CN211102551U - Operation tool for precisely installing hole inner bushing - Google Patents
Operation tool for precisely installing hole inner bushing Download PDFInfo
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- CN211102551U CN211102551U CN201922063980.0U CN201922063980U CN211102551U CN 211102551 U CN211102551 U CN 211102551U CN 201922063980 U CN201922063980 U CN 201922063980U CN 211102551 U CN211102551 U CN 211102551U
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Abstract
Description
技术领域technical field
本实用新型涉及零件组装用的作业工具,具体是一种孔内衬套精密安装用的作业工装,其特别适宜航空发动机机匣上的轴件安装孔内的衬套安装。The utility model relates to a working tool for assembling parts, in particular to a working tool for precise installation of a bushing in a hole, which is particularly suitable for bushing installation in a shaft fitting hole on an aero-engine casing.
背景技术Background technique
在轴件的安装结构中,为了减少轴件和/或座体之间运动摩擦造成的磨损,轴件通常以硬度较低、耐磨性较好的衬套装配在座体上的安装孔内(为了方便描述,以下将此类孔统称为“衬套安装孔”),衬套在座体上的衬套安装孔内以过盈配合,衬套与轴件以间隙配合。当轴件和座体之间在长期的运动磨擦中发生一定程度的磨损时,通过对衬套的更换,就能节约因更换轴件和/或座体的成本。可见,衬套是运动部件中实现密封、磨损保护等作用的重要配套件。In the installation structure of the shaft, in order to reduce the wear caused by the motion friction between the shaft and/or the seat, the shaft is usually assembled in the mounting hole on the seat with a bushing with lower hardness and better wear resistance ( For the convenience of description, such holes are collectively referred to as "bushing mounting holes" hereinafter), the bushing is fitted in the bushing mounting hole on the seat body with interference fit, and the bushing and the shaft piece are fitted with clearance. When a certain degree of wear occurs between the shaft member and the seat body during long-term motion friction, the replacement of the bushing can save the cost of replacing the shaft member and/or the seat body. It can be seen that the bushing is an important accessory for sealing and wear protection in moving parts.
航空发动机内存在诸多的、复杂的轮系结构,其属于典型的运动部件之一。航空发动机中的轮系结构的轴件如上所述的那样,通常是以衬套安装在机匣上的对应衬套安装孔内的,例如,航空发动机内的惰轮的轴件在机匣上的惰轮轴安装孔内以衬套进行安装。There are many complex gear train structures in aero-engines, which are one of the typical moving parts. As mentioned above, the shaft member of the wheel train structure in the aero-engine is usually installed with a bushing in the corresponding bushing mounting hole on the casing. For example, the shaft member of the idler in the aero-engine is on the casing. Install it with a bushing in the idler shaft mounting hole of .
航空发动机在长期的运行过程中,其机匣上的对应轮系结构的衬套安装孔内所装配的衬套会因磨损而失效,这就需要将机匣上的对应衬套安装孔内的原衬套进行拆除,并将新衬套在该衬套安装孔内进行安装,甚至还会涉及到对机匣上的对应衬套安装孔进行扩孔的操作,扩孔后必然会涉及到对应衬套的安装。During the long-term operation of the aero-engine, the bushings assembled in the bushing mounting holes corresponding to the gear train structure on the casing will fail due to wear, which requires the corresponding bushing mounting holes on the casing. The original bushing is removed, and the new bushing is installed in the bushing mounting hole. It even involves the operation of reaming the corresponding bushing mounting hole on the receiver. Installation of bushings.
基于航空发动机的高精密性,其机匣上的对应轮系结构的衬套安装孔内的衬套装配等操作均属于高精密操作,衬套在机匣上的对应衬套安装孔内的安装需要同时满足如下两个技术条件:Based on the high precision of aero-engines, operations such as assembling the bushings in the bushing mounting holes corresponding to the gear train structure on the casing are all high-precision operations, and the bushings are installed in the corresponding bushing mounting holes on the casing. The following two technical conditions need to be met at the same time:
1. 装入机匣上的对应衬套安装孔内的衬套需要垂直于该衬套安装孔在机匣上所成型的表面,即衬套需要在对应衬套安装孔内保持精准的轴向状态;1. The bushing installed in the corresponding bushing mounting hole on the casing needs to be perpendicular to the surface formed by the bushing mounting hole on the casing, that is, the bushing needs to maintain a precise axial direction in the corresponding bushing mounting hole state;
2. 装入机匣上的对应衬套安装孔内的衬套端面不得高于该衬套安装孔在机匣上所成型的表面,即衬套是以齐平或内沉的方式(通常是齐平方式)装入对应衬套安装孔内的。2. The end face of the bushing installed in the corresponding bushing mounting hole on the casing shall not be higher than the surface formed by the bushing mounting hole on the casing, that is, the bushing shall be flush or inward (usually flush way) into the corresponding bushing mounting hole.
上述两个安装技术条件直接影响着对应轮系结构的轴件在机匣上的安装及后续运动的精密性、稳定性和可靠性。The above two installation technical conditions directly affect the precision, stability and reliability of the installation of the shaft corresponding to the gear train structure on the casing and the subsequent movement.
目前,衬套在航空发动机机匣上的对应衬套安装孔内的安装因缺乏行之有效地专用作业工装,主要是以榔头敲击的传统作业方式进行安装的,具体作业过程是:先将衬套对接在机匣上的对应衬套安装孔处;再以一个台阶结构的冲杆顶住衬套的外端面;然后采用榔头敲击冲杆的尾端,将衬套推入机匣上的对应衬套安装孔内。At present, the installation of the bushing in the corresponding bushing mounting hole on the aero-engine casing is mainly performed by the traditional operation method of hammer knocking due to the lack of effective special work tooling. The specific operation process is: first The bushing is docked at the corresponding bushing mounting hole on the casing; then a stepped punch rod is used to press against the outer end face of the bushing; then the tail end of the punch rod is hit with a hammer to push the bushing onto the casing in the corresponding bushing mounting holes.
由上述安装作业过程可以清楚看出,其衬套在对应衬套安装孔内的安装推力来自于榔头对冲杆的敲击,敲击力的大小因操作者的主观行为而决定,敲击力过小无法使衬套有效地装入衬套安装孔内,会在衬套安装孔的外缘处多少有所外伸,敲击力过大容易使冲杆对衬套安装孔所成型的机匣表面造成损伤,因而,整个安装过程操作难度较大,不易掌控。更甚的是,在衬套的安装过程中,敲击榔头的方向不一定是正轴向的,从而使得衬套所承受的推力就不一定全是轴向的,还存在径向的推力,这会使冲杆对衬套的内壁面造成损伤,而且衬套在装入过程中会产生倾斜,不但无法满足于安装技术条件的要求,还会对机匣上的衬套安装孔孔壁面造成损伤,这些都会对衬套的安装精密性造成不利影响。It can be clearly seen from the above installation operation process that the installation thrust of the bushing in the corresponding bushing installation hole comes from the knocking of the hammer on the ram, and the knocking force is determined by the operator's subjective behavior. If the bushing is too small, it will not be able to fit the bushing into the bushing mounting hole effectively, and it will protrude somewhat at the outer edge of the bushing mounting hole. If the knocking force is too large, it is easy to cause the punch to the casing formed by the bushing mounting hole. The surface is damaged, so the entire installation process is difficult to operate and difficult to control. What's more, during the installation of the bushing, the direction of the hammer is not necessarily positive axial, so that the thrust on the bushing is not necessarily all axial, and there is also a radial thrust, which The punch will damage the inner wall of the bushing, and the bushing will be inclined during the installation process, which not only fails to meet the requirements of installation technical conditions, but also damages the wall of the bushing mounting hole on the casing. , which will adversely affect the installation precision of the bushing.
实用新型内容Utility model content
本实用新型的技术目的在于:针对上述衬套精密安装的特殊性和现有作业工装的技术不足,提供一种能够使衬套轻松、高效、高质量的精密安装于零件体上的对应衬套安装孔内的作业工装。The technical purpose of the present utility model is to provide a corresponding bushing that can make the bushing easy, efficient and high-quality precisely mounted on the part body in view of the particularity of the above-mentioned bushing precision installation and the technical deficiencies of the existing work tooling. Work tooling in the mounting hole.
本实用新型的技术目的是通过下述技术方案实现的:一种孔内衬套精密安装用作业工装,所述作业工装包括操作杆和定位基座,所述定位基座具有能够在零件体上进行定位的定位面、以及在定位状态下能够与所述零件体上的衬套安装孔轴向对应的导向孔,所述操作杆以轴向可位移结构伸入所述定位基座的导向孔内,且所述操作杆在所述导向孔内连接有能够轴向可位移而推送衬套的压头。The technical purpose of the present utility model is achieved through the following technical solutions: a working tool for precision installation of a bushing in a hole, the working tool includes an operating rod and a positioning base, and the positioning base has a function that can be mounted on the part body A positioning surface for positioning, and a guide hole that can axially correspond to the bushing mounting hole on the part body in a positioning state, and the operating rod extends into the guide hole of the positioning base with an axially displaceable structure Inside, and the operating rod is connected with a pressing head capable of being axially displaceable to push the bushing in the guide hole.
作为优选方案之一,所述定位基座具有处在所述导向孔轴向外侧的螺套部,所述操作杆以螺纹配合结构通过所述螺套部而伸入所述导向孔内。进一步的,所述定位基座的导向孔内设有处在所述操作杆和压头之间的推力转换件。再进一步的,所述推力转换件为减摩垫圈或推力球轴承。所述操作杆的轴向上具有手柄部和杆体部,所述杆体部上具有连接所述定位基座的螺纹结构,所述手柄部处在所述定位基座的外部。更进一步的,所述操作杆的轴向上还具有处在杆体部前端的连接颈和限位部,所述连接颈用作配合所述限位部而套接压头,所述限位部以螺纹结构与压头配合连接;所述操作杆连接所述压头的螺纹方向与所述操作杆连接所述螺套部的螺纹方向相反;所述压头的轴向上具有靠近推力转换件一侧的螺纹孔段和靠近推送表面一侧的限位沉孔段,所述限位沉孔段的内径大于所述螺纹孔段的内径。As one of the preferred solutions, the positioning base has a threaded sleeve portion located at the axial outer side of the guide hole, and the operating rod extends into the guide hole through the threaded sleeve portion in a threaded fitting structure. Further, the guide hole of the positioning base is provided with a thrust conversion member between the operating rod and the pressing head. Still further, the thrust conversion member is an anti-friction washer or a thrust ball bearing. The operating rod has a handle part and a rod body part in the axial direction, the rod body part has a threaded structure connected with the positioning base, and the handle part is located outside the positioning base. Further, the operating rod also has a connecting neck and a limit portion located at the front end of the rod body in the axial direction, the connecting neck is used to fit the limit portion to sleeve the pressure head, and the limit portion It is connected with the pressure head in a threaded structure; the thread direction of the operation rod connecting the pressure head is opposite to the thread direction of the operation rod connecting the screw sleeve part; the axial direction of the pressure head is close to the thrust conversion member The threaded hole section on one side and the limit counterbore section on the side close to the pushing surface, the inner diameter of the limit counterbore section is larger than the inner diameter of the threaded hole section.
作为优选方案之一,所述定位基座主要由导向筒、螺套部和底座板组成,所述导向筒的轴向上具有导向孔,所述螺套部以径向内折结构处在所述导向筒的一端,所述底座板以径向外折结构处在所述导向筒的另一端。进一步的,所述底座板上具有至少一个能够与零件体上的定位孔相对应的腰型孔。所述导向筒与所述螺套部为分体组合结构。所述导向筒与所述底座板为一体成型结构。As one of the preferred solutions, the positioning base is mainly composed of a guide cylinder, a screw sleeve part and a base plate, the guide cylinder has a guide hole in the axial direction, and the screw sleeve part is located in a radially inwardly folded structure. One end of the guide cylinder, the base plate is located at the other end of the guide cylinder in a radially outward folded structure. Further, the base plate has at least one waist-shaped hole corresponding to the positioning hole on the part body. The guide cylinder and the screw sleeve part are of a separate combined structure. The guide cylinder and the base plate are integrally formed.
作为优选方案之一,所述零件体为航空发动机的机匣。进一步的,所述零件体上的衬套安装孔为惰轮轴安装孔。As one of the preferred solutions, the part body is a casing of an aero-engine. Further, the bushing mounting hole on the part body is an idler shaft mounting hole.
本实用新型的有益技术效果是:The beneficial technical effects of the present utility model are:
1. 本实用新型以定位基座对零件体上对接的衬套进行定位、扶持,以能够在定位基座的导向孔内进行轴向位移的操作杆和压头对应衬套实现正轴向的推送,防止衬套在进入衬套安装孔时产生倾斜,亦不会对零件体和衬套造成损伤,操作容易,能够使衬套轻松、高效、高质量的精密安装于零件体上的对应衬套安装孔内;1. The utility model uses the positioning base to position and support the butt-jointed bushings on the part body, so that the corresponding bushings of the operating rod and the pressure head that can be axially displaced in the guide holes of the positioning base can achieve positive axial Push, prevent the bushing from tilting when entering the bushing installation hole, and will not cause damage to the part body and the bushing, easy to operate, and can make the bushing easy, efficient, and high-quality precision installation on the corresponding bushing on the part body inside the mounting hole;
2. 本实用新型的操作杆与定位基座之间的螺纹配合结构,使得操作杆在定位基座的导向孔内的轴向位移过程稳定、可调,推送衬套时,衬套所承受的推力相对均衡,有利于对零件体和衬套实现保护;2. The screw fitting structure between the operating rod and the positioning base of the present invention makes the axial displacement process of the operating rod in the guide hole of the positioning base stable and adjustable. The thrust is relatively balanced, which is conducive to the protection of the part body and the bushing;
3. 本实用新型的操作杆与压头之间的推力转换件,能够将操作杆周向旋转的轴向位移推力可靠地转换为压头直线运动的轴向位移推力,从而在衬套推送时,减少压头与衬套之间的相对周向摩擦运动,以保护衬套;3. The thrust conversion element between the operating rod and the indenter of the present invention can reliably convert the axial displacement thrust of the circumferential rotation of the operating rod into the axial displacement thrust of the linear motion of the indenter, so that when the bushing is pushed , reduce the relative circumferential friction movement between the pressure head and the bushing to protect the bushing;
4. 本实用新型的操作杆与压头之间的连接结构,既能够有效确保二者相对配合关系的稳定性,又具有二者组装、拆卸操作轻松、容易的特点,还能够使二者实现高精密的装配,不会影响衬套的推送安装,亦不会对衬套造成损伤;4. The connection structure between the operating rod and the indenter of the present invention can not only effectively ensure the stability of the relative matching relationship between the two, but also has the characteristics of easy and easy assembly and disassembly of the two, and can also enable the two to achieve High-precision assembly will not affect the push installation of the bushing, nor will it cause damage to the bushing;
5. 本实用新型的定位基座成型结构,有利于在零件体上进行稳定、可靠地安装定位,特别是底座板上的腰型孔结构有利于灵活调节定位基座在零件体上的安装位置,从而有效确保定位基座上的导向孔与零件体上的衬套安装孔能够可靠地轴向对中;此外,螺套部与导向筒之间的分体组合结构,有利于降低定位基座加工制作时的工艺难度。5. The forming structure of the positioning base of the present invention is conducive to stable and reliable installation and positioning on the part body, especially the waist-shaped hole structure on the base plate is conducive to flexibly adjust the installation position of the positioning base on the part body , so as to effectively ensure that the guide hole on the positioning base and the bushing mounting hole on the part body can be axially centered reliably; in addition, the split combination structure between the threaded sleeve part and the guide cylinder is conducive to lowering the positioning base The difficulty of the craftsmanship during processing.
附图说明Description of drawings
图1为本实用新型的一种结构示意图。Fig. 1 is a kind of structure schematic diagram of the utility model.
图2为图1的A-A视图。FIG. 2 is an A-A view of FIG. 1 .
图3为本实用新型的外形立体图。FIG. 3 is an external perspective view of the utility model.
图4为本实用新型的使用状态参考图。FIG. 4 is a reference diagram of the use state of the present invention.
图中代号含义:1—操作杆;11—手柄部;12—杆体部;13—传力部;14—连接颈;15—限位部;2—定位基座;21—螺套部;22—导向筒;23—底座板;24—导向孔;25—腰型孔;26—销钉;3—推力转换件;4—压头;41—螺纹孔段;42—限位孔段;5—零件体;51—衬套安装孔;52—定位孔;6—定位螺钉;7—衬套。The meaning of the code in the figure: 1—operating lever; 11—handle part; 12—rod body part; 13—force transmission part; 14—connecting neck; 15—limiting part; 2—positioning base; 21—screw sleeve part; 22 - Guide cylinder; 23 - Base plate; 24 - Guide hole; 25 - Waist hole; 26 - Pin; 3 - Thrust conversion part; 4 - Press head; 41 - Threaded hole section; Part body; 51 - bushing mounting hole; 52 - positioning hole; 6 - positioning screw; 7 - bushing.
具体实施方式Detailed ways
本实用新型涉及零件组装用的作业工具,具体是一种孔内衬套精密安装用的作业工装,下面以航空发动机机匣上的惰轮轴安装孔内的衬套安装作为对象(即下述的零件体为航空发动机机匣,衬套安装孔为航空发动机机匣上的惰轮轴安装孔),通过多个实施例对本实用新型的主体技术内容进行详细说明,其中,实施例1结合说明书附图-即图1、图2、图3和图4对本实用新型的主体技术内容进行清楚、直观的详细说明,其它实施例虽未再单独绘制对应附图,但其主体技术方案仍可参照实施例1的附图。The utility model relates to a working tool for parts assembly, in particular to a working tool for precise installation of a bushing in a hole. The following takes the bushing installation in the idler shaft mounting hole on the aero-engine casing as the object (that is, the following The part body is an aero-engine casing, and the bushing mounting hole is an idler shaft mounting hole on the aero-engine casing). The main technical content of the present utility model is described in detail through a number of embodiments, among which,
在此需要特别说明的是,本实用新型的附图是示意性的,其为了清楚本实用新型的技术目的已经简化了不必要的细节,以避免模糊了本实用新型贡献于现有技术的技术方案。It should be noted here that the accompanying drawings of the present invention are schematic, and unnecessary details have been simplified for the purpose of clarifying the technical purpose of the present invention, so as to avoid obscuring the technology that the present invention contributes to the prior art Program.
实施例1Example 1
参见图1、图2、图3和图4所示,本实用新型包括操作杆1和定位基座2。Referring to FIG. 1 , FIG. 2 , FIG. 3 and FIG. 4 , the present invention includes an operating
其中,定位基座2主要由导向筒22、螺套部21和底座板23组成。导向筒22为圆筒型结构,其内部的轴向上具有通孔结构的导向孔24,该导向孔24为轴向等径结构,导向孔24的内径至少应等于零件体5上的衬套安装孔51的内径(孔口处),通常是略大于零件体5上的衬套安装孔51的内径。定位基座2在零件体5上定位好时(即处于定位状态下),导向筒22的导向孔24能够与零件体5上的衬套安装孔51轴向对应。The
螺套部21与导向筒22为分体组合结构。具体的,螺套部21的外轮廓呈上大、下小的同轴台阶结构,螺套部21的上部外径基本匹配于导向筒22的外径,螺套部21的下部外径匹配于导向筒22的导向孔24内径;螺套部21通过下部轴向插入导向筒22的导向孔24上端,从而在导向筒22的上端形成径向内折结构。为了保证螺套部21与导向筒22之间连接的可靠性和稳定性,在导向筒22与螺套部21之间套叠区域的周向上开设有多组一一对应的销孔,每一组销孔内插装有一个销钉26,由多个销钉26将导向筒22和螺套部21在周向上和轴向上均锁定;通常,每个销钉26与导向筒22之间以过盈装配,与螺套部21为间隙装配。此外,螺套部21的内部轴向上具有通孔结构的螺纹孔,该螺纹孔用作穿装操作杆1,螺套部21的螺纹孔与导向筒22的导向孔4基本呈同轴心布置。The
底座板23与导向筒22为一体成型结构,底座板23在导向筒22的下端以径向外折结构成型,底座板23和导向筒22构成倒T型结构,底座板23的存在不应影响导向筒22上的导向孔24。径向延伸出导向筒22的底座板23上具有两个腰型孔25,这两个腰型孔25的朝向一致,要求在与零件体5接触配合时,底座板23上的这两个腰型孔25应当能够与零件体5上的衬套安装孔51两侧的定位孔52相对应,即底座板23上的这两个腰型孔25应当能够与零件体5上的定位孔52相对应。此外,上述结构的定位基座2在与零件体5接触配合时,该定位基座2是以底座板23的底面作为结合面的,因而底座板23的底面作为定位基座2能够在零件体5上进行定位的定位面,这也就要求底座板23的底面轮廓型线吻合于零件体5上的衬套安装孔51所在的成型表面。The
操作杆1的轴向上依次具有手柄部11、杆体部12、传力部13、连接颈14和限位部15,手柄部11的直径最大,整个操作杆1呈T型结构。The operating
杆体部12上具有连接定位基座2上的螺套部21的螺纹结构,即杆头部12上的螺纹结构与螺套部21上的螺纹结构相匹配,杆体部12以螺纹结构通过螺套部21轴向伸入定位基座2的导向孔24内。The
手柄部11处在杆体部12的上端,杆体部12轴向伸入定位基座2的导向孔24内时,手柄部11处在定位基座2的外部。在手柄部11的外周设置有手捏增摩结构,例如网状滚花结构。The
传力部13处在杆体部12上的螺纹结构下方,其以径向平面结构成型,即传力部13处的杆体为同轴台阶结构。The
连接颈14处在传力部13的下方,连接颈14为轴向的光杆结构。传力部13的端面内径基本等同于连接颈14的外径,传力部13的端面外径大于连接颈14的外径。The connecting
限位部15处在连接颈14的下方,限位部15的外径略大于连接颈14的外径。限位部15上设置有螺纹结构,该螺纹结构的螺旋方向与杆体部12上螺纹结构的螺旋方向相反,设定杆体部12上的螺纹结构为右旋螺纹,则限位部15上的螺纹结构为左旋螺纹。The limiting
上述结构的操作杆1通过周向可旋进的螺纹结构,以轴向可位移结构伸入上述结构的定位基座2的导向孔24内,操作杆1基本与定位基座2保持同轴心配合,操作杆1在导向孔24内连接有推力转换件3和压头4。The operating
推力转换件3为青铜结构的环形减摩垫圈,其套装在操作杆1的连接颈14处,并与定位基座2的导向孔24内部形成间隙配合。推力转换件3的上侧表面与操作杆1上的传力部13形成面接触配合。推力转换件3的下侧表面与压头4的顶面形成面接触配合。该推力转换件3的作用在于,将操作杆1的周向旋转运动转变为压头4的直线位移运动。The
压头4为匹配定位基座2上的导向孔24的柱体结构,压头4与导向孔24保持间隙配合。压头4的外径至少应该等于所要安装的衬套7的外径,通常情况下,压头4的外径略大于所要安装的衬套7的外径。压头4的底端面作为推送衬套7的表面,其需要与衬套7之间形成平整接触,因而,压头4的底端面为平面结构。压头4的内部具有轴向上的通孔结构,该通孔结构用作连接操作杆1,且该通孔结构的内径必须小于所要安装的衬套7的内径。具体的,压头4的内部轴向上具有靠近推力转换件3一侧的螺纹孔段41和靠近推送表面(即底端面)一侧的限位沉孔段42,压头4上的螺纹孔段41具有吻合于上述操作杆1上的限位部15的螺纹结构,螺纹孔段41的深度一般小于上述操作杆1上的连接颈14的长度;限位沉孔段42的内径大于螺纹孔段41的内径,亦就大于上述操作杆1上的限位部15的外径,限位沉孔段42的深度一般大于上述操作杆1的限位部15的长度。前述结构的压头4通过内部轴向上的螺纹孔段41和/或限位沉孔段42连接在上述操作杆1的限位部15和/或连接颈14上。The
参见图4所示,用本实用新型在零件体5上的衬套安装孔51内安装衬套7的操作过程大致是:Referring to Fig. 4, the operation process of installing the
-将衬套7轴向对接在零件体5上的衬套安装孔51的孔口处;- Axially butt the
-将定位基座2的导向孔24与零件体5上的衬套7及衬套安装孔51轴向对正,使导向孔24套住衬套7,确保定位基座2上的定位面与零件体5上的衬套安装孔51的成型表面形成面接触;在此基础上,以零件体5上的定位孔52为目标而调整定位基座2,使底座板23上的腰型孔25与零件体5上的定位孔52保持对应,在对应的腰型孔25与定位孔52中装入定位螺钉6,以此将定位基座2定位在零件体5上;- Align the
-以能够使操作杆1向下位移的方向旋转操作杆1(例如顺时针),操作杆1的周向旋转推力通过推力转换件3作用在压头4上,压头4在导向孔24内直线位移下行、并与衬套7的上端面接触,继续如此操作,压头4轴向推送衬套7,使衬套7被全部推送压入零件体5上的衬套安装孔51内,压头4作用在零件体5表面、无法下行时则表面安装到位,此时的衬套7端面与衬套安装孔51端面形成平整配合。- Rotate the operating
在上述安装过程中,操作杆1的前端与压头4之间形成浮动连接;至于压头4在导向孔24内的直线位移上行,则通过反方向旋转操作杆1即可实现对压头4的提升,基于操作杆1上的两处螺纹结构的螺旋方向相反,操作杆1的反向旋转不会使限位部15旋入压头4的螺纹孔段41中,从而可以可靠地带动压头4轴向的直线向上移动。During the above installation process, a floating connection is formed between the front end of the operating
实施例2Example 2
本实施例的其它内容与实施例1相同,不同之处在于:推力转换件为推力球轴承。The other contents of this embodiment are the same as those of
实施例3Example 3
本实施例的其它内容与实施例1相同,不同之处在于:定位基座的螺套部与导向筒为一体成型结构。The other contents of this embodiment are the same as those of
实施例4Example 4
本实施例的其它内容与实施例1相同,不同之处在于:定位基座的底座板与导向筒为分体组合结构。The other contents of this embodiment are the same as those of
以上各实施例仅用以说明本实用新型,而非对其限制。尽管参照上述各实施例对本实用新型进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对上述各实施例的具体技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本实用新型的精神和范围。The above embodiments are only used to illustrate the present invention, but not to limit it. Although the present utility model has been described in detail with reference to the above-mentioned embodiments, those of ordinary skill in the art should understand that: it is still possible to modify the specific technical solutions of the above-mentioned embodiments, or to perform equivalent replacements to some of the technical features; and These modifications or substitutions do not make the essence of the corresponding technical solutions depart from the spirit and scope of the present invention.
Claims (10)
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113369839A (en) * | 2021-05-27 | 2021-09-10 | 成都飞机工业(集团)有限责任公司 | High-precision bushing assembling and centering device and bushing centering and assembling method |
| CN113928588A (en) * | 2021-11-16 | 2022-01-14 | 中国人民解放军第五七一九工厂 | Air pressure reducer graphite lining crack repairing method |
| CN114888749A (en) * | 2022-05-23 | 2022-08-12 | 成都飞机工业(集团)有限责任公司 | Mounting tool and mounting method for eccentric bushing |
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| CN116117739A (en) * | 2022-12-14 | 2023-05-16 | 中国航发贵州黎阳航空动力有限公司 | Front support casing bushing assembly fixture |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113369839A (en) * | 2021-05-27 | 2021-09-10 | 成都飞机工业(集团)有限责任公司 | High-precision bushing assembling and centering device and bushing centering and assembling method |
| CN113928588A (en) * | 2021-11-16 | 2022-01-14 | 中国人民解放军第五七一九工厂 | Air pressure reducer graphite lining crack repairing method |
| CN113928588B (en) * | 2021-11-16 | 2024-08-06 | 中国人民解放军第五七一九工厂 | Repairing method for cracks of graphite bushing of air pressure reducer |
| CN114918645A (en) * | 2022-02-21 | 2022-08-19 | 邵亮 | Large-scale spiale sleeve location circle bush installation device |
| CN114918645B (en) * | 2022-02-21 | 2024-09-06 | 南京东升冶金机械有限公司 | A large shaft sleeve positioning circular bushing installation device |
| CN114918872A (en) * | 2022-03-15 | 2022-08-19 | 邵亮 | Large-scale spiale sleeve location circle bush dismounting device |
| CN114918872B (en) * | 2022-03-15 | 2024-05-28 | 南京尚科得科技发展有限公司 | A large shaft sleeve positioning circular bushing disassembly device |
| CN114888749A (en) * | 2022-05-23 | 2022-08-12 | 成都飞机工业(集团)有限责任公司 | Mounting tool and mounting method for eccentric bushing |
| CN116117739A (en) * | 2022-12-14 | 2023-05-16 | 中国航发贵州黎阳航空动力有限公司 | Front support casing bushing assembly fixture |
| CN119665766A (en) * | 2024-11-14 | 2025-03-21 | 中国航发南方工业有限公司 | A method for installing and detecting deep hole bushings of aircraft engines |
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