摘要：【中文】本发明提供了一种分离装置，该装置包括：支撑装置；输送管道，设置于支撑装置，用于接收包含有铁基物质的物料；磁性分离机构，设置于支撑装置，用于对物料中的铁基物质进行吸引，以使铁基物质从物料中分离出来；输送管道还用于将分离出的铁基物质和分离后的物料分别输出。本发明中，通过磁性分离机构对输送管道中的铁基物质进行吸引，使得铁基物质从物料中分离出来，实现了物料与铁基物质的分离，降低了物料中铁基催化剂的含量，分离过程中无需添加其他物质，也就不会如现有技术中那样产生危废物质，也无需进行过滤，能够保证连续进行分离，不间断地循环处理，提高了分离效率，降低了劳动强度，结构简单，无需多套装置备用，降低了生产成本。 【EN】The present invention provides a separation device, comprising: a support device; the conveying pipeline is arranged on the supporting device and used for receiving materials containing iron-based substances; the magnetic separation mechanism is arranged on the supporting device and used for attracting the iron-based substances in the materials so as to separate the iron-based substances from the materials; the conveying pipeline is also used for respectively outputting the separated iron-based substances and the separated materials. According to the invention, the iron-based substance in the conveying pipeline is attracted by the magnetic separation mechanism, so that the iron-based substance is separated from the material, the separation of the material and the iron-based substance is realized, the content of the iron-based catalyst in the material is reduced, other substances are not required to be added in the separation process, no hazardous waste substance is generated as in the prior art, no filtration is required, continuous separation can be ensured, uninterrupted circulating treatment is carried out, the separation efficiency is improved, the labor intensity is reduced, the structure is simple, multiple sets of devices are not required for standby, and the production cost is reduced.

摘要：【中文】本发明属于新型材料技术领域，公开了一种基于尿醛树脂的微胶囊密封剂的工程应用方法，包括：S1，将烘干后的微胶囊颗粒与固化剂按质量比为100:17的比例进行混合；S2，在S1得到的混合物中加入胶黏剂，并混合均匀；S3，将S2得到的混合物预涂覆在试件表面，并进行烘干；S4，将预涂覆后的试件表面在常温下固化预设时间，完成预涂覆，实现基于尿醛树脂的微胶囊密封剂工程应用，大幅提高设备的生产装配效率。 【EN】The invention belongs to the technical field of novel materials, and discloses an engineering application method of a microcapsule sealant based on urea-formaldehyde resin, which comprises the following steps: s1, mixing the dried microcapsule particles with a curing agent according to the mass ratio of 100: 17; s2, adding an adhesive into the mixture obtained in the step S1, and uniformly mixing; s3, pre-coating the mixture obtained in the step S2 on the surface of a test piece, and drying; s4, solidifying the surface of the pre-coated test piece for a preset time at normal temperature to finish pre-coating, realizing the engineering application of the microcapsule sealant based on the urea-formaldehyde resin, and greatly improving the production and assembly efficiency of the equipment.

摘要：【中文】本发明属于飞机结构腐蚀环境要素监控领域，具体一种飞机表面湿度在线监测传感探头。该探头包括：第一线电极、第二线电极、绝缘载体板，其中，第一线电极和第二线电极为同种材料电极并且第一线电极和第二线电极平行地设置在载体板上，第一线电极和第二线电极的间距小于第一线电极和第二线电极的线宽度。该探头监测电极之间的阻抗，可快速反映结构表面是否有液膜或水分存在，该探头重量轻、体积小，可直接贴在飞机结构表面，原位监测，不破坏原有结构，不影响飞机重量、气动外形。 【EN】The invention belongs to the field of monitoring of corrosive environment elements of airplane structures, and particularly relates to an on-line monitoring sensing probe for the surface humidity of an airplane. The probe includes: the first linear electrode and the second linear electrode are electrodes made of the same material and are arranged on the carrier plate in parallel, and the distance between the first linear electrode and the second linear electrode is smaller than the linear width of the first linear electrode and the second linear electrode. The probe can be used for monitoring the impedance between the electrodes, can quickly reflect whether a liquid film or water exists on the surface of the structure, has light weight and small volume, can be directly attached to the surface of the airplane structure, monitors in situ, does not damage the original structure, and does not influence the weight and the aerodynamic appearance of the airplane.

摘要：【中文】本发明属于飞机结构腐蚀环境要素监控领域，具体涉及一种飞机环境严酷度在线监测传感探头。该探头包括第一电极、第二电极，其中第一电极与第二电极平行并且通过绝缘材料粘接，在第一电极的一端设置有第一电极引出端，在第二电极的一端设置有第二电极引出端。该探头监测时不需要与机体结构直接接触，监测电极表面液膜之间的阻抗，可快速反映局部环境的腐蚀严酷性；探头监测时不需要电解质溶液。 【EN】The invention belongs to the field of monitoring of elements of a corrosion environment of an airplane structure, and particularly relates to an online monitoring sensing probe for the environment severity of an airplane. The probe comprises a first electrode and a second electrode, wherein the first electrode and the second electrode are parallel and are bonded through an insulating material, a first electrode leading-out end is arranged at one end of the first electrode, and a second electrode leading-out end is arranged at one end of the second electrode. When the probe is used for monitoring, the probe does not need to be in direct contact with a machine body structure, the impedance between liquid films on the surfaces of the electrodes is monitored, and the corrosion severity of a local environment can be quickly reflected; no electrolyte solution is required for probe monitoring.

摘要：【中文】本发明涉及一种基于周边环境的风电机组的性能评估方法，步骤为(1)对障碍物和风电机组进行建模；(2)采用矩形截面风沿设定间隔的位置角对所述风电机组进行扫略，并判断障碍物对风电机组是否造成影响；(3)对风电机组没有影响的位置角进行剔除，得到对风电机组有影响的位置角；(4)构建所述有影响的位置角的流体模型；(5)根据所述流体模型，对风电机组模型进行有障碍仿真计算；(6)根据所述有障碍仿真计算的结果进行评估。该评估过程考虑了障碍物对风电机组的实际影响，因此仿真结果更加准确，评估结果更加可靠，而且仅对剔除后的有影响的位置角进行仿真分析，可以提高模型仿真计算的效率。 【EN】The invention relates to a performance evaluation method of a wind turbine generator based on the surrounding environment, which comprises the steps of (1) modeling a barrier and the wind turbine generator; (2) sweeping the wind turbine generator along set spaced position angles by adopting rectangular section wind, and judging whether the wind turbine generator is influenced by obstacles; (3) eliminating the position angle which has no influence on the wind turbine generator to obtain the position angle which has influence on the wind turbine generator; (4) constructing a fluid model of the influential location angle; (5) carrying out obstacle simulation calculation on the wind turbine generator model according to the fluid model; (6) and evaluating according to the result of the obstacle simulation calculation. The actual influence of the obstacles on the wind turbine generator is considered in the evaluation process, so that the simulation result is more accurate, the evaluation result is more reliable, and only the position angle with the influence after elimination is subjected to simulation analysis, so that the efficiency of model simulation calculation can be improved.

摘要：【中文】本发明实施例公开了一种先进增强结构的涂层防护处理方法，该方法包括：根据对先进增强结构应用部位的环境分析，初步确定先进增强结构的待选涂层的防护体系；通过对初步确定的待选涂层的防护体系的试验验证，选取出符合应用部位环境的先进增强结构的防护体系；对选取的防护体系进行环境综合评估分析，验证防护体系的有效性和耐久性。采用本发明实施例提供的方案，可以提高腐蚀环境下先进增强结构腐蚀防护性能，加快先进增强结构在飞机的工程化应用，实现延长飞机检修间隔及寿命，提高飞机安全性及经济性的目标。 【EN】The embodiment of the invention discloses a coating protection treatment method of an advanced reinforced structure, which comprises the following steps: preliminarily determining a protection system of a coating to be selected of the advanced reinforced structure according to the environmental analysis of the application part of the advanced reinforced structure; the protection system of the advanced enhancement structure which accords with the environment of the application part is selected through the test verification of the preliminarily determined protection system of the coating to be selected; and carrying out comprehensive environmental evaluation and analysis on the selected protection system, and verifying the effectiveness and durability of the protection system. By adopting the scheme provided by the embodiment of the invention, the corrosion protection performance of the advanced reinforced structure in a corrosion environment can be improved, the engineering application of the advanced reinforced structure in an airplane is accelerated, the aims of prolonging the overhaul interval and the service life of the airplane and improving the safety and the economy of the airplane are fulfilled.

摘要：【中文】本发明实施例公开了一种先进增强结构的防腐密封处理方法，该方法包括：选取与金属材料和复合材料性能匹配的密封剂材料；确定先进增强结构的密封形式，密封形式包括密封方法和密封结构形式；对已选取的密封剂材料和已确定的密封结构进行密封性能验证。采用本发明实施例提供的方案，可以防止腐蚀介质进入胶层影响先进增强结构的性能，从而有效提高先进增强的抗腐蚀密封性能，延长结构检修间隔及寿命，提高飞机安全性及经济性。 【EN】The embodiment of the invention discloses an anti-corrosion sealing treatment method for an advanced reinforced structure, which comprises the following steps: selecting a sealant material with the performance matched with that of the metal material and the composite material; determining a sealing form of the advanced reinforcing structure, wherein the sealing form comprises a sealing method and a sealing structure form; and carrying out sealing performance verification on the selected sealant material and the determined sealing structure. By adopting the scheme provided by the embodiment of the invention, the corrosion medium can be prevented from entering the glue layer to influence the performance of the advanced reinforced structure, so that the advanced reinforced corrosion-resistant sealing performance is effectively improved, the structure overhaul interval and the service life are prolonged, and the safety and the economical efficiency of the airplane are improved.

摘要：【中文】本发明实施例公开了一种先进增强结构的结构处理方法，该方法包括：对先进增强结构进行构型选取，构型包括胶接形式和构型形状；对先进增强结构进行尺寸选择；对先进增强结构进行铺层设置，铺层设置包括铺层方式，铺层方向和结构层数；对先进增强结构进行边角处理。本发明实施例提供的方案，可以快速实现先进增强结构在飞机上的工程化应用，降低飞机构件在服役过程中裂纹产生及扩展的速率，延长飞机检修间隔及寿命，实现飞机减重、提高安全性及经济性。 【EN】The embodiment of the invention discloses a structure processing method of an advanced enhancement structure, which comprises the following steps: selecting the configuration of the advanced reinforced structure, wherein the configuration comprises a cementing form and a configuration shape; selecting the size of the advanced reinforcing structure; carrying out layering arrangement on the advanced reinforced structure, wherein the layering arrangement comprises a layering mode, a layering direction and a structural layer number; corner processing is performed on the advanced reinforcement structure. The scheme provided by the embodiment of the invention can quickly realize the engineering application of the advanced reinforced structure on the airplane, reduce the generation and expansion rate of cracks of airplane components in the service process, prolong the overhaul interval and the service life of the airplane, realize the weight reduction of the airplane and improve the safety and the economy.

摘要：【中文】本发明涉及一种绝缘试片批量放电装置，其技术特点是：包括放电簧片和放电器支架；放电簧片由缺少一侧圆弧的金属圆片构成，在金属圆片表面正上方和左右两侧制有三个通孔，该金属圆片两侧圆弧分别向上下两个方向翻折形成斜板，根据左右侧弯曲方向不同分为两类放电簧片；放电器支架包括安装在一起的底座、三根支撑杆、顶板，在顶板上安装压力器；两类放电簧片交替安装在放电支架上，在两类放电簧片之间安装绝缘试片。本发明设计合理，能够在48小时内一次性进行大量绝缘试片的放电工作，极大地提升绝缘试片放电效率，缩短连续进行高电压试验的绝缘试片准备时间，可广泛应用于绝缘材料的高电压试验中。 【EN】The invention relates to an insulating test piece batch discharge device, which is technically characterized in that: comprises a discharge reed and a discharger bracket; the discharge reed is composed of a metal wafer lacking an arc on one side, three through holes are formed right above the surface of the metal wafer and on the left side and the right side of the surface of the metal wafer, the arcs on the two sides of the metal wafer are respectively turned over towards the upper direction and the lower direction to form an inclined plate, and the discharge reed is divided into two types of discharge reeds according to different bending directions of the left side and the right side; the discharger support comprises a base, three supporting rods and a top plate which are arranged together, and a pressure device is arranged on the top plate; the two types of discharge reeds are alternately arranged on the discharge support, and an insulating test piece is arranged between the two types of discharge reeds. The invention has reasonable design, can discharge a large number of insulating test pieces at one time within 48 hours, greatly improves the discharge efficiency of the insulating test pieces, shortens the preparation time of the insulating test pieces for continuously carrying out high-voltage tests, and can be widely applied to the high-voltage tests of insulating materials.

摘要：【中文】本发明提供的一种超导电缆的骨架结构，括用于冷却介质的波纹管；该波纹管具有通入冷却介质的通道，以及环绕该通道的波纹结构的基材，所述基材的内壁与冷却介质相接触，所述基材的外壁与超导电缆的功能层相接触；所述基材具有多个开口部，冷却介质通过该开口部与超导电缆的功能层相接触；本发明的骨架结构液氮可以直接透过波纹管屏障，与通电导体功能层直接接触，传热路径缩短，接触热阻被大量排除，传热效果得到很大程度的提升，从而会提高通电导体内部的温度均匀性，有利于功能层热耗散的及时导出，有利于超导电缆通电导体的稳定性。 【EN】The invention provides a skeleton structure of a superconducting cable, which comprises a corrugated pipe for cooling a medium; the corrugated pipe has a passage into which a cooling medium is introduced, and a base material of a corrugated structure surrounding the passage, an inner wall of the base material being in contact with the cooling medium, and an outer wall of the base material being in contact with a functional layer of the superconducting cable; the base material has a plurality of openings through which the cooling medium is brought into contact with the functional layer of the superconducting cable; the liquid nitrogen with the skeleton structure can directly penetrate through the corrugated pipe barrier and directly contact with the functional layer of the electrified conductor, so that the heat transfer path is shortened, the contact thermal resistance is greatly eliminated, and the heat transfer effect is greatly improved, thereby improving the temperature uniformity in the electrified conductor, facilitating the timely conduction of the heat dissipation of the functional layer and facilitating the stability of the electrified conductor of the superconducting cable.