Provided is an anti-collision device for LED screen, comprising a box body (1), a telescopic rotating mechanism, an anti-collision sheet (4) and a display module (2); the peripheral side of the box body (1) is provided with a mounting hole (12) and a receiving groove (11); the telescopic rotating mechanism is embedded in the mounting hole (12) and movably connected with the box body (1); the anti-collision sheet (4) is fixedly connected with the telescopic rotating mechanism. When the telescopic rotating mechanism is not subjected to external force, the telescopic rotating mechanism enables the anti-collision sheet (4) to shield the peripheral side of the display module (2) outside the receiving groove (11); when the telescopic rotating mechanism is subjected to external force, the telescopic rotating mechanism drives the anti-collision sheet (4) to retract and rotate to be embedded in the receiving groove (11).

The invention relates to a modular assembly that comprises at least two housing parts (1), in which in each case a circuit board (L) is received, at least one internal connecting means (17), one cover element and one closing element. Each housing part (1) is formed from a base plate (3), a rear wall (5) and side walls (4) that are connected to said rear wall. The housing parts (1) are stacked in such a manner that the side walls (4) combine to form a first (6) and a second complete side wall (7), and that the rear walls (5) combine to form a complete rear wall (8). At least two of the housing parts (1) are stacked in such a manner that the base plate (3) of the one housing part (1) is connected to the side walls (4) of the other housing part (1). The at least one internal connecting means (17) extends in a direction perpendicular to the base plates (3) and connects multiple circuit boards (L) by way of first connectors (18). The cover element lies on the side walls (4) of precisely one housing part (1). The closing element is attached to a front side on the housing parts (1), said front side lying opposite the complete rear wall (8).

One embodiment provides a system, including: a base module housing comprising a top, a bottom, and at least one lateral edge comprising a top side and a bottom side, the base module housing comprising: a processor; a memory device operatively coupled to the processor; and at least one connector, disposed at the top side of the base module housing, for facilitating electrical connections; and a cap module housing comprising a top, a bottom, at least one lateral edge comprising a top side and a bottom side, the cap module housing comprising: at least one receiver, disposed at the bottom side of the cap module housing, for receiving at least one connector; wherein the base module housing and cap module housing are vertically connectable using at least one latch mechanism; wherein at least a portion of the at least one latch mechanism is disposed at the top side of the base module housing; and wherein at least a portion of the at least one latch mechanism is disposed at the bottom side of the cap module housing. Other aspects are described and claimed.

A Common Bus Structure for Avionics and Satellites (CBSAS) (10) as shown in FIG. 1 is comprised of a module lid (14), module floor (38), module stack base (16), module compression bolts (22) and stackable modules (12). Stackable modules (12) are sub-dividable to create module scaled chamber volumes (45) individually as required, while stackable modules (12) simultaneously create at least one collectively continuous raceway sealed chamber volume (44) perpendicular to individual stackable modules (12) in the vertical direction where no module floor (38) is present, in order to internally electrically interconnect the contents of any stackable module (12) with the contents of any other stackable module (12) via internal connector raceway system (24). Raceway sealed chamber volume (44) therefore collectively and continuously traverses all present stackable modules (12) positioned between module lid (14) and module stack base (16). Modules are interchangeable and inter-connectable in any order, and contain all required electronic or mechanical components required for CBSAS (10) to function as a single box consolidated avionics system that is equally functional in the atmosphere or the vacuum of space, while also being fully functional as a single complete stand-alone satellite system. CBSAS (10) enables a paradigm shift in the aerospace industry whereby all legacy and current multiple black-box systems on aerospace platforms such as missiles, rockets, satellites and aircraft are extremely inefficient when compared to the size, weight and power attributes of CBSAS (10). The ability for CBSAS (10) to be instantly employable as either a single box consolidated avionics system for use within the atmosphere or in space while also being fully functional as a stand-alone satellite enables a hardware, firmware and software capability never before manifested in the aerospace industry.

A shielding cage with an improved construction is disclosed that permits such cages to be more closely spaced together when a plurality of them are arranged in side-by-side arrays of cages. The cage is formed from a sheet metal blank that is stamped and formed to define sidewalls, top wall, bottom wall and a rear wall. In one embodiment, the ends of the blank are formed with interengaging elements in the form of tabs and slots that interfit within the plane of one of the cage walls, thereby eliminating the need for projections disposed on the sidewalls of the cage.

A storage module installed with multiple M.2 SSDs includes a frame, at least one circuit assembly, and plural M.2 SSDs. The circuit assembly is fixed to the frame along a direction. The circuit assembly includes plural circuit modules and a power connector. The circuit modules are electrically connected to each other in series. Each of the circuit modules includes a circuit board, a M.2 slot, and a signal connector. The circuit board is fixed to the frame. The M.2 slot is fixed to the circuit board. The signal connector is electrically connected to the circuit board and located outside the frame. The power connector is electrically connected to the circuit board of a corresponding one of the circuit modules. The M.2 SSDs plug into the M.2 slots of the circuit modules respectively.

Plug having common specifications are arranged on the side surfaces of each of the devices of different types included in the drive apparatus that controls an electric motor, and the plugs are positioned such that the side surfaces of the devices are in close contact with each other by connecting the plugs and the devices of different types are integrated.

A modular casing for electronic equipment comprises edge portions and corner portions. Each corner portion is interlocked with adjacent edge portions to form a framework. The casing also includes panels which are retained in the casing by engagement with edge portions. The dimensions of the casing can be selected to suit particular requirements by varying the length of the edge portions or the number of edge portions along each edge of the casing.

A foldable display apparatus that may realize one seamless screen by using two display panels is discussed. The foldable display apparatus can include a first display panel having a first display area; a second display panel having a second display area; and a panel supporter supporting the first and second display panels to mutually fold or unfold the first and second display panels, wherein boundary portions of the first display area of the first display panel and the second display area of the second display panel are matched with each other in a state that the first and second display panels are unfolded.

A combined inverter is arranged, which includes at least two separate box bodies connected detachably, all components of the combined inverter are placed into the box bodies separately, and at least one electrical connection terminal is arranged outside each of the box bodies, and the electrical connection terminal of one of the box bodies is capable of being connected to the electrical connection terminal of another of the box bodies. Therefore, a structure connection and an electrical connection of the combined inverter is achieved, weight of the whole combined inverter is dismantled effectively on the premise of ensuring normal operation of the combined inverter, construction difficult of installation and transportation is reduced, and the combined inverter has high applicability even when having high power.