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1:
[发明]
【中文】数据处理方法、装置及电子设备 【EN】Data processing method and device and electronic equipment
申请号:
201811063852.X
公开号:CN110895593A 主分类号:G06F16/955
申请人:
【中文】阿里巴巴集团控股有限公司【EN】Alibaba Group Holding Ltd.
申请日:2018.09.12 公开日:2020.03.20
发明人:
【中文】孙建亮【EN】
Sun Jianliang
摘要:【中文】本申请实施例提供一种数据处理方法、装置及电子设备,其中方法包括:获取网站服务器与终端设备之间传输的网页的下行数据;判断所述下行数据是否满足预设条件;若满足,则查找所述下行数据对应的上行数据;根据所述上行数据确定所述网页对应的URL。本申请实施例提供的数据处理方法、装置及电子设备,能够快速、准确地利用网站服务器与终端设备之间传输的真实数据来查找满足预设条件的网页URL,获取到的网页内容与实际展示给用户的网页内容一致,同时通过上行数据来确定网页URL,有效提高了网页提取的准确性和效率。 【EN】The embodiment of the application provides a data processing method, a data processing device and electronic equipment, wherein the method comprises the following steps: acquiring downlink data of a webpage transmitted between a website server and terminal equipment; judging whether the downlink data meets a preset condition or not; if yes, searching uplink data corresponding to the downlink data; and determining the URL corresponding to the webpage according to the uplink data. According to the data processing method, the data processing device and the electronic equipment, the webpage URL meeting the preset conditions can be quickly and accurately searched by using real data transmitted between the website server and the terminal equipment, the acquired webpage content is consistent with the webpage content actually displayed to the user, and meanwhile, the webpage URL is determined through uplink data, so that the accuracy and the efficiency of webpage extraction are effectively improved.
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2:
[发明]
【中文】一种新超声速飞行器振动环境外推方法 【EN】Novel supersonic aircraft vibration environment extrapolation method
申请号:
201911194593.9
公开号:CN111191187A 主分类号:G06F17/17
申请人:
【中文】北京机电工程研究所【EN】BEIJING RESEARCH INSTITUTE OF MECHANICAL AND ELECTRICAL TECHNOLOGY
申请日:2019.11.28 公开日:2020.05.22
发明人:
【中文】刘小平
;
孙建亮【EN】Liu Xiaoping
;
Sun Jianliang
摘要:【中文】本发明涉及一种新超声速飞行器振动环境外推方法,属于环境计算技术领域。该方法包括以下步骤:选定一种与新超声速飞行器具有相似气动外形的相似飞行器;依次测量相似飞行器的离散化振动数据,并对每次测量的振动数据进行傅里叶变换后计算得到振动量级,同时计算每次测量对应的动压;通过对不同测量次数的所述振动量级与对应的动压进行线性拟合得到线性拟合曲线的系数,并通过设定的置信区间上限对所述线性拟合曲线的系数进行修正;根据所述线性拟合关系以及新超声速飞行器的动压得到新超声速飞行器的振动量级。本发明实施例解决了现有飞行器振动环境计算方法不适用于新超声速飞行器,导致新超声速飞行器难以确定振动环境的问题。 【EN】The invention relates to a novel supersonic aircraft vibration environment extrapolation method, and belongs to the technical field of environment calculation. The method comprises the following steps: selecting a similar aircraft with a similar aerodynamic shape with the new supersonic aircraft; measuring discretization vibration data of similar aircrafts in sequence, calculating vibration magnitude after Fourier transform is carried out on the vibration data measured each time, and meanwhile calculating dynamic pressure corresponding to each measurement; carrying out linear fitting on the vibration magnitude of different measurement times and the corresponding dynamic pressure to obtain a coefficient of a linear fitting curve, and correcting the coefficient of the linear fitting curve through a set confidence interval upper limit; and obtaining the vibration magnitude of the new supersonic aircraft according to the linear fitting relation and the dynamic pressure of the new supersonic aircraft. The method and the device solve the problem that the vibration environment of the new supersonic aircraft is difficult to determine due to the fact that the existing aircraft vibration environment calculation method is not suitable for the new supersonic aircraft.
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3:
[发明]
【中文】一种精轧机组轧制线标高优化方法 【EN】Method for optimizing rolling line elevation of finishing mill group
申请号:
201911388335.4
公开号:CN111014309A 主分类号:B21B37/72
申请人:
【中文】河北工程大学【EN】HEBEI UNIVERSITY OF ENGINEERING
申请日:2019.12.30 公开日:2020.04.17
发明人:
【中文】张明
;
彭艳
;
孙建亮
;
姚瑶【EN】Zhang Ming
;
Peng Yan
;
Sun Jianliang
;
Yao Yao
摘要:【中文】本发明提供了一种精轧机组轧制线标高优化方法,该方法包括以下步骤:a、计算每组轧辊出口处带钢中性层上半部分和下半部分的中心线长度;b、取轧辊出口处带钢中性层上、下半部分中心线长度的差值为头部翘曲判别因子,用来表征带钢的头部翘曲程度;c、确定优化变量,优化变量包括各组轧辊的压下量和咬入倾斜角;e、确定约束条件,需要带钢在轧制过程中始终保持向上翘曲;f、根据带钢经过最后组的轧辊轧制后,头部的翘曲量最小,得出优化目标函数;g、根据约束条件优化目标函数,得出精轧机组各架轧机的轧辊倾斜角和压下率最优值。 【EN】The invention provides a method for optimizing the elevation of a rolling line of a finishing mill group, which comprises the following steps: a. calculating the lengths of the central lines of the upper half part and the lower half part of the neutral layer of the strip steel at the outlet of each group of rollers; b. taking the difference of the lengths of the central lines of the upper half part and the lower half part of the neutral layer of the strip steel at the roller outlet as a head warping discrimination factor to represent the head warping degree of the strip steel; c. determining optimization variables, wherein the optimization variables comprise the rolling reduction and the biting inclination angle of each group of rollers; e. determining constraint conditions, wherein the strip steel needs to be always upwards warped in the rolling process; f. obtaining an optimized objective function according to the minimum warping amount of the head of the strip steel after the strip steel is rolled by the last group of rollers; g. and optimizing the objective function according to the constraint condition to obtain optimal values of the roll inclination angle and the reduction rate of each frame of rolling mill of the finishing mill group.
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4:
[发明]
【中文】连杆活塞销挡圈自动装配机 【EN】Automatic assembling machine for check ring of connecting rod piston pin
申请号:
201910194718.1
公开号:CN111230472A 主分类号:B23P21/00
申请人:
【中文】重庆炜海自动化科技有限公司【EN】Chongqing Weihai Automation Technology Co., Ltd.
申请日:2019.03.14 公开日:2020.06.05
发明人:
【中文】戴建良
;
张雷元
;
孙登明【EN】Dai Jianliang
;
Zhang Leiyuan
;
Sun Dengming
摘要:【中文】本发明公开了一种连杆活塞销挡圈自动装配机,包括工作台,所述工作台上依次平行设置有活塞销压装线、挡圈压装线和成品暂存线,三者之间设置有取卸料抓手总成,所述取卸料抓手总成具有取料抓手和卸料抓手,所述取料抓手和卸料抓手与同一移动副板相连;所述活塞销压装线具有活塞定位座A,挡圈压装线具有活塞定位座B,所述成品暂存线包括基板C,以及活动设置于该基板C上的存放台,所述存放台上具有至少一个活塞定位槽,所述存放台沿基板C长度方向滑动,可使活塞定位槽与活塞定位座A和活塞定位座B共线。采用以上方案,整体布局结构紧凑,大大缩减占用空间,此外精简零部件,优化机构,提高装配效率,同时降低成本,保证系统运转可靠性。 【EN】The invention discloses an automatic assembling machine for a connecting rod piston pin retainer ring, which comprises a workbench, wherein a piston pin press-mounting line, a retainer ring press-mounting line and a finished product temporary storage line are sequentially arranged on the workbench in parallel, a material taking and discharging gripper assembly is arranged among the piston pin press-mounting line, the retainer ring press-mounting line and the finished product temporary storage line, the material taking and discharging gripper assembly is provided with a material taking gripper and a material discharging gripper, and the material taking gripper and the material discharging gripper are connected with the same moving; the piston pin press-mounting line is provided with a piston positioning seat A, the check ring press-mounting line is provided with a piston positioning seat B, the finished product temporary storage line comprises a base plate C and a storage table movably arranged on the base plate C, at least one piston positioning groove is formed in the storage table, and the storage table slides along the length direction of the base plate C and can enable the piston positioning groove to be collinear with the piston positioning seat A and the piston positioning seat B. By adopting the scheme, the whole layout structure is compact, the occupied space is greatly reduced, parts are simplified, the mechanism is optimized, the assembly efficiency is improved, the cost is reduced, and the operation reliability of the system is ensured.
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5:
[发明]
【中文】一种化霜模式启动与否的判定方法、处理器、空调器和热泵热水器 【EN】Defrosting mode starting or not judging method, processor, air conditioner and heat pump water heater
申请号:
201911120870.1
公开号:CN110925954A 主分类号:F24F11/42
申请人:
【中文】浙江中广电器股份有限公司【EN】ZHEJIANG ZHONGGUANG ELECTRIC APPLIANCE CO., LTD.
申请日:2019.11.15 公开日:2020.03.27
发明人:
【中文】叶方明
;
袁晓军
;
孙建良
;
朱建军【EN】Ye Fangming
;
Yuan Xiaojun
;
Sun Jianliang
;
Zhu Jianjun
摘要:【中文】本发明提供了一种定频空调器及其提升化霜的判定方法,属于热交换设备技术领域。它解决了现有技术设计压缩空气消耗大等问题。本化霜模式启动与否的判定方法适用于采用定频压缩机的空调器机组或热泵热水器机组,包括以下步骤:系统初始化,上机开电,将预设的室外环境温度T
1
、室外换热器上的热交换部件的外表面温度T
2
、ΔT=T
1
‑T
2
、ΔT
min
的值初始化为0;启动定频压缩机,使本机组进入制热模式;每隔设定的时间段t
jcjg
获取相关温度数据值并存储等。本定频空调器及其提升化霜的判定方法的优点在于:通过改变是否启动化霜模式的判定条件,做到有霜化霜,无霜不化,且当系统配置发生变化时,无需做重新确定化霜的进入条件参数也能做到有霜化霜,无霜不化。 【EN】The invention provides a fixed-frequency air conditioner and a judgment method for improving defrosting of the fixed-frequency air conditioner, and belongs to heat exchange equipmentThe technical field is as follows. It has solved the big scheduling problem of prior art design compressed air consumption. The method for judging whether the defrosting mode is started or not is suitable for an air conditioner unit or a heat pump water heater unit adopting a fixed-frequency compressor, and comprises the following steps of: initializing the system, powering on and powering on, and setting the preset outdoor environment temperature T
1
The outer surface temperature T of the heat exchange part on the outdoor heat exchanger
2
、ΔT=T
1
‑T
2
、ΔT
min
Is initialized to 0; starting a fixed-frequency compressor to enable the unit to enter a heating mode; every set time period t
jcjg
Acquiring and storing relevant temperature data values, and the like. The fixed-frequency air conditioner and the judgment method for improving defrosting have the advantages that: the defrosting is carried out and the defrosting is not carried out by changing the judgment condition whether the defrosting mode is started, and when the system configuration is changed, the defrosting can be carried out and the defrosting is not carried out without re-determining the entering condition parameters of the defrosting.
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6:
[发明]
【中文】用于微纳卫星的电子拓扑架构 【EN】Electronic topology framework for micro-nano satellite
申请号:
201911142456.0
公开号:CN111030746A 主分类号:H04B7/185
申请人:
【中文】上海卫星工程研究所【EN】Shanghai Institute of Satellite Engineering
申请日:2019.11.20 公开日:2020.04.17
发明人:
【中文】孙建亮
;
陈锋
;
沈朱泉
;
王瑞
;
周英庆【EN】
Sun Jianliang
;
Chen Feng
;
Shen Zhuquan
;
Wang Rui
;
Zhou Yingqing
摘要:【中文】本发明涉及星载电子系统领域内的适用于微纳卫星的电子拓扑架构,由一台单机组成,包括处理器模块A/B、功能模块、对地扩频测控模块、小S中继测控模块、数据保护模块、固存和AOS模块、GPS/BD模块组成、数传发射机组成;在信息拓扑上,将数据管理软件和姿轨控软件合并运行、遥测组帧和遥控处理由FPGA统一处理、具备对地扩频和小S中继两套测控冗余链路、集成数传链路的数据处理与对地传输功能。本发明实现了微纳卫星电子信息功能综合、集中控制,具备扩展性和通用性。 【EN】The invention relates to an electronic topology framework suitable for a micro-nano satellite in the field of satellite-borne electronic systems, which consists of a single machine, a plurality of single machines and a plurality of data transmission machines, wherein the single machine comprises a processor module A/B, a functional module, a ground spread spectrum measurement and control module, a small S relay measurement and control module, a data protection module, a solid storage and AOS module, a GPS/BD module and a data transmission machine; on the aspect of information topology, data management software and attitude and orbit control software are merged to run, telemetering framing and remote control processing are uniformly processed by an FPGA (field programmable gate array), and the system has the functions of ground spread spectrum, small S relay two sets of measurement and control redundant links and integrated data processing and ground transmission of a data transmission link. The invention realizes the comprehensive and centralized control of the functions of the electronic information of the micro/nano satellite, and has expansibility and universality.
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7:
[发明]
【中文】一种终炼串联均化炼胶工艺及系统 【EN】Final mixing series connection homogenizing rubber mixing process and system
申请号:
202010023407.1
公开号:CN111195994A 主分类号:B29B7/74
申请人:
【中文】浦林成山(青岛)工业研究设计有限公司【EN】PULIN CHENGSHAN (QINGDAO) INDUSTRIAL RESEARCH DESIGN Co.,Ltd.
申请日:2020.01.09 公开日:2020.05.26
发明人:
【中文】许建欣
;
谭建良
;
胥建刚
;
慈婷楠
;
孙蕾【EN】Xu Jianxin
;
Tan Jianliang
;
Xu Jiangang
;
Ci Tingnan
;
Sun Lei
摘要:【中文】本发明公开了一种终炼串联均化炼胶工艺及系统。其中工艺包括下述步骤:(1)将胶料和配合剂进行低速低温终炼;(2)将终炼好的胶料进行冷却压片;(3)将冷却压片后的胶料进行低温均化混炼;(4)将低温均化混炼后的胶料进行压片及收胶,以制得胶料;步骤(3)中低温均化混炼包括多个程序,多个程序的辊距、挡胶板宽度、堆积胶占比、辊筒速度及捣胶时间为,程序一:辊距为0.8mm‑1.5mm,挡胶板宽度为1.0m‑2.1m,堆积胶占比为15%‑30%,辊筒速度为30m/min‑50m/min,捣胶时间为20s‑50s;程序二:辊距为8.0mm‑10.0mm,挡胶板宽度为1.5m‑2.1m,堆积胶占比为5%‑15%,辊筒速度为20m/min‑50m/min,捣胶时间为100s‑400s。冷却压片迅速降低终炼胶温度,避免胶料物理性能降低;均化混炼中采用变辊距、变速度、适量堆积胶使胶料充分剪切、混合均匀,达到均化效果。 【EN】The invention discloses a final mixing series homogenizing rubber mixing process and a system. The process comprises (1) low-speed low-temperature final refining of rubber and compounding agent; (2) cooling and tabletting the finally refined rubber material; (3) homogenizing and mixing the cooled and tabletted rubber material at low temperature; (4) tabletting and collecting the rubber material after low-temperature homogenization and mixing to obtain the rubber material; the low-temperature homogenizing and mixing in the step (3) comprises a plurality of procedures, wherein the roll spacing, the width of the rubber baffle plate, the accumulated rubber ratio, the speed of the roller and the time for rubber smashing of the plurality of procedures are as follows: the roller spacing is 0.8mm-1.5mm, the width of the rubber baffle plate is 1.0m-2.1m, the accumulation rubber accounts for 15% -30%, the roller speed is 30m/min-50m/min, and the rubber smashing time is 20s-50 s; and a second procedure: the roller spacing is 8.0mm-10.0mm, the width of the rubber baffle plate is 1.5m-2.1m, the accumulation rubber accounts for 5% -15%, the roller speed is 20m/min-50m/min, and the rubber smashing time is 100s-400 s. Cooling and tabletting to quickly reduce the temperature of final rubber mixing and avoid the reduction of the physical properties of rubber materials; in the homogenizing and mixing process, the rubber material is fully sheared and uniformly mixed by adopting variable roll spacing, variable speed and proper amount of accumulated rubber, so as to achieve the homogenizing effect.
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8:
[发明]
【中文】一种热泵热水器及其加热控制方法 【EN】Heat pump water heater and heating control method thereof
申请号:
201911365819.7
公开号:CN111121287A 主分类号:F24H4/02
申请人:
【中文】浙江中广电器股份有限公司【EN】ZHEJIANG ZHONGGUANG ELECTRIC APPLIANCES Co.,Ltd.
申请日:2019.12.26 公开日:2020.05.08
发明人:
【中文】游晓健
;
孙建良
;
张树前
;
周锦杨【EN】You Xiaojian
;
Sun Jianliang
;
Zhang Shuqian
;
Zhou Jinyang
摘要:【中文】本发明提供了一种热泵热水器及其加热控制方法,属于空气源热泵技术领域。它解决了现有技术由于双电同时运行,存在安全隐患等问题。本热泵热水器的加热控制方法适用于包括一种其内同时设有位于相对上侧的上电加热件和位于相对下侧的下电加热件且其外周侧绕设有换热器的水箱的热泵热水器,上电加热件运行功率大于下电加热件的运行功率,本加热控制方法包括节能模式和速热模式等。本一种热泵热水器及其加热控制方法的优点在于:使上、下两个电加热互斥地开启,在不同场合开启,下电加热在不用水的情况对整个水箱内的水进行加热,水箱水温均匀,上电加热只对水箱内的上半部分水加热,在用水的时候使水速热,减缓水箱水温下降的趋势,延长用水时间。 【EN】The invention provides a heat pump water heater and a heating control method thereof, and belongs to the technical field of air source heat pumps. It has solved prior art because two electricity move simultaneously, has potential safety hazard scheduling problem. The heating control method of the heat pump water heater is suitable for the heat pump water heater which comprises a water tank, wherein an upper electric heating element and a lower electric heating element are arranged in the water tank, the upper electric heating element is positioned on the opposite upper side, the lower electric heating element is positioned on the opposite lower side, and a heat exchanger is arranged around the outer periphery of the water tank. The heat pump water heater and the heating control method thereof have the advantages that: the upper electric heating and the lower electric heating are mutually exclusive and are started in different occasions, the lower electric heating heats the water in the whole water tank under the condition of not using the water, the water temperature of the water tank is uniform, the upper electric heating only heats the upper half part of the water in the water tank, the water is quickly heated when the water is used, the trend of the water temperature reduction of the water tank is slowed down, and the water using time is prolonged.
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9:
[发明]
【中文】适用于全球范围内的卫星业务数据实时下传系统 【EN】Satellite service data real-time downloading system suitable for global scope
申请号:
201911396458.2
公开号:CN111147128A 主分类号:H04B7/185
申请人:
【中文】上海卫星工程研究所【EN】Shanghai Institute of Satellite Engineering
申请日:2019.12.30 公开日:2020.05.12
发明人:
【中文】孙建亮
;
陈锋
;
刘登岭
;
周英庆【EN】
Sun Jianliang
;
Chen Feng
;
Liu Dengling
;
Zhou Yingqing
摘要:【中文】本发明提供了一种卫星业务数据下传领域内的适用于全球范围内的卫星业务数据实时下传系统,包括星载计算机、数传发射机及天线、对地应答机及天线、中继应答机及功放/天线,系统具备三种数据链路通信能力,即数传链路、中继链路和对地测控链路。在业务数据的存储设计上,全部业务数据通过数传数据帧实时下传,并将重要业务数据在遥测数据帧中进行编排下传;在下传工作模式设计上,境内采用实时数传、实时对地遥测方式,境外采用实时中继遥测方式。本发明实现了业务数据的实时下传,提升天地一体化系统接收业务数据的时效性,尤其适合天基应急系统应用。 【EN】The invention provides a satellite service data real-time downloading system suitable for the global scope in the satellite service data downloading field, which comprises an on-board computer, a data transmission transmitter and an antenna, an earth responder and an antenna, a relay responder and a power amplifier/antenna, wherein the system has three data link communication capabilities, namely a data transmission link, a relay link and an earth measurement and control link. In the storage design of service data, all service data are downloaded in real time through data transmission data frames, and important service data are arranged and downloaded in the telemetering data frames; on the design of a download working mode, a real-time data transmission and real-time ground telemetering mode is adopted in the interior, and a real-time relay telemetering mode is adopted in the exterior. The invention realizes real-time downloading of the service data, improves the timeliness of the heaven and earth integrated system for receiving the service data, and is particularly suitable for application of a space-based emergency system.
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10:
[发明]
【中文】一种用于动力学模拟的飞行器内部设备连接建模方法 【EN】Aircraft interior equipment connection modeling method for dynamics simulation
申请号:
201911222254.7
公开号:CN111104758A 主分类号:G06F30/23
申请人:
【中文】北京机电工程研究所【EN】BEIJING RESEARCH INSTITUTE OF MECHANICAL AND ELECTRICAL TECHNOLOGY
申请日:2019.12.03 公开日:2020.05.05
发明人:
【中文】蒲东东
;
孙建亮
;
高贵福
;
张青虎【EN】Pu Dongdong
;
Sun Jianliang
;
Gao Guifu
;
Zhang Qinghu
摘要:【中文】本发明涉及用于动力学模拟的飞行器内部设备连接建模方法,属于飞行器动力学建模技术领域,解决了现有方法建立的模型计算速度慢精度低的问题。飞行器内部设备连接建模方法包括:构建飞行器内部设备的结构模型;确定结构模型中的所有连接处的连接形式;将每个连接处的连接形式简化为结构与结构之间的强连接、无减震的设备安装连接、限位销或长螺栓连接和有减震的设备安装连接中的一种;限位销或长螺栓连接采用一维梁模型进行模拟;根据简化后的连接形式采用的模型,确定模型参数,并建立所有连接处的模型;对整个结构模型进行网格划分,完成整个结构模型的有限元模型建立。本发明简化了计算过程,提高了有限元仿真效率。 【EN】The invention relates to an aircraft interior equipment connection modeling method for dynamics simulation, belongs to the technical field of aircraft dynamics modeling, and solves the problems that a model established by the existing method is low in calculation speed and low in accuracy. The aircraft interior equipment connection modeling method comprises the following steps: constructing a structural model of the internal equipment of the aircraft; determining the connection form of all the connections in the structural model; simplifying the connection form of each connection part into one of strong connection between structures, shock-free equipment installation connection, limit pin or long bolt connection and shock-absorbing equipment installation connection; the connection of the limiting pin or the long bolt is simulated by adopting a one-dimensional beam model; determining model parameters according to a model adopted by the simplified connection form, and establishing models of all connection positions; and carrying out mesh division on the whole structure model to complete the establishment of the finite element model of the whole structure model. The invention simplifies the calculation process and improves the finite element simulation efficiency.
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