76 results about "Electronic computer" patented technology

A liquid cooling dissipation device for electronic / computer products includes a top cover with a coolant cold plate and two cooling brackets. The cold plate has at least two sets of flow channels for accommodating coolant and connects to multiple heating elements. It features inlets and outlets at both ends, all connected to the flow channels. Tubes with mounting brackets at the top end are installed at these points. A condenser, mounted on the mounting brackets and featuring side brackets, includes at least two cooling flow channels, multiple heat-conducting plates, and several heat dissipation fins. The cold plate consists of four laminated layers: a first-layer bottom plate, a second-layer composite plate, a third-layer metal plate, and a fourth-layer top plate. Heat from the heating elements vaporizes the coolant, which the condenser returns to liquid, circulating via siphon effect and pressure differential.

This invention provides a satellite photoelectric guidance method and system for space observation. The method includes: First, a photoelectric sensing device senses targets around the satellite, completes target measurement and orbit calculation, and after orbit recursion, matches the target data with a ground-based target database to update the target database and preliminarily search for and identify potential collision sources and interference sources; Second, an onboard integrated electronic computer requests target observation data from the photoelectric sensing device and receives the target observation data; Third, the onboard integrated electronic computer filters and sorts the received targets, locating collision sources and interference sources requiring key attention; Finally, the onboard integrated electronic computer programmatically activates the optical payload equipment and electronic payload equipment, and sends angle information to the optical payload equipment and electronic payload equipment to achieve detailed observation of space targets.

The invention discloses an image point cloud extraction method for face registration, which comprises the following steps: S1, acquiring an electronic computed tomography image of the head of a patient to obtain a skin surface model of the patient, and converting the skin surface model into a point cloud; s2, transforming the point cloud obtained in the step S1 to a standard coordinate system; s3, roughly extracting the point clouds, clustering the point clouds obtained in the step S2 to obtain four clustering centers, and filtering out the point clouds meeting a first preset condition according to the four clustering centers; and S4, finely extracting the point clouds, clustering the point clouds obtained in the step S3 to obtain three clustering centers, and filtering out the point clouds meeting a second preset condition according to the three clustering centers. Using a clustering method to reversely determine an area which needs to be extracted and has unobvious feature points from a plurality of clustering centers of the obtained point clouds through the plurality of clustering centers; clustering and extraction are carried out step by step, the number of clustering points each time is controlled, and the influence of noise features is eliminated.

The avionics computer, in particular a flight management system, comprises a processing unit configured to compare a first altitude with what is referred to as a threshold altitude, the first altitude corresponding to the altitude of a missed approach point relative to the runway, the threshold altitude being equal to the sum of a second altitude corresponding to the altitude of the runway and of a threshold crossing height, and to determine a terminal point that has an altitude equal to the threshold altitude and that forms, with the position of the missed approach point, a straight line segment that has a slope equal to the slope of the straight line segment defined by the missed approach point and a final approach fix, said terminal point being capable of being used as anchor point, the avionics computer thus having improved properties especially in terms of availability and robustness.

The invention provides a satellite-borne high-function-density comprehensive electronic computer based on an SM750 processor. Comprising a casing, and a first general processing and small solid memory module, a second general processing and small solid memory module, a first secondary power supply module, a second secondary power supply module, a channel gateway module, an I-type comprehensive interface module, an II-type comprehensive interface module, a serial port communication module, an initiating explosive device and power distribution module and a power driving module which are arranged on the casing, the system comprises a relay responder module, a measurement and transmission integrated responder module, a navigation module and an internal bus mother board. According to the invention, a satellite platform measurement and control function, a measurement and transmission integrated function, a satellite service management function, a time base function, an attitude and orbit control management function, a power supply and distribution management function, an initiating explosive device and hot knife driving function, a thermal control management function, a mechanism pointing trajectory planning function and a navigation function are integrated in one single machine, so that the integration level of core functions of the satellite platform can be improved; and the quality and power consumption overhead of basic functions of the platform are effectively reduced.

HIGH-STABILITY, HIGH-AGILITY THREE-SAILING SURFACE AIRCRAFT The three-sail aircraft (1), (2), and (3) is equipped with movable flaps (6), (7), and (8) on each of the lifting surfaces. The flaps of the upstream lifting surface (6) are connected to the flaps of the main wing (7) by a rigid linkage with a deflection angle ratio of 50%. The forces on the downstream lifting surface (horizontal tail) (3) reverse between takeoff (negative lift) and cruise (positive lift). Stabilizing fins (5) are positioned at the rear of the fuselage in the lower section at an angle of 30° to the aircraft's centerline. A weighted control rod (22) located in the vertical tail (4) provides stabilization for the aircraft in the presence of severe turbulence.The propulsion system is located at the rear of the fuselage and consists of either a piston engine driving a multi-bladed propeller, one or two turboshaft engines driving a multi-bladed propeller or two contra-rotating propellers, a turbojet engine, or one or two electric motors driving a multi-bladed propeller or two contra-rotating propellers. This aircraft can be piloted either by a human pilot on board or by an electronic computer controlled from the ground or autonomously.

The images shown in the figure represent the graphical user interface of a patient application, and are used to indicate body parts or specific body parts to be displayed when the user administers injections or other procedures. These images are available separately for men and women, or for both sexes, and may show, for example, a specific body part where an injection was administered, a problematic body part, or multiple specific body parts that the user wants to highlight. Furthermore, the figure shows the right side view, left side view, top view, and bottom view of a computer with a function for exchanging information with patients that displays the above images.

A semiconductor quantum dot upconversion fluorescence spectrum detection system, including laser, the pulsed laser emitted by laser is transmitted to the half mirror after being expanded by first and second lenses in turn, and the pulsed laser is divided into two light paths; in the reflected light path, the incident pulsed laser passing through the objective lens is focused on the surface of the semiconductor quantum dot sample, the semiconductor quantum dot sample radiates upconversion fluorescence after being excited, and the upconversion fluorescence and the reflected pulsed laser of the surface of the semiconductor quantum dot sample are transmitted to the half mirror through the objective lens into the transmitted light path after acting on the fluorescence enhancement substrate; in the transmitted light path, the transmitted fluorescence and the reflected pulsed laser passing through the half mirror enter the third lens through the optical filter, and then enter the spectrometer and EMCCD camera for fluorescence spectrum collection, the spectrometer and EMCCD camera are regulated and data processed by using the electronic computer, and the fluorescence spectrum of the semiconductor quantum dot sample is displayed, and the present application provides technical support for temperature detection in the living cells of biological organisms.

Method for determining the use of a vehicle safety belt (4) comprising a webbing (5), a tongue (6) held on the webbing (5), and a buckle (7), and assigned to a seat (3) of a vehicle, wherein a sensor device (8) of the buckle (7) detects a closed state of the buckle (8) resulting from the insertion of an element into the buckle (7), characterized in that: - by means of an electronic computing device (9), a second time interval (Z2) is determined within a first time interval (Z1) extending from a first time point (t1), at which the closed state of the buckle (7) beginning at the first time point (t1) is detected by the sensor device (8), to a second time point (t2), at which a first event is detected, during which the closed state of the buckle (7) is continuously detected by the sensor device (8).which extends from a third time point (t3) between the first time point (t1) and the second time point (t2), at which a second event is recorded, up to the second time point (t2); - the first event includes the opening of a vehicle door; - the second event includes the unoccupancy of the seat (3); - the second time period (Z2) is compared with a threshold value by means of the electronic computing device (9); and - a feigned use of the seat belt (4) is determined by means of the electronic computing device (9) if the comparison of the second time period (Z2) with the threshold value determines that the second time period (Z2) exceeds the threshold value.

The objective is to develop a system and method for determining the weights of consensus odds among sportsbooks. [Solution] The system includes a function to calculate consensus odds based on the odds of each wager at each wagering venue, and each wager's odds at each wagering venue has a weight relative to the consensus odds that is proportional to the total amount wagered at each wagering venue among multiple wagering venues in the market.

The avionics computer comprises a processing unit configured to compare the distance between a first position and a second position with a predetermined distance, the first position corresponding to the position of an initial anchor point of an initial terminal segment and the second position corresponding to the position of a landing threshold point of the runway, to check whether the initial terminal segment of the virtual path crosses the threshold of the runway and, if the distance between the first position and the second position is less than the predetermined distance and if the initial terminal segment of the virtual path crosses the threshold of the runway, to define the landing threshold point as an anchor point of a terminal segment of a virtual path for a non-precision FLS approach mode, the avionics computer thus making it possible to increase availability to implement FLS mode.

Electronic computer device for document analysis

This invention discloses a modular integrated acquisition and storage card and a computer, belonging to the field of electronic computer technology. The invention includes a PCIe interface, a mounting base, and a side mounting plate. A side-mounted rotating latch allows for quick installation and removal of the PCIe interface. Compared to existing mounting bases where the latches are located at both ends, often obstructed by graphics cards or acquisition and storage card interfaces, this invention solves the problem of existing end-face interfaces not using a spring-loaded structure and relying on friction damping, which requires significant force for installation and removal, easily damaging the PCB and gold fingers, and is difficult to operate.

1. Name of the product in this design: Intelligent Electronic Computer (A15XP-206T). 2. Intended use of this design: This design is intended for use in computers. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.

A system for supporting activities in a shipyard during construction of a ship has at least one local electronic computer installed in a watchtower of the ship and operatively connected to at least one central electronic computer remote from the ship, a first plurality of electronic apparatuses operatively connected by respective wired connection backbone cables to form one or more tree network topologies, each electronic apparatus representative of a root node of a respective tree network topology being operatively connected to the at least one local electronic computer, and a plurality of sensors adapted to detect information representative of the shipyard and operatively connected by respective wired connection cables to form one or more network topologies from one or more electronic apparatuses. Each electronic apparatus is configured to manage network connectivity and safety of the shipyard based on the information representative of the shipyard detected by the plurality of sensors.

Electronic Computer Device for Policy Impact and Economic Risk Assessment

The article to which this design relates is a smartphone-type electronic computer. It has the function of remotely controlling a passenger car. In the reference front view, the area indicated by leader line 1 is the area that displays the state and status of the passenger car being remotely controlled. The area indicated by leader line 2 is the area where operation buttons for frequently performed operations such as opening and closing door locks are located. The area indicated by leader line 3 is the area for performing other operations. The operation buttons in the area indicated by leader line 2 can slide left and right, and change as shown in the front view in the changed state.

A system for controlling actuators in an aircraft. The system including at least a first actuator and a second actuator. Each of the actuators including a movement member, at least one measurement sensor, and a computing member internally connected to the movement member and configured to be connected to at least one electronic computer of the aircraft. The computing member having a function for controlling the movement member, the measurement sensor of the first actuator being externally connected to the computing member of the second actuator, the computing member of the second actuator also having a monitoring function for monitoring the movement member of the first actuator.

This invention provides a satellite telemetry scheduling and processing method and system suitable for spread spectrum hopping mode, comprising: collecting telemetry source packets from various satellite subsystems; performing secondary screening on all telemetry source packets and recombining important telemetry parameter packets in spread spectrum hopping mode; grouping important telemetry parameter packets in spread spectrum hopping mode into virtual channel data units according to the virtual channel identifier of spread spectrum hopping mode; scrambling the virtual channel data units according to the selected scrambling polynomial and initial phase; adding frame synchronization words to group channel access data units; performing frame selection processing under different modes according to different telemetry rate switching modes; dividing the selected telemetry frames into equal parts and inserting the equally divided telemetry data into different spread spectrum hopping downlink measurement frames for transmission. This invention effectively meets the compatibility processing requirements of integrated electronic computers for conventional noncoherent spread spectrum mode and spread spectrum hopping mode, ensures the transmission of important telemetry in spread spectrum hopping mode, and facilitates ground processing.

The application discloses a multi-model segmentation method, a surgical robot and related products. The method comprises the following steps: based on a first model and a second model, a first segmentation result of a first tissue of a target object and a second segmentation result of a second tissue of the target object are segmented from a first three-dimensional electronic computed tomography image; and then, based on the positions of the first segmentation result and the second segmentation result in the first three-dimensional CT image, the first segmentation result and the second segmentation result are combined to obtain a target segmentation result comprising the first tissue and the second tissue of the target object. The confidence of the target segmentation result can be improved by the method.

The present application provides a touchpad module and an electronic computer with the touchpad module. The touchpad module includes a touchpad, a first substrate, a second substrate and two elastic elements. The first substrate is arranged below the touchpad and includes a first stop portion and a second stop portion. The second substrate is arranged between the touchpad and the first substrate and includes a third stop portion and a fourth stop portion. The third stop portion is engaged with the first stop portion and the fourth stop portion is engaged with the second stop portion. The elastic elements are arranged between the first substrate and the second substrate. According to the touch pressure of external force, the touchpad swings towards the first substrate with the engaged position of the second stop portion and the fourth stop portion as the fulcrum, and simultaneously drives the second substrate to swing, so that the second substrate presses one of the elastic elements and the third stop portion is disengaged from the first stop portion.

The invention provides an electronic computer part assembling workbench, and relates to the technical field of assembling workbenches. The device comprises a table top assembly, a lifting assembly, a frame body assembly, a storage assembly, a locking assembly, a clamping assembly, a lighting assembly and a placement box, and the table top assembly is used for providing a supporting plane; the lifting assembly is arranged below the table top assembly and used for changing the height of the table top assembly. The frame body assembly is arranged at the center of the front part of the table board assembly and is used for providing an assembly position in a horizontal state and an inclined state; the storage assembly is arranged below the table board assembly and used for storing tools. The locking assembly is arranged on the side face of the frame body assembly and used for locking the inclined state of the frame body assembly. By arranging the frame body assembly and the locking assembly, assembling positions in a horizontal state and an inclined state can be provided, and the assembling device is suitable for assembling and using of the electronic computer, easy to operate and low in manufacturing cost.

An avionics electronic computer with a virtual machine management hypervisor, and an aircraft comprising such a computer. This avionics electronic computer on board an aircraft comprises a group of computing electronic card(s) (25) having computing resources and storage resources (40); a set of microservices executed independently of each other, with at least a part of the resources; a set of software application(s) to call one or more of the microservices; and a set of orchestrator(s) (55, 56) to implement the set of microservices by allocating at least a part of the resources.The orchestrator set includes several orchestrators (55, 56), and the computing card group comprises at least two virtual machines (50) and a virtual machine management hypervisor (45), common to the computing card group and configured to distribute at least some of the resources among the virtual machines (50), each hosting one of the orchestrators and making its resources available to that orchestrator. See Figure 2 for abbreviations.

1. The name of the design product: external device connection part of power monitor. 2. The use of the design product: the whole product is arranged in a place such as a factory, and is used for power measurement and leakage monitoring by means of a host device such as an electronic computer; the part to be protected is a connection part for connecting an external device. 3. The design points of the design product: in the shape of the solid line drawing. 4. The picture or photo that best indicates the design points: perspective view 1. 5. Other circumstances that need to be explained: the design is a partial design, and the part shown by the solid line in the view is the part to be protected.

1. The name of the design product: portable electronic computer. 2. The use of the design product: is a portable electronic computer. 3. The design points of the design product: in the shape shown in the perspective view 1. 4. The picture or photo that best shows the design points: perspective view 1. 5. Other circumstances that need to be explained: the change state is the closed cover state; the A-A sectional view is a diagram omitting the internal mechanism; the B-B sectional view is a diagram omitting the internal mechanism.

1. Name of the product in this design: Mouse (G75). 2. Purpose of this design: This design is used to assist in the operation and control of electronic computers. 3. The key design features of this product are the combination of shape and pattern. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

The invention provides a full-electronic computer interlocking intelligent fault diagnosis method and device and a medium, and belongs to the technical field of track circuits. By adding a device monitoring technical means, customized research and development are carried out on a signal device acquisition sensor, application data of a signal device state is recorded in real time and analyzed online, and a fault diagnosis result is obtained. And the equipment state and related electrical characteristic parameter changes during fault are reproduced through a playback function, so that dynamic tracking is realized. Alarm reminding is carried out when the electrical characteristics of part of equipment exceed the standard, and a powerful basis is provided for fault judgment and analysis and instant state capture. Indoor and outdoor fault positioning is distinguished, reasonable processing suggestions are given after fault reasons are comprehensively judged in combination with maintenance logs, effective alarms are quickly given in real time, and the workload of alarm information analysis of maintenance personnel is reduced.

The invention relates to the technical field of data transmission, in particular to a data transmission system of an electronic computer server, which comprises a data preprocessing module, a transmission encryption module, a link maintenance module, a bandwidth adjustment module, a file fragmentation module, an edge storage and buffer module, an off-peak scheduling module and a data verification module. And the data preprocessing module is used for sensitive field identification and desensitization processing. According to the method, accurate identification and desensitization of sensitive data are realized by setting data preprocessing, the data transmission security is effectively improved, data encryption and integrity verification are further enhanced, the data transmission process is prevented from being tampered, faults can be automatically detected, a link can be quickly reconstructed, transmission interruption is avoided, bandwidth can be dynamically allocated according to flow, and the data transmission efficiency is improved. The resource utilization rate is improved, the large file transmission efficiency is optimized, the transmission delay is shortened through hotspot data caching and path optimization, the transmission loads in peak and low peak periods are balanced, the correctness of received data is ensured, and errors can be repaired.