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372 results about "Configuration design" patented technology

Configuration design is a kind of design where a fixed set of predefined components that can be interfaced (connected) in predefined ways is given, and an assembly (i.e. designed artifact) of components selected from this fixed set is sought that satisfies a set of requirements and obeys a set of constraints.

Streamlined, readily towable marine seismic energy source for creating intense swept-frequency and pulse-coded signals in a body of water

Streamlined, towable, marine seismic energy vibrator for creating intense swept-frequency and pulse-coded seismic signals in a body of water has a sleek, fish-like configuration designed for towing with minimum drag. The vibrator has a streamlined hollow towing head and a streamlined hollow tail head mounted onto front and rear of a long cylindrical tubular wall which is modular, comprising cylinder sections joined in end-to-end axial alignment. Within this long tubular cylinder wall is an axially vibratable multi-piston assembly having a plurality of pistons on a long piston rod. One piston is positioned in each of the cylinder chambers. These chambers hive multiple ports opening out through the long cylindrical wall. An elongated circular cylindrical elastomeric bladder forms a water-filled bladder chamber encircling the wall. An actuator piston is vibrated by a remotely controllably hydraulic circuit, thereby vibrating the multi-piston assembly for vibrating water out and in through multiple ports communicating with the water-filled bladder chamber for vibrating the exterior of the bladder shown having diameter "D" of 18 inches and length "L" of 118.5 inches, providing a 6,700 square inch vibration area contacting the ambient water. A multi-piston position sensor enables synchronization of the vibrator with companion sources being towed. An axial passage in the long piston rod feeds low-pressure compressed air into the cylinder chambers forming air cushions behind the pistons vibrating water in these cylinder chambers.
Owner:BOLT TECH CORP

Image library configuration design system for integrated supervision software

The invention discloses an image library configuration design system for integrated supervision software. The image library configuration design system for the integrated supervision software comprises a base object library module which is in charge of storage and providing all supporting base objects; an image library editing module which is in charge of completing image library editing based on a class template, combining the base objects provided by the base object library module into a graphics primitive, relating the graphics primitive with class attributes, and setting a communal response event script processing method; a configuration editing module which is in charge of dragging the graphics primitive edited by the image library editing module to a configuration picture for setting; and a configuration running module which is in charge of running the configuration picture and checking actual running effects of a graphics primitive demon in the configuration picture. The image library configuration design system for the integrated supervision software can achieve editable combination of image libraries, increase flexibility of image library configuration, enable editing of the image libraries to be convenient and visualized, improve reuse ratios of the image libraries, reduce amount of repetition work of the configuration, and improve configuration efficiency.
Owner:SHANGHAI BAOSIGHT SOFTWARE CO LTD

Novel hybrid vertical/short take-off and landing (V/STOL) unmanned aerial vehicle

The invention discloses a novel hybrid vertical / short take-off and landing (V / STOL) unmanned aerial vehicle, aiming at solving the problems of complicated structure, high cost and the like of the existing aerial vehicles. The unmanned aerial vehicle comprises a body, a main wing, take-off and landing auxiliary wings arranged on the main wing, canards arranged at the front part of the body, a vertical tail arranged at the rear part of the body, a landing gear, an accumulator battery, a control system, a power supply management system and the like, wherein the landing gear, the accumulator battery, the control system, the power supply management system and the like are arranged below the body. The unmanned aerial vehicle adopts a ducted fan to provide a lift and assist balance during vertical take off and landing, and adopts an engine to provide the main push force and to automatically generate electricity so as to effectively utilize oil-electricity complement, simultaneously the reasonable hybrid use of fuel oil and electric energy is achieved through the structure and aerodynamic configuration design of the aerial vehicle, thereby achieving vertical and short take-off and landing, reducing the control difficulty of the aerial vehicle and solving the problem of inconsistence between difficult control and short voyage of the existing V / STOL unmanned aerial vehicles; the novel hybrid vertical / short take-off and landing (V / STOL) unmanned aerial vehicle disclosed by the invention can achieve vertical / short take-off and landing, and has the advantages of flexible and steady flight, wide application range and the like.
Owner:SOUTHWEAT UNIV OF SCI & TECH

Method for determining sheltering of solar cell array during in-orbit running of satellite and application of method

ActiveCN102700728AExplain the abnormal current problemSolving Optimal Design ProblemsCosmonautic power supply systemsConfiguration designSolar cell
The invention relates to a method for determining the sheltering of a solar cell array during the in-orbit running of a satellite and the application of the method. The method comprises the following steps of: making researches on solar illumination angle annual average change rules of a satellite orbit and the conditions of change of solar elevation along with the latitude during the in-orbit running of the satellite, judging whether the solar cell array of the satellite is sheltered or not by star, combining the configuration characteristics of the satellite, calculating a sheltered area, and obtaining the change trends of the sheltered area within one orbit and a year, so that the problem of abnormal charging array current caused by the sheltering of the solar cell array during the in-orbit running of the satellite can be solved according to results, and the problem of the optimal design of a cell distribution mode for solar cells of the satellite is also solved. The configuration design rationality of a spacecraft such as the satellite adopting the solar cell array as a main energy supply is improved, the utilization efficiency of the solar cells is improved, and good effects are achieved. The application has the advantages of lowering the cost of the cells of the spacecraft, improving the effective power supply capability of the spacecraft, improving the performance of the spacecraft, and the like.
Owner:SHANGHAI SATELLITE ENG INST

Multi-ship collaborative navigation formation configuration method based on underwater acoustic communication

The invention discloses a multi-ship collaborative navigation formation configuration method based on underwater acoustic communication. The method comprises the steps as follows: a system state equation and a measurement equation are established according to a collaborative navigation system model; a nonlinear system Lee derivative observability theory is used for performing observability analysis on the equations; an underwater acoustic communication blind zone model is established according to wake flows generated by propellers at the tails of ships; a safety zone model is determined according to safety distances among the ships; and finally, an unmanned ship formation configuration design scheme is obtained on the basis that the observability, the wake flow communication blind zone and the safety distance zones among the ships are comprehensively considered. According to the method, collaborative navigation system formation configuration optimization design is realized, and the method is applicable to formation configuration designs under multi-ship collaborative navigation conditions. According to the method, the formation configuration layout obtained without consideration of wake flow influences has a high practical value on the collaborative navigation system formation configuration design.
Owner:HARBIN ENG UNIV
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