An apparatus permitting VESA compliant devices to be mounted onto a flat surface, or placed onto a mobile, securable, and rotatable base plate is disclosed. The apparatus consists of a hollow stem with two (2) ends, one which can be affixed to a “VESA mounting plate”, with the opposing end affixed onto a flat surface directly flush, onto a base, or other mounting plate. The stem ends and accessory components are engineered to permit fast installation and support for multiple mounting options for on-surface or behind-the-surface mounting, as well as standalone mounting with theft-deterrent features, plus support for add-ons that permit easy lateral rotation of the assembly with cable management.

A latch includes a ferrule defining a hollow interior region and a ferrule opening that opens into the hollow interior region. A washer is positioned adjacent an end of the ferrule. The washer defines a washer opening. A stud has an elongated body extending along a stud axis, and the stud is positioned to extend through the ferrule opening and keyed to the washer opening such that the stud rotates about the stud axis along with the washer. A lever is pivotably connected to the stud. Rotation of the lever about the pivot axis causes translation of the stud along the stud axis with respect to the ferrule between a latched position, in which an end of the stud protrudes beyond a connection end of the ferrule, and an unlatched position, in which the end of the stud is contained within the interior region defined by the ferrule.

A radio frequency identification host, which includes: a host body (1) for radio frequency identification, a mounting structure (2) is provided at one end of the host body (1) for fixing the radio frequency identification host body (1) on an external holding pole, the mounting structure (2) includes a first mounting frame (21) fixedly connected to one end of the host body (1), a hinge of the first mounting frame (21) is connected with a second mounting frame (22), and the second mounting frame (22) is fixedly connected to the first mounting frame (21) by bolts (23).

The mounting system and device secures a container, such as a lockable container to a pole. A housing restricts access to the fasteners and other attachments that secure the container to the pole. A unitary fastener, such as a U-bolt, secures the housing to the pole. The two ends of the unitary fastener enter a first section of a rear wall and a second section of the rear wall to attach to the housing at an interior attachment surface. A curvature in the rear wall separates the first section and the second section of the rear wall. The curvature of the rear wall contacts the pole. The housing, the guard plate, and the container cover the fasteners to reduce access to the fasteners.

A security apparatus for a launch monitor comprises a guide member extending from a first end to a second end. The guide member comprises a top surface defining one or more top surface features, and opposing side surfaces defining one or more side surface features. A mount is configured to moveably couple to the guide member. The mount comprises a mount body, and a plurality of securing members. Each of the securing members includes a retainer configured to retain and secure a portion of the launch monitor to the mount body and enable the launch monitor to be moved relative to the guide member.

The present disclosure provides a linkage structure including an upper bracket and a lower bracket, wherein said upper bracket includes a first linkage unit, a second linkage unit, a middle piece and two sets of adjusting pieces, one end of said middle piece is connected to said first linkage unit and the other end is connected to said second linkage unit; wherein at least one adjusting piece in each set of adjusting pieces is connected rotatably to said first linkage unit or said second linkage unit. According to the linkage structure of the present disclosure, mechanical tilt can be achieved by driving two sets of adjusting pieces to move in coordination, it can ensure the accuracy of mechanical tilt, realize mechanical tilt at any angle, and the operation process is friendly and safe.

The present invention relates to a device and a method associated with the device. With respect to the device, it is a structural connector for fastening structural components in insulated concrete formwork (ICF). The structural connector consists of a double threaded cylinder bolt assembly that aligns through openings in the ICF wall. One end of the cylinder bolt assembly embeds into the cavity of the ICF wall where openings in the cylinder bolt assembly receive concrete and reinforcement bars. The other end of the cylinder bolt assembly is threaded to receive a double threaded washer head bolt. The cylinder bolt assembly is used to mount ledger boards, floor joist hangers and roof truss connectors to the ICF wall, locking them together acting as one unit in withstanding bending and uplift loads imposed by large forces such as floor and roof truss systems.

The sensor adaptor includes a case body of which a front end is closed and a rear end is open, a cap body being engageable with the rear end of the case body, a seal member interposed between the case body and the cap body, and a fixing portion configured to fix the case body to the mounting portion. A part of the sensor is inserted into an accommodation space of the case body, and the remaining portion of the sensor is drawn out to the outside via an opening of the cap body. The seal member is disposed on a rear end side of the case body to surround the sensor. The seal member is brought into close contact with the case body and the sensor. Accordingly, a gap between the part of the sensor and the case body is sealed from an external space by the seal member.

The present embodiments relate to a novel clamping assembly. More specifically, present embodiments relate to a clamping assembly for blind flange installation which provides an air tight seal for piping applications including, but not limited to, low pressure high-density polyethylene (HDPE) piping applications.

A linking part for an aircraft is disclosed having an elongated section including an internal longitudinal seat and a tenon mounted in the seat. The tenon includes a linking element at a free longitudinal end thereof and configured in a retracted position in which the tenon is fully inserted in the seat and does not create an obstruction, enabling the linking part to be easily moved towards the support element, or a deployed position (P2) in which the free longitudinal end of the tenon is outside the seat and is able to be linked using the linking element to the support element, thereby enabling a link to be made simply and quickly.