Penetration test structure and penetration tester
By adopting a combination of an annular isolation groove and an annular sealing groove in the air permeability testing device, the problem of insufficient sealing performance of multi-cavity equipment is solved, efficient sealing effect and detection accuracy are achieved, and the increase of structural complexity is avoided.
Patent Information
- Application Number
- CN202422711458.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-07
- Publication Date
- 2025-09-23
- Estimated Expiration
- 2034-11-07
AI Technical Summary
When the sealing performance of the multi-cavity equipment of the traditional gas permeability testing device is insufficient, the accuracy of the test results is reduced, and increasing the structural complexity to improve the sealing performance will increase the manufacturing cost.
A penetration test structure was designed, which adopted a combination of an annular isolation groove and an annular sealing groove. By setting an annular isolation groove and an annular sealing groove between the detection cavity and the penetration cavity, the cavity was sealed and isolated by using a flowing sealing medium, and a pressure area was formed in the annular sealing groove to prevent gas leakage.
The sealing effect of the multi-cavity equipment is improved, the increase of the structural complexity is avoided, and the accuracy of the test results and the detection efficiency are ensured.
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Figure CN223377153U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of detection equipment, and in particular to a penetration test structure and a penetration tester. Background Art
[0002] Gas permeability testing is a key test in materials science, widely used in the evaluation of packaging materials and other applications. Gas permeability testing equipment is typically used to determine a material's permeability to gases and other media, including but not limited to differential pressure and equal pressure methods. The test principle involves using a test specimen to separate the test chamber into an upper chamber and a lower chamber. The upper chamber is filled with the test gas, while the lower chamber is connected to a gas sensor for real-time monitoring of gas permeation, thereby evaluating the sample's gas permeability.
[0003] Traditional permeability testers are primarily categorized into single-chamber and multi-chamber types, depending on the number of test chambers. Single-chamber devices can only test a single sample, limiting test efficiency. Multi-chamber devices can simultaneously test a sample with multiple gases and other media, significantly improving test efficiency. However, insufficient sealing between test chambers can negatively impact the accuracy of test results. Improving sealing performance often requires increasing structural complexity, which in turn increases manufacturing costs. Utility Model Content
[0004] Based on this, it is necessary to provide a penetration test structure and a penetration tester that can improve the sealing effect and avoid increasing the complexity of the structure in order to address the above problems.
[0005] A penetration test structure, comprising a detection body and a penetration body, wherein the detection body is provided with a first detection cavity and a second detection cavity, the second detection cavity being an annular groove, the second detection cavity being provided on the outer side of the first detection cavity, at least two annular isolation grooves spaced apart from each other are formed between the first detection cavity and the second detection cavity, an annular isolation groove spaced apart from the second detection cavity is further provided on the outer side of the second detection cavity, the annular isolation groove being used for passing a sealing medium; the penetration body is provided with a first penetration cavity and a second penetration cavity, the second penetration cavity being an annular groove, the second penetration cavity being provided on the outer side of the first penetration cavity, at least two annular sealing grooves spaced apart from each other are formed between the first penetration cavity and the second penetration cavity, an annular sealing groove spaced apart from the second penetration cavity is further provided on the outer side of the second penetration cavity;
[0006] When the permeation body is disposed on the detection body, the first permeation cavity is opposite to the first detection cavity, the second permeation cavity is opposite to the second detection cavity, and each of the annular isolation grooves is opposite to a corresponding annular sealing groove.
[0007] In one embodiment, the two opposite surfaces of the detection body are respectively a test surface and a mounting surface, the first detection cavity and the second detection cavity are both formed on the test surface, and an air intake docking area and an exhaust docking area are formed on the mounting surface. The number of the air intake docking areas and the number of the exhaust docking areas are consistent with the number of the detection cavities, and are all arranged at intervals.
[0008] In one embodiment, a first air inlet channel is formed in the detection body, one end of the first air inlet channel is connected to the first detection cavity, and the other end is connected to one of the air inlet docking areas; a second air inlet channel is formed in the detection body, one end of the second air inlet channel is connected to the second detection cavity, and the other end is connected to another of the air inlet docking areas.
[0009] In one embodiment, a first exhaust channel is also formed in the detection body, one end of the first exhaust channel is connected to the first detection cavity, and the other end is connected to the exhaust docking area; the positions where the first air inlet channel and the first exhaust channel are respectively connected to the first detection cavity are arranged symmetrically relative to the first detection cavity.
[0010] In one embodiment, a second exhaust channel is also formed in the detection body, one end of the second exhaust channel is connected to the second detection cavity, and the other end is connected to another exhaust docking area, and the positions where the second air inlet channel and the second exhaust channel are respectively connected to the second detection cavity are arranged symmetrically relative to the second detection cavity.
[0011] In one embodiment, a sealed air intake channel, a sealed exhaust channel and a series channel are formed in the detection body, and the number of the sealed air intake channels is the same as that of the sealed exhaust channels; wherein, the number of the sealed air intake channel and the sealed exhaust channel are both one, and each of the annular isolation grooves is connected in series through the series channel, one end of the sealed air intake channel and one end of the sealed exhaust channel are respectively connected to the two outermost annular isolation grooves on the series path, the other end of the sealed air intake channel is connected to one of the air intake docking areas, and the other end of the sealed exhaust channel is connected to one of the exhaust docking areas.
[0012] In one embodiment, the number of the sealed air inlet channels and the sealed air exhaust channels are both two, wherein the two annular isolation grooves are connected through the series channel, wherein one end of one of the sealed air inlet channels and one end of one of the sealed air exhaust channels are respectively connected to the two annular isolation grooves connected in series, and one end of the other sealed air inlet channel and one end of the other sealed air exhaust channel are connected to the other annular isolation groove, and the other ends of the two sealed air inlet channels are respectively connected to the two air inlet docking areas or both are connected to one of the air inlet docking areas, and the other ends of the two sealed air exhaust channels are respectively connected to the two exhaust docking areas or both are connected to one of the exhaust docking areas.
[0013] In one embodiment, an air intake docking groove is formed in the air intake docking area, an air intake portion and an air intake ring are provided in the air intake docking groove, a first air intake hole is provided in the air intake portion, the air intake ring is sleeved outside the air intake portion and spaced apart from the air intake portion, and a second air intake hole is provided on the air intake ring; the sealed air intake channel is connected to one of the first air intake hole and the second air intake hole, and the first air intake channel or the second air intake channel is connected to the other of the first air intake hole and the second air intake hole.
[0014] In one embodiment, an exhaust docking groove is formed in the exhaust docking area, an exhaust portion and an exhaust ring are provided in the exhaust docking groove, a first exhaust hole is provided in the exhaust portion, the exhaust ring is sleeved outside the exhaust portion and spaced apart from the exhaust portion, and a second exhaust hole is provided on the exhaust ring; the sealed exhaust channel is connected to one of the first exhaust hole and the second exhaust hole, and the first exhaust channel or the second exhaust channel is connected to the other of the first exhaust hole and the second exhaust hole.
[0015] In one embodiment, a first connecting channel and a first docking channel are formed in the permeable body, one end of the first docking channel and one end of the first connecting channel are both connected to the first permeable cavity, and the other end of the first docking channel and the other end of the first connecting channel are both connected to the surface of the permeable body to form the first permeable cavity.
[0016] In one embodiment, a second connecting channel and a second docking channel are formed in the permeable body, one end of the second docking channel and one end of the second connecting channel are both connected to the second permeable cavity, and the other end of the second docking channel and the other end of the second connecting channel are both connected to the surface of the permeable body to form the second permeable cavity.
[0017] In one embodiment, a first infiltration air inlet, a first infiltration air exhaust hole, a second infiltration air inlet and a second infiltration air exhaust hole are also formed on the test surface of the detection body, which penetrate into the mounting surface; when the infiltration body is set on the detection body, the other end of the first connecting channel is connected to the first infiltration air inlet, the other end of the first docking channel is connected to the first infiltration air exhaust hole, the other end of the second connecting channel is connected to the second infiltration air inlet, and the other end of the second docking channel is connected to the second infiltration air exhaust hole.
[0018] In one embodiment, the positions where the first communicating channel and the first docking channel are connected to the first osmosis cavity are symmetrically arranged relative to the first osmosis cavity; the positions where the second communicating channel and the second docking channel are connected to the second osmosis cavity are symmetrically arranged relative to the second osmosis cavity.
[0019] In one embodiment, a sealing ring is provided in the annular sealing groove.
[0020] In one embodiment, a protective air inlet channel and a protective air exhaust channel are formed in the permeable body, and both the protective air inlet channel and the protective air exhaust channel are communicated with the annular sealing groove.
[0021] In one embodiment, the area of the first detection cavity is consistent with the area of the second detection cavity; the area of the first osmosis cavity is consistent with the area of the second osmosis cavity.
[0022] In one embodiment, the number of the second detection cavities is one, two or more. When the number of the second detection cavities is two or more, the second detection cavities are radially arranged with the first detection cavity as the center, and at least two annular isolation grooves are formed between two adjacent second detection cavities. The number of the second permeation cavities is consistent with the number of the second detection cavities, and each of the second permeation cavities can correspond to one of the second detection cavities. The number of the annular sealing grooves is greater than or equal to the number of the annular isolation grooves, and each of the annular isolation grooves can correspond to one of the annular sealing grooves.
[0023] A penetration tester comprises the penetration test structure described above.
[0024] In the aforementioned permeation test structure and permeation tester, the sample to be tested is positioned between the permeation body and the detection body. Different test media can then be introduced into the first and second detection chambers, respectively. The test medium in the first detection chamber can permeate the sample into the first permeation chamber, and the test medium in the second detection chamber can permeate the sample into the second permeation chamber. This allows simultaneous permeability testing of both test media for the sample to be tested. Since at least two annular isolation grooves are spaced apart between the first and second detection chambers, a sealing medium is introduced into the two annular isolation grooves. The inner annular isolation groove isolates and protects the first detection chamber, while the outer annular isolation groove and the outer annular isolation groove of the second detection chamber isolate and protect the second detection chamber, effectively achieving a sealed separation between the first and second detection chambers. Simultaneously, the flowing sealing medium is introduced, effectively filling each position in the annular isolation grooves. If the sample deforms at the position opposite the annular sealing grooves, the flowing sealing medium can adapt to the deformation and provide a seal. Furthermore, the flowing sealing medium can form a constant pressure region within the annular sealing grooves, thereby preventing gas leakage from the first and second detection chambers. BRIEF DESCRIPTION OF THE DRAWINGS
[0025] The drawings that constitute a part of this application are used to provide further understanding of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute improper limitations on this application.
[0026] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following briefly introduces the drawings required for use in the description of the embodiments. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.
[0027] In addition, the drawings are not drawn to a 1:1 scale, and the relative sizes of various elements are drawn only as examples in the drawings and are not necessarily drawn to true scale.
[0028] Figure 1 1 is an exploded view of a penetration test structure in one embodiment.
[0029] Figure 2 for Figure 1 The main view of the detection entity in .
[0030] Figure 3 for Figure 2 The main view of the internal structure of the detection body is shown.
[0031] Figure 4 for Figure 2 Sectional view along line AA.
[0032] Figure 5 for Figure 2 Cross-sectional view along line BB.
[0033] Figure 6 for Figure 2 Cross-sectional view along line CC.
[0034] Figure 7 for Figure 1 Schematic diagram of the structure of the detection entity in another perspective.
[0035] Figure 8 for Figure 1 Schematic diagram of the structure of the penetration entity in .
[0036] Figure 9 for Figure 8 A front view of the infiltration body is shown.
[0037] Figure 10 for Figure 9 The front view of the internal structure of the infiltration body is shown.
[0038] Figure 11 for Figure 9 Cross-sectional view along line DD.
[0039] Figure 12 for Figure 9 Cross-sectional view along line EE.
[0040] Description of reference numerals:
[0041] Penetration test structure 10; test body 100; test surface 101; mounting surface 102; first test chamber 110; first air inlet channel 112; first exhaust channel 114; second test chamber 120; second air inlet channel 122; second exhaust channel 124; annular isolation groove 130; sealed air inlet channel 131; sealed exhaust channel 132; series channel 133; air inlet docking groove 141; air inlet portion 142; air inlet ring 143; first air inlet hole 144; second air inlet hole 145; exhaust docking groove 151; exhaust portion 152; exhaust ring 153; first exhaust hole 154; second exhaust hole 155; first infiltration air inlet hole 161; first infiltration air exhaust hole 162; second infiltration air inlet hole 163; second infiltration air exhaust hole 164; infiltration body 200; first infiltration cavity 210; first connecting channel 212; first docking channel 214; second infiltration cavity 220; second connecting channel 222; second docking channel 224; annular sealing groove 230. DETAILED DESCRIPTION
[0042] To make the above-mentioned objects, features, and advantages of the present application more clearly understood, the specific embodiments of the present application are described in detail below with reference to the accompanying drawings. The following description sets forth many specific details to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways than those described herein, and those skilled in the art can make similar improvements without violating the scope of the present application. Therefore, the present application is not limited to the specific embodiments disclosed below.
[0043] See Figure 1 The penetration test structure 10 of one embodiment of the present invention can at least improve the sealing effect and avoid increasing the structural complexity. The penetration test structure 10 includes a detection body 100 and a penetration body 200. The sample to be tested is placed between the detection body 100 and the penetration body 200. By passing the test medium through one side of the detection body 100, the test medium's transmittance of the sample to be tested is tested.
[0044] See Figure 1 and Figure 2 Specifically, the detection body 100 is provided with a first detection chamber 110 and a second detection chamber 120. The second detection chamber 120 is an annular groove disposed on the outer side of the first detection chamber 110. At least two annular isolation grooves 130 are formed between the first and second detection chambers 110, 120. An annular isolation groove 130 is further disposed outside the second detection chamber 120, spaced apart from the second detection chamber 120. The annular isolation grooves 130 are used to pass a sealing medium. The annular isolation grooves 130 seal and isolate the first and second detection chambers 110, 120.
[0045] See Figure 8 and Figure 9 Specifically, the permeation body 200 is provided with a first permeation cavity 210 and a second permeation cavity 220. The second permeation cavity 220 is an annular groove disposed on the outer side of the first permeation cavity 210. At least two annular sealing grooves 230 are formed between the first and second permeation cavities 210 and 220, respectively. An annular sealing groove 230 is also disposed on the outer side of the second permeation cavity 220, spaced apart from the second permeation cavity 220. The provision of the annular sealing grooves 230 enables sealing and isolation between the first and second permeation cavities 210 and 220. When the permeation body 200 is disposed on the detection body 100, the first permeation cavity 210 faces the first detection cavity 110, and the second permeation cavity 220 faces the second detection cavity 120. Each annular isolation groove 130 corresponds to an annular sealing groove 230. In this embodiment, the number of annular isolation grooves 130 and annular sealing grooves 230 may be the same or different.
[0046] During use, the sample to be tested is placed between the permeation body 200 and the detection body 100, and then different test media can be introduced into the first detection chamber 110 and the second detection chamber 120 respectively. The test medium in the first detection chamber 110 can penetrate into the first permeation chamber 210 through the sample, and the test medium in the second detection chamber 120 can penetrate into the second permeation chamber 220 through the sample, thereby simultaneously performing transmittance tests of the two test media on the sample to be tested. Since there are at least two annular isolation grooves 130 spaced apart between the first detection chamber 110 and the second detection chamber 120, the two annular isolation grooves 130 are filled with sealing media. The inner annular isolation groove 130 can isolate and protect the first detection chamber 110, and the outer annular isolation groove 130 and the outer annular isolation groove 130 of the second detection chamber 120 can isolate and protect the second detection chamber 120, effectively achieving sealed isolation between the first detection chamber 110 and the second detection chamber 120. Simultaneously, the flowing sealing medium effectively fills every position within the annular isolation groove 130. If the sample deforms in the position where the annular sealing groove 230 faces the annular isolation groove 130, the flowing sealing medium adapts to the deformation and seals the sample. Furthermore, the flowing sealing medium creates a constant pressure zone within the annular sealing groove 230, preventing gas leakage from the first and second detection cavities 110, 120.
[0047] In one embodiment, the area of the first detection chamber 110 is consistent with the area of the second detection chamber 120. The area of the first permeation chamber 210 is consistent with the area of the second permeation chamber 220. By setting the areas of the first detection chamber 110 and the second detection chamber 120 to be the same, the areas of the two test media to be tested are consistent, facilitating the statistical analysis of subsequent test results. In other embodiments, the areas of the first detection chamber 110 and the second detection chamber 120 may be different, while the cross-sectional shape and size of the first permeation chamber 210 are consistent with those of the first detection chamber 110, and the cross-sectional shape and size of the second permeation chamber 220 are consistent with those of the second detection chamber 120.
[0048] In one embodiment, the number of second detection cavities 120 is one, two, or more. When the number of second detection cavities 120 is two or more, each second detection cavity 120 is radially spaced apart with the first detection cavity 110 as the center, and at least two annular isolation grooves 130 are formed between two adjacent second detection cavities 120. The number of second permeation cavities 220 is the same as the number of second detection cavities 120. Each second permeation cavity 220 can correspond to a second detection cavity 120. The number of annular sealing grooves 230 is greater than or equal to the number of annular isolation grooves 130. Each annular isolation groove 130 can correspond to an annular sealing groove 230. In the present application, the number of second detection cavities 120 is one, and the first detection cavity 110 and the second detection cavity 120 are used for detecting oxygen and water vapor, respectively. In other embodiments, the number of second detection cavities 120 can be two or more. By providing more second detection cavities 120, more test media can be tested simultaneously, further improving detection efficiency. The two adjacent second detection chambers 120 are sealed and isolated by the annular isolation groove 130 to ensure the sealing of the test.
[0049] See Figure 1 and Figure 7 In one embodiment, the two opposing surfaces of the detection body 100 are respectively a test surface 101 and a mounting surface 102. The first detection cavity 110 and the second detection cavity 120 are both formed on the test surface 101. The mounting surface 102 is formed with air intake and exhaust docking areas. The number of these air intake and exhaust docking areas is the same as the number of detection cavities, and they are spaced apart. By providing both the air intake and exhaust docking areas on the mounting surface 102 of the detection body 100, air intake and exhaust of the first detection cavity 110 and the second detection cavity 120 can be facilitated from the same side, improving the convenience of installing and docking the air intake and exhaust pipelines.
[0050] See Figure 3 、 Figure 4 and Figure 7 In one embodiment, a first air inlet channel 112 is formed in the detection body 100 , one end of the first air inlet channel 112 is connected to the first detection cavity 110 , and the other end of the first air inlet channel 112 is connected to an air inlet docking area.
[0051] Specifically, a first exhaust channel 114 is formed within the detection body 100. One end of the first exhaust channel 114 communicates with the first detection chamber 110, and the other end of the first exhaust channel 114 communicates with an exhaust docking area. Air is introduced into the first detection chamber 110 via the first air inlet channel 112, and gas within the first detection chamber 110 is exhausted via the first exhaust channel 114. The transmittance of the sample can be tested using the isobaric method. In other embodiments, the first exhaust channel 114 can be omitted, and the first detection chamber 110 can then perform transmittance testing on the sample using the differential pressure method.
[0052] Furthermore, the positions at which the first air inlet channel 112 and the first exhaust channel 114 communicate with the first detection chamber 110 are symmetrically arranged relative to the first detection chamber 110. After the test medium enters the first detection chamber 110 through the first air inlet channel 112, it can be evenly diffused within the first detection chamber 110 before being discharged through the first exhaust channel 114. Furthermore, the first air inlet channel 112 and the first exhaust channel 114 are of the same length. This symmetrical arrangement allows one channel to be selected as the first air inlet channel 112 and the other as the first exhaust channel 114 during use, improving ease of use.
[0053] See Figure 3 、 Figure 5 and Figure 7 In one embodiment, a second air inlet channel 122 is formed in the detection body 100 , one end of the second air inlet channel 122 is connected to the second detection cavity 120 , and the other end of the second air inlet channel 122 is connected to another air inlet docking area.
[0054] Specifically, a second exhaust channel 124 is formed within the detection body 100. One end of the second exhaust channel 124 communicates with the second detection chamber 120, and the other end of the second exhaust channel 124 communicates with another exhaust docking area. Air is introduced into the second detection chamber 120 via the second air inlet channel 122, and gas within the second detection chamber 120 is exhausted via the second exhaust channel 124. In the second detection chamber 120, the transmittance of the sample can be tested using the isobaric method. In other embodiments, the second exhaust channel 124 can be omitted, in which case the second detection chamber 120 can perform transmittance testing on the sample using the differential pressure method.
[0055] Furthermore, the positions at which the second air inlet channel 122 and the second exhaust channel 124 communicate with the second detection chamber 120 are symmetrically arranged relative to the second detection chamber 120. After the test medium enters the second detection chamber 120 through the second air inlet channel 122, it is evenly diffused within the second detection chamber 120 before being discharged. Furthermore, the second air inlet channel 122 and the second exhaust channel 124 are of the same length. During use, one channel can be selected as the second air inlet channel 122 and the other as the second exhaust channel 124, improving ease of use.
[0056] In one embodiment, a sealing ring is provided in the annular sealing groove 230. A flowing sealing medium, such as a protective gas, is introduced into the annular isolation groove 130. The elasticity of the sealing ring can press against the sample to be tested. The sealing medium can fill the entire space in the annular isolation groove 130 and can press the sample to be tested against the sealing ring under a certain pressure, thereby improving the reliability of the seal. The present application improves the reliability of the seal by introducing a flowing sealing medium, such as a protective gas, on one side and providing a sealing ring on the other side without increasing the complexity of the structure.
[0057] In other embodiments, the permeation body 200 may further include a protective air inlet channel and a protective air exhaust channel, both of which are in communication with the annular sealing groove 230. Protective gas is introduced into the annular sealing groove 230 through the protective air inlet channel. For example, when harmful gas is introduced into the detection chamber or the permeation chamber, the introduction of protective gas reduces the possibility of gas leakage. Specifically, the annular sealing grooves 230 may be partially or completely connected in series, and protective gas may be introduced into each annular sealing groove 230.
[0058] See Figure 3 、 Figure 6 and Figure 7 In one embodiment, a sealed air inlet channel 131, a sealed air exhaust channel 132, and a series channel 133 are formed within the detection body 100. The number of sealed air inlet channels 131 and sealed air exhaust channels 132 is the same; there is only one sealed air inlet channel 131 and one sealed air exhaust channel 132, respectively. Each annular isolation groove 130 is connected in series via the series channel 133. One end of the sealed air inlet channel 131 and one end of the sealed air exhaust channel 132 are respectively connected to the two outermost annular isolation grooves 130 on the series path. The other end of the sealed air inlet channel 131 is connected to one of the air inlet docking areas, and the other end of the sealed air exhaust channel 132 is connected to one of the air exhaust docking areas. By connecting the annular isolation grooves 130 in series, it is only necessary to control the sealing medium to enter through one sealed air inlet channel 131 and to be discharged through one sealed air exhaust channel 132.
[0059] In another embodiment, there are two sealed air inlet channels 131 and two sealed air exhaust channels 132, wherein the two annular isolation grooves 130 are connected via a series channel 133, wherein one end of one sealed air inlet channel 131 and one end of one sealed air exhaust channel 132 are respectively connected to the two annular isolation grooves 130 connected in series, and one end of another sealed air inlet channel 131 and one end of another sealed air exhaust channel 132 are respectively connected to the other annular isolation groove 130, and the other ends of the two sealed air inlet channels 131 are respectively connected to two air inlet docking areas or both are connected to one of the air inlet docking areas, and the other ends of the two sealed air exhaust channels 132 are respectively connected to two air exhaust docking areas or both are connected to one of the air exhaust docking areas. The air inlet of the annular isolation groove 130 and the air inlet of the first detection chamber 110 or the second detection chamber 120 are located in the same area, facilitating simultaneous docking of the air inlet pipe joints; the same applies to the air exhaust. For example, in this embodiment, there are two air intake docking areas and two exhaust docking areas, so the number of sealed air intake channels 131 and sealed exhaust channels 132 is less than or equal to two, so as to avoid increasing the air intake and exhaust docking areas due to the need to pass the sealing medium through the annular isolation groove 130.
[0060] Specifically, the two annular isolation grooves 130 adjacent to the second detection cavity 120 are connected via a series channel 133 , so as to facilitate isolation and sealing of the inner and outer sides of the second detection cavity 120 with the same sealing medium.
[0061] In this embodiment, the position where the sealed air inlet channel 131 communicates with the annular isolation groove 130 and the position where the sealed air exhaust channel 132 communicates with the annular isolation groove 130 are arranged symmetrically relative to the annular isolation groove 130. When the sealing medium enters the annular isolation groove 130, it can be discharged after being evenly diffused, so that the sealing medium effectively fills the annular isolation groove 130.
[0062] In other embodiments, each annular isolation groove 130 may be connected to a sealed inlet channel 131 and a sealed exhaust channel 132. Alternatively, some of the annular isolation grooves 130 may be connected in series. The number of sealed inlet channels 131 may be less than or equal to the number of inlet docking areas, and the number of sealed exhaust channels 132 may be less than or equal to the number of exhaust docking areas.
[0063] See Figure 3 and Figure 7In one embodiment, the air intake docking area is formed with an air intake docking groove 141. An air intake portion 142 and an air intake ring 143 are disposed within the air intake docking groove 141. A first air intake hole 144 is defined within the air intake portion 142. The air intake ring 143 is sleeved around the air intake portion 142 and spaced apart from the air intake portion 142. A second air intake hole 145 is defined within the air intake ring 143. The sealed air intake passage 131 communicates with one of the first air intake hole 144 and the second air intake hole 145, while the first air intake passage 112 or the second air intake passage 122 communicates with the other of the first air intake hole 144 and the second air intake hole 145. Taking one of the air intake docking areas as an example, when the air intake connector is docked in the air intake docking groove 141, the test medium can effectively enter the first air intake channel 112 or the second air intake channel 122, while the sealing medium can also enter the sealed air intake channel 131 through the air intake docking groove 141, thereby improving installation and docking efficiency. In other embodiments, the shape and structure of the air intake docking area can be determined by the shape of the docking air intake connector.
[0064] In one embodiment, the exhaust docking area is formed with an exhaust docking groove 151. An exhaust portion 152 and an exhaust ring 153 are disposed within the exhaust docking groove 151. A first exhaust hole 154 is defined within the exhaust portion 152. The exhaust ring 153 is sleeved over and spaced from the exhaust portion 152, and a second exhaust hole 155 is defined within the exhaust ring 153. The sealed exhaust channel 132 communicates with either the first exhaust hole 154 or the second exhaust hole 155, while either the first exhaust channel 114 or the second exhaust channel 124 communicates with the other of the first exhaust hole 154 and the second exhaust hole 155. The provision of the exhaust docking groove 151, the exhaust portion 152, and the exhaust ring 153 improves installation and docking efficiency.
[0065] Specifically, each air intake docking area is evenly arranged on the mounting surface 102 , and each exhaust docking area is evenly arranged on the mounting surface 102 .
[0066] See Figure 10 and Figure 11 In one embodiment, a first connecting channel 212 and a first docking channel 214 are formed in the permeation body 200. One end of the first docking channel 214 and one end of the first connecting channel 212 are both connected to the first permeation cavity 210, and the other end of the first docking channel 214 and the other end of the first connecting channel 212 are both connected to the surface of the permeation body 200 to form the first permeation cavity 210. Figure 1 、 Figure 7 and Figure 10Specifically, the test surface 101 of the detection body 100 is further formed with a first permeation air inlet 161 and a first permeation air outlet 162 that extend through to the mounting surface 102. When the permeation body 200 is mounted on the detection body 100, the other end of the first connecting channel 212 connects to the first permeation air inlet 161, and the other end of the first connecting channel 214 connects to the first permeation air outlet 162. The first permeation cavity 210 connects to the mounting surface 102 through the first connecting channel 212 and the first permeation air inlet 161, and also connects to the mounting surface 102 through the first connecting channel 214 and the first permeation air outlet 162. The mounting surface 102 is formed with an air intake docking area and an air exhaust docking area, allowing air intake and exhaust of the first permeation cavity 210 to be achieved through one side of the mounting surface 102.
[0067] Specifically, the positions at which the first connecting channel 212 and the first docking channel 214 communicate with the first osmosis chamber 210 are symmetrical relative to the first osmosis chamber 210, facilitating uniform diffusion and subsequent discharge of the medium entering the first osmosis chamber 210. Furthermore, the first connecting channel 212 and the first docking channel 214 are of the same length.
[0068] See Figure 10 and Figure 12 In one embodiment, a second connecting channel 222 and a second docking channel 224 are formed in the permeation body 200. One end of the second docking channel 224 and one end of the second connecting channel 222 are both connected to the second permeation cavity 220, and the other end of the second docking channel 224 and the other end of the second connecting channel 222 are both connected to the surface of the permeation body 200 forming the second permeation cavity 220. Figure 1 、 Figure 7 and Figure 10 In one embodiment, the test surface 101 of the detection body 100 further includes a second permeation air inlet 163 and a second permeation air outlet 164 extending through the mounting surface 102. When the permeation body 200 is mounted on the detection body 100, the other end of the second connecting channel 222 connects to the second permeation air inlet 163, and the other end of the second connecting channel 224 connects to the second permeation air outlet 164. Similarly, air intake and exhaust for the first permeation cavity 210, the second permeation cavity 220, the first detection cavity 110, the second detection cavity 120, and the annular isolation groove 130 are all completed on the mounting surface 102, further facilitating the connection and docking of the gas paths.
[0069] Specifically, the positions at which the second connecting channel 222 and the second docking channel 224 communicate with the second osmosis chamber 220 are symmetrical relative to the second osmosis chamber 220, facilitating uniform diffusion and subsequent discharge of the medium entering the second osmosis chamber 220. Furthermore, the second connecting channel 222 and the second docking channel 224 are of the same length.
[0070] See Figure 1 、 Figure 7 and Figure 8 The present application also discloses a penetration tester, comprising the penetration test structure 10 in any one of the above embodiments.
[0071] The two test areas in the above-mentioned penetration tester and penetration test structure 10 of the present application can be tested using the isobaric method, or the pressure differential method, or the two areas can be tested using the isobaric method and the pressure differential method respectively, realizing an isobaric method-pressure differential method all-in-one machine, which is different from the traditional all-in-one machine. The above-mentioned penetration test structure 10 has a symmetrical gas path arrangement position to minimize the connection of complex gas paths. At the same time, it is necessary to consider the convenience of connection with the air intake pipe and the exhaust pipe, which are all arranged on the mounting surface 102 of the detection body 100.
[0072] In the description of this application, it should be understood that if the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. appear, the orientation or position relationship indicated by these terms is based on the orientation or position relationship shown in the accompanying drawings, which is only for the convenience of describing this application and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on this application.
[0073] In addition, if the terms "first" or "second" appear, these terms are used for descriptive purposes only and should not be understood to indicate or imply relative importance or implicitly specify the number of technical features indicated. Therefore, a feature specified as "first" or "second" may explicitly or implicitly include at least one of such features. In the description of this application, if the term "plurality" appears, "plurality" means at least two, for example, two, three, etc., unless otherwise specifically defined.
[0074] In this application, unless otherwise specified or limited, the terms "mounted," "connected," "connected," "fixed," etc., should be interpreted broadly. For example, these terms may refer to fixed connections, removable connections, or integration; mechanical connections or electrical connections; direct connections or indirect connections through an intermediary; and internal communication between two components or interaction between two components, unless otherwise specified. Those skilled in the art will understand the specific meanings of these terms in this application based on the specific circumstances.
[0075] In this application, unless otherwise expressly specified or limited, if a first feature is described as being "above" or "below" a second feature, or similar descriptions, this may mean that the first and second features are in direct contact, or that the first and second features are in indirect contact through an intermediate medium. Furthermore, when a first feature is described as being "above," "above," or "above" a second feature, it may mean that the first feature is directly above or diagonally above the second feature, or simply means that the first feature is at a higher level than the second feature. When a first feature is described as being "below," "below," or "below" a second feature, it may mean that the first feature is directly below or diagonally below the second feature, or simply means that the first feature is at a lower level than the second feature.
[0076] It should be noted that if an element is referred to as being "fixed to" or "disposed on" another element, it may be directly on the other element or there may be an intermediate element. If an element is considered to be "connected to" another element, it may be directly connected to the other element or there may be an intermediate element. If any, the terms "vertical", "horizontal", "upper", "lower", "left", "right" and similar expressions used in this application are for illustrative purposes only and do not represent the only embodiment.
[0077] The technical features of the above-mentioned embodiments can be combined arbitrarily. In order to make the description concise, not all possible combinations of the technical features in the above-mentioned embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.
[0078] The above-described embodiments merely represent several implementation methods of the present application. While the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the patent application. It should be noted that a person of ordinary skill in the art may make various modifications and improvements without departing from the spirit of the present application, and these modifications and improvements fall within the scope of protection of the present application. Therefore, the scope of protection of the present patent application shall be determined by the appended claims.
Claims
1. A penetration testing structure, characterized in that: The penetration test structure includes: A detection body, wherein the detection body is provided with a first detection cavity and a second detection cavity, the second detection cavity is an annular groove, the second detection cavity is provided on the outer side of the first detection cavity, at least two annular isolation grooves spaced apart are formed between the first detection cavity and the second detection cavity, and an annular isolation groove spaced apart from the second detection cavity is further provided on the outer side of the second detection cavity, the annular isolation groove being used to pass a sealing medium; and A permeable body, wherein the permeable body is provided with a first permeable cavity and a second permeable cavity, wherein the second permeable cavity is an annular groove, and the second permeable cavity is provided on the outer side of the first permeable cavity, and at least two annular sealing grooves spaced apart from each other are formed between the first permeable cavity and the second permeable cavity, and an annular sealing groove spaced apart from the second permeable cavity is further provided on the outer side of the second permeable cavity; When the permeation body is disposed on the detection body, the first permeation cavity is opposite to the first detection cavity, the second permeation cavity is opposite to the second detection cavity, and each of the annular isolation grooves is opposite to a corresponding annular sealing groove.
2. The penetration test structure according to claim 1, characterized in that: The two opposite surfaces of the detection body are respectively a test surface and a mounting surface, the first detection cavity and the second detection cavity are both formed on the test surface, and the mounting surface is formed with an air intake docking area and an exhaust docking area, the number of the air intake docking areas and the number of the exhaust docking areas are consistent with the number of the detection cavities, and are arranged at intervals; A first air inlet channel is formed in the detection body, one end of the first air inlet channel is connected to the first detection cavity, and the other end is connected to the air inlet docking area; A second air inlet channel is formed in the detection body, one end of the second air inlet channel is connected to the second detection cavity, and the other end is connected to the other air inlet docking area.
3. The penetration test structure according to claim 2, characterized in that: A first exhaust channel is further formed in the detection body, one end of the first exhaust channel is connected to the first detection cavity, and the other end is connected to the exhaust docking area; the positions where the first air inlet channel and the first exhaust channel are connected to the first detection cavity are symmetrically arranged relative to the first detection cavity; A second exhaust channel is also formed in the detection body, one end of the second exhaust channel is connected to the second detection cavity, and the other end is connected to the other exhaust docking area, and the positions where the second air inlet channel and the second exhaust channel are respectively connected to the second detection cavity are arranged symmetrically relative to the second detection cavity.
4. The penetration test structure according to claim 3, characterized in that: The detection body is formed with a sealed air intake channel, a sealed air exhaust channel and a series channel, and the number of the sealed air intake channels is the same as that of the sealed air exhaust channels; wherein the number of the sealed air inlet channel and the number of the sealed air exhaust channel are both one, the annular isolation grooves are connected in series through the series channel, one end of the sealed air inlet channel and one end of the sealed air exhaust channel are respectively connected to the two outermost annular isolation grooves on the series path, the other end of the sealed air inlet channel is connected to one of the air inlet docking areas, and the other end of the sealed air exhaust channel is connected to one of the air exhaust docking areas; or, There are two sealed air inlet channels and two sealed air exhaust channels, wherein the two annular isolation grooves are connected through the series channel, wherein one end of one sealed air inlet channel and one end of one sealed air exhaust channel are respectively connected to the two annular isolation grooves connected in series, and one end of another sealed air inlet channel and one end of another sealed air exhaust channel are connected to the other annular isolation groove, and the other ends of the two sealed air inlet channels are respectively connected to the two air inlet docking areas or are both connected to one of the air inlet docking areas, and the other ends of the two sealed air exhaust channels are respectively connected to the two exhaust docking areas or are both connected to one of the exhaust docking areas.
5. The penetration test structure according to claim 4, characterized in that: An air intake docking groove is formed in the air intake docking area, an air intake portion and an air intake ring are arranged in the air intake docking groove, a first air intake hole is opened in the air intake portion, the air intake ring is sleeved outside the air intake portion and spaced from the air intake portion, and a second air intake hole is opened on the air intake ring; the sealed air intake channel is connected to one of the first air intake hole and the second air intake hole, and the first air intake channel or the second air intake channel is connected to the other of the first air intake hole and the second air intake hole; and / or An exhaust docking groove is formed in the exhaust docking area, an exhaust portion and an exhaust ring are arranged in the exhaust docking groove, a first exhaust hole is opened in the exhaust portion, the exhaust ring is sleeved outside the exhaust portion and spaced from the exhaust portion, and a second exhaust hole is opened on the exhaust ring; the sealed exhaust channel is connected to one of the first exhaust hole and the second exhaust hole, and the first exhaust channel or the second exhaust channel is connected to the other of the first exhaust hole and the second exhaust hole.
6. The penetration test structure according to claim 2, characterized in that: A first connecting channel and a first docking channel are formed in the permeable body, one end of the first docking channel and one end of the first connecting channel are both connected to the first permeable cavity, and the other end of the first docking channel and the other end of the first connecting channel are both connected to the surface of the permeable body forming the first permeable cavity; A second communication channel and a second docking channel are formed in the permeable body, one end of the second docking channel and one end of the second communication channel are both connected to the second permeable cavity, and the other end of the second docking channel and the other end of the second communication channel are both connected to the surface of the permeable body forming the second permeable cavity; The test surface of the detection body is also formed with a first infiltration air inlet hole, a first infiltration exhaust hole, a second infiltration air inlet hole and a second infiltration exhaust hole that penetrate into the mounting surface; when the infiltration body is set on the detection body, the other end of the first connecting channel is connected to the first infiltration air inlet hole, the other end of the first docking channel is connected to the first infiltration exhaust hole, the other end of the second connecting channel is connected to the second infiltration air inlet hole, and the other end of the second docking channel is connected to the second infiltration exhaust hole.
7. The penetration test structure according to claim 6, characterized in that: The positions where the first communicating channel and the first docking channel are connected to the first permeation cavity are symmetrically arranged relative to the first permeation cavity; the positions where the second communicating channel and the second docking channel are connected to the second permeation cavity are symmetrically arranged relative to the second permeation cavity.
8. The penetration test structure according to any one of claims 1 to 7, characterized in that: A sealing ring is provided in the annular sealing groove; or A protective air inlet channel and a protective air exhaust channel are formed in the permeable body, and both the protective air inlet channel and the protective air exhaust channel are communicated with the annular sealing groove.
9. The penetration test structure according to any one of claims 1 to 7, characterized in that: The area of the first detection cavity is consistent with the area of the second detection cavity; the area of the first permeation cavity is consistent with the area of the second permeation cavity; and / or The number of the second detection cavities is one, two or more. When the number of the second detection cavities is two or more, the second detection cavities are radially arranged with the first detection cavity as the center, and at least two annular isolation grooves are formed between two adjacent second detection cavities. The number of the second permeation cavities is consistent with the number of the second detection cavities, and each of the second permeation cavities can correspond to one of the second detection cavities. The number of the annular sealing grooves is greater than or equal to the number of the annular isolation grooves, and each of the annular isolation grooves can correspond to one of the annular sealing grooves.
10. A penetration tester, characterized in that: The penetration tester comprises the penetration test structure according to any one of claims 1 to 9.