CN114986137B - A special tightening equipment for aviation equipment nuts - Google Patents
A special tightening equipment for aviation equipment nuts Download PDFInfo
- Publication number
- CN114986137B CN114986137B CN202210449031.XA CN202210449031A CN114986137B CN 114986137 B CN114986137 B CN 114986137B CN 202210449031 A CN202210449031 A CN 202210449031A CN 114986137 B CN114986137 B CN 114986137B
- Authority
- CN
- China
- Prior art keywords
- nut
- gear
- tightening
- flexible cable
- sleeve
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
- B23P19/06—Screw or nut setting or loosening machines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
Abstract
Description
技术领域Technical field
本发明属于航空装备装配技术领域,特别是涉及一种航空装备螺母专用拧紧设备。The invention belongs to the technical field of aviation equipment assembly, and in particular relates to a special tightening equipment for aviation equipment nuts.
背景技术Background technique
在航空领域中,诸多航空装备在圆周方向上是通过螺栓与螺母实现紧固连接的,并且现阶段螺母安装拧紧工作主要依靠人工方式完成,由于航空装备的特殊性,通常对螺母的拧紧力矩有严格的要求,而且螺母安装拧紧工艺还通常会有“拧紧→放松→再拧紧”的要求,从而导致工人的劳动强度非常高,工作效率也十分低下。In the aviation field, many aviation equipment are tightly connected in the circumferential direction through bolts and nuts. At present, the installation and tightening of nuts is mainly done manually. Due to the particularity of aviation equipment, the tightening torque of nuts is usually limited. Strict requirements, and the nut installation and tightening process usually has the requirement of "tightening → loosening → tightening again", which results in very high labor intensity for workers and very low work efficiency.
此外,一些航空装备的紧固位置还可能存在于高温、空间狭小等严苛的工作环境下,工人难以长时间在严苛的工作环境下进行螺母拧紧作业,从而进一步降低了工作效率。In addition, the fastening positions of some aviation equipment may exist in harsh working environments such as high temperatures and small spaces. It is difficult for workers to tighten nuts in harsh working environments for a long time, further reducing work efficiency.
发明内容Contents of the invention
针对现有技术存在的问题,本发明提供一种航空装备螺母专用拧紧设备,具有结构简单、工作可靠的特点,能够替代人工方式完成螺母拧紧工作,有效降低工人的劳动强度,即使紧固位置处于严苛的工作环境下,也可以高效完成螺母安装拧紧作业。In view of the problems existing in the existing technology, the present invention provides a special tightening equipment for aviation equipment nuts, which has the characteristics of simple structure and reliable operation. It can replace the manual method to complete the nut tightening work, effectively reducing the labor intensity of workers, even if the tightening position is at Even in harsh working environments, nut installation and tightening operations can be completed efficiently.
为了实现上述目的,本发明采用如下技术方案:一种航空装备螺母专用拧紧设备,包括机架、拧紧机、旋拧电机、三通道柔索牵拉机构、空心支杆及螺母拧紧扳手;所述机架与拧紧机的动力输出轴固定连接;所述旋拧电机和三通道柔索牵拉机构均安装在机架上;所述空心支杆一端与机架固定连接,所述螺母拧紧扳手连接在空心支杆另一端;所述空心支杆与旋拧电机的电机轴同轴分布,在空心支杆内部设置有一根传力轴,传力轴的一端与旋拧电机的电机轴同轴固连,传力轴的另一端与螺母拧紧扳手传动连接;所述三通道柔索牵拉机构通过三根柔索与螺母拧紧扳手传动连接。In order to achieve the above object, the present invention adopts the following technical solution: a special tightening equipment for aviation equipment nuts, including a frame, a tightening machine, a screwing motor, a three-channel flexible cable pulling mechanism, a hollow support rod and a nut tightening wrench; The frame is fixedly connected to the power output shaft of the tightening machine; the screwing motor and the three-channel flexible cable pulling mechanism are installed on the frame; one end of the hollow support rod is fixedly connected to the frame, and the nut tightening wrench is connected At the other end of the hollow support rod; the hollow support rod is coaxially distributed with the motor shaft of the screwing motor. A power transmission shaft is provided inside the hollow support rod. One end of the power transmission shaft is coaxially fixed with the motor shaft of the screwing motor. The other end of the power transmission shaft is transmission connected with the nut tightening wrench; the three-channel flexible cable pulling mechanism is transmission connected with the nut tightening wrench through three flexible cables.
所述螺母拧紧扳手包括壳体、封盖、输入端齿轮、中间传动齿轮组、输出端齿轮、螺母旋拧套筒、螺母拧紧控制组件和螺母拾取控制组件;所述输入端齿轮、中间传动齿轮组、输出端齿轮及螺母旋拧套筒沿直线顺序布设在壳体内部;所述封盖与壳体固定连接,壳体内部空间由封盖进行封隔;所述输入端齿轮的齿轮轴与壳体和封盖均通过轴承转动连接,且输入端齿轮的齿轮轴一端穿过封盖延伸至壳体外部,所述旋拧电机的电机轴通过空心支杆内部的传力轴与输入端齿轮的齿轮轴同轴固连;所述中间传动齿轮组内所有中间传动齿轮的齿轮轴与壳体和封盖均通过轴承转动连接,所述输入端齿轮与中间传动齿轮组啮合传动;所述输出端齿轮的齿轮轴与壳体和封盖均通过轴承转动连接,输出端齿轮与中间传动齿轮组啮合传动;所述螺母旋拧套筒通过套筒限位片设置在壳体内,螺母旋拧套筒在套筒限位片的限位下仅具有回转自由度;所述套筒限位片通过限位片挡块与壳体固定连接;在与所述螺母旋拧套筒正对的壳体上开设有套筒穿出孔;所述螺母拧紧控制组件位于套筒穿出孔外部且设置在壳体上;所述螺母拾取控制组件位于套筒穿出孔外部且设置在螺母拧紧控制组件上。The nut tightening wrench includes a housing, a cover, an input gear, an intermediate transmission gear set, an output gear, a nut tightening sleeve, a nut tightening control component and a nut picking control component; the input gear and intermediate transmission gear The set, the output end gear and the nut screwing sleeve are arranged in linear order inside the casing; the cover is fixedly connected to the casing, and the internal space of the casing is sealed by the cover; the gear shaft of the input end gear is connected to the casing. The casing and the cover are rotationally connected through bearings, and one end of the gear shaft of the input gear extends through the cover to the outside of the casing. The motor shaft of the screw motor communicates with the input gear through the transmission shaft inside the hollow support rod. The gear shafts are coaxially connected; the gear shafts of all intermediate transmission gears in the intermediate transmission gear set are rotationally connected to the housing and cover through bearings, and the input end gear meshes with the intermediate transmission gear set for transmission; the output The gear shaft of the end gear, the housing and the cover are all rotationally connected through bearings, and the output end gear meshes with the intermediate transmission gear set for transmission; the nut screwing sleeve is set in the housing through the sleeve limiter, and the nut screwing sleeve The sleeve only has a degree of freedom of rotation under the limit of the sleeve limit piece; the sleeve limit piece is fixedly connected to the shell through the limit piece stopper; in the shell opposite to the nut screwing sleeve There is a sleeve penetration hole; the nut tightening control assembly is located outside the sleeve penetration hole and is arranged on the housing; the nut pick-up control assembly is located outside the sleeve penetration hole and is arranged on the nut tightening control assembly .
在所述螺母旋拧套筒在外表面沿轴向分别设置有传动外齿圈和棘齿齿圈;所述传动外齿圈所在处的螺母旋拧套筒位于壳体内部,传动外齿圈与输出端齿轮啮合传动;所述棘齿齿圈所在处的螺母旋拧套筒位于壳体外部;位于所述壳体外部的螺母旋拧套筒内表面设为十二角孔,十二角孔与待拧紧的螺母配合使用;所述螺母旋拧套筒与拧紧机的动力输出轴同轴设置。A transmission outer ring gear and a ratchet ring gear are respectively provided on the outer surface of the nut screwing sleeve along the axial direction; the nut screwing sleeve where the transmission outer ring gear is located is located inside the housing, and the transmission outer ring gear and the ratchet ring gear are located inside the housing. The output end gear meshes and drives; the nut screwing sleeve where the ratchet ring gear is located is located outside the casing; the inner surface of the nut screwing sleeve located outside the casing is set as a twelve-angle hole, and the twelve-angle hole is It is used in conjunction with the nut to be tightened; the nut screwing sleeve is coaxially arranged with the power output shaft of the tightening machine.
所述螺母拧紧控制组件包括支撑架、左棘爪及右棘爪;所述支撑架与壳体固定连接;所述左棘爪和右棘爪镜像对称设置在支撑架内部;所述左棘爪的根部与支撑架相铰接,在左棘爪的顶部设置有棘齿,左棘爪通过其顶部的棘齿与螺母旋拧套筒上的棘齿齿圈配合使用;在所述左棘爪与支撑架之间设置有左棘爪复位弹簧;所述左棘爪与三通道柔索牵拉机构之间通过第一柔索相连;所述右棘爪的根部与支撑架相铰接,在右棘爪的顶部设置有棘齿,右棘爪通过其顶部的棘齿与螺母旋拧套筒上的棘齿齿圈配合使用;在所述右棘爪与支撑架之间设置有右棘爪复位弹簧;所述右棘爪与三通道柔索牵拉机构之间通过第二柔索相连。The nut tightening control assembly includes a support frame, a left pawl and a right pawl; the support frame is fixedly connected to the housing; the left pawl and the right pawl are mirror-symmetrically arranged inside the support frame; the left pawl The root of the left pawl is hinged with the support frame, and a ratchet is provided on the top of the left pawl. The left pawl uses the ratchet on the top to cooperate with the ratchet gear ring on the nut screwing sleeve; the left pawl and A left pawl return spring is provided between the support frames; the left pawl and the three-channel flexible cable pulling mechanism are connected through a first flexible cable; the root of the right pawl is hinged with the support frame, and the right pawl is connected to the three-channel flexible cable pulling mechanism. The top of the pawl is provided with a ratchet, and the right pawl is used in conjunction with the ratchet gear on the nut screwing sleeve through the ratchet on the top; a right pawl return spring is provided between the right pawl and the support frame. ; The right pawl and the three-channel flexible cable pulling mechanism are connected through a second flexible cable.
所述螺母拾取控制组件包括定位架及螺母压板;所述定位架与支撑架固定连接;所述螺母压板设置在定位架内部,在螺母压板与支撑架之间设置有压板复位弹簧;所述螺母压板与待拧紧的螺母配合使用;所述螺母压板与三通道柔索牵拉机构之间通过第三柔索相连;在所述壳体外部还设置有用于对第一柔索、第二柔索及第三柔索进行位置限定的柔索限位板。The nut pick-up control assembly includes a positioning frame and a nut pressure plate; the positioning frame is fixedly connected to the support frame; the nut pressure plate is arranged inside the positioning frame, and a pressure plate return spring is provided between the nut pressure plate and the support frame; the nut The pressure plate is used in conjunction with the nut to be tightened; the nut pressure plate and the three-channel flexible cable pulling mechanism are connected through a third flexible cable; a device for tightening the first flexible cable and the second flexible cable is also provided outside the housing. and a flexible cable limiting plate for limiting the position of the third flexible cable.
本发明的有益效果:Beneficial effects of the present invention:
本发明的航空装备螺母专用拧紧设备,具有结构简单、工作可靠的特点,能够替代人工方式完成螺母拧紧工作,有效降低工人的劳动强度,即使紧固位置处于严苛的工作环境下,也可以高效完成螺母安装拧紧作业。The special tightening equipment for aviation equipment nuts of the present invention has the characteristics of simple structure and reliable operation. It can replace the manual method to complete the nut tightening work, effectively reduce the labor intensity of workers, and can be efficient even if the fastening position is in a harsh working environment. Complete the nut installation and tightening work.
附图说明Description of drawings
图1为本发明的一种航空装备螺母专用拧紧设备的结构示意图;Figure 1 is a schematic structural diagram of a special tightening equipment for aviation equipment nuts according to the present invention;
图2为本发明的螺母拧紧扳手的结构示意图;Figure 2 is a schematic structural diagram of the nut tightening wrench of the present invention;
图3为本发明的螺母拧紧扳手的爆炸视图;Figure 3 is an exploded view of the nut tightening wrench of the present invention;
图4为本发明的螺母拧紧扳手的结构示意图(壳体、封盖等外部遮挡构件未示出);Figure 4 is a schematic structural diagram of the nut tightening wrench of the present invention (external shielding components such as the shell and cover are not shown);
图5为本发明的螺母旋拧套筒的结构示意图;Figure 5 is a schematic structural diagram of the nut screwing sleeve of the present invention;
图6为本发明的螺母旋拧套筒与左棘爪和右棘爪的配合示意图(初始状态);Figure 6 is a schematic diagram of the cooperation between the nut screwing sleeve and the left and right pawls of the present invention (initial state);
图7为本发明的螺母旋拧套筒与左棘爪和右棘爪的配合示意图(大力矩拧紧状态);Figure 7 is a schematic diagram of the cooperation between the nut screwing sleeve and the left and right pawls of the present invention (high torque tightening state);
图8为本发明的螺母旋拧套筒与左棘爪和右棘爪的配合示意图(大力矩放松状态);Figure 8 is a schematic diagram of the cooperation between the nut screwing sleeve and the left and right pawls of the present invention (large torque relaxation state);
图中,1—机架,2—拧紧机,3—旋拧电机,4—三通道柔索牵拉机构,5—空心支杆,6—螺母拧紧扳手,7—壳体,8—封盖,9—输入端齿轮,10—中间传动齿轮组,11—输出端齿轮,12—螺母旋拧套筒,13—螺母拧紧控制组件,14—螺母拾取控制组件,15—套筒限位片,16—限位片挡块,17—传动外齿圈,18—棘齿齿圈,19—十二角孔,20—支撑架,21—左棘爪,22—右棘爪,23—左棘爪复位弹簧,24—右棘爪复位弹簧,25—定位架,26—螺母压板,27—压板复位弹簧,28—第一柔索,29—第二柔索,30—第三柔索,31—柔索限位板。In the figure, 1—frame, 2—tightening machine, 3—screwing motor, 4—three-channel flexible cable pulling mechanism, 5—hollow rod, 6—nut tightening wrench, 7—casing, 8—cover , 9—Input gear, 10—Intermediate transmission gear set, 11—Output gear, 12—Nut tightening sleeve, 13—Nut tightening control component, 14—Nut pickup control component, 15—Sleeve limit piece, 16—limiting piece block, 17—transmission external ring gear, 18—ratchet ring gear, 19—twelve angular holes, 20—support frame, 21—left pawl, 22—right pawl, 23—left pawl Pawl return spring, 24-right pawl return spring, 25-positioning frame, 26-nut pressure plate, 27-pressure plate return spring, 28-first flexible cable, 29-second flexible cable, 30-third flexible cable, 31 —Flexible cable limit plate.
具体实施方式Detailed ways
下面结合附图和具体实施例对本发明做进一步的详细说明。The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
如图1~8所示,一种航空装备螺母专用拧紧设备,包括机架1、拧紧机2、旋拧电机3、三通道柔索牵拉机构4、空心支杆5及螺母拧紧扳手6;所述机架1与拧紧机2的动力输出轴固定连接;所述旋拧电机3和三通道柔索牵拉机构4均安装在机架1上;所述空心支杆5一端与机架1固定连接,所述螺母拧紧扳手6连接在空心支杆5另一端;所述空心支杆5与旋拧电机3的电机轴同轴分布,在空心支杆5内部设置有一根传力轴,传力轴的一端与旋拧电机3的电机轴同轴固连,传力轴的另一端与螺母拧紧扳手6传动连接;所述三通道柔索牵拉机构4通过三根柔索与螺母拧紧扳手6传动连接。As shown in Figures 1 to 8, a special tightening equipment for aviation equipment nuts includes a frame 1, a tightening machine 2, a screwing motor 3, a three-channel flexible cable pulling mechanism 4, a hollow support rod 5 and a nut tightening wrench 6; The frame 1 is fixedly connected to the power output shaft of the tightening machine 2; the screwing motor 3 and the three-channel flexible cable pulling mechanism 4 are both installed on the frame 1; one end of the hollow support rod 5 is connected to the frame 1 Fixed connection, the nut tightening wrench 6 is connected to the other end of the hollow strut 5; the hollow strut 5 is coaxially distributed with the motor shaft of the screwing motor 3, and a power transmission shaft is provided inside the hollow strut 5. One end of the force shaft is coaxially connected to the motor shaft of the screwing motor 3, and the other end of the force transmission shaft is drivingly connected to the nut tightening wrench 6; the three-channel flexible cable pulling mechanism 4 uses three flexible cables and the nut tightening wrench 6 Transmission connection.
所述螺母拧紧扳手6包括壳体7、封盖8、输入端齿轮9、中间传动齿轮组10、输出端齿轮11、螺母旋拧套筒12、螺母拧紧控制组件13和螺母拾取控制组件14;所述输入端齿轮9、中间传动齿轮组10、输出端齿轮11及螺母旋拧套筒12沿直线顺序布设在壳体7内部;所述封盖8与壳体7固定连接,壳体7内部空间由封盖8进行封隔;所述输入端齿轮9的齿轮轴与壳体7和封盖8均通过轴承转动连接,且输入端齿轮9的齿轮轴一端穿过封盖8延伸至壳体7外部,所述旋拧电机3的电机轴通过空心支杆5内部的传力轴与输入端齿轮9的齿轮轴同轴固连;所述中间传动齿轮组10内所有中间传动齿轮的齿轮轴与壳体7和封盖8均通过轴承转动连接,所述输入端齿轮9与中间传动齿轮组10啮合传动;所述输出端齿轮11的齿轮轴与壳体7和封盖8均通过轴承转动连接,输出端齿轮11与中间传动齿轮组10啮合传动;所述螺母旋拧套筒12通过套筒限位片15设置在壳体7内,螺母旋拧套筒12在套筒限位片15的限位下仅具有回转自由度;所述套筒限位片15通过限位片挡块16与壳体7固定连接;在与所述螺母旋拧套筒12正对的壳体7上开设有套筒穿出孔;所述螺母拧紧控制组件13位于套筒穿出孔外部且设置在壳体7上;所述螺母拾取控制组件14位于套筒穿出孔外部且设置在螺母拧紧控制组件13上。The nut tightening wrench 6 includes a housing 7, a cover 8, an input gear 9, an intermediate transmission gear set 10, an output gear 11, a nut tightening sleeve 12, a nut tightening control assembly 13 and a nut picking control assembly 14; The input gear 9, the intermediate transmission gear set 10, the output gear 11 and the nut screw sleeve 12 are sequentially arranged inside the housing 7 along a straight line; the cover 8 is fixedly connected to the housing 7, and the inside of the housing 7 The space is sealed by the cover 8; the gear shaft of the input gear 9 is rotationally connected to the housing 7 and the cover 8 through bearings, and one end of the gear shaft of the input gear 9 extends through the cover 8 to the housing 7 Externally, the motor shaft of the screwing motor 3 is coaxially connected to the gear shaft of the input gear 9 through the power transmission shaft inside the hollow support rod 5; the gear shafts of all intermediate transmission gears in the intermediate transmission gear set 10 The input gear 9 meshes with the intermediate transmission gear set 10 for rotation with the housing 7 and the cover 8 through bearings. The gear shaft of the output gear 11 rotates with the housing 7 and the cover 8 through bearings. connection, the output end gear 11 meshes with the intermediate transmission gear set 10 for transmission; the nut screwing sleeve 12 is set in the housing 7 through the sleeve limiting piece 15, and the nut screwing sleeve 12 is in the sleeve limiting piece 15 It only has the degree of freedom of rotation under the limit; the sleeve limit piece 15 is fixedly connected to the housing 7 through the limit piece stopper 16; there is an opening on the housing 7 facing the nut screwing sleeve 12 There is a sleeve penetration hole; the nut tightening control assembly 13 is located outside the sleeve penetration hole and is arranged on the housing 7; the nut pick-up control assembly 14 is located outside the sleeve penetration hole and is arranged on the nut tightening control assembly 13 on.
在所述螺母旋拧套筒12在外表面沿轴向分别设置有传动外齿圈17和棘齿齿圈18;所述传动外齿圈17所在处的螺母旋拧套筒12位于壳体7内部,传动外齿圈17与输出端齿轮11啮合传动;所述棘齿齿圈18所在处的螺母旋拧套筒12位于壳体7外部;位于所述壳体7外部的螺母旋拧套筒12内表面设为十二角孔19,十二角孔19与待拧紧的螺母配合使用;所述螺母旋拧套筒12与拧紧机2的动力输出轴同轴设置。A transmission external ring gear 17 and a ratchet gear 18 are respectively provided on the outer surface of the nut screwing sleeve 12 along the axial direction; the nut screwing sleeve 12 where the transmission external ring gear 17 is located is located inside the housing 7 , the transmission outer ring gear 17 meshes with the output end gear 11 for transmission; the nut screwing sleeve 12 where the ratchet ring gear 18 is located is located outside the housing 7; the nut screwing sleeve 12 located outside the housing 7 The inner surface is configured as a twelve-cornered hole 19, which is used in conjunction with the nut to be tightened; the nut screwing sleeve 12 is coaxially arranged with the power output shaft of the tightening machine 2.
所述螺母拧紧控制组件13包括支撑架20、左棘爪21及右棘爪22;所述支撑架20与壳体7固定连接;所述左棘爪21和右棘爪22镜像对称设置在支撑架20内部;所述左棘爪21的根部与支撑架20相铰接,在左棘爪21的顶部设置有棘齿,左棘爪21通过其顶部的棘齿与螺母旋拧套筒12上的棘齿齿圈18配合使用;在所述左棘爪21与支撑架20之间设置有左棘爪复位弹簧23;所述左棘爪21与三通道柔索牵拉机构4之间通过第一柔索28相连;所述右棘爪22的根部与支撑架20相铰接,在右棘爪22的顶部设置有棘齿,右棘爪22通过其顶部的棘齿与螺母旋拧套筒12上的棘齿齿圈18配合使用;在所述右棘爪22与支撑架20之间设置有右棘爪复位弹簧24;所述右棘爪22与三通道柔索牵拉机构4之间通过第二柔索29相连。The nut tightening control assembly 13 includes a support frame 20, a left pawl 21 and a right pawl 22; the support frame 20 is fixedly connected to the housing 7; the left pawl 21 and the right pawl 22 are arranged in mirror symmetry on the support. Inside the frame 20; the root of the left pawl 21 is hingedly connected to the support frame 20, and a ratchet is provided on the top of the left pawl 21. The left pawl 21 screws the nut on the sleeve 12 through the ratchet at the top and the nut. The ratchet gear 18 is used in conjunction; a left pawl return spring 23 is provided between the left pawl 21 and the support frame 20; the left pawl 21 and the three-channel flexible cable pulling mechanism 4 are connected by a first The flexible rope 28 is connected; the root of the right pawl 22 is hingedly connected to the support frame 20, and a ratchet is provided on the top of the right pawl 22. The right pawl 22 is screwed onto the sleeve 12 through the ratchet on the top and the nut. The ratchet gear 18 is used in conjunction; a right pawl return spring 24 is provided between the right pawl 22 and the support frame 20; the right pawl 22 and the three-channel flexible cable pulling mechanism 4 are connected by a third Two flexible ropes 29 are connected.
所述螺母拾取控制组件14包括定位架25及螺母压板26;所述定位架25与支撑架20固定连接;所述螺母压板26设置在定位架25内部,在螺母压板26与支撑架20之间设置有压板复位弹簧27;所述螺母压板26与待拧紧的螺母配合使用;所述螺母压板26与三通道柔索牵拉机构4之间通过第三柔索30相连;在所述壳体7外部还设置有用于对第一柔索、第二柔索及第三柔索进行位置限定的柔索限位板31。The nut pick-up control assembly 14 includes a positioning frame 25 and a nut pressure plate 26; the positioning frame 25 is fixedly connected to the support frame 20; the nut pressure plate 26 is arranged inside the positioning frame 25, between the nut pressure plate 26 and the support frame 20 A pressure plate return spring 27 is provided; the nut pressure plate 26 is used in conjunction with the nut to be tightened; the nut pressure plate 26 and the three-channel flexible cable pulling mechanism 4 are connected through a third flexible cable 30; in the housing 7 A flexible cable limiting plate 31 is also provided on the outside for limiting the positions of the first flexible cable, the second flexible cable and the third flexible cable.
下面结合附图说明本发明的一次使用过程:The one-time use process of the present invention will be described below in conjunction with the accompanying drawings:
首先选配一台机械臂,将本发明的航空装备螺母专用拧紧设备作为该机械臂的端拾器,具体通过拧紧机2与机械臂进行装配连接。First, a robotic arm is selected, and the special tightening equipment for aviation equipment nuts of the present invention is used as the end picker of the robotic arm. Specifically, the tightening machine 2 is used for assembly and connection with the robotic arm.
在机械臂覆盖的范围内,设置两个区域,一个作为航空装备的装配区,另一个作为零件区,将待安装的螺母放置到零件区。Within the range covered by the robotic arm, two areas are set up, one as an assembly area for aviation equipment, and the other as a parts area. The nuts to be installed are placed in the parts area.
首先通过机械臂将本发明的航空装备螺母专用拧紧设备移动到零件区,使螺母拧紧扳手6内部的螺母旋拧套筒12位于螺母正上方,然后控制螺母拧紧扳手6下落,直到螺母的上半部分准确进入螺母旋拧套筒12的十二角孔19内。First, the special tightening equipment for aviation equipment nuts of the present invention is moved to the parts area through a mechanical arm, so that the nut tightening sleeve 12 inside the nut tightening wrench 6 is located directly above the nut, and then the nut tightening wrench 6 is controlled to drop until the upper half of the nut Part of it accurately enters the twelve-corner hole 19 of the nut screwing sleeve 12.
当螺母进入螺母旋拧套筒12的十二角孔19后,启动三通道柔索牵拉机构4,对第三柔索30进行放线,在压板复位弹簧27的推力作用下,会通过螺母压板26将螺母压紧固定在螺母拧紧扳手6上。When the nut enters the twelve-corner hole 19 of the nut screwing sleeve 12, the three-channel flexible cable pulling mechanism 4 is started to pay out the third flexible cable 30. Under the thrust of the pressure plate return spring 27, it will pass through the nut. The pressure plate 26 presses and fixes the nut on the nut tightening wrench 6 .
当螺母夹持固定在螺母拧紧扳手6上后,通过机械臂将本发明的航空装备螺母专用拧紧设备移动到装配区,使夹持固定在螺母拧紧扳手6上的螺母位于航空装备相应位置处的螺杆正上方,然后控制螺母拧紧扳手6下落,直到螺母准确落到螺杆的顶端。After the nut is clamped and fixed on the nut tightening wrench 6, the special tightening equipment for aviation equipment nuts of the present invention is moved to the assembly area through the mechanical arm, so that the nut clamped and fixed on the nut tightening wrench 6 is located at the corresponding position of the aviation equipment. directly above the screw, and then control the nut tightening wrench 6 to drop until the nut accurately falls to the top of the screw.
当螺母落到螺杆的顶端后,启动三通道柔索牵拉机构4,对第三柔索30进行收线,通过第三柔索30将螺母压板26拉离螺母,压板复位弹簧27恢复压缩状态。When the nut falls to the top of the screw, the three-channel flexible cable pulling mechanism 4 is started to take up the third flexible cable 30. The nut pressure plate 26 is pulled away from the nut through the third flexible cable 30, and the pressure plate return spring 27 returns to the compressed state. .
当螺母压板26被拉离螺母后,启动旋拧电机3,带动空心支杆5内部的传力轴转动,通过转动的传力轴依次带动输入端齿轮9、中间传动齿轮组10及输出端齿轮11转动,进而通过转动的输出端齿轮11带动与之啮合的传动外齿圈17转动,最终带动螺母旋拧套筒12转动,并通过转动的螺母旋拧套筒12带动十二角孔19内的螺母转动,实现螺母在螺杆上的旋拧,螺母旋拧过程中螺母拧紧扳手6在机械臂的控制下沿螺杆轴向进行随动,直到螺母旋拧到位。When the nut pressure plate 26 is pulled away from the nut, the screwing motor 3 is started to drive the transmission shaft inside the hollow support rod 5 to rotate, and the input gear 9, the intermediate transmission gear set 10 and the output gear are sequentially driven through the rotating transmission shaft. 11 rotates, and then the rotating output gear 11 drives the meshed transmission outer ring gear 17 to rotate, and finally drives the nut screwing sleeve 12 to rotate, and drives the twelve-angle hole 19 through the rotating nut screwing sleeve 12 The nut rotates to realize the screwing of the nut on the screw. During the nut screwing process, the nut tightening wrench 6 follows the axial direction of the screw under the control of the mechanical arm until the nut is screwed in place.
当螺母在螺杆上旋拧到位后,首先启动三通道柔索牵拉机构4,对第一柔索28进行放线,在左棘爪复位弹簧23的推力作用下,会使左棘爪21顶部棘齿与螺母旋拧套筒12上的棘齿齿圈18啮合,然后正向启动拧紧机2,由拧紧机2的动力输出轴带动机架1进行摆转,由于机架1通过空心支杆5与螺母拧紧扳手6的壳体7固连为整体,因此机架1的摆转运动和同步转换为螺母拧紧扳手6的摆转运动,最终通过螺母拧紧扳手6的摆转运动对螺母实施大力矩拧紧。When the nut is screwed in place on the screw, first start the three-channel flexible cable pulling mechanism 4 to pay out the first flexible cable 28. Under the thrust of the left pawl return spring 23, the top of the left pawl 21 will be The ratchet meshes with the ratchet ring 18 on the nut screwing sleeve 12, and then starts the tightening machine 2 in the forward direction, and the power output shaft of the tightening machine 2 drives the frame 1 to rotate. Since the frame 1 passes through the hollow support rod 5 is fixedly connected to the housing 7 of the nut tightening wrench 6 as a whole, so the swing motion and synchronization of the frame 1 are converted into the swing motion of the nut tightening wrench 6, and finally the nut is greatly tightened through the swing motion of the nut tightening wrench 6. Torque tighten.
当螺母完成大力矩拧紧后,根据工艺要求,还需要对首次拧紧的螺母进行放松,之后再进行二次拧紧,因此为了满足工艺要求,首先启动三通道柔索牵拉机构4,对第一柔索28进行收线,通过第一柔索28将左棘爪21拉离棘齿齿圈18,左棘爪复位弹簧23恢复压缩状态;同时,对第二柔索29进行放线,在右棘爪复位弹簧24的推力作用下,会使右棘爪22顶部棘齿与螺母旋拧套筒12上的棘齿齿圈18啮合,然后反向启动拧紧机2,由拧紧机2的动力输出轴带动机架1进行摆转,进而同步带动螺母拧紧扳手6进行摆转,最终通过螺母拧紧扳手6的摆转运动对螺母实施大力矩放松。After the nut is tightened with a large torque, according to the process requirements, the nut that was tightened for the first time needs to be loosened and then tightened a second time. Therefore, in order to meet the process requirements, the three-channel flexible cable pulling mechanism 4 is first started, and the first flexible cable pulling mechanism 4 is started. The cable 28 is retracted, and the left pawl 21 is pulled away from the ratchet ring 18 through the first flexible cable 28, and the left pawl return spring 23 returns to the compressed state; at the same time, the second flexible cable 29 is paid out, and the left pawl 21 is pulled away from the ratchet ring 18 through the first flexible cable 28. Under the thrust of the pawl return spring 24, the top ratchet of the right pawl 22 will mesh with the ratchet gear 18 on the nut screwing sleeve 12, and then the tightening machine 2 will be started in reverse, and the power output shaft of the tightening machine 2 will The machine frame 1 is driven to rotate, and then the nut tightening wrench 6 is synchronously driven to rotate, and finally the nut is loosened with a large torque through the swinging motion of the nut tightening wrench 6 .
当螺母完成大力矩放松后,在工艺要求下,启动三通道柔索牵拉机构4,对第二柔索29进行收线,通过第二柔索29将右棘爪22拉离棘齿齿圈18,右棘爪复位弹簧24恢复压缩状态;同时,对第一柔索28进行放线,在左棘爪复位弹簧23的推力作用下,会使左棘爪21顶部棘齿与螺母旋拧套筒12上的棘齿齿圈18啮合,然后正向启动拧紧机2,由拧紧机2的动力输出轴带动机架1进行摆转,进而同步带动螺母拧紧扳手6进行摆转,最终通过螺母拧紧扳手6的摆转运动对螺母实施大力矩放松,从而实现螺母的二次拧紧。After the nut is loosened with a large torque, and under the process requirements, the three-channel flexible cable pulling mechanism 4 is started to take up the second flexible cable 29 and pull the right pawl 22 away from the ratchet ring through the second flexible cable 29 18. The right pawl return spring 24 returns to the compressed state; at the same time, the first flexible cable 28 is unwound. Under the thrust of the left pawl return spring 23, the top ratchet of the left pawl 21 and the nut are screwed together. The ratchet ring 18 on the barrel 12 engages, and then the tightening machine 2 is started in the forward direction, and the power output shaft of the tightening machine 2 drives the frame 1 to rotate, and then simultaneously drives the nut tightening wrench 6 to rotate, and finally tightens the nut. The swinging motion of the wrench 6 loosens the nut with a large torque, thereby achieving secondary tightening of the nut.
当该螺母完成了“拧紧→放松→再拧紧”的工艺要求后,启动三通道柔索牵拉机构4,对第一柔索28进行收线,通过第一柔索28将左棘爪21拉离棘齿齿圈18,左棘爪复位弹簧23恢复压缩状态,此时左棘爪21和右棘爪22均处于脱离棘齿齿圈18的初始状态,之后控制螺母拧紧扳手6上移,使拧紧后的螺母与螺母旋拧套筒12的十二角孔19脱离,最后通过机械臂将本发明的航空装备螺母专用拧紧设备再次移动到零件区,重复首个螺母的安装过程,完成后续其它螺母的安装拧紧工作。After the nut completes the process requirements of "tightening → loosening → tightening again", the three-channel flexible cable pulling mechanism 4 is started to take up the first flexible cable 28 and pull the left pawl 21 through the first flexible cable 28 away from the ratchet ring gear 18, the left pawl return spring 23 returns to the compressed state. At this time, both the left pawl 21 and the right pawl 22 are in the initial state of being separated from the ratchet ring gear 18. Afterwards, the nut tightening wrench 6 is controlled to move upward, so that The tightened nut is separated from the twelve-cornered hole 19 of the nut screwing sleeve 12. Finally, the special tightening equipment for aviation equipment nuts of the present invention is moved to the parts area again through the mechanical arm, and the installation process of the first nut is repeated to complete other subsequent tasks. Installation and tightening of nuts.
实施例中的方案并非用以限制本发明的专利保护范围,凡未脱离本发明所为的等效实施或变更,均包含于本案的专利范围中。The solutions in the examples are not intended to limit the scope of patent protection of the present invention. Any equivalent implementation or modification that does not depart from the scope of the present invention is included in the patent scope of this case.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210449031.XA CN114986137B (en) | 2022-04-27 | 2022-04-27 | A special tightening equipment for aviation equipment nuts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210449031.XA CN114986137B (en) | 2022-04-27 | 2022-04-27 | A special tightening equipment for aviation equipment nuts |
Publications (2)
Publication Number | Publication Date |
---|---|
CN114986137A CN114986137A (en) | 2022-09-02 |
CN114986137B true CN114986137B (en) | 2024-03-22 |
Family
ID=83026267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210449031.XA Active CN114986137B (en) | 2022-04-27 | 2022-04-27 | A special tightening equipment for aviation equipment nuts |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114986137B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115648113B (en) * | 2022-11-01 | 2024-04-26 | 中国航发沈阳黎明航空发动机有限责任公司 | Auxiliary steel rope connecting device of aeroengine steel rope tractor |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0671065U (en) * | 1993-03-19 | 1994-10-04 | 旭金属工業株式会社 | Ratchet wrench and tightening tool |
KR101415580B1 (en) * | 2014-05-02 | 2014-07-04 | 주식회사 우정티엠에스 | Open type ratchet wrench |
CN108544409A (en) * | 2018-07-02 | 2018-09-18 | 四川汇智众创科技有限公司 | A kind of Quick fastening spanner being applied to interlocking double nut |
CN208051780U (en) * | 2018-04-09 | 2018-11-06 | 新昌县羽林街道元洋机械厂 | A kind of nut tightening device with self-locking |
CN110757140A (en) * | 2019-11-01 | 2020-02-07 | 深圳市圆梦精密技术研究院 | screw nut device |
CN110814716A (en) * | 2019-11-01 | 2020-02-21 | 深圳市圆梦精密技术研究院 | Nut-screwing device and nut-screwing mechanism |
CN112045405A (en) * | 2020-09-22 | 2020-12-08 | 沈阳航空航天大学 | Fast and large torque tightening device and tightening method for blind cavity in narrow and long space |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TW567123B (en) * | 2002-07-22 | 2003-12-21 | Hou-Fei Hu | Ratchet wrench capable of fast rotation |
US20190118350A1 (en) * | 2017-10-25 | 2019-04-25 | Aficial Co., Ltd. | Ratchet wrench |
-
2022
- 2022-04-27 CN CN202210449031.XA patent/CN114986137B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0671065U (en) * | 1993-03-19 | 1994-10-04 | 旭金属工業株式会社 | Ratchet wrench and tightening tool |
KR101415580B1 (en) * | 2014-05-02 | 2014-07-04 | 주식회사 우정티엠에스 | Open type ratchet wrench |
CN208051780U (en) * | 2018-04-09 | 2018-11-06 | 新昌县羽林街道元洋机械厂 | A kind of nut tightening device with self-locking |
CN108544409A (en) * | 2018-07-02 | 2018-09-18 | 四川汇智众创科技有限公司 | A kind of Quick fastening spanner being applied to interlocking double nut |
CN110757140A (en) * | 2019-11-01 | 2020-02-07 | 深圳市圆梦精密技术研究院 | screw nut device |
CN110814716A (en) * | 2019-11-01 | 2020-02-21 | 深圳市圆梦精密技术研究院 | Nut-screwing device and nut-screwing mechanism |
CN112045405A (en) * | 2020-09-22 | 2020-12-08 | 沈阳航空航天大学 | Fast and large torque tightening device and tightening method for blind cavity in narrow and long space |
Also Published As
Publication number | Publication date |
---|---|
CN114986137A (en) | 2022-09-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN114986137B (en) | A special tightening equipment for aviation equipment nuts | |
KR101118786B1 (en) | Reaction arm for power-driven torque intensifier | |
WO2007097166A1 (en) | Bolt-tightening tool | |
CN108673121A (en) | A kind of pre-tightening apparatus for nut assembly | |
CN110487469A (en) | A kind of measurement high-strength bolt fastens the device of axle power and torque coefficient | |
CN108081189A (en) | A connecting rod type tightening mechanism and method suitable for tightening in an inner cavity structure | |
GB2083392A (en) | Wrench with rapid rotation facility | |
CN109048960A (en) | A kind of detachable automated machine pawl | |
CN208977821U (en) | A kind of detachable automated machine pawl | |
US20050277513A1 (en) | Compact actuator | |
CN109277798A (en) | Automatic tightening machine and using method thereof | |
CN111390793A (en) | Be used for high-tension line drainage fastener bolt preloading device | |
CN216940429U (en) | Bolt fastening device | |
CN115091180A (en) | Bolt fastening robot end tool capable of screwing at opposite sides | |
CN114952690A (en) | A visual anti-rotation electric tightening gun | |
CN213859007U (en) | Spanner for power transmission line based on unmanned aerial vehicle | |
CN211304645U (en) | Electric hand riveter | |
CA2362519A1 (en) | Crowd rope take-up system for a shovel | |
CN222449184U (en) | A two-way folding and unfolding special tightening device for aviation equipment nuts | |
JPS6216796B2 (en) | ||
CN212399443U (en) | Operating device and mechanical type installation extracting tool are dismantled in installation | |
JPH02274474A (en) | Screwdriver for pipe joint | |
CN112878936A (en) | Go up compensation arrangement that breaks out | |
CN118595807A (en) | A two-way folding and unfolding special tightening device for aviation equipment nuts | |
CN221186305U (en) | Small-space screw fastening device |
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 | ||
GR01 | Patent grant | ||
GR01 | Patent grant |