Power tools are power tools configured to deliver a high torque output by storing energy in a rotating mass and delivering it suddenly through an output shaft to a fastener. In order to function properly, power tools may be regularly scheduled for maintenance.
The Detailed Description is described with reference to the accompanying figures. The use of the same reference numbers in different instances in the description and the figures may indicate similar or identical items.
Although the subject matter has been described in language specific to structural features and/or process operations, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms of implementing the claims.
Overview
Impact tools (e.g., impact wrenches, etc.) are designed to deliver a high torque output with minimal exertion by the user. Impact mechanisms include a rotating mass (e.g., a hammer) that stores energy in impact jaws. The impact jaws abruptly deliver the stored energy to an anvil connected to an output shaft, subjecting the anvil to repeated and sudden shock loading.
In order for an impact tool to operate optimally, the impact mechanism is lubricated. Lubricants may reduce the heat generated by the impact of the impact mechanism jaws to the anvil, or the wear of an impact bearing to a cam shaft and hammer of the impact mechanism by creating a film between the two impacting surfaces. The lubricant reduces friction and improves the efficiency and performance of the impact tool. This lubrication is typically, but not always, a specially formulated grease that is installed at the factory. Overtime this lubrication tends to break down or migrate away from the areas of impact and wear, resulting in a dry impact assembly condition. This dry impact assembly condition may lead to premature wearing of mechanism parts resulting in a performance reduction or in more severe cases a stalling, or a locking up, condition rendering the tool inoperable.
Impact tools may contain a grease fitting located either on the hammer case or at the rear of the tool for lubricating the impact mechanism. The downside of locating the grease fittings around the hammer case is that the injected grease lubricates the outside of the mechanism and not directly on the impact jaws where it is needed. Tools with rear grease ports tend to do a better job of getting the lubrication where at the impact jaws but require a rotor of the drive mechanism to have a through hole, which is not always feasible. For impact tools that do not contain a grease fitting, or the location in need of lubrication is too internal for the grease to migrate efficiently to this area, the tool must be disassembled to manually apply grease directly to the areas of stress and wear in the impact mechanism.
The impact tool described herein includes a front lubrication assembly that directs a lubricant injected from a front end of the impact tool directly into the main areas of stress in the impact mechanism (e.g., anvil jaws, hammer jaws, impact bearing, helical grooves, etc.) of the impact mechanism assembly. The front lubrication assembly includes a lubrication passage that extends through the anvil assembly and along an axis of rotation of the impact tool. The lubrication passage splits the flow of the lubricant into lubrication channels that extend away from the lubrication passage and deliver the lubricant flow to the areas of stress and wear in the impact mechanism.
The anvil assembly may be a split anvil assembly having an internal anvil portion fixed inside a housing of the impact tool and an external anvil portion outside the housing. The external anvil portion is removably connected to the internal anvil portion. The front lubrication assembly may be accessed when the external anvil portion is disengaged from the internal anvil portion and an inlet of the lubrication passage is accessible through an internal anvil portion cavity.
The external anvil portion may be selected from a plurality of replaceable anvil attachments, including but not limited to anvils with different drive sizes, socket extensions, custom sockets, etc. that are interchangeable without disassembling the impact tool.
Referring generally to
In embodiments, the drive mechanism 105 comprises a pneumatic (compressed air) motor powered by a source of compressed air (not shown). However, it is contemplated that the impact tool assembly 100 may also include an electric motor (not shown) powered by a power source such as a removable battery, an internal battery, or an external power source via an electric cord. In other embodiments, the impact tool assembly 100 may be hydraulically operated.
The hammer 106 includes at least one hammer jaw 112 extending radially from the axis 100A. The impact assembly 110 further includes an anvil assembly 115, for example, the one shown in
In example embodiments, the anvil assembly 115 may be a split anvil assembly. The split anvil assembly may include an external anvil portion 120 and an internal anvil portion 130, where the internal anvil portion 130 is fixed inside the hammercase 104 and the external anvil portion extends longitudinally from the front end 101 and is removably attached to the internal anvil portion 130. In this embodiment, the external anvil portion 120 extends longitudinally from the front end 101 outside of the hammercase 104 and the housing 102. The internal anvil portion 130 includes at least one anvil jaw 132 configured to be repeatedly struck by the at least one hammer jaw 112. As the hammer 106 continuously and intermittently impacts against the internal anvil portion 130 of the split anvil assembly 115, the external anvil portion 120 continuously rotates when the external anvil portion 120 is engaged and secured to the internal anvil portion 130. An output shaft 125 extends from the external anvil portion 120 and may receive a connector, a socket, or other device that engages a fastener (e.g., a bolt, a nut, a screw, etc.) to be tightened or loosened.
The impact tool assembly 100 includes a front lubrication assembly 140. The front lubrication assembly 140 includes a lubrication passage 141 defined through the anvil assembly 115 and extending axially along axis 100A. The front lubrication assembly 140 may include a grease fitting 145 having a ball 146 and a spring 148. In example embodiments, the ball 146 is pushed against the spring 148 by an outside pressure (e.g., a grease gun) and a lubricant is injected into the impact assembly 110. The lubricant injected by a user (e.g., grease) passes into a channel 147 of the grease fitting 145 and flows into the lubrication passage 141 and through at least one lubrication channel 142, and directly to the impact jaws (e.g., hammer jaw, anvil jaw) of the impact assembly 110. The at least one lubrication channel 142 extends away from the lubrication passage 141. For example, the at least one lubrication channel 142 may extend radially away from, or perpendicular to, the lubrication passage 141. In other embodiments (not shown) the at least one lubrication channel 142 may extend at an angle between zero degrees (0°) and ninety degrees (90°) with respect to the lubrication passage 141 or the axis 100A. The grease fitting 145 may be fixedly attached to the anvil assembly 115 by a tapered thread at the inlet of the lubrication passage 141, as a straight push-fit arrangement, or by another arrangement.
In example embodiments, the external anvil portion 120 defines an external anvil portion cavity 126 including a retaining cavity 128, and a retaining orifice 121. The external anvil portion cavity 126 houses a retaining pin 124. The retaining pin 124 is configured to engage with the access port 131 of the internal anvil portion 130, thereby effectively locking the external anvil portion 120 and the internal anvil portion 130. Upon retraction of the retaining pin 124, the external anvil portion 120 disengages with the internal anvil portion 130, exposing the internal anvil portion cavity 135.
The retaining cavity 128 houses a biasing member 122 that retains the retaining pin 124 within the retaining orifice 121. In embodiments, when the external anvil portion 120 is engaged with the internal anvil portion 130, the biasing member 122 biases the retaining pin 124 outward towards the access port 131 of the internal anvil portion 130, locking the two portions of the split anvil assembly 115 together. In order to separate the external anvil portion 120 and the internal anvil portion 130, the retaining pin 124 may be depressed with an elongated tool (not shown) until the retaining pin 124 is fully depressed out of the access port 131. The output shaft 125 of the split anvil assembly 115 can be replaced by inserting an appropriately sized elongated tool (e.g., a screwdriver) through the access port 131 and depressing the retaining pin 124.
It should be understood that other attachment methods may be used to retain the external anvil portion 120 into the internal anvil portion cavity 135. Other retaining assemblies may include, but are not limited to, actuation buttons to actuate the retaining pin 124, retaining caps, retaining rings, retractable ball detent mechanisms on at least one of the internal anvil portion and/or the external anvil portion, hog rings, among others.
In the embodiment shown in
Referring to
The cam shaft 150 and the hammer 106 each include a pair of opposed helical grooves 152 and 156, respectively. The hammer grooves 156 have open ends facing the anvil assembly 115. Thus, the cam shaft groove 152 is partially defined by a forward facing wall 152a and a rearward facing wall 152b, while the hammer groove 156 is partially defined by a forward facing wall 156a and lacks a rearward facing wall. A pair of balls 154b forming the impact bearing 154 couple the cam shaft 150 to the hammer 106. Each ball 154b is received in a race formed by the hammer groove 156 and the corresponding cam shaft groove 152.
A spring member 149 is disposed between the planetary gear carrier 153 and the hammer 106 to bias the hammer 106 away from the planetary gear carrier 153. A forward-facing end of the hammer 106 includes a pair of hammer jaws 112 for driving rotation of the anvil assembly 115. The anvil assembly 115 likewise includes a pair of anvil jaws 132 for cooperating with the hammer jaws 112.
The biasing force of the spring member 149 forces the hammer 106 away from the planetary gear carrier 153. The forward-facing wall 156a of the hammer groove 156 presses against a rearward portion of the balls 154. This presses a forward portion of the balls 154b against the rearward-facing surface 152b of the cam shaft groove 152. The balls 154b are thereby trapped between the cam shaft 150 and the hammer 106 and couple the hammer 106 to the cam shaft 150.
In this embodiment, the front lubrication assembly 140 includes the lubrication port inlet 144 defined on the internal anvil cavity wall 130a. The lubrication passage 141 extends to and through an anvil rear wall 130b, where the anvil rear wall 130b abuts with the cam shaft 150. A cam shaft passage 161 is located within the cam shaft 150. The cam shaft passage 161 is aligned with the lubrication passage 141 and may be parallel with the axis 100A. The cam shaft passage 161 may include at least one cam shaft channel 162 having a cam shaft channel outlet 163. The cam shaft channel 162 extends away from the cam shaft passage 161. For example, the cam shaft channel 162 may extend radially away from, or perpendicular to, the lubrication passage 141. In other embodiments (not shown) the at least one cam shaft channel 162 may extend at an angle between zero degrees (0°) and ninety degrees (90°) with respect to the cam shaft passage 141 or the axis 100A.
The lubrication assembly 140 delivers the lubricant injected into the grease fitting 145 to the impact assembly 110. In embodiments, the cam shaft channel outlet 163 is located proximate to or adjacent to the impact bearing 154. The lubricant flow exits the cam shaft channel outlet 163 and lubricates the impact bearing 154 and the opposing helical grooves, the cam shaft groove 152 and the hammer groove 156. Additionally, the axial repetitive motion of the hammer 106 with respect to the cam shaft 150 may also transport at least a portion of the lubricant flow to the at least one anvil jaw 132 and/or the at least one hammer jaw 112. In other embodiments, both the lubrication passage 141 and the cam shaft passage 161 include a lubrication channel 142 and a cam shaft channel 162 extending radially away from their respective passages.
In other embodiments, the split anvil assembly may define the front lubrication assembly 140 having the lubrication passage 141 extend along both the external anvil portion 120 and the internal anvil portion 130. The lubrication port inlet 144 may be defined on a frontal end 129 of the output shaft 125 of the external anvil portion 120. In this embodiment, a lubrication seal may be disposed between the external anvil portion 120 and the internal anvil portion 130.
The impact tool assembly 100 having a front lubrication port 145 may use interchangeable output shafts 125 having different drive diameters, extended anvils, or accessories such as socket extensions and socket adapters. For example, different embodiments of the anvil assembly 115 may have different sizes of output shaft 125. The output shaft 125 of anvil assembly 115 may range from one-quarter of an inch (¼ in.), to two and one-half inches (2-½ in.). For example, the output shaft may be sized for drive sizes of ¼ in., ⅜ in., ½ in., ¾ in., 1 in. 1-½ in., and 2-½ in. It should be understood that these drive sizes are examples and not limiting to any sizes in metric and/or U.S. units.
While the subject matter has been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only example embodiments have been shown and described and that all changes and modifications that come within the spirit of the subject matters are desired to be protected. In reading the claims, it is intended that when words such as “a,” “an,” “at least one,” or “one of a plurality of” are used there is no intention to limit the claim to only one item unless specifically stated to the contrary in the claim. Unless specified or limited otherwise, the terms “mounted” and “connected” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, and couplings. Further, “connected” is not restricted to physical or mechanical connections or couplings.
The present application claims priority under 35 U.S.C. § 119(e) of U.S. Provisional Application Ser. No. 63/404,063, filed Sep. 6, 2022, and titled “Impact Tool with Split Anvil and Lubrication Port”. U.S. Provisional Application Ser. No. 63/404,063 and the co-pending Non-Provisional application Ser. No. ------ titled “Impact Tool with Split Anvil,” dated Aug. 29, 2023, are incorporated by reference herein in their entireties.
Number | Date | Country | |
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63404063 | Sep 2022 | US |