ROTARY IMPACT ASSEMBLY STRUCTURE
20190202037 ยท 2019-07-04
Inventors
Cpc classification
B25B21/007
PERFORMING OPERATIONS; TRANSPORTING
B25B17/02
PERFORMING OPERATIONS; TRANSPORTING
B25B13/065
PERFORMING OPERATIONS; TRANSPORTING
B25B23/00
PERFORMING OPERATIONS; TRANSPORTING
B25B23/0035
PERFORMING OPERATIONS; TRANSPORTING
International classification
B25B21/00
PERFORMING OPERATIONS; TRANSPORTING
B25B17/02
PERFORMING OPERATIONS; TRANSPORTING
B25B19/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A rotary impact assembly structure includes a rotary tool and a rotary impact assembly. The rotary tool is assembled with the rotary impact assembly so that the rotary impact assembly is driven by the rotary tool to rotate. The rotary impact assembly has a counterweight plate. The counterweight plate has a first surface and a second surface at two sides thereof. The first surface is provided with a socket portion having an insertion hole at a center thereof. The second surface is provided with a plug portion at a center thereof. The rotary impact assembly structure is able to increase the rotational inertia and the amount of torque to quickly loosen or tighten a fastener and has a simple and convenient operation.
Claims
1. A rotary impact assembly structure, comprising a rotary tool and a rotary impact assembly, the rotary tool is assembled with the rotary impact assembly so that the rotary impact assembly is driven by the rotary tool to rotate, characterized by: the rotary impact assembly having a counterweight plate, the counterweight plate having a first surface and a second surface at two sides thereof, the first surface being provided with a socket portion having an insertion hole at a center thereof, the second surface being provided with a plug portion at a center thereof.
2. The rotary impact assembly structure as claimed in claim 1, wherein the first and second surfaces of the counterweight plate each have an annular recess.
3. The rotary impact assembly structure as claimed in claim 1, wherein the counterweight plate has a plurality of through holes.
4. The rotary impact assembly structure as claimed in claim 1, wherein the socket portion of the counterweight plate has a positioning assembly.
5. The rotary impact assembly structure as claimed in claim 1, wherein the plug portion of the counterweight plate has a positioning assembly.
6. The rotary impact assembly structure as claimed in claim 4, wherein the positioning assembly includes a spring and a steel ball.
7. The rotary impact assembly structure as claimed in claim 5, wherein the positioning assembly includes a spring and a steel ball.
8. The rotary impact assembly structure as claimed in claim 1, wherein the rotary tool is a pneumatic tool or an electric tool.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0015]
[0016]
[0017]
[0018]
[0019]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0020] Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings.
[0021] First of all, referring to
[0022] It should be noted that the rotary impact assembly A has a counterweight plate 20. The counterweight plate 20 has a first surface 21 and a second surface 22 at two sides thereof. The first surface 21 is provided with a socket portion 23 having an insertion hole 231 at a center thereof. The second surface 22 is provided with a plug portion 24 at a center thereof.
[0023] The first and second surfaces 21, 22 of the counterweight plate 20 each have an annular recess 25 at a predetermined position.
[0024] The counterweight plate 20 has a plurality of through holes 26.
[0025] The socket portion 23 of the counterweight plate 20 has a positioning assembly (not shown in the drawings) at a predetermined position.
[0026] The plug portion 24 of the counterweight plate 20 has a positioning assembly (not shown in the drawings) at a predetermined position.
[0027] The positioning assembly includes a spring and a steel ball (not shown).
[0028] The rotary tool 10 is a pneumatic tool or an electric tool.
[0029] As shown in
[0030] After that, a connecting socket 30 (shown in
[0031] It should be noted that in the present embodiment, the counterweight plate 20 has a diameter greater than that of the connecting socket 30, so the inertial gravitational acceleration is based on the counterweight plate 20. When the fastener is loosened or tightened, the torque or rotational speed of the rotary tool 10 will increase at a multiple of the diameter of the counterweight plate 20 and the connecting socket 30.
[0032] In addition, the counterweight plate 20 of the present invention can be matched with a plurality of connecting sockets 30 which may be in different sizes. It is convenient for use and can effectively reduce the purchase cost and is very practical.
[0033] Although particular embodiments of the present invention have been described in detail for purposes of illustration, various modifications and enhancements may be made without departing from the spirit and scope of the present invention. Accordingly, the present invention is not to be limited except as by the appended claims.