AIR CAVITY PACKAGE WITH IMPROVED CONNECTIONS BETWEEN COMPONENTS
20220051956 · 2022-02-17
Assignee
Inventors
Cpc classification
H01L23/3142
ELECTRICITY
H01L2924/00014
ELECTRICITY
H01L21/481
ELECTRICITY
H01L23/10
ELECTRICITY
H01L2924/00014
ELECTRICITY
International classification
H01L23/10
ELECTRICITY
Abstract
An air cavity package with one or more dovetail recesses configured with a first recess and a coincident second recess. The first recess has a first depth and the second recess has a second depth. The first recess has a lower width and an upper width smaller than the first lower width creating a dovetail shape. Individual dovetail recesses are created by creating a first recess in the flange at a first width and depth. A second recess with a second width and second depth and coincident with the first recess is pressed into the flange. The second width is greater than the first width and the second depth is smaller than the first depth. Pressing the second recess causes the first width at an upper portion to decrease, causing the first recess to develop a dovetail shape.
Claims
1. A method for creating an individual dovetail recess in a flange of an air cavity package, comprising the steps of: creating a first recess in the flange having a first width and first depth; pressing a second recess into the flange, the second recess being coincident with the first recess and having a second width and a second depth, wherein the second width it greater than the first width and the second depth is smaller than the first depth; and wherein pressing the second recess causes the first width at an upper portion of the first recess to decrease, causing the first recess to develop a dovetail shape.
2. The method of claim 1 wherein the first recess is elliptical.
3. The method of claim 2 wherein the second recess is elliptical.
4. The method of claim 1 wherein the first recess is rectangular.
5. The method of claim 4 wherein the second recess is rectangular.
6. The method of claim 1 wherein a plurality of individual dovetail recesses are created in the flange proximate the location of attachment of an air cavity package sidewall.
7. An air cavity package, comprising a flange having a plurality of individual dovetail recesses about a flange perimeter proximate the location of attachment of an air cavity package sidewall.
8. The air cavity package of claim 7 wherein at least one of the individual dovetail recesses is elliptical.
9. The air cavity package of claim 7 wherein at least one of the individual dovetail recesses is rectangular.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] The accompanying drawings are included to provide a further understanding of the disclosure and are incorporated in and constitute a part of this specification, illustrate embodiments of the disclosure, and together with the description serve to explain the principles of the disclosure, wherein like numerals denote like elements and wherein:
[0009]
[0010]
[0011]
[0012]
[0013]
[0014]
DETAILED DESCRIPTION
[0015] Persons skilled in the art will readily appreciate that various aspects of the present disclosure can be realized by any number of structures, components, and systems configured to perform various functions disclosed herein. Stated differently, other such structures, components, and systems can be incorporated herein to perform the intended functions. It should also be noted that the accompanying drawing figures referred to herein are not all necessarily drawn to scale and may be exaggerated to illustrate various aspects of the present disclosure, and in that regard, the drawing figures should not be construed as limiting.
[0016] With reference to
[0017] As noted above, a variety of conventionally known ways to assemble the components of ACPs 100 exist such as by using adhesives and epoxies. This assembly includes attaching the sidewalls 140 to the flange 130, and potentially, any number of other components of the ACP 100 that need to be attached to complete ACP 100. However, as also noted above, adhesives and expoxies can fail. Thus, in accordance with the present disclosure, mechanisms for improving the connection between components are provided.
[0018] For example, with reference to
[0019] The shape of the first and second recesses 172, 174 may vary. For example, the first and second recesses 172, 174 may be formed as ellipsoid (e.g., circular, oval, etc.), polygonal (e.g., rectangular, octagonal, etc.), or other shape having an individual dovetail profile, as described in detail below. Additionally, the first recess 172 and the second recess 174 may have shapes that differ from one another. Additionally, though the description herein is directed largely at a dovetail recess 170 in a portion of a flange 130, it should be appreciated that multiple individual dovetail recesses 170 may be included in one flange 130.
[0020] The first recess 172 has a first lower width LW1 and a first upper width UW1 which is smaller than the first lower width LW1. The shape of the first recess 172 is thus one commonly known as a “dovetail” which provides an “overhang.” Because of this overhang, when the sidewall 140 is molded to and fills in the first recess 172, because the portion of the sidewall 140 located proximate the first lower width LW1 of the first recess 172 is greater than the first upper width UW1 of the first recess 172, the sidewall 140 is more securely connected to the flange.
[0021] In accordance with the present disclosure, the second recess 174 has a second depth D2 and a second width W2 that is generally the same along the second depth D2 (though the width may vary based on the application). The second width W2 is greater than either of the first upper width UW1 and the first lower width LW1. The larger width of the second width W2 of the second recess 174 facilitates the formation of the dovetail shape of the first recess 172.
[0022] For example, with reference now to
[0023] In accordance with the present disclosure, multiple dovetail recesses 170 may be used to secure the sidewall 140 to the flange 130. For example, with reference to
[0024] Finally, the foregoing description emphasizes particular embodiments and examples of the contemplated disclosure. However, as those skilled in the art will recognize, however, the scope of the present disclosure extends as well to variations and modifications of the above, in terms of materials, operating conditions, operating procedures, and other parameters and their components and of procedures for their assembly.
[0025] Likewise, numerous characteristics and advantages have been set forth in the preceding description, including various alternatives together with details of the structure and function of the methods and systems described herein. The disclosure is intended as illustrative only and as such is not intended to be exhaustive. It will be evident to those skilled in the art that various modifications may be made, especially in matters of order, process, structure, elements, components, and arrangement including combinations of the same within the principles of the disclosure, to the full extent indicated by the broad, general meaning of the terms in which the appended claims are expressed. To the extent that these various modifications do not depart from the spirit and scope of the appended claims, they are intended to be encompassed therein.