The present application claims priority to Japanese Application Number 2019-055574, filed Mar. 22, 2019, the disclosure of which is hereby incorporated by reference herein in its entirety.
The present invention relates to component fitting technology, and particularly relates to a component fitting structure and an automatic assembly system having a disengagement prevention function.
A component assembly utilizing a snap fit makes it possible to fit components to each other with ease without tools, and has been therefore widely adopted.
JP H9-280219 A discloses a one-touch joint in which a guide pin is inserted into a guide hole and expands a guide pin through-hole by overcoming a compression force of a ring spring that tightens a mating female member, and the mating female member is matedly locked with a locking step of the guide pin.
JP 2016-180489 A discloses a driving unit that includes a gear that is rotatably supported by a fixed shaft that is provided on a first base member protruding therefrom, and a second base member disposed opposing the first base member so as to cover the gear, in which the first base member is provided with a locking piece which locks the gear to prevent falling thereof and is locked to the second base member.
JP 2009-180323 A discloses a snap fit in which, in a snap fit in which snap pieces each having a leg portion and a locking head portion are disposed symmetrically with a deformation space interposed therebetween, a space expansion portion obtained by partially expanding the deformation space is provided on a tip part of the snap piece.
Component assembly that utilizes a snap fit has good assembly workability, but cannot fully fix a component unlike a component fitting by screwing or the like, and therefore, there is a risk that the snap fit may be disengaged when force is applied to the component.
Although there are various fitting methods in addition to the snap fit, as shown in a table below, assembly workability and engagement strength between components (structural strength) are in a trade-off relationship, and a component fitting structure that achieves both the assembly workability and the engagement strength between components is therefore desired. The assembly workability is an important viewpoint, particularly in automatic assembly by a robot.
Accordingly, an object of the present invention is to provide a component fitting technology provided with at least a disengagement prevention function.
One aspect of the present disclosure is to provide a component fitting structure including: a first component including an elastic column provided with an engaging piece; and a second component including a cutout capable of being engaged by the engaging piece, in which the engaging piece includes a first protrusion protruding laterally from the elastic column and a second protrusion protruding in a direction opposite to a protrusion direction of the first protrusion, and the cutout includes a first edge configured to oppose the first protrusion and a second edge configured to oppose a part of the second protrusion and open a remainder of the second protrusion, after the first component and the second component are fitted.
Embodiments of the present disclosure will be described in detail below with reference to the accompanying drawings. In each of the drawings, identical or similar constituent elements are given identical or similar reference signs. Additionally, the embodiments described below are not intended to limit the technical scope of the invention or the meaning of terms set forth in the claims.
As illustrated in
As illustrated in
As illustrated in
Furthermore, after assembly of the first component 12 and the second component 14, a gap S is desirably formed between the second protrusion 16 and the second edge 18. Although a portion where the engaging piece 10 is hooked is only the first edge 17 due to the gap S described above, since a moment caused by the second edge 18 does not act on the second protrusion 16, even if force acts in the direction in which the second component 14 is pulled out, the elastic column 11 does not tilt downward on a paper plane of
As illustrated in
In the above-described behavior of the component fitting structure at the time of component assembly, the operation is performed by one component being pushed into the other component using the tapered shape (i.e., first sliding surface 20 and second sliding surface 21) provided on the engaging piece 10. That is, when the components are pressed to each other, the snap fit automatically operates and an engaged state is obtained. Thus, according to the tapered shape as described above, the components can be assembled in the same manner as the related snap fit. Additionally, the component fitting structure of the present example can also be applied to an automatic assembly system provided with a robot that assembles the first component 12 and the second component 14.
According to the present embodiment, even if force acts in a direction in which the component is disengaged and the elastic column 11 tilts, the elastic column 11 hits the second edge 18, so that the engagement does not automatically disengage. In other words, since the second edge 18 plays the role of a stopper, the engagement strength between the components is improved.
Although some embodiments have been described in this specification, the present invention is not limited to the above-described embodiment, and it is to be understood that various changes can be made without departing from the scope of the appended claims.
Number | Date | Country | Kind |
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JP2019-055574 | Mar 2019 | JP | national |
Number | Name | Date | Kind |
---|---|---|---|
20120321379 | Wang | Dec 2012 | A1 |
20140298638 | Colombo | Oct 2014 | A1 |
20160236592 | Peniche | Aug 2016 | A1 |
20180180076 | Betancourt Santana | Jun 2018 | A1 |
20180209457 | Snoeyink | Jul 2018 | A1 |
20190072120 | Santillan Gutierrez | Mar 2019 | A1 |
Number | Date | Country |
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H1176987 | Dec 1989 | JP |
H88554 | Jan 1996 | JP |
H9-280219 | Oct 1997 | JP |
2004249378 | Sep 2004 | JP |
2009-180323 | Aug 2009 | JP |
2016-180489 | Oct 2016 | JP |
2016192493 | Nov 2016 | JP |
2017173701 | Sep 2017 | JP |
Number | Date | Country | |
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20200298353 A1 | Sep 2020 | US |