CN115568195A - Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable - Google Patents
Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable Download PDFInfo
- Publication number
- CN115568195A CN115568195A CN202211058856.5A CN202211058856A CN115568195A CN 115568195 A CN115568195 A CN 115568195A CN 202211058856 A CN202211058856 A CN 202211058856A CN 115568195 A CN115568195 A CN 115568195A
- Authority
- CN
- China
- Prior art keywords
- cabin
- cable
- penetrating
- metal boss
- shielding
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000035515 penetration Effects 0.000 title claims abstract description 15
- 229910052751 metal Inorganic materials 0.000 claims abstract description 39
- 239000002184 metal Substances 0.000 claims abstract description 39
- 230000000149 penetrating effect Effects 0.000 claims description 21
- 239000002390 adhesive tape Substances 0.000 claims description 7
- 229920001721 polyimide Polymers 0.000 claims description 6
- 238000004804 winding Methods 0.000 claims description 4
- 238000005452 bending Methods 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 8
- 230000005855 radiation Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
- H05K9/0007—Casings
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/52—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
- H01Q1/526—Electromagnetic shields
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
- H05K9/0007—Casings
- H05K9/0015—Gaskets or seals
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Insulated Conductors (AREA)
Abstract
一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽结构和方法,屏蔽结构包括连接于舱体内侧的金属凸台,穿舱电缆穿过金属凸台、舱体的电缆穿舱孔,穿舱电缆的插接件与舱体内设备插接;镀铝膜包裹穿舱电缆、包裹插接件直到与设备外壳搭接、包裹金属凸台外壁直到与舱体搭接;屏蔽方法包括:用镀铝膜包裹穿舱电缆,包裹的起点和终点为插件底座和穿舱电缆穿舱位置,两端均预留镀铝膜;接插件插入设备后,将预留镀铝膜完全包裹住接插件并与设备外壳良好搭接;在电缆穿舱孔位置安装金属凸台,将穿舱电缆通过金属凸台穿出舱体,将预留的镀铝膜完全包裹金属凸台外壁且与舱板良好搭接。成本低、操作简便、易于实现,并且能够有效控制穿舱电缆对舱体屏蔽效能的破坏。
A shielding structure and method for an unshielded cable to penetrate a cabin with high shielding requirements. The shielding structure includes a metal boss connected to the inside of the cabin, and the cable passing through the cabin passes through the metal boss, the cable through the cabin hole of the cabin, and passes through the cabin. The connector of the cable is plugged into the equipment in the cabin; the aluminized film wraps the cable through the cabin, wraps the connector until it overlaps with the equipment shell, wraps the outer wall of the metal boss until it overlaps with the cabin; shielding methods include: The film wraps the cable through the cabin. The starting point and the end point of the package are the plug-in base and the position of the cable through the cabin. Both ends are reserved with aluminized film; after the connector is inserted into the device, the reserved aluminized film is completely wrapped around the connector and connected The equipment shell is well lapped; install a metal boss at the position of the cable penetration hole, pass the cable through the metal boss out of the cabin, completely wrap the reserved aluminized film on the outer wall of the metal boss and have a good lap with the deck . The utility model has the advantages of low cost, simple and convenient operation and easy realization, and can effectively control damage to the shielding effectiveness of the cabin body by the penetration cable.
Description
技术领域technical field
本发明涉及一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽结构和方法,属于舱体/箱体屏蔽技术领域。The invention relates to a shielding structure and method for an unshielded cable to penetrate a cabin with high shielding requirements, and belongs to the technical field of cabin/cabinet shielding.
背景技术Background technique
卫星等航天器越来越多的配置高灵敏电子接收机,为了保证接收机不会受到航天器本身辐射的干扰影响,航天器本体要求非常高的屏蔽效能设计,即保证航天器本体内部的设备及电缆辐射发射的干扰信号不会传导至航天器外部干扰高灵敏接收天线。More and more spacecraft such as satellites are equipped with high-sensitivity electronic receivers. In order to ensure that the receiver will not be affected by the interference of the spacecraft itself, the spacecraft body requires a very high shielding efficiency design, that is, to ensure that the equipment inside the spacecraft body The interference signal emitted by the cable and the cable will not be transmitted to the external interference high-sensitivity receiving antenna of the spacecraft.
针对航天器本体高屏蔽效能的设计,最难处理的是穿透本体的电缆,其中又以非屏蔽电缆最难施加屏蔽措施,其对本体屏蔽效能的破坏极其严重。因此,亟需设计一种有效并且方便实施的非屏蔽电缆穿透高屏蔽要求舱体的屏蔽方法,以适应型号应用的需求。For the design of high shielding effectiveness of the spacecraft body, the most difficult thing to deal with is the cable that penetrates the body. Among them, the unshielded cable is the most difficult to apply shielding measures, which seriously damages the shielding effectiveness of the body. Therefore, there is an urgent need to design an effective and convenient shielding method for unshielded cables to penetrate the cabin with high shielding requirements, so as to meet the needs of model applications.
发明内容Contents of the invention
本发明的技术解决问题是:提出一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽结构和方法,在保证非屏蔽电缆正常传输信号的前提下,减少其对舱体屏蔽效能的破坏,有效提升舱体的屏蔽能力。The technical solution of the present invention is to propose a shielding structure and method for an unshielded cable to penetrate a cabin with high shielding requirements, and to reduce its damage to the shielding effectiveness of the cabin under the premise of ensuring the normal transmission of signals by the unshielded cable, effectively Improve the shielding ability of the cabin.
本发明的技术解决方案是:Technical solution of the present invention is:
一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽结构,包括:A shielding structure in which an unshielded cable penetrates a cabin with high shielding requirements, including:
金属凸台,连接于舱体内侧,穿舱电缆穿过金属凸台、并通过电缆穿舱孔穿过舱体,穿舱电缆的插接件与舱体内设备插接;The metal boss is connected to the inside of the cabin body, the cable through the cabin passes through the metal boss, and passes through the cabin body through the cable hole, and the connector of the cable through the cabin is plugged into the equipment in the cabin;
镀铝膜,包裹穿舱电缆,且两端分别包裹穿舱电缆的插接件直到与设备外壳良好搭接、包裹金属凸台外壁直到与舱体良好搭接。Aluminized film wraps the cable through the cabin, and wraps the connectors of the cable through the cabin at both ends until it overlaps with the equipment shell, and wraps the outer wall of the metal boss until it overlaps with the cabin.
所述金属凸台为圆管状,金属凸台的外壁一端设置有底座,底座通过螺钉连接于舱体。The metal boss is in the shape of a circular tube, and one end of the outer wall of the metal boss is provided with a base, and the base is connected to the cabin body by screws.
所述凸台向舱内凸起的高度为40-60mm,金属凸台的内径与电缆穿舱孔直径一致。The height of the boss protruding into the cabin is 40-60mm, and the inner diameter of the metal boss is consistent with the diameter of the cable penetration hole.
所述镀铝膜为双面或单面带孔膜,厚度为18-25μm,包裹电缆后在两端预留的长度为200-500mm;镀铝膜为镀铝聚酰亚胺膜。The aluminized film is a double-sided or single-sided porous film with a thickness of 18-25 μm, and the length reserved at both ends after wrapping the cable is 200-500 mm; the aluminized film is an aluminized polyimide film.
在所述镀铝膜从穿舱电缆包裹至与设备外壳搭接的部分,任意两点电阻小于10mΩ;At the part where the aluminized film wraps from the penetrating cable to overlaps with the equipment shell, the resistance of any two points is less than 10mΩ;
在镀铝膜从穿舱电缆包裹至金属凸台外壁并与舱板搭接的部分,任意两点的电阻小于10mΩ。At the part where the aluminized film wraps from the penetrating cable to the outer wall of the metal boss and overlaps with the deck, the resistance of any two points is less than 10mΩ.
所述金属凸台的底座与舱体之间电阻小于10mΩ。The resistance between the base of the metal boss and the cabin body is less than 10mΩ.
在所述镀铝膜包裹穿舱电缆后的部分,任意两点的电阻小于15mΩ。In the part after the aluminized film wraps the penetrating cable, the resistance of any two points is less than 15mΩ.
所述镀铝膜的褶皱或弯折缝隙处使用胶带固定,胶带为导电胶带。The folds or bending gaps of the aluminized film are fixed with adhesive tape, and the adhesive tape is conductive adhesive tape.
所述镀铝膜包裹电缆的方法为:裁减镀铝膜每条宽度约30-50mm,缠绕时镀铝膜前后两圈互叠约40-60%;穿舱电缆成束用镀铝膜包裹两层,两层的顺逆时针方向相反;一根镀铝膜缠绕完成后,下一根镀铝膜从上一根结束的位置向后100-200mm开始包裹,镀铝膜接触的地方采用胶带固定。The method of wrapping the cable with the aluminized film is as follows: cut the width of each aluminized film to about 30-50 mm, and overlap the front and rear circles of the aluminized film by about 40-60% when winding; The two layers are opposite in clockwise direction; after one aluminized film is wound, the next aluminized film is wrapped 100-200mm backward from the position where the previous one ends, and the place where the aluminized film touches is fixed with tape .
一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽方法,步骤如下:A shielding method for an unshielded cable to penetrate a cabin with high shielding requirements, the steps are as follows:
(1)采用镀铝聚酰亚胺膜包裹需要穿舱的电缆,包裹的起点和终点分别为电缆接插件底座底部和电缆穿舱的位置,两端均预留一定长度的镀铝膜;(1) Use aluminized polyimide film to wrap the cables that need to pass through the cabin. The starting point and end point of the package are the bottom of the cable connector base and the position where the cable goes through the cabin respectively, and a certain length of aluminized film is reserved at both ends;
(2)电缆接插件插入设备后,将预留的镀铝膜包裹至接插件直至镀铝膜完全包裹住接插件并与设备外壳良好搭接;(2) After the cable connector is inserted into the equipment, wrap the reserved aluminized film to the connector until the aluminized film completely wraps the connector and overlaps well with the equipment shell;
(3)在电缆穿舱孔位置安装金属凸台,凸台是底座用螺钉固定在舱板上,有一个凸向舱内的圆柱形管道;将穿舱电缆通过凸台圆柱形管道出舱,将预留的镀铝膜包裹至凸台管道外壁,直至管道外壁完全包裹且与舱板良好搭接。(3) Install a metal boss at the position of the cable penetration hole. The boss is a base fixed on the deck with screws, and has a cylindrical pipe protruding into the cabin; the cable passing through the cabin is passed out of the cabin through the cylindrical pipe of the boss. Wrap the reserved aluminized film to the outer wall of the boss pipe until the outer wall of the pipe is completely wrapped and well lapped with the deck.
步骤(1)所述镀铝聚酰亚胺膜应选择双面或单面带孔膜,厚度为18μm,包裹电缆后在两端预留200mm;所述镀铝膜包裹电缆的方法为:裁减镀铝膜每条宽度约40mm,缠绕时镀铝膜前后两圈互叠约50%;电缆成束用镀铝膜包裹两层,两层的顺逆时针方向相反;一根镀铝膜缠绕完成后,下一根镀铝膜应从上一根结束的位置向后100-200mm开始包裹;电缆包覆时要保证镀铝膜缠绕电缆足够紧,互叠处无缝隙,弯折处的缝隙用镀铝胶带包扎固定,防止缝隙出现;应使用全新的无褶皱镀铝膜包裹电缆,保证镀铝膜一次性完成包裹,少折痕,以保证镀铝膜的电连续性,镀铝膜任意两点的电阻应小于15mΩ。The aluminized polyimide film in step (1) should be double-sided or single-sided with holes, the thickness is 18 μm, and 200mm is reserved at both ends after wrapping the cable; the method of wrapping the cable with the aluminized film is: The width of each aluminum-coated film is about 40mm, and the front and rear circles of the aluminum-coated film overlap each other by about 50% when winding; the cables are bundled and wrapped with two layers of aluminum-coated film, and the clockwise and counterclockwise directions of the two layers are opposite; one aluminum-coated film is wound. Finally, the next aluminized film should be wrapped 100-200mm backward from the end position of the previous one; when wrapping the cable, ensure that the aluminized film is wrapped around the cable tightly enough, there is no gap at the overlapping place, and the gap at the bend is covered with a plated film. The aluminum tape is wrapped and fixed to prevent gaps; the cable should be wrapped with a brand-new non-wrinkled aluminized film to ensure that the aluminized film is wrapped at one time, with less creases to ensure the electrical continuity of the aluminized film. Any two points on the aluminized film The resistance should be less than 15mΩ.
步骤(2)所述镀铝膜完全包裹接插件并与设备外壳良好搭接,需要使用镀铝胶带对电缆至接插件过渡地方产生的褶皱进行紧密绑扎,不露缝隙;镀铝膜、接插件与设备外壳应形成电连续体,镀铝膜与设备外壳搭接电阻应小于10mΩ。The aluminized film in step (2) completely wraps the connector and overlaps well with the equipment shell. It is necessary to use aluminized tape to tightly bind the folds generated at the transition point between the cable and the connector without revealing the gap; the aluminized film, the connector It should form an electrical continuum with the equipment shell, and the lap resistance between the aluminized film and the equipment shell should be less than 10mΩ.
步骤(3)所述凸台底座至少用四个螺钉紧固在舱板上,凸台底座与舱板电阻应小于10mΩ;凸台向舱内凸起的高度为40-60mm,圆柱形管道内径与电缆穿舱孔直径一致。所述镀铝膜包裹至凸台圆柱形管道外壁并与舱板良好搭接,任意两者的电阻应小于10mΩ。In step (3), the boss base is fastened on the deck with at least four screws, and the resistance between the boss base and the deck should be less than 10mΩ; Consistent with the diameter of the cable penetration hole. The aluminized film is wrapped to the outer wall of the cylindrical pipe of the boss and well overlapped with the deck, and the resistance of any two should be less than 10mΩ.
综上所述,本申请至少包括以下有益技术效果:In summary, the present application at least includes the following beneficial technical effects:
(1)本发明方法大大减少了非屏蔽电缆穿透舱体对舱体屏蔽效能的破坏,优化了舱体的屏蔽效能,从而减少了宇航器舱内辐射信号泄漏至舱外干扰高灵敏接收天线;(1) The method of the present invention greatly reduces the damage to the shielding effectiveness of the cabin by unshielded cables penetrating the cabin, optimizes the shielding effectiveness of the cabin, thereby reducing the leakage of the radiation signal in the spacecraft cabin to the high-sensitivity receiving antenna outside the cabin ;
(2)使用本发明方法还能够减少舱外干扰信号通过穿舱非屏蔽电缆传导至宇航器舱内进行辐射,从而提高了舱内其它设备的抗外界电磁环境的能力。(2) The use of the method of the present invention can also reduce the interference signal outside the cabin to be transmitted to the spacecraft cabin for radiation through the unshielded cable through the cabin, thereby improving the ability of other equipment in the cabin to resist the external electromagnetic environment.
附图说明Description of drawings
图1为本发明屏蔽处理示意图;Fig. 1 is the schematic diagram of shielding treatment of the present invention;
图2为本发明流程示意图。Fig. 2 is a schematic flow chart of the present invention.
附图标记说明:1、舱体;2、电缆穿舱孔;3、穿舱电缆;4、金属凸台;5、镀铝膜。Explanation of reference signs: 1. cabin body; 2. cable penetration hole; 3. cabin penetration cable; 4. metal boss; 5. aluminized film.
具体实施方式detailed description
下面结合附图和具体实施例对本申请作进一步详细的描述:Below in conjunction with accompanying drawing and specific embodiment the application is described in further detail:
本申请实施例公开一种非屏蔽电缆穿透高屏蔽要求舱体的屏蔽结构和方法,参照图1,屏蔽结构包括金属凸台4和镀铝膜5,金属凸台4连接于舱体1(图中未示出)内侧,穿舱电缆3穿过金属凸台4、并通过电缆穿舱孔2穿过舱体1,穿舱电缆3的插接件与舱体1内设备插接;镀铝膜5包裹穿舱电缆3,且两端分别包裹穿舱电缆3的插接件直到与设备外壳良好搭接、包裹金属凸台4外壁直到与舱体1的舱板良好搭接。The embodiment of the present application discloses a shielding structure and method for an unshielded cable to penetrate a cabin with high shielding requirements. Referring to FIG. Not shown in the figure) inside, the
金属凸台4为圆管状,金属凸台4的外壁一端设置有底座,底座通过螺钉连接于舱体1。凸台向舱内凸起的高度为40-60mm,金属凸台4的内径与电缆穿舱孔2直径一致。金属凸台4材料一般为铝合金,壁厚为3mm左右,金属凸台4底座应能完全封堵舱板的穿舱。The metal boss 4 is in the shape of a circular tube, and one end of the outer wall of the metal boss 4 is provided with a base, and the base is connected to the cabin body 1 by screws. The height that the boss protrudes into the cabin is 40-60mm, and the inner diameter of the metal boss 4 is consistent with the diameter of the
镀铝膜5为镀铝聚酰亚胺膜。镀铝聚酰亚胺膜应选择双面或单面带孔膜,厚度为18μm,包裹电缆后在两端预留的长度为200mm。The aluminized film 5 is an aluminized polyimide film. The aluminized polyimide film should be double-sided or single-sided with holes, the thickness is 18μm, and the length reserved at both ends after wrapping the cable is 200mm.
如图2所示,屏蔽方法方法包括:As shown in Figure 2, the shielding method methods include:
第一步:采用双面或单面带孔镀铝膜5包裹需要穿舱体1的穿舱电缆3,镀铝膜5厚度为18μm,包裹的起点和终点分别为穿舱电缆3接插件底座底部和电缆穿舱的位置,两端均预留200-500mm的镀铝膜5,本实施例中,两端均预留200mm的镀铝膜5。包裹时,先将镀铝膜5裁减每条宽度约40mm,缠绕时镀铝膜5前后两圈互叠约50%;穿舱电缆3成束用镀铝膜5包裹两层,两层的顺逆时针方向相反,如第一层为顺时针缠绕,第二次则为逆时针缠绕;一根镀铝膜5缠绕完成后,下一根镀铝膜5应从上一根结束的位置向后100-200mm开始包裹,镀铝膜5接触的地方采用镀铝胶带固定;包裹穿舱电缆3时要保证镀铝膜5缠绕穿舱电缆3足够紧,互叠处无缝隙,弯折处的缝隙用镀铝胶带包扎固定,防止缝隙出现;应使用全新的无褶皱镀铝膜5包裹电缆,保证镀铝膜5一次性完成包裹,少折痕,以保证镀铝膜5的任意两点的电阻应小于15mΩ。Step 1: Use double-sided or single-sided perforated aluminized film 5 to wrap the penetrating
第二步:穿舱电缆3的接插件插入设备后,将预留的镀铝膜5包裹至接插件直至镀铝膜5完全包裹住接插件,用镀铝胶带对穿舱电缆3至接插件过渡地方产生的褶皱进行紧密绑扎,不露缝隙;镀铝膜5、接插件与设备外壳应形成电连续体,镀铝膜5与设备外壳搭接电阻应小于10mΩ。Step 2: After the connector of the through-
第三步:在电缆穿舱孔2位置安装金属凸台4,金属凸台4底座用至少4个螺钉固定在舱板上,金属凸台4底座与舱板电阻应小于10mΩ;金属凸台4向舱内凸起的高度为50mm,金属凸台4为圆柱形管道,圆柱形管道内径与电缆穿舱孔2直径一致;将穿舱电缆3穿过凸台出舱,将预留的镀铝膜5包裹至金属凸台4外壁,直至金属凸台4外壁完全包裹且与舱板良好搭接,镀铝膜5、金属凸台4和舱体1的舱板任意两点的电阻应小于10mΩ。Step 3: Install the metal boss 4 at the position of the
本发明说明书中未作详细描述的内容属本领域技术人员的公知技术。The content that is not described in detail in the description of the present invention belongs to the well-known technology of those skilled in the art.
以上均为本申请的较佳实施例,并非依此限制本申请的保护范围,故:凡依本申请的结构、形状、原理所做的等效变化,均应涵盖于本申请的保护范围之内。All of the above are preferred embodiments of the application, and are not intended to limit the protection scope of the application. Therefore, all equivalent changes made according to the structure, shape, and principle of the application should be covered by the protection scope of the application. Inside.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211058856.5A CN115568195A (en) | 2022-08-30 | 2022-08-30 | Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211058856.5A CN115568195A (en) | 2022-08-30 | 2022-08-30 | Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable |
Publications (1)
Publication Number | Publication Date |
---|---|
CN115568195A true CN115568195A (en) | 2023-01-03 |
Family
ID=84738288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211058856.5A Pending CN115568195A (en) | 2022-08-30 | 2022-08-30 | Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115568195A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116500348A (en) * | 2023-06-30 | 2023-07-28 | 北京智芯微电子科技有限公司 | Low-frequency electromagnetic measuring device and system |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103491756A (en) * | 2013-10-22 | 2014-01-01 | 中国舰船研究设计中心 | Shielding treatment device for shielded compartment penetration cable for ship |
CN107404096A (en) * | 2017-08-31 | 2017-11-28 | 上海振华重工(集团)股份有限公司 | A kind of submerged cable crossing cabin part and waterstop sealing method |
CN207011205U (en) * | 2017-05-18 | 2018-02-13 | 北京空间飞行器总体设计部 | A kind of high shield effectiveness device for satellite |
CN110112611A (en) * | 2019-04-25 | 2019-08-09 | 中国科学院声学研究所 | A kind of pressure balance type high-voltage electricity crossing cabin connector and connection method |
CN110676781A (en) * | 2019-10-23 | 2020-01-10 | 上海海洋大学 | Pressure-resistant sealing structure of watertight cabin-penetrating joint and manufacturing method |
CN213426792U (en) * | 2020-08-27 | 2021-06-11 | 北京空间飞行器总体设计部 | Electromagnetic shielding equipment for spacecraft radio frequency cable cabin penetrating hole |
-
2022
- 2022-08-30 CN CN202211058856.5A patent/CN115568195A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103491756A (en) * | 2013-10-22 | 2014-01-01 | 中国舰船研究设计中心 | Shielding treatment device for shielded compartment penetration cable for ship |
CN207011205U (en) * | 2017-05-18 | 2018-02-13 | 北京空间飞行器总体设计部 | A kind of high shield effectiveness device for satellite |
CN107404096A (en) * | 2017-08-31 | 2017-11-28 | 上海振华重工(集团)股份有限公司 | A kind of submerged cable crossing cabin part and waterstop sealing method |
CN110112611A (en) * | 2019-04-25 | 2019-08-09 | 中国科学院声学研究所 | A kind of pressure balance type high-voltage electricity crossing cabin connector and connection method |
CN110676781A (en) * | 2019-10-23 | 2020-01-10 | 上海海洋大学 | Pressure-resistant sealing structure of watertight cabin-penetrating joint and manufacturing method |
CN213426792U (en) * | 2020-08-27 | 2021-06-11 | 北京空间飞行器总体设计部 | Electromagnetic shielding equipment for spacecraft radio frequency cable cabin penetrating hole |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116500348A (en) * | 2023-06-30 | 2023-07-28 | 北京智芯微电子科技有限公司 | Low-frequency electromagnetic measuring device and system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102610304B (en) | Differential signal transmission cable | |
CN115568195A (en) | Shielding structure and method for cabin with high shielding requirement for penetration of unshielded cable | |
CN110212378A (en) | The shielding construction and production method that cable assembly is connect with electric connector | |
CN201084483Y (en) | A shielded connecting wire | |
CN113628792A (en) | Anti-electromagnetic interference method for vehicle wiring harness and anti-electromagnetic interference vehicle wiring harness | |
CN207011205U (en) | A kind of high shield effectiveness device for satellite | |
CN211208838U (en) | Control cable for measuring air temperature behind engine fan | |
CN203180478U (en) | Cable wrapping type joint | |
WO2015096762A1 (en) | Base station antenna cable | |
CN210430351U (en) | Wire harness structure with fireproof and anti-electromagnetic interference functions | |
CN207009144U (en) | A kind of multiple twin shields CAN | |
US6710243B2 (en) | Structure of signal line | |
CN111834035A (en) | A cable with Z shield | |
CN201975636U (en) | Plug of data connector | |
CN107833704B (en) | EMC shielding treatment process of electronic conductive parts outside the cabin of electronic reconnaissance satellite | |
JP2005259385A (en) | Communication cable | |
CN211530157U (en) | Ultralow-loss phase-stable microwave coaxial cable | |
CN221746886U (en) | Coaxial cable | |
WO2021128522A1 (en) | Shielding film for cable and method for connecting cable and connector | |
CN218525837U (en) | Grounding structure of shielded wire and vehicle | |
CN206639626U (en) | A kind of spacecraft of high electromagnet shield effect multicore LVDS cables | |
CN220627441U (en) | Double-layer protective layer composite cable | |
CN222168859U (en) | An innovative electromagnetic shielding structure for port cable connector | |
CN222380306U (en) | Multi-core control cable with high frequency signal crosstalk suppression | |
CN117790070A (en) | Shielding structure of cable assembly |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |