CN101901990A - Plug-in locking device for field replaceable modules - Google Patents
Plug-in locking device for field replaceable modules Download PDFInfo
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- CN101901990A CN101901990A CN 201010259955 CN201010259955A CN101901990A CN 101901990 A CN101901990 A CN 101901990A CN 201010259955 CN201010259955 CN 201010259955 CN 201010259955 A CN201010259955 A CN 201010259955A CN 101901990 A CN101901990 A CN 101901990A
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- 230000037431 insertion Effects 0.000 abstract description 4
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- 230000006835 compression Effects 0.000 description 5
- 238000007906 compression Methods 0.000 description 5
- 210000002105 tongue Anatomy 0.000 description 5
- 210000004247 hand Anatomy 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
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- 238000010586 diagram Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
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Abstract
本发明属于紧固件技术,涉及一种用于航空机载电子设备的外场可更换模块用插拔锁紧装置。插拔锁紧装置包括锁钩、扭簧、销轴、紧定螺钉、提手、压簧、锁舌、压板、沉头螺钉。本装置是一种用于航空机载电子设备外场可更换模块的插入、拔出和锁紧的机械装置。主要用来克服推入和拔出模块时电连接器的插拔力,保证模块装卸时的运动轨迹为直线滑移,使模块在受冲击和振动时,电连接器完全保持啮合,保证信号传输正常。而且保证模块所受外力不会传递到电联接器端子上造成机械损伤或电性能失效。本发明装置具有把模块插入、拔出、锁紧到机箱的三重功能。
The invention belongs to the technology of fasteners, and relates to a plug-and-pull locking device for an outfield replaceable module used in aviation airborne electronic equipment. The plug-in locking device includes a lock hook, a torsion spring, a pin shaft, a set screw, a handle, a stage clip, a dead bolt, a pressing plate, and a countersunk screw. The device is a mechanical device used for inserting, pulling out and locking the field replaceable modules of aviation airborne electronic equipment. It is mainly used to overcome the insertion and withdrawal force of the electrical connector when the module is pushed in and out, to ensure that the movement track of the module is a linear slip when the module is loaded and unloaded, so that the electrical connector is completely kept engaged when the module is impacted and vibrated, and the signal transmission is ensured. normal. Moreover, it is ensured that the external force on the module will not be transmitted to the terminals of the electrical connector to cause mechanical damage or electrical performance failure. The device of the invention has triple functions of inserting, pulling out and locking the module to the chassis.
Description
技术领域technical field
本发明属于紧固件技术,涉及一种用于航空机载电子设备的外场可更换模块用插拔锁紧装置。The invention belongs to the technology of fasteners, and relates to a plug-and-pull locking device for an outfield replaceable module used in aviation airborne electronic equipment.
背景技术Background technique
随着航空电子设备的轻量化和小型化的发展趋势,对设备的快速安装和拆卸提出更高的要求。严格的外场平均修复时间(MTTR)要求使得外场可更换模块的概念应运而生,而插拔装置(Insertion/Extraction Device,IED)是外场可更换模块应用中必不可少的重要部件。在模块推入和拔出设备机箱时,模块印制板子板和机箱母板的电连接器啮合或分离,而插拔装置的作用就是提供和克服这种电连接器啮合或分离时所需要的插拔力,保证模块装卸时的运动轨迹为直线滑移,从而保证模块所受外力不会传递到电联接器端子上造成机械损伤或电性能失效。目前航空系统所应用的大部分装置均是由一根类似杠杆的装置将模块撬起,此种装置只具有将模块从机箱中拔出的功能,无法克服模块插入时电连接器啮合所产生的力,使模块的电连接器端子极易受损,并且在机箱中无法锁定模块。With the development trend of lightweight and miniaturization of avionics equipment, higher requirements are put forward for the rapid installation and disassembly of the equipment. Strict field mean time to repair (MTTR) requirements make the concept of field replaceable modules emerge as the times require, and the Insertion/Extraction Device (IED) is an essential and important component in the application of field replaceable modules. When the module is pushed into and pulled out of the equipment chassis, the electrical connector of the module printed board sub-board and the chassis motherboard engages or separates, and the function of the plug-in device is to provide and overcome the need for this electrical connector to engage or separate The insertion force ensures that the movement track of the module is a linear slip when loading and unloading, so as to ensure that the external force on the module will not be transmitted to the electrical connector terminals to cause mechanical damage or electrical performance failure. Most of the devices currently used in aviation systems use a lever-like device to pry up the module. This device only has the function of pulling the module out of the chassis, and cannot overcome the problem caused by the engagement of the electrical connector when the module is inserted. force, making the module's electrical connector terminals highly susceptible to damage and making it impossible to lock the module in the chassis.
发明内容Contents of the invention
本发明的目的是提出一种同时具有插入、拔出、锁紧功能的外场可更换模块用插拔锁紧装置。本发明的技术解决方案是,插拔锁紧装置包括锁钩、扭簧、销轴、紧定螺钉、提手、压簧、锁舌、压板、沉头螺钉,锁钩用螺钉、弹簧垫圈、垫圈固定在模块的前面板上,提手为“U”形,提手两个侧壁的一端的凸缘上对称设有两个凸耳,锁钩用销轴连接在提手的两个凸耳上,扭簧置于销轴的中间,锁钩上的锁头的顶部有一个斜面;提手的底平面上开有与锁钩的锁头相对应位置处开有一个方孔,在提手底面内侧靠近锁钩的一端设有两个螺纹孔,提手另一端的两侧壁上对称设有两个通孔,锁舌的中间有一个长方形孔,长方形孔的一个侧壁为斜面,长方形孔的斜面与锁头顶部的斜面相对应;提手的底面内侧与锁舌中间的长方形孔相对应的位置上设有一个长方形凹槽,长方形凹槽与锁舌的长方形孔形成一个空腔,压簧位于空腔中,压板对应空腔的位置上开有一个方形开口,方形开口的根部与锁舌的接触面上设有限位块,压板开口的一端通过两个沉头螺钉固定在提手的螺纹孔中,两个螺钉通过压板两个侧壁上的螺纹孔把压板的另一端固定在提手侧壁上。The object of the present invention is to propose a plug-in and pull-out locking device for field-replaceable modules that simultaneously has the functions of plugging in, pulling out, and locking. The technical solution of the present invention is that the plug-in locking device includes a lock hook, a torsion spring, a pin shaft, a set screw, a handle, a compression spring, a dead bolt, a pressure plate, a countersunk screw, a screw for the lock hook, a spring washer, The washer is fixed on the front panel of the module, the handle is "U" shape, two lugs are symmetrically arranged on the flanges at one end of the two side walls of the handle, and the lock hook is connected to the two lugs of the handle with a pin shaft. On the ear, the torsion spring is placed in the middle of the pin shaft, and the top of the lock head on the lock hook has a slope; Two threaded holes are arranged on the inner side of the bottom surface of the hand near the lock hook, two through holes are symmetrically arranged on the two side walls of the other end of the handle, and there is a rectangular hole in the middle of the dead bolt, and one side wall of the rectangular hole is an inclined plane. The slope of the rectangular hole corresponds to the slope at the top of the lock head; a rectangular groove is provided on the inner side of the bottom surface of the handle corresponding to the rectangular hole in the middle of the deadbolt, and the rectangular groove forms a cavity with the rectangular hole of the deadbolt , the compression spring is located in the cavity, and there is a square opening on the position of the pressure plate corresponding to the cavity. A limit block is provided on the contact surface between the root of the square opening and the lock tongue, and one end of the opening of the pressure plate is fixed on the lifting handle by two countersunk screws. In the threaded hole of the hand, two screws fix the other end of the pressure plate on the handle side wall through the threaded holes on the two side walls of the pressure plate.
所述的锁钩还可以固定在模块的侧面或其中的印制电路板上。The locking hook can also be fixed on the side of the module or the printed circuit board therein.
所述的扭簧还可以为片簧。The torsion spring can also be a leaf spring.
本发明具有的优点和有益效果,本装置是一种用于航空机载电子设备外场可更换模块(LRM)的插入、拔出和锁紧的机械装置。主要用来克服模块推入和拔出时背后电连接器啮合、分离时所需要的插拔力,保证模块装卸时的运动轨迹为直线滑移,使模块在受冲击和振动时,电连接器的完全保持啮合,信号传输正常。而且保证模块所受外力不会传递到电联接器端子上造成机械损伤或电性能失效。The invention has the advantages and beneficial effects. The device is a mechanical device used for inserting, pulling out and locking the field replaceable module (LRM) of the aviation airborne electronic equipment. It is mainly used to overcome the plugging force required when the electrical connector on the back is engaged and separated when the module is pushed in and pulled out, so as to ensure that the movement track of the module is a linear slip when the module is loaded and unloaded, so that when the module is impacted and vibrated, the electrical connector The fully engaged, the signal transmission is normal. Moreover, it is ensured that the external force on the module will not be transmitted to the terminals of the electrical connector to cause mechanical damage or electrical performance failure.
该装置有以下特点:The device has the following features:
1.外场可更换模块插拔过程中不需要调整和借助外部工具;1. There is no need to adjust and use external tools during the plugging and unplugging of the field replaceable modules;
2.在电连接器完全啮合到位时,该装置提供视觉和听觉的的明确指示;2. When the electrical connector is fully engaged in place, the device provides a clear visual and auditory indication;
3.在锁紧外场可更换模块时,其电连接器啮合时可容许的位置度误差为1.5mm、锁紧时名义线性行程小于7mm;3. When locking the replaceable module in the field, the allowable position error when the electrical connector is engaged is 1.5mm, and the nominal linear stroke is less than 7mm when locking;
4.外场可更换模块锁止方向与振动方向垂直,可防止误操作开锁;4. The locking direction of the replaceable module in the field is perpendicular to the vibration direction, which can prevent unlocking by misoperation;
5.装置结构简单,插拔迅速、锁止可靠,外形符合人机工程学原理。5. The device has a simple structure, quick insertion and removal, reliable locking, and the shape conforms to the principles of ergonomics.
附图说明Description of drawings
图1是本发明在机载设备上安装位置示意图;Fig. 1 is a schematic diagram of the installation position of the present invention on airborne equipment;
图2是本发明的轴侧外形示意图;Fig. 2 is a schematic view of the shaft side profile of the present invention;
图3是本发明的轴侧爆炸图;Fig. 3 is an exploded view of the shaft side of the present invention;
图4是本发明在机箱中正常锁紧状态时的纵向剖视图;Fig. 4 is a longitudinal sectional view of the present invention in a normally locked state in the cabinet;
图5是本发明把模块从机箱中拔出时的纵向剖视图;Fig. 5 is a longitudinal sectional view of the present invention when the module is pulled out from the chassis;
图6是本发明中压板8的轴侧视图;Fig. 6 is an axial side view of the
图7是本发明中锁钩1的轴侧视图。Fig. 7 is a side view of the
具体实施方式Detailed ways
下面结合附图对本发明作详细说明。本发明在航空机载电子设备中的应用位置如图1所示。插拔锁紧装置10通常成对应用,对称安装在模块11的前面板上,而模块11则插入和固定在机箱12中。The present invention will be described in detail below in conjunction with the accompanying drawings. The application position of the present invention in aviation airborne electronic equipment is shown in FIG. 1 . The plug-in
从图3可以看出,插拔锁紧装置10共有9种零件,分别是锁钩1、扭簧2、销轴3、紧定螺钉4、提手5、压簧6、锁舌7、压板8、沉头螺钉9。It can be seen from Fig. 3 that the plug-in
锁钩1用螺钉13、弹簧垫圈14、垫圈15固定在模块11的前面板上,提手5为一个“U”形结构,提手5一端的两个侧壁的凸缘上对称设有两个凸耳17,锁钩1用销轴3连接在提手5的两个凸耳17上,扭簧2套在销轴3的中间,锁钩1上的锁头18的顶部有一个斜面19;提手5的底平面上开有与锁钩1的锁头18相对应位置处开有一个方孔20,在提手5底面内侧靠近锁钩1的一端设有两个螺纹孔21,提手5另一端的两侧壁上对称设有两个通孔22,锁舌7的中间有一个长方形孔23,长方形孔23的一个侧壁为斜面24,斜面24与锁头18顶部的斜面19相对应;提手5的底面内侧与锁舌7中间的长方形孔23相对应的位置上设有一个长方形凹槽25,长方形凹槽25与锁舌7的长方形孔23形成一个空腔26,压簧6位于空腔26中,压板8对应空腔26的位置上开有一个方形开口27,方形开口27的根部与锁舌7的接触面上设有限位块28,压板8开口的一端通过两个沉头螺钉9固定在提手5的螺纹孔21中,两个螺钉4通过压板8两个侧壁上的螺纹孔29把压板8的另一端固定在提手5侧壁上。
在图3的装配中,扭簧2和锁钩1通过销轴3固定在提手5上,而这四个零件一起通过螺钉13、弹簧垫圈14、垫圈15固定在模块11的前面板上(见图4、图5),插拔模块11时插拔锁紧装置10绕销轴3旋转,此时的提手5就成为一个杠杆,它的叉形上颚和下颚成为拔出和插入时力的支点。扭簧2的扭矩保证了提手5和模块11的前面板在未插入时成固定的角度,这使得在插入模块11时不需要再调整插拔锁紧装置10的位置。压板8通过两个沉头螺钉9和两个紧定螺钉4固定在提手5上,为压簧6和锁舌7的机构动作提供了空间,同时也是其行程的机械限位。In the assembly of Fig. 3, the
要把模块11插入机箱12时,只需用双手大拇指分别按压两个插拔锁紧装置10的提手5,锁舌7上的斜坡面24和锁钩1上相应位置的斜坡面19接触滑动,锁舌7先向外伸出然后缩回,同时发出“叭”的一声,锁舌7上的箭头标志30(见图2)完全外露,此时模块11已经啮合到位,对于散热要求苛刻的机箱,可以在模块11上再用楔形锁紧块16锁紧,见图4所示。此时扭簧2和压簧6都处于压缩状态,提手5的叉形下颚和机箱12的凹槽突出部分紧密贴合,模块11可靠固定。When inserting the
拔出模块11的过程正好相反,用双手大拇指分别把两个插拔锁紧装置10的锁舌7朝箭头指示方向按压,同时绕销轴3旋转扳开,直到模块11电连接器和机箱12的母板电连接器成功分离。The process of pulling out the
模块11储运过程中,插拔锁紧装置10应处于图4所示的锁止状态。During storage and transportation of the
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Cited By (13)
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CN102738653A (en) * | 2012-07-04 | 2012-10-17 | 华为技术有限公司 | Plugging mechanism and finished circuit board internally provided with same as well as plugging frame |
WO2013189191A1 (en) * | 2012-06-21 | 2013-12-27 | 华为技术有限公司 | Plug device of circuit board and server |
CN103616148A (en) * | 2013-10-18 | 2014-03-05 | 中国电子科技集团公司第十研究所 | Method of decomposing and obtaining LRM (Line Replaceable Module) vibration test condition in electronic module integration rack |
CN106922099A (en) * | 2017-03-03 | 2017-07-04 | 中航光电科技股份有限公司 | Rack and its electrical module component, driver-extractor |
CN108063341A (en) * | 2016-11-08 | 2018-05-22 | 波凯特有限及两合公司 | For the electronic module of I/O modular systems |
CN108235635A (en) * | 2016-12-14 | 2018-06-29 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of electronic module tightening plug mechanism |
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WO2013189191A1 (en) * | 2012-06-21 | 2013-12-27 | 华为技术有限公司 | Plug device of circuit board and server |
US9214749B2 (en) | 2012-06-21 | 2015-12-15 | Huawei Technologies Co., Ltd. | Pluggable apparatus of circuit board, and server |
CN102738653A (en) * | 2012-07-04 | 2012-10-17 | 华为技术有限公司 | Plugging mechanism and finished circuit board internally provided with same as well as plugging frame |
CN102738653B (en) * | 2012-07-04 | 2014-09-03 | 华为技术有限公司 | Plugging mechanism and finished circuit board internally provided with same as well as plugging frame |
CN103616148A (en) * | 2013-10-18 | 2014-03-05 | 中国电子科技集团公司第十研究所 | Method of decomposing and obtaining LRM (Line Replaceable Module) vibration test condition in electronic module integration rack |
CN103616148B (en) * | 2013-10-18 | 2015-11-18 | 中国电子科技集团公司第十研究所 | Decompose the method obtaining LRM vibration test condition in electronic module integrated installation frame |
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CN108063341A (en) * | 2016-11-08 | 2018-05-22 | 波凯特有限及两合公司 | For the electronic module of I/O modular systems |
CN108235635A (en) * | 2016-12-14 | 2018-06-29 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of electronic module tightening plug mechanism |
CN106922099A (en) * | 2017-03-03 | 2017-07-04 | 中航光电科技股份有限公司 | Rack and its electrical module component, driver-extractor |
CN108811420A (en) * | 2017-04-28 | 2018-11-13 | 王付华 | A module lifting device |
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CN114390842A (en) * | 2021-11-29 | 2022-04-22 | 中航光电科技股份有限公司 | Locking device of airborne electronic equipment |
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