The present invention generally relates to threaded insert insertion tools and, more particularly, to a threaded insert installation tool for areas with limited access and to a method for installing threaded inserts in areas with limited access.
Threaded inserts, such as Heli-Coil® inserts (Heli-Coil® is a registered trademark of Emhart® Teknologies), provide positive means for protecting and strengthening all tapped threads. Threaded inserts are typically precision-formed screw thread coils of stainless steel wire having a diamond shaped cross-section. When the treaded inserts are installed into tapped holes, the threaded inserts provide permanent 60-degree internal screw threads that accommodate any standard bolt or screw. The threaded insert is typically larger in diameter than the tapped hole. During installation of the threaded insert with an installation tool, the installation tool applies torque to the insert reducing the diameter of the leading coil allowing the leading coil to enter the tapped hole. After installation, the threaded insert expands outwards with a spring force that permanently anchors the insert in place. When installed, a threaded insert provides a precision female thread of high surface finish and strength. Threaded inserts may increase the thread life of a tapped hole, especially in materials having a low hardness, such as aluminum, by eliminating the erosion of the thread due to friction. Furthermore, threaded inserts may make a tapped hole stronger by distributing the load applied to the threads by an inserted fastener evenly to each coil. Threaded inserts are typically available in two designs, the standard insert, which has a free-running thread, and the screw-lock insert, which provides a locking torque on the mating fastener using chord on one or more coils of the insert. Threaded inserts were invented in the late 1930's to provide a solution for the repair of aircraft engines. Currently, threaded inserts are used in automotive, communication, aerospace, military and defense industries. Presently, in many applications, for example in the aircraft industry, threaded inserts are part of the original design to prevent the need to repair threads of a tapped hole. Furthermore, the use of threaded inserts yields a much stronger assembly than a tapped hole of the parent material, for example, aluminum, could provide.
Installation of threaded inserts may be achieved with a driving tang, which is removed after assembly. To permit the removal of the tang, a notch is cut into the section of a threaded insert to provide a shear point. The driving tang is engaged in an abutment or slot of an insertion tool and prewound into a nozzle. After placing the insertion tool over the correctly tapped hole, further winding will install the threaded insert to the correct depth. After withdrawal of the insertion tool, the tang needs to be removed to allow a fastener, such as a bolt or screw, to pass through the insert. Threaded inserts may be installed into a tapped hole using an appropriate hand or power insertion tool. Hand tools are typically designed with a threaded mandrel and a driving contour that allows the correct and efficient installation of the threaded insert. Hand tools may be operated with an offset handle. Power tools typically consist of the same front-end assembly as manual operated insertion tools, which include a prewinder, a mandrel and spacers, an adapter, and a reversible motor. Existing hand and power insertion tools for threaded inserts may not be operable in tight spaces or spaces with limited access. For some applications, for example, for insertion of threaded inserts in a space having an extended depth and a close proximity to surrounding walls, such as inside a cylinder or a barrel, prior art insertion tools may be impractical. It may be necessary to remove the offset handle from a prior art manually operated insertion tool and to use an additional tool, such as a wrench, to operate the front-end assembly of the insertion tool.
Prior art threaded insert insertion tools include, for example, U.S. Pat. No. 6,000,114 issued to Newton et al. The insertion tool disclosed by Newton et al. may be used for insertion of a tang-free threaded coil insert into a threaded opening. The prior art insertion tool includes a blade, which is formed with a drive hook. Although the prior art insertion tool enables the insertion of a threaded coil insert fully within a threaded opening of a support structure such that the trailing end of the insert is flush with the external surface of the support structure adjacent to the opening, the insertion tool may not be suitable for insertion of threaded inserts in tight spaces and in close proximity to walls of a cylindrical structure.
As can be seen, there is a need for an installation tool for a threaded insert that may be used in tight spaces and spaces with limited access. Furthermore, there is a need for an installation tool that enables the insertion of a threaded insert into a tapped hole inside a barrel that extends for a length and that has a relatively small diameter.
There has, therefore, arisen a need to provide an installation tool for threaded inserts that may be used in areas with limited access. There has further arisen a need to provide an installation tool that may be power operated in areas with limited access. There has still further arisen a need for a method to install threaded fasteners in tight spaces where the tapped hole may be positioned in close proximity to a wall and at an extended depth.
The present invention provides a threaded insert installation tool that may be used in areas with limited access. The present invention provides a threaded installation tool that may be driven by a cordless screwdriver. The present invention provides a threaded installation tool that has an extended reach, and that can be operated within close wall clearance of a structure. The present invention provides a threaded insert installation tool that is suitable for, but not limited too, applications in the aircraft industry, both commercial and military, as well as in the defense industry as a whole.
In one aspect of the present invention, a threaded insert installation tool comprises an adapter assembly, and a front-end assembly. The adapter assembly includes a drive shaft that extends in longitudinal direction along an axis. The front-end assembly includes a mandrel that extends in longitudinal direction along the axis and that is in a rigid connection with the drive shaft.
In another aspect of the present invention, a threaded insert installation tool comprises a clamping ring, a bracket, a housing extending longitudinally along an axis from a back end to a front end, a drive shaft, and an internal assembly. The bracket is in a fixed connection with the clamping ring. The back end of the housing is connected with the bracket opposite from the clamping ring. The drive shaft extends longitudinally along the axis from a back end to a front end. The drive shaft is positioned within the housing. The drive shaft extends the housing into the clamping ring. The internal assembly is covered by the housing.
In a further aspect of the present invention, a method for installation of a threaded insert in an area with limited access comprises the steps of: connecting a front-end assembly with a driver using an adapter assembly to assemble a threaded insert installation tool; applying torque with the driver to the adapter assembly and the front-end assembly to pre-wind the threaded insert; placing the threaded insert installation tool over tapped hole; and applying torque to the adapter assembly and the front-end assembly with the driver to install the threaded insert. The tapped hole is positioned within a barrel at an extended length and in close proximity to a wall of the barrel.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following drawings, description and claims.
a is a side view of a drive shaft according to one embodiment of the present invention;
The following detailed description is of the best currently contemplated modes of carrying out the invention. The description is not to be taken in a limiting sense, but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.
Broadly, the present invention provides a threaded insert installation tool that may be used in areas with limited access and that is operated with a battery-powered screwdriver. An embodiment of the present invention provides a threaded insert installation tool that is suitable for, but not limited too, applications in the automotive, communication, aerospace, military and defense industries. The threaded insert installation tool as in one embodiment of the present invention may be used to install threaded inserts in tapped holes that are positioned in a space having an extended depth and a close proximity to surrounding walls, such as inside a cylinder or a barrel. The threaded insert installation tool as in one embodiment of the present invention may be used to install threaded inserts, for example, inside a missile shell.
In one embodiment, the present invention provides a threaded insert installation tool that may include an adapter assembly that connects a front-end assembly with a cordless screwdriver. By attaching the adapter assembly to the front-end assembly, an extended reach may be provided for the threaded insert installation tool as in one embodiment of the present invention compared to prior art insertion tools. Furthermore, by using the adapter assembly as in one embodiment of the present invention, a close wall clearance of the threaded insert application tool can be realized. A close wall clearance at an extended depth may not be realized with a prior art manual insertion tool for installation of threaded inserts since the prior art manual insertion tool typically includes an offset handle that is used to operate the prior art insertion tool. By attaching the cordless, battery-powered screwdriver to the end of the adapter assembly opposite from the front-end assembly, the operation of the threaded insert installation tool as in one embodiment of the present invention may be automated contrary to the manual operation of prior art insertion tools. Consequently, threaded inserts may be installed more rapidly using the battery-operated threaded insert installation tool as in one embodiment of the present invention compared to using a prior art manual operated insertion tool. Furthermore, the threaded insert installation tool as in one embodiment of the present invention has a more ergonomic design than prior art manual operated insertion tools. Still further, operating the threaded insert installation tool as in one embodiment of the present invention may be less tedious and less exhausting than operating a prior art manual insertion tool where the offset handle had to be removed due to space restrictions, and that needed to be driven with another tool, for example, a wrench.
In one embodiment, the present invention provides a sliding drive feature that may include a drive shaft that may have a square cross-section that may slide in linear direction within a square-hole sleeve converting the rotary motion provided by the cordless screwdriver into a linear feed, which is not possible using prior art insertion tools, where the mandrel is in a rigid connection with the offset handle. By providing the sliding drive feature of the threaded insert installation tool as in one embodiment of the present invention, it may be possible to match the pitch (threads per inch) of the threaded insert, which is not possible using a prior art insertion tool, where the mandrel is in a rigid connection with the drive.
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A first operation mode, where the mandrel 13 is retracted, is shown in
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It should be understood, of course, that the foregoing relates to exemplary embodiments of the invention and that modifications may be made without departing from the spirit and scope of the invention as set forth in the following claims.
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Number | Date | Country | |
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20060265857 A1 | Nov 2006 | US |