10 results about "Computer design" patented technology

The invention discloses a honeycomb nested lattice porous structure and a design method thereof, and relates to the technical field of computer design and structural design, the honeycomb nested lattice porous structure comprises a plurality of honeycomb nested lattice units, the plurality of honeycomb nested lattice units form the honeycomb nested lattice porous structure in an array, each honeycomb nested lattice unit is composed of honeycomb unit cell lattices and unit cell lattices, the unit cell lattice is embedded in the honeycomb unit cell lattice, and the honeycomb unit cell lattice is of a regular hexagon structure. According to the honeycomb nested lattice porous structure and the design method thereof, the honeycomb structure has the advantages of being light in weight, high in specific strength and capable of buffering and absorbing energy, the side face mechanical property of the honeycomb structure is well enhanced, and the inherent defect that the side face mechanical property of the honeycomb structure is poor is overcome.

1. Name of the product in this design: Graphical User Interface for Computers with StarMap Cloud Developer Platform Data. 2. Purpose of this design: This design is used to run the StarMap Cloud Developer Platform processing program and display data information. The display screen panel is used with a computer. 3. The key design features of this product are shown in Figure 3, which illustrates the changing state of the interface. 4. Images or photos that best illustrate the design points: Interface change state diagram 3. 5. As is customary in computer design, rear view, left view, right view, top view, and bottom view are omitted. 6. Purpose of the graphical user interface: Used for data access, algorithm invocation, page design, data model design, logic orchestration and application deployment in the TuYun developer platform program. 7. The area of ​​the graphical user interface in the product: the entire area of ​​the computer screen. 8. Human-computer interaction method of graphical user interface: Users can perform different functions by clicking different areas or icons displayed on the interface with the mouse. 9. Description of the changing states of the graphical user interface: The main view is the initial page of the developer platform. Click the "Digital Earth Component" in the left toolbar, click "Earth" and drag it to the canvas, and set the percentage full screen from the top toolbar. The information display method is shown in Figure 1, which shows the interface change state. Based on state diagram 1, click "Built-in Resources" in the left toolbar, then click "Interface" and "Background Image" in sequence and drag them to the canvas. Click the basic toolbar components, select "Text" and add it to the canvas. Edit the text to "Digital Earth". Adjust the size and position of the text and background image. The information display method is shown in state diagram 2. Based on state diagram 2, click "Chart Components" in the left toolbar, then drag "Column Chart" → "Stacked Bar Chart", "Pie Chart" → "Gallery Chart" to the canvas and adjust their positions. The information display method is shown in state diagram 3. Based on state diagram 3, click "Plugins" in the left toolbar, drag "Plotting" to the canvas and adjust its position. Its information is displayed as shown in state diagram 4 of the interface change. Based on state diagram 4, clicking "Preview" in the upper right corner will display information as shown in state diagram 5. Based on state diagram 5, click "New", "Basic Element", "Point", "Scan Wave" in sequence and add it to the target location on the middle map. The information is displayed as shown in state diagram 6.

The invention discloses an automatic generation upper computer design method for peripheral drive software development, which comprises the following steps of: firstly completing basic development of peripheral chip drive, and arranging functions which can be realized by a drive file into a configuration file; splitting each function point of the driving software into independent method interfaces and generation components; filling the split interfaces according to a format standard of an upper computer configuration file and generating a function requirement configuration file; the configuration file is imported into an upper computer, the upper computer automatically analyzes and generates visual chip configuration options, and realizable functions and configuration items of the chip are clearly presented; a user starts a corresponding function by checking a target configuration option; and the upper computer automatically generates a drive file corresponding to the demand function. The method has the advantages that the problems that traditional peripheral chip driver development is low in efficiency, prone to errors, high in threshold, difficult to maintain and the like are solved, labor cost is liberated, omissions and software defects which are prone to occurring in manual writing are avoided, and the driver development threshold is lowered.

A method for iterative design using a computer numerical control (CNC) machine for automated changing of a CNC computer design program controlling the CNC machine may install an executable application to the CNC computer design program. The executable application may have a plurality of instructions, when executed by a processor, may cause the processor to display a customer tab on a home screen of the CNC computer design program, wherein the customer tab displays a plurality of icons. The plurality of instructions, when executed by a processor, may cause the processor to synchronize settings of the CNC computer design program to settings on the CNC machine so the settings on the CNC computer design program mirror the settings on the CNC machine when an import icon of the plurality of icons is selected is selected.

1. Name of this design product: Graphical User Interface for Importing Architectural Model Files into Computers (AECity). 2. Purpose of this design: For running programs. 3. The key design features of this product are the graphical user interface content on the screen. 4. The image or photograph that best illustrates the design's key features: the front view. 5. As is customary in computer design, the rear view, left view, right view, top view, and bottom view are omitted. 6. Purpose of the graphical user interface: Used to import architectural model files. 7. Human-computer interaction method of graphical user interface: The main view displays the login page, which requires an account and password to enter the software; clicking the "Login" button in the main view leads to interface change state diagram 1; clicking the "New Project" button in the upper right corner of interface change state diagram 1 leads to interface change state diagram 2; clicking the "OK" button in interface change state diagram 2 leads to interface change state diagram 3; clicking the "File" menu in the upper left corner of interface change state diagram 3, and then clicking "Select Import File" in the drop-down menu leads to interface change state diagram 4.

1. Name of the product subject to this design: Tablet PC and its main body. 2. Application of the product of this design: The product of design 1 as a whole and the protected part shall be used as a tablet computer; the product of design 2 shall be used as a tablet computer. 3. The key design features of this product are the shape of the part to be protected in Design 1 and the shape shown in Design 2. 4. The image or photograph that best illustrates the key design points: Design 1 3D view. 5. Design 1 is designated as the basic design. 6. Other situations requiring explanation: The parts drawn with solid lines in the view are the parts that are protected by this design. The gray area in the reference diagram represents the tablet computer's display screen. This design does not require color protection.

The invention belongs to the technical field of ruggedized computer design and manufacturing, and provides a modular packaging and protecting device of a ruggedized computer and a system and equipment thereof.The device comprises a rigid protective shell unit used for packaging and fixing a customized function module circuit board so that the customized function module circuit board can be physically isolated from the internal environment of a host, and the rigid protective shell unit is used for packaging and fixing the customized function module circuit board; the unit is composed of a box body and a box cover. The integrated interface management unit is arranged on the side wall of the box body and is provided with two spatially separated notches which are respectively used for connecting a computer mainboard and an external aviation plug; and the integrated mounting structure is arranged at the bottom of the shell unit and is used for detachably mounting the device on a computer bottom plate as an independent module. According to the device, the problem that a host is damaged by a falling object when a customized module is impacted and vibrated is solved, and the reliability and durability of the ruggedized computer in severe environments such as sand dust, high and low temperature, damp heat, salt mist and rain are remarkably improved through the structure, material and sealing design.

1. The name of the design product: tablet computer and its main body. 2. The use of the design product: the whole and part of design 1 are used for tablet computer, and design 2 is used for tablet computer. 3. The design points of the design product: in shape. 4. The picture or photo that best shows the design points: the perspective view 1 of design 1. 5. Design 1 is specified as the basic design. 6. Other circumstances that need to be explained: design 1 requests to protect the partial appearance design of the product, and the part represented by the solid line in the figure is the part to be protected.

The invention provides an intelligent power supply control method for an airborne comprehensive core processor, and relates to the field of aviation airborne embedded computer design, and the method comprises the steps: determining a plurality of working states of an airplane, respectively configuring corresponding power supply configuration tables for the plurality of working states, and defining a corresponding power supply configuration table for each power supply configuration table in the corresponding working state, combining power supply attributes of each LRM module in the avionics system; when the working state of the aircraft is switched, the avionics system calls a target power supply configuration table corresponding to the working state according to the target working state; and through a power management module in the avionics system, according to the power supply attributes defined in the target power supply configuration table, controlling all related LRM modules to perform power supply state switching. According to the invention, multi-module power supply can be rapidly switched, the power supply safety of the avionics system is ensured, later maintenance, change and reuse are facilitated, the maintainability and reusability of the system are remarkably improved, the operation burden of the avionics system is effectively reduced, and the power supply safety is ensured.

Skill intelligence computer design for enterprise performance execution