The present invention relates generally to impact tools. More particularly, the present invention relates to torque-limited impact tool.
An impact wrench is one illustrative embodiment of an impact tool, which may be used to install and remove threaded fasteners. An impact wrench generally includes a motor coupled to an impact mechanism that converts the torque of the motor into a series of powerful rotary blows directed from a hammer to an output shaft called an anvil.
According to one aspect of the present disclosure, an impact tool may comprise a shaft adapted to rotate about an axis, the shaft having a first helical groove, a hammer having a second helical groove and a hammer jaw with an obtuse impact surface, a ball received in the first and second helical grooves, wherein the ball rotationally couples the hammer to the shaft and permits axial travel of the hammer relative to the shaft, and an anvil having an anvil jaw with an acute impact surface, wherein the obtuse impact surface of the hammer jaw is adapted to impact the acute impact surface of the anvil jaw when the shaft rotates in a first direction.
In some embodiments, the hammer jaw may include a forward impact face having a hammer lug extending outwardly from the forward impact face, the obtuse impact surface forming an edge of the hammer lug. The obtuse impact surface may be disposed at an obtuse angle with respect to the forward impact face. The obtuse angle may be greater than 90 degrees and less than 180 degrees. The obtuse angle may be greater than 105 degrees and less than 165 degrees.
In some embodiments, the anvil jaw may include a central section and an anvil lug extending outwardly from the central section, the acute impact surface forming an edge of the anvil lug. The central section and the anvil lug may form a rearward impact face of the anvil jaw, and the acute impact surface may be disposed at an acute angle with respect to the rearward impact face. The acute angle may be greater than 0 degrees and less than 90 degrees. The acute angle may be greater than 15 degrees and less than 75 degrees.
In some embodiments, the hammer lug may include a first vertical impact surface and the anvil lug may include a second vertical impact surface, the first vertical impact surface being adapted to impact the second vertical impact when the shaft rotates in a second direction. A sum of the obtuse and acute angles may be about 180 degrees.
According to another aspect of the present disclosure, an impact tool may include a hammer configured to selectively rotate in a first direction and in a second direction opposite the first direction, the hammer including a hammer jaw with a forward impact face, an anvil including an output shaft and an anvil jaw with a rearward impact face, a spring biasing the hammer toward a first position in which the forward impact face of the hammer jaw is in contact with the rearward impact face of the anvil jaw, and a cam configured to push the hammer at predetermined rotational intervals to a second position in which the forward impact face of the hammer jaw is out of contact with the rearward impact face of the anvil jaw. The hammer jaw may include a hammer lug having an obtuse impact surface disposed at an obtuse angle with respect to the forward impact face of the hammer jaw, and the anvil jaw may include an anvil lug having an acute impact surface disposed at an acute angle with respect to the rearward impact face of the anvil jaw.
In some embodiments, the obtuse angle may be greater than 105 degrees and less than 165 degrees. The acute angle may be greater than 15 degrees and less than 75 degrees. A sum of the obtuse and acute angles may be about 180 degrees.
In some embodiments, the obtuse impact surface of the hammer lug may be adapted to impact the acute impact surface of the anvil lug when the hammer rotates in the first direction. The hammer lug may further include a first vertical impact surface and the anvil lug may further include a second vertical impact surface, the first vertical impact surface being adapted to impact the second vertical impact when the hammer rotates in the second direction.
According to yet another aspect of the present disclosure, a method of operating an impact tool may include rotating a shaft of the impact tool about an axis in a first direction and pushing a hammer coupled to the shaft against an anvil at predetermined rotational intervals such that a first impact surface of the hammer contacts a second impact surface of the anvil, the first impact surface being disposed at an angle of greater than 90 degrees and less than 180 degrees with respect to the axis and the second impact surface being disposed at an angle greater than 0 degrees and less than 90 degrees with respect to the axis.
In some embodiments, the method may further include rotating the shaft about the axis in a second direction opposite the first direction and pushing the hammer against the anvil at predetermined rotational intervals such that a third impact surface of the hammer contacts a fourth impact surface of the anvil, the third and fourth impact surfaces being disposed parallel to the axis.
In some embodiments, angle at which the first impact surface is disposed with respect to the axis may be greater than 105 degrees and less than 165 degrees. The angle at which the second impact surface is disposed with respect to the axis may be greater than 15 degrees and less than 75 degrees. A sum of the angle at which the first impact surface is disposed with respect to the axis and the angle at which the second impact surface is disposed with respect to the axis may be about 180 degrees.
The concepts described in the present disclosure are illustrated by way of example and not by way of limitation in the accompanying figures. For simplicity and clarity of illustration, elements illustrated in the figures are not necessarily drawn to scale. For example, the dimensions of some elements may be exaggerated relative to other elements for clarity. Further, where considered appropriate, reference labels have been repeated among the figures to indicate corresponding or analogous elements.
While the concepts of the present disclosure are susceptible to various modifications and alternative forms, specific exemplary embodiments thereof have been shown by way of example in the figures and will herein be described in detail. It should be understood, however, that there is no intent to limit the concepts of the present disclosure to the particular forms disclosed, but on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the present disclosure.
One illustrative embodiment of an torque-limited impact tool 10 is depicted in
The impact mechanism 14 of the impact tool 10 is of the type commonly known as a ball-and-cam impact mechanism. U.S. Pat. No. 2,160,150 to Emerson et al., the entire disclosure of which is hereby incorporated by reference, describes at least one embodiment of such a ball-and-cam impact mechanism. Other illustrative embodiments of ball-and-cam impact mechanisms are described in U.S. Pat. No. 7,673,702 to Johnson et al., the entire disclosure of which is hereby incorporated by reference.
Referring now to
The cam shaft 22 includes a pair of helical grooves 50, and the hammer 28 includes two helical grooves 52. The hammer grooves 52 have open ends facing the anvil 30 for ease of machining and assembly. Thus, as best seen in
A spring 62 and a washer 64 are disposed between the planetary gear carrier 40 and the hammer 28 to bias the hammer 28 away from the planetary gear carrier 40. The washer 64 and an end portion of the spring 62 are received within the annular recess 46 in the hammer 28 and abut the bearing 24.
A cylindrical flange 66 extends forward from the planetary gear carrier 40 for aligning the spring 62 between the planetary gear carrier 40 and the hammer 28. The cylindrical flange 66 may include blind holes 68 for receiving the pins 44 extending through the planetary gear carrier 40. While the cylindrical flange 66 is shown as being integral with the planetary gear carrier 40, the cylindrical flange 66 may be a separate piece sandwiched between the planetary gear carrier 40 and the spring 62.
A flexible O-ring 69 and a retaining ring 71 are disposed over an end of the output shaft 16 to aid in holding the output shaft 16 within a socket of a tool to be attached to the output shaft 16. While the output shaft 16 is shown as being a square drive output shaft, the principles of the present disclosure may be used with any suitable output shaft.
Referring to
The obtuse impact surface 78 is disposed at an obtuse angle A1 with respect to the impact face 72. In some illustrative embodiments, the angle A1 is greater than 90 degrees and less than 180 degrees. In further illustrative embodiments, the angle A1 is between about 105 degrees and about 165 degrees. In still further illustrative embodiments, the angle A1 is between about 120 degrees and about 150 degrees. The obtuse impact surface 78 is also disposed at an obtuse angle A2 with respect to the longitudinal axis 32 (or an axis parallel to the longitudinal axis 32). In some illustrative embodiments, the angle A2 is greater than 90 degrees and less than 180 degrees. In further illustrative embodiments, the angle A2 is between about 105 degrees and about 165 degrees. In still further illustrative embodiments, the angle A2 is between about 120 degrees and about 150 degrees.
As best seen in
The acute impact surface 98 is disposed at an angle A3 with respect to the rearward impact face 96. In some illustrative embodiments, the angle A3 is greater than 0 degrees less than 90 degrees. In further illustrative embodiments, the angle A3 is between about 15 degrees and about 75 degrees. In still further illustrative embodiments, the angle A3 is between about 30 degrees and about 60 degrees. The acute impact surface 98 is also disposed at an acute angle A4 with respect to the longitudinal axis 32 (or an axis parallel to the longitudinal axis 32). In some illustrative embodiments, the angle A4 is greater than 0 degrees less than 90 degrees. In further illustrative embodiments, the angle A4 is between about 15 degrees and about 75 degrees. In still further illustrative embodiments, the angle A4 is between about 30 degrees and about 60 degrees.
To assemble the impact mechanism 14, the spring 62 and the washer 64 are inserted over the cam shaft 22. The bearing 24 is placed within the annular recess 46 and the hammer 28 is inserted over the cam shaft 22 to receive the washer 64 and an end portion of the spring 62 within the annular recess 46. Next, the hammer 28 is moved toward the cylindrical flange 66 against the force of the spring 62. As the hammer 28 moves axially towards the cylindrical flange 66, there is a clearance between the cam shaft 22 and the hammer 28 at the hammer grooves 52, so that the cam shaft grooves 50 are exposed. This clearance is provided by the open end of the hammer grooves 52, and is slightly greater than a diameter of the ball bearings 60. One ball bearing 60 is inserted into each of the grooves 52 of the hammer 28 and a corresponding cam shaft groove 50, and the hammer 28 is released. The biasing force of the spring 62 forces the hammer 28 away from the cylindrical flange 66. The forward-facing wall 52a of the hammer groove 52 presses against a rearward portion of the ball bearings 60. This presses a forward portion of the ball bearings 60 against the rearward-facing surface 50b of the cam shaft groove 50. The ball bearings 60 are thereby trapped between the cam shaft 22 and the hammer 28, and couple the hammer 28 to the cam shaft 22. The cam shaft grooves 50 need not be aligned with the hammer grooves 52 to permit installation. Rather, as the hammer 28 moves away from the cam shaft 22 when released, the hammer 28 rotates slightly over the ball bearings 60 to align the hammer grooves 52 with the cam shaft grooves 50 in a neutral position.
The impact mechanism 14 may further include an axial stop for limiting axial displacement of the hammer 28 towards the rear end 20. The axial stop may include a first stop member 120 formed by the cylindrical flange 66 (or on another, separate piece disposed adjacent the planetary gear carrier 40) facing the hammer 28 and a pair of opposing second stop members 122 on the hammer 28 facing the cylindrical flange 66. In the illustrative embodiment, the stop members 120, 122 are a flange and bosses, respectively. In other embodiments (not shown), the stop members 120, 122 may have different shapes.
In operation, the motor 12 drives rotation of the cam shaft 22 about the longitudinal axis 32. During nut rundown, (i.e., when rotation of the anvil 30 is not significantly opposed), the hammer 28 rotates with the cam shaft 22 over the bearing 24. Rotational torque is transferred from the cam shaft 22 to the hammer 28 through the impact bearing 26. The hammer lugs 74 cooperate with the anvil lugs 94 to drive rotation of the anvil 30 and thereby the output shaft 16.
The motor 12 and the impact mechanism 14, which includes the hammer 28 and the anvil 30, are adapted to rotate the output shaft 16 in both clockwise and counterclockwise directions, for tightening or loosening various fasteners.
The obtuse impact surfaces 78 of the lugs 74 of the hammer jaw 70 are configured to impact the acute impact surfaces 98 of the lugs 94 of the anvil jaw 90. In one illustrative embodiment, the angles A1 and A3 formed by the obtuse and acute impact surfaces 78, 98, respectively, with respect to the forward impact and rearward impact faces 72, 96 total about 180 degrees. Similarly, the angles A2 and A4 formed by the obtuse and acute impact surfaces 78, 98, respectively, with respect to the longitudinal axis 32 may total about 180 degrees. In other embodiments, the angles A1 and A3 and/or the angles A2 and A4 may total other than 180 degrees. The obtuse impact surfaces 78 of the hammer 28 and the acute impact surfaces 98 of the anvil 30 provide a torque-limiting feature for the impact tool 10. In particular, in a first direction (for example the clockwise direction), the impact of the obtuse impact surfaces 78 of the lugs 74 of the hammer 28 upon the acute impact surfaces 98 of the lugs 94 of the anvil jaw 90 limit the amount of energy that can be transferred from the hammer 28 into the anvil 30, thus reducing output torque of the impact tool 10. This limits torque, for example, during tightening or fastening, thus preventing over-tightening of fasteners.
In a second direction opposite the first direction (for example the counterclockwise direction), the generally vertical impact surfaces 80 of the lugs 74 of the hammer jaw 70 impact the generally vertical impact surfaces 102 of the lugs 94 of the anvil jaw 90. The generally vertical orientation of the vertical impact surfaces 80, 102, would allow for high torque output, for example, during removal of fasteners.
Each of the lugs 74, 94 of the hammer and the anvil jaws 70, 90, respectively, as described in detail above, are asymmetrical in the illustrative embodiment. In this manner, the hammer and anvil jaws 70, 90 provide different torque outputs in the clockwise and counterclockwise directions. In other illustrative embodiments, the obtuse and acute impact surfaces 78, 98 may be switched with the generally vertical impact surfaces 80, 102, respectively, for some applications.
While certain illustrative embodiments have been described in detail in the figures and the foregoing description, such an illustration and description is to be considered as exemplary and not restrictive in character, it being understood that only illustrative embodiments have been shown and described and that all changes and modifications that come within the spirit of the disclosure are desired to be protected. There are a plurality of advantages of the present disclosure arising from the various features of the apparatus, systems, and methods described herein. It will be noted that alternative embodiments of the apparatus, systems, and methods of the present disclosure may not include all of the features described yet still benefit from at least some of the advantages of such features. Those of ordinary skill in the art may readily devise their own implementations of the apparatus, systems, and methods that incorporate one or more of the features of the present disclosure.
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Chinese Office Action and English Translation for Chinese Patent Application No. 201310681033.2, dated May 7, 2015. |
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