secured to a user's head by a headgear. The patient interface comprises a seal, a frame and a gas delivery conduit. The frame is configured to secure the seal and gas delivery conduit together. The frame comprises a recessed channel and/or headgear retaining features configured to connect the headgear to the patient interface. The frame can include an inlet collar that connects to a gas delivery conduit. The inlet collar can include bias flow holes. The headgear comprises a top strap, a pair of side arms, a yoke and a rear strap. The yoke is configured to connect to the recessed channel of the frame. The top strap, side arms and yoke form an integrally formed closed loop. The top strap can include two portions adjustably connected to each other.