The present disclosure relates power tools, and more particularly to impact tools, such as impact drivers and impact wrenches.
Impact tools typically include an impact mechanism with a camshaft, a hammer, and an anvil. The hammer is typically biased toward the anvil by a coil spring. During operation, the hammer may move away from the anvil along the camshaft, compressing and storing energy in the coil spring. This energy is then released, propelling the anvil back toward the anvil while rotating the hammer about the camshaft. The amount of impact energy imparted from the hammer to the anvil is dependent upon the amount of energy that can be stored in the coil spring, which is in turn dependent upon the spring constant and compressible length of the coil spring.
Embodiments described herein relate to an impact power tool including a housing, a motor disposed within the housing, a gear assembly disposed within the housing, and an impact mechanism disposed within the housing. The gear assembly driven by an output of the motor. The impact mechanism is driven by an output of the gear assembly. The impact mechanism includes a camshaft coupled to the output of the gear assembly, an anvil rotatably supported by the housing, a hammer coupled to the camshaft, and a chamber surrounding the camshaft. The camshaft is configured to rotate about a rotational axis. The anvil includes a drive portion able to receive a tool bit. The hammer is configured to rotate about the rotational axis and move axially along the camshaft to selectively apply rotational impacts to the anvil. The hammer is configured to move in a first direction away from the anvil in response to an axial force along the rotational axis. The chamber is filled with a compressible fluid. The hammer is configured to compress the compressible fluid as the hammer moves in the first direction. The compressible fluid applies a biasing force against the hammer in a second direction opposite to the first direction in response to the hammer reaching a maximum axial displacement from the anvil.
Embodiments described herein relate to an impact power tool including a housing including a sealed region filled with a compressible fluid, a motor disposed within the housing, a gear assembly disposed within the housing, an impact mechanism disposed within the housing. The gear assembly driven by an output of the motor. The impact mechanism driven an output of the gear assembly. The impact assembly includes a camshaft coupled to the output of the gear assembly, an anvil rotatably supported by the housing, and a hammer coupled to the camshaft. The camshaft configured to rotate about a rotational axis. The anvil includes a drive portion able to receive a tool bit. The hammer configured to rotate about the rotational axis and move axially along the camshaft to selectively apply rotational impacts to the anvil. The hammer is configured to move in a first direction away from the anvil in response to an axial force along the rotational axis. The hammer is also configured to compress the compressible fluid in the sealed region of the housing as the hammer moves in the first direction. The compressible fluid applies a biasing force against the hammer in a second direction opposite to the first direction in response to the hammer reaching a maximum axial displacement from the anvil.
Other features and aspects of the disclosure will become apparent by consideration of the following detailed description and accompanying drawings.
Before any embodiments of the disclosure are explained in detail, it is to be understood that the disclosure is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The disclosure is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting.
The housing 14 includes a head housing portion 22 and a handle portion 26 extending downwardly from the head housing portion 22. In the illustrated embodiment, the handle portion 26 is covered or surrounded by a grip portion 27. The illustrated housing 14 further includes an end cap 30 coupled to a rear portion of the head housing portion 22 (e.g., by a second plurality of fasteners 31). In the illustrated embodiment, the end cap 30 spans across both of the clamshell halves 18a, 18b. In other embodiments, the end cap 30 may be integrally formed with the head housing portion 22, such that the head housing portion 22 is defined entirely by the clamshell halves 18a, 18b.
The power tool 10 further includes a battery 34 removably coupled to a battery receptacle 38 located at a bottom end or foot 40 of the handle portion 26 (
The gear assembly 46 and impact mechanism 50 will now be described with reference to
The planet gears 58 are coupled to a camshaft 64 of the impact mechanism 50 such that the camshaft 64 acts as a planet carrier. Accordingly, rotation of the output shaft 52 rotates the planet gear 58, which then advance along the inner circumference of the ring gear 60 and thereby rotate the camshaft 64. The impact mechanism 50 further includes a hammer 68 supported on and axially slidable relative to the camshaft 64. The hammer 68 is coupled to the camshaft 64 via ball bearings (not shown) positioned within cooperating, generally helical grooves formed in the hammer 68 and camshaft 64. This connection causes the hammer 68 to move axially along the camshaft 64 in response to relative rotation between the camshaft 64 and the hammer 68.
With continued reference to
The hammer 68 is configured to reciprocate axially along the camshaft 64 to deliver rotational impacts to the anvil 72 and thereby rotate the tool bit. The chamber 70 acts as a gas-spring to store potential energy as the hammer 68 moves in a first direction (i.e., away from the anvil 72) and to release the stored energy as kinetic energy, propelling the hammer 68 forward (i.e., in a second direction toward the anvil 72) to deliver a rotational impact to the anvil 72.
In the illustrated embodiment, the seal 71, which may be an elastomeric seal, such as an O-ring, is carried by the hammer 68 to seal between the hammer 68 and the wall 73 of the chamber 70. The elastomeric or other suitable form of seal may also be integrated into the wall of the chamber 70 in other embodiments. An additional seal (not shown) may be provided between the hammer 68 and the camshaft 64. Thus, as the hammer 68 moves in the first direction, the effective volume of the chamber 70 is decreased, and a compressible fluid in the chamber 70 (e.g., air, nitrogen, or any other compressible fluid) is compressed. The elevated pressure of the compressible fluid acts on the rear face 69 of the hammer 68 to exert a biasing or restoring force on the hammer 68. This restoring force propels the hammer 68 back toward the anvil 72 as the gas in the chamber 70 expands.
Also in the illustrated embodiment, the chamber 70 may include vents 74 to allow air to flow into and out of the chamber 70. The vents 74 fluidly connect the gas chamber 70 with atmospheric conditions of the environment and are positioned circumferentially on an outer surface of the chamber 70. As the hammer 68 moves in the first direction (i.e., away from the anvil 72), the rear face 69 of the hammer 68 may block the vents 74 and seal the chamber 70 with the seal 71. When the hammer 68 moves in the second direction, the rear face 69 of the hammer 68 may clear the vents 74 as the hammer 68 reaches the anvil 72 to reestablish communication between the chamber 70 and the atmosphere. In other embodiments, the vents 74 may be omitted, such that the chamber 70 remains sealed.
In some embodiments, a mechanical spring (e.g., a coil spring) may also be provided within the chamber 70 or any other suitable region of the impact tool 10 to supplement the restoring force of the gas-spring. The camshaft 64 extends through the chamber 70 in the illustrated embodiment; however, the chamber 70 be located elsewhere in other embodiments. In such embodiments, the hammer 68 may be coupled to a piston (via a mechanical connection or a fluid connection) to cause a piston to move within the chamber 70 and compress gas within the chamber 70.
In operation, lugs on the hammer 68 are configured to engage corresponding lugs on the anvil 72, so that the camshaft 64, hammer 68, and anvil 72 may all rotate together. However, when a reaction torque on the anvil 72 exceeds a predetermined limit, the anvil 72 and hammer 68 will stop rotating, while the camshaft 64 continues to rotate. The relative rotation between the camshaft 64 and the hammer 68 causes the hammer 68 to start retracting away from the anvil 72 in the first direction. As the hammer 68 moves in the first direction, the rear face 69 of the hammer 68 moves further into the chamber 70 and compresses the gas inside the chamber 70, which may initially be at atmospheric pressure or at a pressure above atmospheric pressure.
The hammer 68 continues to move away from the anvil 72 until it reaches a maximum axial displacement from the anvil 72 at which point the lugs on the hammer 68 clear the lugs on the anvil 72, releasing the hammer 68 and allowing it to rotate. The pressure in the chamber 70 is at its maximum when the hammer 68 is in its rearmost position, thus storing the maximum potential energy when the tool is performing its highest demanding applications. The elevated pressure of the compressed gas acts on the rear face 69 of the hammer 68 to exert a biasing or restoring force on the hammer 68. Once the hammer lugs have cleared the anvil lugs and the hammer 68 is free to rotate, the restoring force from the compressed gas propels the hammer 68 back toward the anvil 72 as the gas in the chamber 70 expands. The hammer 68 rotates as it moves along the camshaft 64, such that the hammer 68 may deliver a rotational impact to the anvil 72 and apply torque to a workpiece. Once the anvil 72 has been impacted, rotation of the hammer and anvil 72 may stop again, and the process repeats.
In operation, lugs on the hammer 168 are configured to engage corresponding lugs on the anvil 172, so that the camshaft 164, hammer 168, and anvil 172 may all rotate together. However, when a reaction torque on the anvil 172 exceeds a predetermined limit, the anvil 172 and hammer 168 will stop rotating, while the camshaft 164 continues to rotate. The relative rotation between the camshaft 164 and the hammer 168 causes the hammer 168 to start retracting away from the anvil 172 in the first direction. As the hammer 168 moves in the first direction, a rear face 169 of the hammer 168 compresses the compressible fluid inside the sealed portion 176 of the head housing portion 122, which may initially be at atmospheric pressure or at a pressure above atmospheric pressure.
The hammer 168 continues to move away from the anvil 172 until the hammer 168 reaches a maximum axial displacement from the anvil 172. When the hammer 158 is at the maximum axial displacement from the anvil 172, the pressure in the sealed portion 176 is at a maximum, thus storing the maximum potential energy when the tool is performing its highest demanding applications. The elevated pressure of the compressed fluid acts on the rear face 169 of the hammer 168 to exert a biasing force on the hammer 168. Once the hammer lugs have cleared the anvil lugs and the hammer 168 is free to rotate, the restoring force from the compressed gas propels the hammer 168 back toward the anvil 172 as the compressible fluid in the sealed portion 176 expands. The hammer 168 rotates as it moves along the camshaft 164, such that the hammer 168 may deliver a rotational impact to the anvil 172 and apply torque to a workpiece. Once the anvil 172 has been impacted, rotation of the hammer and anvil 172 may stop again, and the process repeats.
Although the disclosure has been described in detail with reference to certain preferred embodiments, variations and modifications exist within the scope and spirit of one or more independent aspects of the disclosure as described.
Various features of the disclosure are set forth in the following claims.
This application claims priority to co-pending U.S. Provisional Patent Application No. 63/455,013 filed on Mar. 28, 2023, the entire contents of which are incorporated herein by reference.
Number | Date | Country | |
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63455013 | Mar 2023 | US |