Embodiments of the disclosure relate generally to devices for removing drill bits from a workpiece and more particularly to a system employing an inner element to engage the drill bit and having an externally threaded portion engaged by inner thread on an outer element adapted to engage a surface of the workpiece whereby rotation of the inner element within the outer element withdraws the inner element and bit from the workpiece.
Drill bits may bind within a drill bore in a workpiece. This may be due to the bit dulling, removed material clogging the hole, or other situations. The drill motor can be run in reverse to back the drill bit out, but this may not work for very stuck drill bits (especially, where the removed material jams the flutes of the drill bit). A prying device, such as a claw hammer or pry bar, can be used to pull the drill bit from the workpiece, but these devices pull the drill bit off center during removal, which may damage or alter the hole or workpiece or break the drill bit off in the workpiece. Often, attempted extraction with the drill motor or other machine tool may fracture the bit or damage the workpiece. The bit may become stuck at any depth which complicates removal since a normal collet attachment to the bit requires attachment proximate the end of the shaft which may be spaced from the workpiece allowing undesirable bending torque to be exerted on the bit increasing the likelihood of fracturing the bit.
Several known tools pull a drill bit or similar element out of a workpiece on center with the hole. However, these tools include jaws that are tightened on to the drill bit by using screws through a portion of the jaws. These screws may be difficult to access depending on where the drill bit is or may be time consuming to tighten and loosen. Further, the tools are fairly complicated because they include several different components that need to work together to attach to the drill bit and to pull the drill bit from the workpiece.
Embodiments disclosed herein provide a bit puller incorporating an inner element with a longitudinal axis and having a central shaft, a base with external threads and an engagement mechanism internal to the inner element adapted to engage a drill bit. An outer element is concentric with the inner element and has a foot portion for engaging a work piece. Internal threads in the outer element are adapted to engage the external threads of the base wherein rotation of the inner element with respect to the outer element withdraws the inner element along the longitudinal axis.
The embodiments allow a method for extraction of a drill bit wherein a drill bit is engaged in an attachment mechanism internal to an inner element. An outer element having internal threads is received on external threads on the inner element. The inner element is then rotated with respect to the outer element urging a foot portion of the outer element into contact with a workpiece and withdrawing the inner element on a longitudinal axis thereby extracting the drill bit.
The features, functions, and advantages that have been discussed can be achieved independently in various embodiments of the present disclosure or may be combined in yet other embodiments, further details of which can be seen with reference to the following description and drawings.
The embodiments described herein provide a method and tool for operation to allow removal of drill bits, which may engage the bit at any drill depth. Further, the system is self-engaging for ease in removing the bit.
Embodiments disclosed herein provide a bit puller having an inner element adapted to engage the drill bit and having an external threaded surface. The inner element includes a drive connection for rotation of the inner element. An outer element has an internal thread adapted to concentrically engage the external threaded surface of the inner element at an adjustable height whereby the drill bit may be engaged by the inner element at any depth of penetration at which binding has occurred. The outer element has a foot portion engaging the workpiece concentrically surrounding the drill bit. Rotation of the inner element with the drive connection rotates the outer threads of the inner element within the inner threads of the outer element to withdraw the inner element through the outer element thereby drawing the bit engaged by the inner element from the workpiece. While the embodiments are described herein with respect to removal of a binding drill bit, the structure of the embodiments may be employed for removal of other machine tools or implements which may extend from a workpiece such as end mills, press fit shafts, or even nails.
Referring to the drawings, a first embodiment of a bit puller 110 is shown in
Base 114 additionally has an external thread 118. Outer element 126 is concentrically received over the inner element 112 and has an inner thread 128 which is adapted to engage the external thread 118 on the base 114. Outer element 126 is a hollow cylinder or partial cylinder bifurcated into two sections 130a, 130b which are attached with a longitudinal hinge 132 (parallel to the longitudinal axis 119) at mating first edges 134a and 134b of each section. Hinge 132 allows the two sections 130a and 130b to be opened to a first position as seen in
Upon closing the outer element 126 to a closed position, the inner thread 128 engages the external thread 118. Rotation of the inner element 112 drives external thread 118 within inner thread 128 to longitudinally withdraw the inner element 112 away from the workpiece along the longitudinal axis 119 thereby exerting force on the bit to withdraw the bit from the workpiece. The pitch direction of outer thread 118 and inner thread 128 may be selected to either rotate the base 114 in a driving direction for the bit or a reversing direction.
For the embodiment shown, lever arms 140a and 140b extend from the sections 130a and 130b for assistance in rotation of the section on the hinge 132. When sections 130a and 130b are rotated to a closed position, lever arms 140a and 140b are brought into alignment and may be held closed or a locking mechanism such as a U clamp 142 received over the aligned lever arms 140a, 140b may be employed to lock the sections 130a, 130b in the closed position. For the embodiment shown, free edges 144a and 144b of the sections 130a and 130b are separated by a gap 146 as seen in
In operation, the base 114 of the inner element 112 is inserted onto the bit 124 receiving the bit with the internal attachment mechanism 120 engaging the mating attachment mechanism 122. The outer element 126 is opened by rotating sections 130a and 130b on hinge 132 as seen in
An enhanced embodiment is shown in
The inner element 210 further includes a base, such as a collar 228 positioned concentrically with the central shaft 212 at the lower end 215. The collar 228 includes outer threads 230. The tool further includes an outer element 232 having inner threads 234 that mate with outer threads 230 of collar 228 the inner element 210. The complimentary threads 226 of the grip 224, tapered threads 222 of the central shaft 212, outer threads 230 of the collar 228, and inner threads 234 of the outer element 232 are configured with pitch direction selected to allow rotation of the grip 224 in a single direction to clamp the cavity 214 of the central shaft 212 onto the bit 221 and to rotate the inner element 210 respective to the outer element 232 urging the inner element upward from a workpiece 235 to pull the bit from the workpiece. The outer element 232 includes a foot portion 236 configured to contact and push against the workpiece as the inner element 210 is rotated.
In operation of the enhanced embodiment, the inner element 210 is placed over the bit 221 with the bit 221 extending into the central cavity 214, as seen in
A method for extraction of a binding drill bit employing the embodiments disclosed is shown in
Embodiments of the disclosure may be employed in the context of an aircraft manufacturing and service method 400 (method 400) as shown in
Each of the processes of method 400 may be performed or carried out by a system integrator, a third party, and/or an operator (e.g., a customer). For the purposes of this description, a system integrator may include without limitation any number of aircraft manufacturers and major-system subcontractors; a third party may include without limitation any number of venders, subcontractors, and suppliers; and an operator may be without limitation an airline, leasing company, military entity, service organization, and the like.
As shown in
Apparatus and methods embodied herein and previously described may be employed during any one or more of the stages of the production and service method 400. For example, components or subassemblies corresponding to production process 408 may be fabricated or manufactured in a manner similar to components or subassemblies produced while the aircraft 500 is in service. In addition, one or more apparatus embodiments as described herein, method embodiments described herein, or a combination thereof may be utilized during the production stages 408 and 410, for example, by substantially expediting assembly of or reducing the cost of an aircraft 500. Similarly, one or more of apparatus embodiments, method embodiments, or a combination thereof may be utilized while the aircraft 500 is in service, for example and without limitation, to maintenance and service 416.
Having now described various embodiments of the disclosure in detail as required by the patent statutes, those skilled in the art will recognize modifications and substitutions to the specific embodiments disclosed herein. Such modifications are within the scope and intent of the present disclosure as defined in the following claims.
This application is a divisional of U.S. application Ser. No. 15/055,988 filed on Feb. 29, 2016, now U.S. Pat. No. 10,688,638 issued on Jun. 23, 2020, having a common assignee with the present application, the disclosure of which is incorporated herein by reference.
Number | Name | Date | Kind |
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965054 | Weekes | Jul 1910 | A |
3727491 | Buckwalter | Apr 1973 | A |
6435782 | Hillhouse | Aug 2002 | B1 |
Number | Date | Country | |
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20200139526 A1 | May 2020 | US |
Number | Date | Country | |
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Parent | 15055988 | Feb 2016 | US |
Child | 16734326 | US |