Penetration test structure and penetration tester
By using annular isolation grooves and sealing grooves in the penetration test structure and using flow sealing medium, the problem of insufficient sealing performance of traditional devices is solved, efficient sealing effect and accurate transmittance testing are achieved, and the structural complexity is avoided .
Patent Information
- Application Number
- CN202411582125.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-07
- Publication Date
- 2024-12-27
AI Technical Summary
Traditional transmittance testing devices have problems with insufficient sealing performance, and increasing structural complexity to improve sealing performance will increase manufacturing costs.
Design a penetration testing structure, including the detection body and the permeation body, by setting an annular isolation groove and sealing groove between the detection cavity and the permeation cavity, and sealing and isolation with a flowing sealing medium, adapting to the deformation of the test sample and preventing gas leakage .
It effectively improves the sealing effect, avoids increasing structural complexity, and ensures the accuracy and detection efficiency of test results.
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Figure CN119198489A_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 an important test in the field of materials science and is widely used in the evaluation of packaging materials. Gas permeability testing devices are usually used to determine the permeability of materials to gases and other media, including but not limited to differential pressure method and equal pressure method. The test principle is to use a sample to separate the test chamber into an upper chamber and a lower chamber, where the upper chamber is filled with test gas, and the lower chamber is connected to a gas sensor to monitor the gas permeation in real time, thereby evaluating the gas permeability of the sample.
[0003] Traditional permeability test devices are mainly divided into two types: single-chamber and multi-chamber, according to the number of test chambers. Single-chamber equipment can only test a single sample, which limits the efficiency of the test. Multi-chamber equipment can test multiple gases and other media on the sample at the same time, which significantly improves the efficiency of the test. However, the insufficient sealing performance between the test chambers will have an adverse effect on the accuracy of the test results. In order to improve the sealing performance, it is often necessary to increase the complexity of the structure, which in turn leads to increased manufacturing costs. Summary of the invention
[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, the penetration test structure comprises a detection body and a penetration body, 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 arranged on the outer side of the first detection cavity, at least two annular isolation grooves arranged at intervals are formed between the first detection cavity and the second detection cavity, the outer side of the second detection cavity is also provided with an annular isolation groove arranged at intervals from the second detection cavity, the annular isolation groove is 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 is an annular groove, the second penetration cavity is arranged on the outer side of the first penetration cavity, at least two annular sealing grooves arranged at intervals are formed between the first penetration cavity and the second penetration cavity, the outer side of the second penetration cavity is also provided with an annular sealing groove arranged at intervals from the second penetration cavity; When the permeable body is disposed on the detection body, the first permeable cavity is opposite to the first detection cavity, the second permeable cavity is opposite to the second detection cavity, and each of the annular isolation grooves is opposite to a corresponding annular sealing groove.
[0006] 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 arranged at intervals.
[0007] 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.
[0008] In one of the embodiments, 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 symmetrically arranged relative to the first detection cavity.
[0009] 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 symmetrically arranged relative to the second detection cavity.
[0010] In one embodiment, a sealed air inlet channel, a sealed exhaust channel and a series channel are formed in the detection body, and the number of the sealed air inlet channels is the same as that of the sealed exhaust channels; wherein, the number of the sealed air inlet 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 inlet 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 inlet channel is connected to one of the air inlet docking areas, and the other end of the sealed exhaust channel is connected to one of the exhaust docking areas.
[0011] In one embodiment, the number of the sealed air inlet channels and the number of 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, 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, 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.
[0012] In one of the embodiments, an air intake docking groove is formed in the air intake docking area, an air intake part and an air intake ring are arranged in the air intake docking groove, a first air intake hole is opened in the air intake part, the air intake ring is sleeved outside the air intake part and spaced apart from the air intake part, and a second air intake hole is opened on the air intake ring; the sealed air intake passage is connected to one of the first air intake hole and the second air intake hole, and the first air intake passage or the second air intake passage is connected to the other of the first air intake hole and the second air intake hole.
[0013] In one of the embodiments, 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 apart 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.
[0014] 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.
[0015] 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.
[0016] In one embodiment, a first infiltration air inlet hole, a first infiltration air exhaust hole, a second infiltration air inlet hole and a second infiltration air exhaust hole are formed on the test surface of the detection body, and when the infiltration body is arranged 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 connecting 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 hole, and the other end of the second connecting channel is connected to the second infiltration air exhaust hole.
[0017] In one embodiment, the positions where the first connecting channel and the first docking channel are connected to the first osmosis chamber are symmetrically arranged relative to the first osmosis chamber; the positions where the second connecting channel and the second docking channel are connected to the second osmosis chamber are symmetrically arranged relative to the second osmosis chamber.
[0018] In one of the embodiments, a sealing ring is arranged in the annular sealing groove.
[0019] In one of the embodiments, 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 connected to the annular sealing groove.
[0020] 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 permeation cavity is consistent with the area of the second permeation cavity.
[0021] 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.
[0022] A penetration tester comprises the penetration test structure as described above.
[0023] In the above-mentioned penetration test structure and penetration tester, the sample to be tested is arranged between the penetration body and the detection body, and then different test media can be introduced into the first detection cavity and the second detection cavity respectively. The test medium in the first detection cavity can penetrate into the first penetration cavity through the sample, and the test medium in the second detection cavity can penetrate into the second penetration cavity through the sample, so that the transmittance test of the two test media can be realized for the sample to be tested at the same time. Since there are at least two annular isolation grooves arranged at intervals between the first detection cavity and the second detection cavity, the two annular isolation grooves are introduced with sealing media, and the annular isolation groove located on the inner side can isolate and protect the first detection cavity, and the annular isolation groove on the outer side and the annular isolation groove on the outer side of the second detection cavity can isolate and protect the second detection cavity, effectively realizing the sealing isolation of the first detection cavity and the second detection cavity. At the same time, the flowing sealing medium is introduced, which can effectively fill each position of the annular isolation groove. If the sample is deformed at the relative position of the annular sealing groove and the annular isolation groove, the flowing sealing medium can also adapt to the deformation of the sample for sealing. And the flowing sealing medium can form a certain pressure area in the annular sealing groove, thereby preventing the gas leakage in the first detection cavity and the second detection cavity. BRIEF DESCRIPTION OF THE DRAWINGS
[0024] The drawings constituting a part of the present application are used to provide a further understanding of the present application. The illustrative embodiments of the present application and their descriptions are used to explain the present application and do not constitute an improper limitation on the present application.
[0025] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings required for use in the description of the embodiments will be briefly introduced below. 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 creative work.
[0026] 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 according to the true scale.
[0027] Figure 1 Detailed description of a penetration test structure in one embodiment.
[0028] Figure 2 for Figure 1 The main view of the detection entity in .
[0029] Figure 3 for Figure 2 The front view of the internal structure of the detection body is shown.
[0030] Figure 4 for Figure 2 Sectional view along line AA.
[0031] Figure 5 for Figure 2 Sectional view along line BB.
[0032] Figure 6 for Figure 2 Cross-sectional view along line CC.
[0033] Figure 7 for Figure 1 Schematic diagram of the structure of the detection entity in another perspective.
[0034] Figure 8 for Figure 1 Schematic diagram of the structure of the penetration entity.
[0035] Fig. 9 for Figure 8 A front view of the infiltration body is shown.
[0036] Fig.10 for Fig. 9 A front view of the internal structure of the infiltration body is shown.
[0037] Fig.11 for Fig. 9 Cross-sectional view along line DD.
[0038] Fig.12 for Fig. 9 Cross-sectional view along line EE.
[0039] Description of reference numerals: Penetration test structure 10; test body 100; test surface 101; mounting surface 102; first test cavity 110; first air inlet channel 112; first exhaust channel 114; second test cavity 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 outlet hole 162; second infiltration air inlet hole 163; second infiltration air outlet 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
[0040] In order to make the above-mentioned purposes, features and advantages of the present application more obvious and easy to understand, the specific implementation methods of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without violating the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.
[0041] See also Figure 1 The penetration test structure 10 in one embodiment of the application can at least improve the sealing effect and avoid increasing the complexity of the structure. The penetration test structure 10 includes a detection body 100 and a penetration body 200. The sample to be tested is arranged 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 transmittance of the sample to be tested is detected.
[0042] See also 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, and the second detection chamber 120 is provided on the outer side of the first detection chamber 110, and at least two annular isolation grooves 130 are formed between the first detection chamber 110 and the second detection chamber 120, and an annular isolation groove 130 is also provided on the outer side of the second detection chamber 120 and is spaced from the second detection chamber 120, and the annular isolation groove 130 is used to pass a sealing medium. The annular isolation groove 130 can achieve sealing and isolation of the first detection chamber 110 and the second detection chamber 120.
[0043] See also Figure 8 and Fig. 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, and the second permeation cavity 220 is provided on the outer side of the first permeation cavity 210, and at least two annular sealing grooves 230 are formed between the first permeation cavity 210 and the second permeation cavity 220, and an annular sealing groove 230 is also provided on the outer side of the second permeation cavity 220 and is spaced from the second permeation cavity 220. By providing the annular sealing groove 230, the first permeation cavity 210 and the second permeation cavity 220 can be sealed and isolated. When the permeation body 200 is provided on the detection body 100, the first permeation cavity 210 is opposite to the first detection cavity 110, and the second permeation cavity 220 is opposite to the second detection cavity 120, and each annular isolation groove 130 is correspondingly opposite to an annular sealing groove 230. In this embodiment, the number of the annular isolation grooves 130 and the number of the annular sealing grooves 230 may be the same or different.
[0044] When in use, the sample to be tested is set 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, so that the permeability test of the two test media can be simultaneously performed 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 introduced with sealing media, and the annular isolation groove 130 located on the inner side can isolate and protect the first detection chamber 110, and the annular isolation groove 130 on the outer side and the annular isolation groove 130 on the outer side of the second detection chamber 120 can isolate and protect the second detection chamber 120, effectively realizing the sealed isolation of the first detection chamber 110 and the second detection chamber 120. At the same time, the flowing sealing medium can be effectively filled into each position of the annular isolation groove 130. If the sample is deformed at the position where the annular sealing groove 230 is opposite to the annular isolation groove 130, the flowing sealing medium can also adapt to the deformation of the sample to seal. Moreover, the flowing sealing medium can form a certain pressure area in the annular sealing groove 230 to prevent gas leakage in the first detection cavity 110 and the second detection cavity 120.
[0045] 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 area 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, which facilitates the statistics of subsequent test results. In other embodiments, the areas of the first detection chamber 110 and the second detection chamber 120 may not be consistent, and 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.
[0046] In one embodiment, the number of the second detection chambers 120 is one, two or more. When the number of the second detection chambers 120 is two or more, each second detection chamber 120 is radially spaced with the first detection chamber 110 as the center, and at least two annular isolation grooves 130 are formed between two adjacent second detection chambers 120. The number of second permeation chambers 220 is consistent with the number of second detection chambers 120, and each second permeation chamber 220 can correspond to a second detection chamber 120. The number of annular sealing grooves 230 is greater than or equal to the number of annular isolation grooves 130, and each annular isolation groove 130 can correspond to an annular sealing groove 230. The number of the second detection chamber 120 of the present application is one, and the first detection chamber 110 and the second detection chamber 120 are used for the detection of oxygen and water vapor respectively. In other embodiments, the number of the second detection chambers 120 can be two or more. By setting more second detection chambers 120, more test media can be tested synchronously, further improving the 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.
[0047] See also Figure 1 and Figure 7 In one embodiment, the two opposite 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, and an air intake docking area and an exhaust docking area are formed on the mounting surface 102, the number of the air intake docking area and the number of the exhaust docking area are consistent with the number of the detection cavities, and are both arranged at intervals. By arranging the air intake docking area and the exhaust docking area on the mounting surface 102 of the detection body 100, it is convenient to realize the air intake or exhaust of the first detection cavity 110 and the second detection cavity 120 from the same side, and improve the convenience of installing and docking the air intake and exhaust pipelines.
[0048] See also 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.
[0049] Specifically, a first exhaust channel 114 is also formed in the detection body 100, one end of the first exhaust channel 114 is connected to the first detection chamber 110, and the other end of the first exhaust channel 114 is connected to an exhaust docking area. The first air intake channel 112 is used to intake air into the first detection chamber 110, and the first exhaust channel 114 is used to discharge gas in the first detection chamber 110, and the isobaric method can be used to perform transmittance detection on the sample. In other embodiments, the first exhaust channel 114 can be omitted, so that the first detection chamber 110 can perform transmittance detection on the sample using the differential pressure method.
[0050] Furthermore, the positions where the first air inlet channel 112 and the first exhaust channel 114 are connected to the first detection chamber 110 are arranged symmetrically 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 in the first detection chamber 110 and then discharged through the first exhaust channel 114. Furthermore, the lengths of the first air inlet channel 112 and the first exhaust channel 114 are the same. Through the symmetrical arrangement structure, when in use, one of the channels can be selected as the first air inlet channel 112 and the other channel as the first exhaust channel 114, thereby improving the convenience of use.
[0051] See also 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.
[0052] Specifically, a second exhaust channel 124 is formed in the detection body 100, one end of the second exhaust channel 124 is connected to the second detection chamber 120, and the other end of the second exhaust channel 124 is connected to another exhaust docking area. The second air intake channel 122 is used to intake air into the second detection chamber 120, and the second exhaust channel 124 is used to discharge gas from the second detection chamber 120. In the second detection chamber 120, the isobaric method can be used to perform transmittance detection on the sample. In other embodiments, the second exhaust channel 124 can be omitted, so that the second detection chamber 120 can perform transmittance detection on the sample using the differential pressure method.
[0053] Furthermore, the positions where the second air inlet channel 122 and the second exhaust channel 124 are connected to the second detection chamber 120 are arranged symmetrically relative to the second detection chamber 120. When the test medium enters the second detection chamber 120 from the second air inlet channel 122, it is convenient to be uniformly diffused in the second detection chamber 120 and then discharged. Furthermore, the lengths of the second air inlet channel 122 and the second exhaust channel 124 are the same. When in use, one channel can be selected as the second air inlet channel 122 and the other channel as the second exhaust channel 124 to improve the convenience of use.
[0054] 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, and 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 circulating 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.
[0055] In other embodiments, the permeation body 200 may also be formed with a protective air inlet channel and a protective air exhaust channel, both of which are connected to 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 possibility of gas leakage is reduced by introducing protective gas. Specifically, the annular sealing grooves 230 may be partially connected in series, or not connected in series at all, and protective gas may be introduced into each annular sealing groove 230.
[0056] See also 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 in the detection body 100, and the number of the sealed air inlet channels 131 and the sealed air exhaust channels 132 is the same; wherein, the number of the sealed air inlet channels 131 and the sealed air exhaust channels 132 are both one, and each annular isolation groove 130 is connected in series through 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, and 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 each annular isolation groove 130 in series, it is only necessary to control the sealing medium to enter through a sealed air inlet channel 131 and to be discharged through a sealed air exhaust channel 132.
[0057] In another embodiment, the number of sealed air inlet channels 131 and sealed air exhaust channels 132 are both two, wherein two annular isolation grooves 130 are connected through a series channel 133, wherein one end of a sealed air inlet channel 131 and one end of a sealed air exhaust channel 132 are respectively connected to the two annular isolation grooves 130 connected in series, one end of another sealed air inlet channel 131 and one end of another sealed air exhaust channel 132 are connected to another annular isolation groove 130, the other ends of the two sealed air inlet channels 131 are respectively connected to 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 132 are respectively connected to two air exhaust docking areas or are both 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, so as to facilitate simultaneous docking of the air inlet pipeline joints; the same applies to the air exhaust. For example, in this embodiment, there are two intake docking areas and two exhaust docking areas, so the number of sealed intake channels 131 and sealed exhaust channels 132 is less than or equal to two, so as to avoid increasing the intake and exhaust docking areas due to the need to pass the sealing medium through the annular isolation groove 130.
[0058] Specifically, the two annular isolation grooves 130 adjacent to the second detection cavity 120 are connected via a series channel 133 , so that the inner and outer sides of the second detection cavity 120 are isolated and sealed by using the same sealing medium.
[0059] In this embodiment, the position where the sealed air inlet channel 131 is connected to the annular isolation groove 130 and the position where the sealed air exhaust channel 132 is connected to the annular isolation groove 130 are arranged symmetrically with respect to the annular isolation groove 130. When the sealing medium enters the annular isolation groove 130, it can be discharged after uniform diffusion, so that the sealing medium effectively fills the annular isolation groove 130.
[0060] In other embodiments, a sealed air inlet channel 131 and a sealed air exhaust channel 132 may be connected to each annular isolation groove 130. Alternatively, some of the annular isolation grooves 130 may be connected in series. The number of sealed air inlet channels 131 may be less than or equal to the number of air inlet docking areas, and the number of sealed air exhaust channels 132 may be less than or equal to the number of air exhaust docking areas.
[0061] See also 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 arranged in the air intake docking groove 141, a first air intake hole 144 is opened in the air intake portion 142, the air intake ring 143 is sleeved outside the air intake portion 142 and spaced from the air intake portion 142, and a second air intake hole 145 is opened on the air intake ring 143. The sealed air intake channel 131 is communicated with one of the first air intake hole 144 and the second air intake hole 145, and the first air intake channel 112 or the second air intake channel 122 is communicated 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, and the sealing medium can also enter the sealed air intake channel 131 through the air intake docking groove 141, thereby improving the installation docking efficiency. In other embodiments, the shape and structure of the air intake docking area can be determined by the shape of the docked air intake connector.
[0062] 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 arranged in the exhaust docking groove 151, a first exhaust hole 154 is opened in the exhaust portion 152, the exhaust ring 153 is sleeved outside the exhaust portion 152 and spaced from the exhaust portion 152, and a second exhaust hole 155 is opened on the exhaust ring 153. The sealed exhaust channel 132 is communicated with one of the first exhaust hole 154 and the second exhaust hole 155, and the first exhaust channel 114 or the second exhaust channel 124 is communicated with the other of the first exhaust hole 154 and the second exhaust hole 155. By providing the exhaust docking groove 151, the exhaust portion 152 and the exhaust ring 153, the installation docking efficiency can be improved.
[0063] 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 .
[0064] See also Fig.10 and Fig.11 In one embodiment, a first connecting channel 212 and a first docking channel 214 are formed in the permeable 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 permeable 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 permeable body 200 to form the first permeable cavity 210. Figure 1 , Figure 7 and Fig.10Specifically, the test surface 101 of the detection body 100 is also formed with a first infiltration air inlet 161 and a first infiltration air outlet 162 that penetrate to the mounting surface 102; when the infiltration body 200 is set on the detection body 100, the other end of the first connecting channel 212 is connected to the first infiltration air inlet 161, and the other end of the first connecting channel 214 is connected to the first infiltration air outlet 162. The first infiltration cavity 210 is connected to the mounting surface 102 through the first connecting channel 212 and the first infiltration air inlet 161, and is connected to the mounting surface 102 through the first connecting channel 214 and the first infiltration air outlet 162. The mounting surface 102 is formed with an air inlet docking area and an air outlet docking area, and the air inlet and air outlet of the first infiltration cavity 210 can be realized through one side of the mounting surface 102.
[0065] Specifically, the positions where the first connecting channel 212 and the first docking channel 214 are connected to the first permeation cavity 210 are symmetrically arranged relative to the first permeation cavity 210, so that the medium entering the first permeation cavity 210 can be uniformly diffused and then discharged. Furthermore, the lengths of the first connecting channel 212 and the first docking channel 214 are the same.
[0066] See also Fig.10 and Fig.12 In one embodiment, a second connecting channel 222 and a second docking channel 224 are formed in the permeable 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 permeable 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 permeable body 200 to form the second permeable cavity 220. Figure 1 , Figure 7 and Fig.10 In one embodiment, the test surface 101 of the detection body 100 is further formed with a second infiltration air inlet 163 and a second infiltration air outlet 164 that penetrate to the mounting surface 102. When the infiltration body 200 is set on the detection body 100, the other end of the second connecting channel 222 is connected to the second infiltration air inlet 163, and the other end of the second connecting channel 224 is connected to the second infiltration air outlet 164. In the same way, the air intake and exhaust of the first infiltration cavity 210, the second infiltration 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, thereby making it more convenient to connect and connect the gas path.
[0067] Specifically, the positions where the second connecting channel 222 and the second docking channel 224 are connected to the second permeation cavity 220 are symmetrically arranged relative to the second permeation cavity 220, so that the medium entering the second permeation cavity 220 can be uniformly diffused and then discharged. Furthermore, the second connecting channel 222 and the second docking channel 224 have the same length.
[0068] See also 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.
[0069] The two test areas in the above-mentioned penetration tester and penetration test structure 10 of the present application can be tested by the isobaric method, or by the pressure difference method, or the two areas can be tested by the isobaric method and the pressure difference method respectively, so as to realize the isobaric method-pressure difference method integrated machine, which is different from the traditional integrated machine. The above-mentioned penetration test structure 10 has a symmetrical gas path arrangement position to minimize the connection of the complex gas path. 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.
[0070] In the description of the present 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 the present 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 the present application.
[0071] In addition, if the terms "first" or "second" appear, these terms are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one of the features. In the description of this application, if the term "plurality" appears, "plurality" means at least two, such as two, three, etc., unless otherwise clearly and specifically defined.
[0072] In this application, unless otherwise clearly specified and limited, if the terms "installed", "connected", "connected", "fixed" and the like appear, these terms should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integrated connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to the specific circumstances.
[0073] In the present application, unless otherwise clearly specified and limited, if there is a description that a first feature is "above" or "below" a second feature, etc., or similar descriptions appear, it 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. Moreover, the first feature being "above", "above" and "above" the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. The first feature being "below", "below" and "below" the second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.
[0074] 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 a central 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 a central element at the same time. 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 implementation method.
[0075] The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described 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.
[0076] The above-described embodiments only express several implementation methods of the present application, and the descriptions thereof are relatively specific and detailed, but they cannot be construed as limiting the scope of the patent application. It should be pointed out that, for a person of ordinary skill in the art, several variations and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application. Therefore, the protection scope of the patent application shall be subject to the attached claims.
Claims
1. A penetration test structure, characterized in that: The penetration test structure includes: A detection body, wherein a first detection cavity and a second detection cavity are provided on the detection body, wherein the second detection cavity is an annular groove, and the second detection cavity is provided on the outer side of the first detection cavity, and 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, and the annular isolation groove is used to pass a sealing medium; and A permeable body, wherein a first permeable cavity and a second permeable cavity are provided on the permeable body, 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 arranged at intervals are formed between the first permeable cavity and the second permeable cavity, and an annular sealing groove arranged at intervals from the second permeable cavity is further provided on the outer side of the second permeable cavity; When the permeable body is disposed on the detection body, the first permeable cavity is opposite to the first detection cavity, the second permeable 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 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 both 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 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 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 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 symmetrically arranged 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, and 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, 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, 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: The air intake docking area is formed with an air intake docking groove, 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 passage is connected to one of the first air intake hole and the second air intake hole, and the first air intake passage or the second air intake passage is connected to the other of the first air intake hole and the second air intake hole; and / or The exhaust docking area is formed with an exhaust docking groove, an exhaust part and an exhaust ring are arranged in the exhaust docking groove, a first exhaust hole is opened in the exhaust part, the exhaust ring is arranged outside the exhaust part and is spaced from the exhaust part, 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 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 forming the second permeable cavity; A first infiltration air inlet hole, a first infiltration air exhaust hole, a second infiltration air inlet hole and a second infiltration air exhaust hole are also formed on the test surface of the detection body, and penetrate into the mounting surface; when the infiltration body is arranged 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 connecting 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 hole, and the other end of the second connecting channel is connected to the second infiltration air exhaust hole.
7. The penetration test structure according to claim 6, characterized in that: The positions where the first connecting 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 connecting 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 arranged 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 as described in any one of claims 1-9.
