CN111438472A - Damping hold-down device for bottom welding of rocket tanks - Google Patents
Damping hold-down device for bottom welding of rocket tanks Download PDFInfo
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- CN111438472A CN111438472A CN202010261353.2A CN202010261353A CN111438472A CN 111438472 A CN111438472 A CN 111438472A CN 202010261353 A CN202010261353 A CN 202010261353A CN 111438472 A CN111438472 A CN 111438472A
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- 238000013016 damping Methods 0.000 title claims abstract description 73
- 238000003466 welding Methods 0.000 title claims abstract description 46
- 238000003825 pressing Methods 0.000 claims abstract description 100
- 239000011324 bead Substances 0.000 claims abstract description 15
- 229910000831 Steel Inorganic materials 0.000 claims 1
- 239000010959 steel Substances 0.000 claims 1
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K37/00—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass
- B23K37/04—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass for holding or positioning work
- B23K37/0426—Fixtures for other work
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K37/00—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass
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- Butt Welding And Welding Of Specific Article (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
本发明提供了一种适用于火箭贮箱箱底焊接的阻尼压紧装置,包括:工件2、机械压条3、阻尼构件以及弹性垫板5;所示机械压条3的两端与工作台紧固连接;所示阻尼构件均匀排布安装于机械压条3上;所述弹性垫板5中心线与阻尼构件轴线对齐均匀排布安装于机械压条3上;所述弹性垫板5的另一端处于自由状态;所述阻尼构件向下压紧弹性垫板5的自由端,使弹性垫板5的自由端压紧在工件2上。本发明可实现对任何大曲率半径的球底、锥底工件的压紧,不受限于火箭贮箱箱底的形式,其中的阻尼螺钉可实时自身调节来补偿工件变形量,以达到焊缝单元高质量的要求。
The present invention provides a damping and pressing device suitable for welding the bottom of a rocket tank, comprising: a workpiece 2, a mechanical bead 3, a damping member and an elastic backing plate 5; both ends of the shown mechanical bead 3 are tightly connected to the workbench The damping members shown are evenly arranged and installed on the mechanical bead 3; the centerline of the elastic pad 5 is aligned with the axis of the damping member and evenly arranged and installed on the mechanical bead 3; the other end of the elastic pad 5 is in a free state ; The damping member presses the free end of the elastic backing plate 5 downward, so that the free end of the elastic backing plate 5 is pressed on the workpiece 2 . The invention can realize the pressing of any spherical bottom and cone bottom workpieces with a large radius of curvature, and is not limited to the form of the bottom of the rocket tank. The damping screw can be adjusted in real time to compensate for the deformation of the workpiece, so as to achieve the welding seam unit. high quality requirements.
Description
技术领域technical field
本发明涉及火箭贮箱箱底焊接技术领域,具体地,涉及一种适用于火箭贮箱箱底焊接的阻尼压紧装置。The invention relates to the technical field of rocket tank bottom welding, in particular to a damping pressing device suitable for rocket tank bottom welding.
背景技术Background technique
目前,我国火箭贮箱箱底焊接系统多采用搅拌摩擦焊的焊接工艺方法,焊接火箭贮箱箱底球底或锥底工件纵缝时需要压紧工件,由于搅拌摩擦焊的顶锻力和前进抗力很大,焊接工件时会使工件变形,进而使压紧装置与工件产生间隙引起松动,通常情况下,出现这种情况,会通过人工反复重新调整压紧装置来消除松动,但是这种方式会大大增加工人劳动强度和降低生产效率,由于是人为实时调整,会带来安全隐患,不仅效率低而且可能危及工人的人身安全,更重要的是影响焊缝单元的焊接质量。我国的火箭贮箱箱底焊接系统中还没用过带阻尼的压紧装置,因此发明一种用于火箭贮箱箱底焊接系统的阻尼压紧装置很有必要。At present, the welding system of rocket tank bottom in my country mostly adopts the welding process method of friction stir welding. When welding the longitudinal seam of the spherical bottom or cone bottom workpiece of the rocket tank bottom, the workpiece needs to be pressed. When the workpiece is welded, the workpiece will be deformed, and then the gap between the pressing device and the workpiece will cause loosening. Usually, when this happens, the loosening will be eliminated by manually re-adjusting the pressing device repeatedly, but this method will greatly Increasing the labor intensity of workers and reducing production efficiency, due to artificial real-time adjustment, will bring potential safety hazards, not only low efficiency but also may endanger the personal safety of workers, and more importantly, affect the welding quality of the welding seam unit. my country's rocket tank bottom welding system has not used a compression device with damping, so it is necessary to invent a damping compression device for the rocket tank bottom welding system.
专利文献CN109848889A公开了一种基于阻尼减震的工件压紧装置,包括:底部安装板体、上部支撑板体、多个阻尼减震器、第一矩形支撑杆、第二矩形支撑杆、第一支撑板体、第二支撑板体、定位板体、第一限位定位座、第二限位定位座、耳部支撑座、驱动调节器、摇杆、阶梯型杆体、三角形旋转板、短连杆、长连杆、第一折形压紧体、第一槽型件、第二折形压紧体相连、第二槽型件;在第一折形压紧体和第二折形压紧体的压紧端面上均通过紧固件安装有弹性压紧片。Patent document CN109848889A discloses a workpiece pressing device based on damping and shock absorption, comprising: a bottom mounting plate body, an upper supporting plate body, a plurality of damping shock absorbers, a first rectangular support rod, a second rectangular support rod, a first Support plate body, second support plate body, positioning plate body, first limit positioning seat, second limit positioning seat, ear support seat, drive adjuster, rocker, stepped rod body, triangular rotating plate, short connection The rod, the long connecting rod, the first folding-shaped pressing body, the first groove-shaped piece, the second folding-shaped pressing body are connected, and the second groove-shaped member; the first folding-shaped pressing body and the second folding-shaped pressing body are connected Elastic pressing pieces are installed on the pressing end faces of the body through fasteners.
发明内容SUMMARY OF THE INVENTION
针对现有技术中的缺陷,本发明的目的是提供一种适用于火箭贮箱箱底焊接的阻尼压紧装置。In view of the defects in the prior art, the purpose of the present invention is to provide a damping pressing device suitable for welding the bottom of a rocket tank.
根据本发明提供的一种适用于火箭贮箱箱底焊接的阻尼压紧装置,包括:工件2、机械压条3、阻尼构件以及弹性垫板5;所示机械压条3的两端与工作台紧固连接;所示阻尼构件均匀排布安装于机械压条3上;所述弹性垫板5中心线与阻尼构件轴线对齐均匀排布安装于机械压条3上;所述弹性垫板5的另一端处于自由状态;所述阻尼构件向下压紧弹性垫板5的自由端,使弹性垫板5的自由端压紧在工件2上。A damping pressing device suitable for welding the bottom of a rocket tank according to the present invention includes: a
优选地,所述阻尼构件采用阻尼螺钉4。Preferably, the damping member adopts damping
优选地,所述阻尼螺钉4包括:第三螺钉41、压紧头42、蝶形弹簧43以及钢丝弹簧44。Preferably, the
所述蝶形弹簧43放置于第三螺钉41内孔,压紧状态时,蝶形弹簧43一端紧贴在第三螺钉与蝶形弹簧接触处406,另一端紧贴在蝶形弹簧与压紧头接触处403。The butterfly spring 43 is placed in the inner hole of the
优选地,所述压紧头42放置于第三螺钉41内孔并穿过蝶形弹簧43内孔。Preferably, the
优选地,所述钢丝弹簧44卡在第三螺钉圆弧卡槽401内,自由状态时,钢丝弹簧44把压紧头42挡在钢丝弹簧与压紧头接触处404,所述第三螺钉41安装于机械压条3上,正常压紧时,第三螺钉41通过第三螺钉压紧端405压紧工件2,焊接松动时,压紧头42通过压紧头压紧端402压紧工件2。Preferably, the wire spring 44 is clamped in the
优选地,所示机械压条3通过第一紧固螺钉1两端固定在工作台上。Preferably, the shown
优选地,所述弹性垫板5的一端通过第二紧固螺钉6与机械压条3紧固连接。Preferably, one end of the
与现有技术相比,本发明具有如下的有益效果:Compared with the prior art, the present invention has the following beneficial effects:
1、本发明填充了国内用于火箭贮箱箱底焊接系统的阻尼压紧装置的空白,实现了对产品的高质量、高效率的要求;1. The present invention fills the blank of the damping and pressing device used in the welding system of the bottom of the rocket tank in China, and realizes the requirements of high quality and high efficiency of the product;
2、本发明可实现对任何大曲率半径的球底、锥底工件的压紧,不受限于火箭贮箱箱底的形式,其中的阻尼螺钉可实时自身调节来补偿工件变形量,以达到焊缝单元高质量的要求;2. The present invention can realize the pressing of any spherical bottom and cone bottom workpieces with large curvature radius, and is not limited to the form of the bottom of the rocket tank. The damping screw can be adjusted in real time to compensate for the deformation of the workpiece, so as to achieve welding High quality requirements of seam units;
3、本发明可以大大减轻人工劳动强度,可实现一次安装直至焊接完成的要求;3. The invention can greatly reduce the labor intensity, and can meet the requirements of one installation until the welding is completed;
4、本发明可推广应用于火箭贮箱的其他部位焊接系统。4. The present invention can be applied to the welding system of other parts of the rocket tank.
附图说明Description of drawings
通过阅读参照以下附图对非限制性实施例所作的详细描述,本发明的其它特征、目的和优点将会变得更明显:Other features, objects and advantages of the present invention will become more apparent by reading the detailed description of non-limiting embodiments with reference to the following drawings:
图1为本发明的结构示意图。FIG. 1 is a schematic structural diagram of the present invention.
图2为本发明的剖视示意图。FIG. 2 is a schematic cross-sectional view of the present invention.
图3为本发明中阻尼螺钉的结构示意图。FIG. 3 is a schematic structural diagram of a damping screw in the present invention.
图4为本发明中阻尼螺钉的剖视示意图。4 is a schematic cross-sectional view of the damping screw in the present invention.
图5为本发明中图4的局部放大示意图。FIG. 5 is a partial enlarged schematic view of FIG. 4 in the present invention.
图中:In the picture:
1为第一紧固螺钉 44为钢丝弹簧1 is the first fastening screw 44 is the wire spring
2为工件 201为焊缝单元2 is the
3为机械压条 401为第三螺钉圆弧卡槽3 is the
4为阻尼螺钉 402为压紧头压紧端4 is the
5为弹性垫板 403为蝶形弹簧与压紧头接触处5 is the
6为第二紧固螺钉 404为钢丝弹簧与压紧头接触处6 is the
41为第三螺钉 405为第三螺钉压紧端41 is the
42为压紧头 406为第三螺钉与蝶形弹簧接触处42 is the
43为蝶形弹簧43 is a butterfly spring
具体实施方式Detailed ways
下面结合具体实施例对本发明进行详细说明。以下实施例将有助于本领域的技术人员进一步理解本发明,但不以任何形式限制本发明。应当指出的是,对本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变化和改进。这些都属于本发明的保护范围。The present invention will be described in detail below with reference to specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that, for those skilled in the art, several changes and improvements can be made without departing from the inventive concept. These all belong to the protection scope of the present invention.
如图1-图5所示,根据本发明提供的一种适用于火箭贮箱箱底焊接的阻尼压紧装置,包括:工件2、机械压条3、阻尼构件以及弹性垫板5;所示机械压条3的两端与工作台紧固连接;所示阻尼构件均匀排布安装于机械压条3上;所述弹性垫板5中心线与阻尼构件轴线对齐均匀排布安装于机械压条3上;所述弹性垫板5的另一端处于自由状态;所述阻尼构件向下压紧弹性垫板5的自由端,使弹性垫板5的自由端压紧在工件2上。As shown in Figures 1 to 5, a damping pressing device suitable for welding the bottom of a rocket tank provided according to the present invention includes: a
本发明的目的在于提供一种用于火箭贮箱箱底焊接系统的阻尼压紧装置。该装置能实现任何大曲率半径的球底、锥底工件的压紧,火箭贮箱箱底焊接时工件变形产生松动,通过阻尼螺钉自身调节来补偿工件变形量,确保工件一直处于压紧状态,保证焊接设备对工件的牢固、高质量和高效率的焊接作业,进一步提高火箭贮箱箱底的焊接质量和效率。The purpose of the present invention is to provide a damping and pressing device for a bottom welding system of a rocket tank. The device can realize the pressing of any spherical bottom and cone bottom workpieces with large curvature radius. When the bottom of the rocket tank is welded, the workpiece is deformed and loosened. The amount of deformation of the workpiece is compensated by the self-adjustment of the damping screw to ensure that the workpiece is always in a pressed state. The firm, high-quality and high-efficiency welding of the workpiece by the welding equipment further improves the welding quality and efficiency of the bottom of the rocket tank.
优选地,所述阻尼构件采用阻尼螺钉4。Preferably, the damping member adopts damping
优选地,所述阻尼螺钉4包括:第三螺钉41、压紧头42、蝶形弹簧43以及钢丝弹簧44;所述蝶形弹簧43放置于第三螺钉41内孔,压紧状态时,蝶形弹簧43一端紧贴在第三螺钉与蝶形弹簧接触处406,另一端紧贴在蝶形弹簧与压紧头接触处403。Preferably, the
优选地,所述压紧头42放置于第三螺钉41内孔并穿过蝶形弹簧43内孔。Preferably, the
优选地,所述钢丝弹簧44卡在第三螺钉圆弧卡槽401内,自由状态时,钢丝弹簧44把压紧头42挡在钢丝弹簧与压紧头接触处404,所述第三螺钉41安装于机械压条3上,正常压紧时,第三螺钉41通过第三螺钉压紧端405压紧工件2,焊接松动时,压紧头42通过压紧头压紧端402压紧工件2。Preferably, the wire spring 44 is clamped in the
优选地,所示机械压条3通过第一紧固螺钉1两端固定在工作台上。Preferably, the shown
优选地,所述弹性垫板5的一端通过第二紧固螺钉6与机械压条3紧固连接。Preferably, one end of the
具体地,在一个实施例中,如图1、图2所示,一种用于火箭贮箱箱底焊接系统的阻尼压紧装置,包括第一紧固螺钉1、工件2、机械压条3、阻尼螺钉4、弹性垫板5、第二紧固螺钉6,其中机械压条3通过第一紧固螺钉1两端固定在工作台上,阻尼螺钉4均匀排布安装于机械压条3上,弹性垫板5中心线与阻尼螺钉4轴线对齐均匀排布安装于机械压条3上,弹性垫板5通过第二紧固螺钉6一端固定于机械压条3上、另一端处于自由状态,阻尼螺钉4向下压紧弹性垫板5的自由端,使弹性垫板5的自由端压紧在工件2上。Specifically, in one embodiment, as shown in Figures 1 and 2, a damping and pressing device for a bottom welding system of a rocket tank includes a
正常压紧时,向下拧阻尼螺钉4引起弹性垫板5的自由端变形直至紧贴工件2,继续拧阻尼螺钉4直至达到规定扭矩时,停止拧阻尼螺钉4,此时阻尼螺钉4通过第三螺钉41的第三螺钉压紧端405压紧工件2;During normal pressing, screw down the damping
如图3,4所示,阻尼螺钉4包括第三螺钉41、压紧头42、蝶形弹簧43,钢丝弹簧44,其中所述蝶形弹簧43放置于第三螺钉41内孔,压紧状态时,蝶形弹簧43一端紧贴在第三螺钉与蝶形弹簧接触处406,另一端紧贴在蝶形弹簧与压紧头接触处403,所述压紧头42放置于第三螺钉41内孔并穿过蝶形弹簧43内孔,所述钢丝弹簧44卡在第三螺钉圆弧卡槽401内,自由状态时钢丝弹簧44把压紧头42挡在钢丝弹簧与压紧头接触处404,所述第三螺钉41安装于机械压条3上,正常压紧时,第三螺钉41通过第三螺钉压紧端405压紧工件2,焊接松动时,压紧头42通过压紧头压紧端402压紧工件2。As shown in FIGS. 3 and 4 , the damping
焊接松动时,蝶形弹簧43通过自身变形抵消焊接工件时产生的间隙,蝶形弹簧43推动压紧头42位移直至压紧工件2;When the welding is loose, the butterfly spring 43 offsets the gap generated when welding the workpiece through its own deformation, and the butterfly spring 43 pushes the
本发明可实现对任何大曲率半径的球底、锥底工件的压紧,不受限于火箭贮箱箱底的形式,其中的阻尼螺钉可实时自身调节来补偿工件变形量,以达到焊缝单元高质量的要求。The invention can realize the pressing of any spherical bottom and cone bottom workpieces with a large radius of curvature, and is not limited to the form of the bottom of the rocket tank. The damping screw can be adjusted in real time to compensate for the deformation of the workpiece, so as to achieve the welding seam unit. high quality requirements.
本发明填充了国内用于火箭贮箱箱底焊接系统的阻尼压紧装置的空白,实现了对产品的高质量、高效率的要求;本发明可实现对任何大曲率半径的球底、锥底工件的压紧,不受限于火箭贮箱箱底的形式,其中的阻尼螺钉可实时自身调节来补偿工件变形量,以达到焊缝单元高质量的要求;本发明可以大大减轻人工劳动强度,可实现一次安装直至焊接完成的要求;本发明可推广应用于火箭贮箱的其他部位焊接系统。The invention fills the blank of the damping and pressing device used in the welding system of the bottom of the rocket tank in China, and realizes the requirements of high quality and high efficiency of the product; the invention can realize the workpiece with any large curvature radius of spherical bottom and cone bottom. The compression of the welding seam is not limited to the form of the bottom of the rocket tank, and the damping screw can be adjusted in real time to compensate for the deformation of the workpiece, so as to meet the high quality requirements of the welding seam unit; the invention can greatly reduce the labor intensity, and can achieve The requirement of one-time installation until the welding is completed; the invention can be applied to the welding system of other parts of the rocket tank.
在本申请的描述中,需要理解的是,术语“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本申请和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本申请的限制。In the description of this application, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present application and simplifying the description, rather than indicating or implying the indicated device. Or elements must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as a limitation of the present application.
以上对本发明的具体实施例进行了描述。需要理解的是,本发明并不局限于上述特定实施方式,本领域技术人员可以在权利要求的范围内做出各种变化或修改,这并不影响本发明的实质内容。在不冲突的情况下,本申请的实施例和实施例中的特征可以任意相互组合。Specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the above-mentioned specific embodiments, and those skilled in the art can make various changes or modifications within the scope of the claims, which do not affect the essential content of the present invention. The embodiments of the present application and features in the embodiments may be combined with each other arbitrarily, provided that there is no conflict.
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