Part machining tool clamp
By designing a combined structure of parts processing fixtures, the fixing and loosening processes of aviation parts are simplified and the parts processing efficiency is improved.
Patent Information
- Application Number
- CN202422507535.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-17
- Publication Date
- 2025-09-09
- Estimated Expiration
- 2034-10-17
AI Technical Summary
In the prior art, when clamping aviation parts, a knob needs to be turned to operate a nut to fix and loosen, which makes the fixing operation cumbersome and reduces the part processing efficiency.
A parts processing fixture is designed, which adopts a combined structure of a screw, a sliding column, a movable ring, a side protrusion, a connecting rod, a rotating shaft, a pressure rod and a clamp. The parts are fixed in the open side groove by engaging the rotating shaft, which simplifies the fixing and loosening process.
It realizes the rapid fixing and loosening of parts and improves the processing efficiency.
Smart Images

Figure CN223313821U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of processing tooling, and specifically to a parts processing tooling fixture. Background Art
[0002] Parts are the basic elements of a machine. A machine generally consists of one or more prime movers that receive external energy; an executive part that performs the machine's production functions, transmitting the prime mover's motion and power to the executive part; and a detection and control system that ensures the coordinated operation of all parts in the machine. Further decomposition of the machine reveals various parts.
[0003] Parts are used in machinery manufacturing, electronics industry, aerospace, automobile industry, medical equipment and other fields. For example, when machining aviation parts, machining tooling is required to reliably position and clamp them to prevent displacement and shaking during the machining process.
[0004] For example, the patent with publication number CN219837683U specifically discloses a fixed tooling for processing long-axis parts, including a base, two screws, a positioning plate, a nut, a positioning pad and an elastic clamping strip, so that the nut is adjusted to slide the positioning pad downward and make close contact with the outer wall of the part, while squeezing the outer wall of the part and the outer wall of the elastic clamping strip into close contact until the outer wall of the elastic clamping strip is fully in contact with the part, so that the positioning pad and the elastic clamping strip cooperate to fix the long-axis part between them.
[0005] The above patent fixes the parts by adjusting two sets of nuts to slide the positioning pad downward and bring the parts into close contact with the outer wall of the elastic clamp when clamping aviation parts. In this way, when processing shaft parts of different diameters, a knob operation must be performed each time the parts are fixed and released. The overall fixing operation is relatively cumbersome, which reduces the efficiency of part processing. Therefore, it is necessary to design a part processing fixture to solve the above problems.
[0006] It should be noted that the above information disclosed in this Background section is only for understanding the background technology of the present application concept, and therefore, it may contain information that does not constitute prior art. Summary of the Invention
[0007] Based on the above-mentioned problems existing in the prior art, the problem to be solved by this application is: to provide a parts processing fixture to solve the problem that when clamping aviation parts in the above-mentioned patent, the positioning pad is adjusted downward by sliding the two sets of nuts to make the parts and the outer wall of the elastic clamp close contact to fix the parts. In this way, when processing shaft parts of different diameters, the knob operation must be performed each time the fixing and loosening is performed. The overall fixing operation is relatively cumbersome, which reduces the parts processing efficiency.
[0008] The technical solution adopted by the present application to solve its technical problem is: a parts processing fixture. It mainly includes: a base, which has a workbench; a fixing assembly, which is installed on the base, and the fixing assembly includes: two sets of screws, which are installed on the base; a sliding column, which is threadedly connected to the screws, and the sliding column includes two sets of circular grooves; a pressure rod, which is sleeved and installed on the two sets of the screws; a locking unit, which is installed on the sliding column, and the locking unit includes: a movable ring, which is sleeved and installed on the circular grooves, and the movable ring is installed with two sets of side protrusions; a connecting rod, which is connected between the two sets of the side protrusions, and the connecting rod is movably sleeved with a rotating shaft; a clamp, which is installed at one end of the rotating shaft; a clamping assembly, which is installed on the pressure rod, and the clamping assembly has an upper clamping block and a lower clamping block for clamping the parts.
[0009] Furthermore, an elastic pad is provided at the contact position between the clamp and the pressure rod.
[0010] Furthermore, an open side groove adapted to the diameter of the rotating shaft is formed at one end of the pressure rod, and an anti-slip pad is provided at the contact position between the rotating shaft and the open side groove.
[0011] Furthermore, the upper clamping block is installed on the pressure rod, the upper clamping block has a fixing sleeve, and the lower clamping block is installed on the workbench.
[0012] Furthermore, the upper clamping block and the lower clamping block both have right-angle clamping grooves.
[0013] Furthermore, silicone pads are provided at the contact positions between the upper clamping block and the lower clamping block and the aviation shaft parts.
[0014] The beneficial effect of the present application is that the present application provides a parts processing fixture, which can fix the position of the pressure rod through the arrangement of a screw rod, a fixed foot, a sliding column, a movable ring, a side protrusion, a connecting rod, a rotating shaft, a pressure rod and a clamp, thereby facilitating the fixing of aviation shaft parts between the upper clamp block and the lower clamp block.
[0015] In addition to the above-described purposes, features and advantages, the present application also has other purposes, features and advantages. The present application will be further described in detail below with reference to the drawings. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The drawings that constitute part of this application are used to provide a further understanding of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute an improper limitation on this application. In the drawings:
[0017] Figure 1This is an overall schematic diagram of a parts processing fixture in this application;
[0018] Figure 2 for Figure 1 Explosion diagram of
[0019] Figure 3 for Figure 2 Schematic diagram of the bottom structure in;
[0020] Among them, the reference numerals in the figures are:
[0021] 1. Base; 101. Support leg; 103. Workbench; 2. Fixing assembly; 201. Screw; 202. Fixed foot; 203. Sliding column; 204. Movable ring; 205. Side protrusion; 206. Connecting rod; 207. Rotating shaft; 208. Press rod; 209. Open side groove; 210. Hole; 211. Clamp; 212. Circular groove; 3. Clamping assembly; 301. Upper clamping block; 302. Lower clamping block; 303. Right-angle clamping groove. DETAILED DESCRIPTION
[0022] It should be noted that, in the absence of conflict, the embodiments and features of the embodiments in this application can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.
[0023] In order to enable those skilled in the art to better understand the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts should fall within the scope of protection of this application.
[0024] like Figure 1-Figure 3 As shown, the present application provides a parts processing fixture, which is used for processing aviation parts, including a base 1, on which support legs 101 are fixedly mounted, and the support legs 101 are used to provide auxiliary support for the base 1, and a workbench 103 is fixedly mounted on the base 1;
[0025] A fixing assembly 2 is mounted on the base 1. The fixing assembly 2 includes two sets of screw rods 201 fixedly mounted on the base 1. A fixing foot 202 is fixedly mounted on one end of the screw rods 201 close to the base 1. The screw rods 201 are fixedly mounted on the base 1 through the fixing foot 202.
[0026] A sliding post 203 is threadedly connected to the screw rod 201. The sliding post 203 includes two sets of annular grooves 212. A screw groove adapted to the screw rod 201 is opened on the sliding post 203. The sliding post 203 is adapted to rotate along the linear direction of the screw rod 201. A pressure rod 208 is movably sleeved on the two sets of screw rods 201. A sleeve hole 210 adapted to the diameter of the screw rod 201 is opened on the pressure rod 208.
[0027] A locking unit is mounted on the sliding column 203. The locking unit includes a movable ring 204 that is movably sleeved on a set of circular grooves 212. Two sets of side protrusions 205 are fixedly mounted on the movable ring 204. A connecting rod 206 is connected between the two sets of side protrusions 205. A rotating shaft 207 is movably sleeved on the connecting rod 206.
[0028] An open side groove 209 is formed at one end of the pressure rod 208, which is adapted to the diameter of the rotating shaft 207. The rotating shaft 207 is adapted to rotate along the rod core of the connecting rod 206 so as to be engaged in the open side groove 209. A clamp 211 is fixedly mounted at one end of the rotating shaft 207. The clamp 211 is adapted to be engaged in the open side groove 209 along with the rotating shaft 207, thereby being adapted to fit on the pressure rod 208 and further adapted to fix the pressure rod 208 on the sliding column 203.
[0029] In the present application, an elastic pad is provided at the contact position between the clamp 211 and the pressure rod 208 so as to fit the clamp 211 tightly onto the pressure rod 208;
[0030] In the present application, an anti-slip pad is provided at the contact position between the rotating shaft 207 and the open side groove 209 to prevent the rotating shaft 207 from falling out of the open side groove 209;
[0031] A clamping assembly 3 is mounted on the pressure rod 208. The clamping assembly 3 includes an upper clamping block 301 mounted on the pressure rod 208 near the workbench 103. The upper clamping block 301 has a fixed sleeve, which is connected to the pressure rod 208 through the fixed sleeve. A lower clamping block 302 is fixedly mounted on the workbench 103. Both the upper clamping block 301 and the lower clamping block 302 have a right-angle clamping groove 303, which is suitable for clamping aviation shaft parts of different sizes.
[0032] In the present application, silicone pads are provided at the contact positions between the upper clamping block 301 and the lower clamping block 302 and the aviation shaft parts, so as to be suitable for tightly clamping the aviation shaft parts between the upper clamping block 301 and the lower clamping block 302;
[0033] Working principle:
[0034] When processing aviation shaft parts, the aviation shaft parts are placed in the right-angle clamping groove 303 on the lower clamping block 302, and the two sets of sliding columns 203 are rotated downward, and then the lower pressure rod 208 is lowered, so that the upper clamping block 301 on the pressure rod 208 is pressed on the aviation shaft parts, and then the knob sliding column 203 is moved upward to support the two ends of the lower pressure rod 208, and then the clamp 211 is held and rotated to make the rotating shaft 207 engage in the open side groove 209, and the clamp 211 is attached to the pressure rod 208, so that the pressure rod 208 can be fixed in position, which makes it easier to fix the aviation shaft parts between the upper clamping block 301 and the lower clamping block 302. Compared with the method of fixing the pressure rod 208 by means of a knob nut, fixing and loosening are simpler and faster.
[0035] The above are merely preferred embodiments of the present application and are not intended to limit the present application. Those skilled in the art will readily appreciate that various modifications and variations are possible. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of the present application shall be included within the scope of protection of the present application.
Claims
1. A parts processing fixture, characterized by: include: A base (1), the base (1) having a workbench (103); A fixing assembly (2), the fixing assembly (2) being mounted on the base (1), the fixing assembly (2) comprising: Two sets of screw rods (201), the screw rods (201) are mounted on the base (1); A sliding post (203), the sliding post (203) being threadedly connected to the screw rod (201), the sliding post (203) comprising two sets of annular grooves (212); A pressure rod (208), the pressure rod (208) is sleeved and mounted on the two sets of screw rods (201); A locking unit, which is mounted on the sliding column (203), and comprises: A movable ring (204), the movable ring (204) being sleeved and mounted on the annular groove (212), and two sets of side protrusions (205) being mounted on the movable ring (204); A connecting rod (206), the connecting rod (206) being connected between the two groups of side protrusions (205), and a rotating shaft (207) being movably sleeved on the connecting rod (206); a clamp (211), the clamp (211) being mounted on one end of the rotating shaft (207); A clamping assembly (3) is mounted on the pressure rod (208), and the clamping assembly (3) comprises an upper clamping block (301) and a lower clamping block (302) for clamping parts.
2. A parts processing fixture according to claim 1, characterized in that: An elastic pad is provided at the contact position between the clamp (211) and the pressure rod (208).
3. A parts processing fixture according to claim 2, characterized in that: An open side groove (209) adapted to the diameter of the rotating shaft (207) is formed at one end of the pressure rod (208), and an anti-slip pad is provided at the contact position between the rotating shaft (207) and the open side groove (209).
4. A parts processing fixture according to claim 3, characterized in that: The upper clamping block (301) is mounted on the pressure rod (208), the upper clamping block (301) has a fixing sleeve, and the lower clamping block (302) is mounted on the workbench (103).
5. A parts processing fixture according to claim 4, characterized in that: The upper clamping block (301) and the lower clamping block (302) both have right-angle clamping grooves (303).
6. A parts processing fixture according to claim 5, characterized in that: Silicone pads are provided at the contact positions of the upper clamping block (301) and the lower clamping block (302) with the aviation shaft parts.
Citation Information
Patent Citations
Fixing tool for long-shaft part machining
CN219837683U