CN201738295U - Probe for cone penetration test - Google Patents
Probe for cone penetration test Download PDFInfo
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- CN201738295U CN201738295U CN2010202817480U CN201020281748U CN201738295U CN 201738295 U CN201738295 U CN 201738295U CN 2010202817480 U CN2010202817480 U CN 2010202817480U CN 201020281748 U CN201020281748 U CN 201020281748U CN 201738295 U CN201738295 U CN 201738295U
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Abstract
The utility model relates to civil exploration instrument, and more particular to a probe for cone penetration test. A probe for cone penetration test is disclosed herein comprising a cone tip, a pore tip sleeve, a core pressure joint, a side wall friction cylinder, a first positioning retainer ring, a first O shaped sealing ring, a hollow shore, a cone tip sensor, a side wall sealing cylinder, a second O shaped sealing ring, a side wall sensor, a side wall shore, a third O shaped sealing ring, a second positioning retainer ring, a support pile casing, a fourth O shaped sealing ring, a circular connection flange, a circular socket, a sealing pile casing, a multi-core shielding cable, and a waterproof cable ferrule, wherein the right part of the cone tip is connected to the left part of the pore pressure joint, the left end part of the cone tip top sleeve being disposed between the cone tip and the pore pressure joint, the right part of the cone tip top sleeve sleeving on the left part of the pore pressure joint. The utility model has the advantages of simple structure and reliable waterproof sealing.
Description
Technical field
The utility model relates to a kind of geotechnique's prospecting plant and instrument, is specifically related to a kind of static sounding probe.
Background technology
Static sounding can be pressed into the mechanics parameter that obtains the soil body in the soil body process to be measured at probe, and wherein the doube bridge probe can obtain static point resistance, sidewall friction power; Three bridges probe can obtain static point resistance, sidewall friction power and pore water pressure.
At present, domestic static sounding doube bridge, three bridges its complex structure of popping one's head in, and can't solve problems such as waterproof, sealing at all; Though and external static sounding doube bridge, three bridges probe is simple in structure, waterproof sealing is effective, its sensor is disassembled the back at the sidewall friction tube and directly exposes, and is subjected to the influence of external force and external environment factor easily.
Summary of the invention
The purpose of this utility model is to provide a kind of simple in structure, reliable static sounding probe of waterproof sealing.
To achieve these goals, technical solution adopted in the utility model is: a kind of static sounding probe, it is characterized in that it comprises the awl point, awl pinnacle cover, connector is pressed in the hole, the sidewall friction tube, first positioning retainer ring, the one O RunddichtringO, hollow fore-set, bore sharp sensor, the sidewall sealing drum, the 2nd O RunddichtringO, the sidewall sensor, the sidewall fore-set, the 3rd O RunddichtringO, second positioning retainer ring, support casing, the 4th O RunddichtringO, the air plug adpting flange, the aviation socket, the sealing casing, shielded multiconductor cable, the water-proof cable cutting ferrule
The right part of awl point presses the left part of connector to be threaded with the hole, and press between the connector at awl point and hole the left part of awl pinnacle cover, and the right part of awl pinnacle cover is enclosed within the hole and presses on the left part of connector;
The left part of sidewall sealing drum is enclosed within the right part that connector is pressed in the hole, and the left part of sidewall sealing drum and hole are pressed between the connector and be provided with first positioning retainer ring and an O RunddichtringO; The left part of sidewall friction tube is enclosed within on the right part of awl pinnacle cover, and the right part of sidewall friction tube is enclosed within on the left part of supporting casing, and the sidewall sealing drum is positioned at the sidewall friction tube; The right part of sidewall sealing drum is enclosed within the right part of hollow fore-set, and the left part of hollow fore-set is positioned at the sidewall sealing drum, is provided with the 3rd O RunddichtringO and second positioning retainer ring between the right part of sidewall sealing drum and the right part of hollow fore-set; The hole presses the right part of connector to be threaded with the left part of hollow fore-set; The right part of hollow fore-set is threaded with the left part of supporting casing; Be provided with the sharp sensor installation cavity of awl, sidewall fore-set installation cavity between hollow fore-set and the sidewall sealing drum, bore sharp sensor installation cavity and be positioned at the left side of sidewall fore-set installation cavity, bore the sharp sensor of awl is installed in the sharp sensor installation cavity, bore sharp sensor and paste on the hollow fore-set, hollow fore-set is linked to each other with the aviation socket by lead; In the sidewall fore-set installation cavity sidewall fore-set is installed, be provided with the 2nd O RunddichtringO between sidewall fore-set and the hollow fore-set, the 2nd O RunddichtringO is positioned at the left side of the 4th aperture, surround sidewall sensor installation cavity between sidewall fore-set and the sidewall sealing drum, be provided with the sidewall sensor in the sidewall sensor installation cavity, the sidewall sensor sticks on the sidewall fore-set, and the sidewall sensor is linked to each other with the aviation socket by lead; Be provided with first through hole in the hollow fore-set, the sidewall fore-set is provided with the 4th aperture, and hollow fore-set is provided with the 5th aperture, and the 5th aperture is connected with first through hole, and the 4th aperture is connected with the 5th aperture, sidewall sensor installation cavity respectively; Support in the casing and be provided with second through hole, second through hole is connected with first through hole, and the right part that supports casing is threaded with the left part of sealing casing, is provided with the 4th O RunddichtringO between the right part of the left end of sealing casing and support casing; Air plug adpting flange, aviation socket all are positioned at the sealing casing, the air plug adpting flange is connected by bolt with the right-hand member that supports casing, the aviation socket is threaded with the air plug adpting flange, the aviation socket links to each other with shielded multiconductor cable, shielded multiconductor cable is with the water-proof cable cutting ferrule outward, and the water-proof cable cutting ferrule is threaded with the right part of sealing casing.
The right part of described awl point and hole are pressed the left part of connector to be threaded and one are bored sharp connector, the left part of boring sharp connector is threaded with the right part of awl point, boring the right part of sharp connector presses the left part of connector to be threaded with the hole, the right part of awl point is with permeable circle, permeable circle is between awl point and awl pinnacle cover, and the left part of awl pinnacle cover is enclosed within on the sharp connector of awl; Permeable circle is the loose structure (loose structure is made of a plurality of first apertures) of even compact, the right part of awl point is provided with second aperture, bore sharp connector and be provided with the 3rd aperture, the hole is pressed in the connector and is provided with hole pressure sensor installing hole, first aperture is connected with second aperture, and second aperture is connected with the 3rd aperture, and the 3rd aperture is connected with hole pressure sensor installing hole, the hole pressure sensor is positioned at hole pressure sensor installing hole, and the hole pressure sensor is linked to each other with the aviation socket by lead.
The beneficial effects of the utility model are: adopt said structure, it is simple in structure, waterproof sealing is reliable.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment 1;
Fig. 2 is the structural representation of the utility model embodiment 2;
Fig. 3 is the structural representation of awl point among the embodiment 1;
Fig. 4 is the structural representation that embodiment 1 mesopore is pressed connector;
Fig. 5 is the structural representation of awl point among the embodiment 2;
Fig. 6 is the structural representation of the sharp connector of awl among the embodiment 2;
Fig. 7 is the structural representation of permeable circle among the embodiment 2;
Fig. 8 is the structural representation (among embodiment 1 and the embodiment 2) of awl pinnacle cover;
Fig. 9 is the structural representation that embodiment 2 mesopores are pressed connector;
Figure 10 is the structural representation of embodiment 2 mesopore pressure sensors;
Figure 11 is the structural representation (among embodiment 1 and the embodiment 2) of sidewall friction tube;
Figure 12 is the structural representation (among embodiment 1 and the embodiment 2) of first positioning retainer ring;
Figure 13 is the structural representation (among embodiment 1 and the embodiment 2) of hollow fore-set;
Figure 14 is the structural representation (among embodiment 1 and the embodiment 2) of sidewall sealing drum;
Figure 15 is the structural representation (among embodiment 1 and the embodiment 2) of second positioning retainer ring;
Figure 16 is the structural representation (among embodiment 1 and the embodiment 2) of sidewall fore-set;
Figure 17 is the structural representation that supports casing (among embodiment 1 and the embodiment 2);
Figure 18 is the structural representation (among embodiment 1 and the embodiment 2) of air plug adpting flange;
Figure 19 is the structural representation (among embodiment 1 and the embodiment 2) of sealing casing;
Among the figure: 1-bores point, and 2-bores sharp connector, the permeable circle of 3-, 4-awl pinnacle cover, connector, 6-hole pressure sensor are pressed in the 5-hole, 7-sidewall friction tube, 8-first positioning retainer ring, 9-the one O RunddichtringO, the hollow fore-set of 10-, 11-bores sharp sensor, 12-sidewall sealing drum, 13-the 2nd O RunddichtringO, 14-sidewall sensor, 15-sidewall fore-set, 16-the 3rd O RunddichtringO, 17-second positioning retainer ring, 18-supports casing, 19-the 4th O RunddichtringO, 20-air plug adpting flange, 21-aviation socket, 22-seals casing, 23-shielded multiconductor cable, 24-water-proof cable cutting ferrule, 25-second aperture, 26-the 3rd aperture, 27-hole pressure sensor installing hole, 28-bores sharp sensor installation cavity, 29-first through hole, 30-the 4th aperture, 31-the 5th aperture, 32-sidewall sensor installation cavity, 33-second through hole.
The specific embodiment
Embodiment 1:
(with the difference of embodiment 2 be: remove the sharp connector 2 of awl, permeable circle 3, hole pressure sensor 6 as shown in Figure 1; Awl point 1 presses the structure of connector 5 different with the hole; The three bridges probe of embodiment 2 can be transformed to the doube bridge probe), the aviation socket 21 that do not draw among Fig. 1, shielded multiconductor cable 23, water-proof cable cutting ferrule 24.
A kind of static sounding probe (doube bridge probe), it comprises awl point 1, awl pinnacle cover 4, connector 5 is pressed in the hole, sidewall friction tube 7, first positioning retainer ring 8, the one O RunddichtringO 9, hollow fore-set 10, bore sharp sensor 11, sidewall sealing drum 12, the 2nd O RunddichtringO 13, sidewall sensor 14, sidewall fore-set 15, the 3rd O RunddichtringO 16, second positioning retainer ring 17, support casing 18, the 4th O RunddichtringO 19, air plug adpting flange 20, aviation socket 21, sealing casing 22, shielded multiconductor cable 23, water-proof cable cutting ferrule 24
The right part of awl point 1 presses the left part of connector 5 to be threaded with the hole, and press between the connector 5 at awl point 1 and hole the left part of awl pinnacle cover 4, and the left part of awl pinnacle cover 4 is enclosed within the right part of awl point 1, and the right part of awl pinnacle cover 4 is enclosed within the hole and presses on the left part of connector 5;
The left part of sidewall sealing drum 12 is enclosed within the right part that connector 5 is pressed in the hole, and the left part of sidewall sealing drum 12 and hole are pressed between the connector 5 and be provided with first positioning retainer ring 8 and an O RunddichtringO 9; The left part of sidewall friction tube 7 is enclosed within on the right part of awl pinnacle cover 4, and the right part of sidewall friction tube 7 is enclosed within on the left part of supporting casing 18, and sidewall sealing drum 12 is positioned at sidewall friction tube 7; The right part of sidewall sealing drum 12 is enclosed within the right part of hollow fore-set 10, and the left part of hollow fore-set 10 is positioned at sidewall sealing drum 12, is provided with the 3rd O RunddichtringO 16 and second positioning retainer ring 17 between the right part of the right part of sidewall sealing drum 12 and hollow fore-set 10; The hole presses the right part of connector 5 to be threaded with the left part of hollow fore-set 10; The right part of hollow fore-set 10 is threaded with the left part of supporting casing 18; Be provided with the sharp sensor installation cavity 28 of awl, sidewall fore-set installation cavity between hollow fore-set 10 and the sidewall sealing drum 12, bore sharp sensor installation cavity 28 and be positioned at the left side of sidewall fore-set installation cavity, bore the sharp sensor 11 of awl is installed in the sharp sensor installation cavity 28, bore sharp sensor 11 and paste on the hollow fore-set 10, hollow fore-set 10 is linked to each other with aviation socket 21 by lead; In the sidewall fore-set installation cavity sidewall fore-set 15 is installed, be provided with the 2nd O RunddichtringO 13 between sidewall fore-set 15 and the hollow fore-set 10, the 2nd O RunddichtringO 13 is positioned at the left side of the 4th aperture 30, surround the sidewall sensor installation cavity 32 of sealing between sidewall fore-set 15 and the sidewall sealing drum 12, be provided with sidewall sensor 14 in the sidewall sensor installation cavity 32, sidewall sensor 14 sticks on the sidewall fore-set 15, and sidewall sensor 14 is linked to each other with aviation socket 21 by lead; Be provided with first through hole 29 in the hollow fore-set 10, sidewall fore-set 15 is provided with the 4th aperture 30, hollow fore-set 10 is provided with the 5th aperture 31, the five apertures 31 and is connected with first through hole 29, and the 4th aperture 30 is connected with the 5th aperture 31, sidewall sensor installation cavity 32 respectively; Be provided with second through hole, 33, the second through holes 33 in the support casing 18 and be connected with first through hole 29, the right part that supports casing 18 is threaded with the left part of sealing casing 22, is provided with the 4th O RunddichtringO 19 between the right part of the left end of sealing casing 22 and support casing 18; Air plug adpting flange 20, aviation socket 21 all are positioned at sealing casing 22, air plug adpting flange 20 is connected by bolt with the right-hand member that supports casing 18, aviation socket 21 is threaded with air plug adpting flange 20, aviation socket 21 links to each other with shielded multiconductor cable 23, the shielded multiconductor cable 23 outer water-proof cable cutting ferrules 24 that are with, water-proof cable cutting ferrule 24 is threaded with the right part of sealing casing 22.
Static point resistance transmits: press connector 5 to pass to hollow fore-set 10 by awl point 1, awl pinnacle cover 4, hole, hollow fore-set 10 distortion backs are detected by the sharp sensor 11 of awl.
Sidewall friction power is transmitted: pass to sidewall fore-set 15 by sidewall friction tube 7, sidewall sealing drum 12, sidewall fore-set 15 distortion backs are detected by sidewall sensor 14.
Embodiment 2:
As shown in Figure 2, a kind of static sounding probe (three bridges probe), it comprises awl point 1, bore sharp connector 2, permeable circle 3, awl pinnacle cover 4, connector 5 is pressed in the hole, hole pressure sensor 6, sidewall friction tube 7, first positioning retainer ring 8, the one O RunddichtringO 9, hollow fore-set 10, bore sharp sensor 11, sidewall sealing drum 12, the 2nd O RunddichtringO 13, sidewall sensor 14, sidewall fore-set 15, the 3rd O RunddichtringO 16, second positioning retainer ring 17, support casing 18, the 4th O RunddichtringO 19, air plug adpting flange 20, aviation socket 21, sealing casing 22, shielded multiconductor cable 23, water-proof cable cutting ferrule 24
The right part of awl point 1 is threaded with the left part of the sharp connector 2 of awl, boring the right part of sharp connector 2 presses the left part of connector 5 to be threaded with the hole, the right part of awl point 1 is with permeable circle 3 (being the right part that permeable circle 3 is enclosed within awl point 1), permeable circle 3 is between awl point 1 and awl pinnacle cover 4, the left part of awl pinnacle cover 4 is enclosed within on the sharp connector 2 of awl, press between the connector 5 at awl point 1 and hole the left part of awl pinnacle cover 4, and the right part of awl pinnacle cover 4 is enclosed within the hole and presses on the left part of connector 5; Permeable circle 3 is the loose structure of even compact (loose structure is made of a plurality of first apertures), the right part of awl point 1 is provided with second aperture 25, bore sharp connector 2 and be provided with the 3rd aperture 26, the hole is pressed in the connector 5 and is provided with hole pressure sensor installing hole 27, first aperture is connected with second aperture 25, second aperture 25 is connected with the 3rd aperture 26, the 3rd aperture 26 is connected with hole pressure sensor installing hole 27, hole pressure sensor 6 is positioned at hole pressure sensor installing hole 27, and hole pressure sensor 6 is linked to each other with aviation socket 21 by lead;
The left part of sidewall sealing drum 12 is enclosed within the right part that connector 5 is pressed in the hole, and the left part of sidewall sealing drum 12 and hole are pressed between the connector 5 and be provided with first positioning retainer ring 8 and an O RunddichtringO 9; The left part of sidewall friction tube 7 is enclosed within on the right part of awl pinnacle cover 4, and the right part of sidewall friction tube 7 is enclosed within on the left part of supporting casing 18, and sidewall sealing drum 12 is positioned at sidewall friction tube 7; The right part of sidewall sealing drum 12 is enclosed within the right part of hollow fore-set 10, and the left part of hollow fore-set 10 is positioned at sidewall sealing drum 12, is provided with the 3rd O RunddichtringO 16 and second positioning retainer ring 17 between the right part of the right part of sidewall sealing drum 12 and hollow fore-set 10; The hole presses the right part of connector 5 to be threaded with the left part of hollow fore-set 10; The right part of hollow fore-set 10 is threaded with the left part of supporting casing 18; Be provided with the sharp sensor installation cavity 28 of awl, sidewall fore-set installation cavity between hollow fore-set 10 and the sidewall sealing drum 12, bore sharp sensor installation cavity 28 and be positioned at the left side of sidewall fore-set installation cavity, bore the sharp sensor 11 of awl is installed in the sharp sensor installation cavity 28, bore sharp sensor 11 and paste on the hollow fore-set 10, hollow fore-set 10 is linked to each other with aviation socket 21 by lead; In the sidewall fore-set installation cavity sidewall fore-set 15 is installed, be provided with the 2nd O RunddichtringO 13 between sidewall fore-set 15 and the hollow fore-set 10, the 2nd O RunddichtringO 13 is positioned at the left side of the 4th aperture 30, surround the sidewall sensor installation cavity 32 of sealing between sidewall fore-set 15 and the sidewall sealing drum 12, be provided with sidewall sensor 14 in the sidewall sensor installation cavity 32, sidewall sensor 14 sticks on the sidewall fore-set 15, and sidewall sensor 14 is linked to each other with aviation socket 21 by lead; Be provided with first through hole 29 in the hollow fore-set 10, first through hole 29 is connected with hole pressure sensor installing hole 27, sidewall fore-set 15 is provided with the 4th aperture 30, hollow fore-set 10 is provided with the 5th aperture 31, the 5th aperture 31 is connected with first through hole 29, and the 4th aperture 30 is connected with the 5th aperture 31, sidewall sensor installation cavity 32 respectively; Be provided with second through hole, 33, the second through holes 33 in the support casing 18 and be connected with first through hole 29, the right part that supports casing 18 is threaded with the left part of sealing casing 22, is provided with the 4th O RunddichtringO 19 between the right part of the left end of sealing casing 22 and support casing 18; Air plug adpting flange 20, aviation socket 21 all are positioned at sealing casing 22, air plug adpting flange 20 is connected by bolt with the right-hand member that supports casing 18, aviation socket 21 is threaded with air plug adpting flange 20, aviation socket 21 links to each other with shielded multiconductor cable 23, the shielded multiconductor cable 23 outer water-proof cable cutting ferrules 24 that are with, water-proof cable cutting ferrule 24 is threaded with the right part of sealing casing 22.
Static point resistance transmits: press connector 5 to pass to hollow fore-set 10 by awl point 1, awl pinnacle cover 4, hole, hollow fore-set 10 distortion backs are detected by the sharp sensor 11 of awl.
Sidewall friction power is transmitted: pass to sidewall fore-set 15 by sidewall friction tube 7, sidewall sealing drum 12, sidewall fore-set 15 distortion backs are detected by sidewall sensor 14.
Pore water pressure transmits: pass to hole pressure sensor 6 through first aperture, second aperture 25, the 3rd aperture 26, hole pressure sensor installing hole 27.
Claims (2)
1. static sounding probe, it is characterized in that it comprises awl point (1), awl pinnacle cover (4), connector (5) is pressed in the hole, sidewall friction tube (7), first positioning retainer ring (8), the one O RunddichtringO (9), hollow fore-set (10), bore sharp sensor (11), sidewall sealing drum (12), the 2nd O RunddichtringO (13), sidewall sensor (14), sidewall fore-set (15), the 3rd O RunddichtringO (16), second positioning retainer ring (17), support casing (18), the 4th O RunddichtringO (19), air plug adpting flange (20), aviation socket (21), sealing casing (22), shielded multiconductor cable (23), water-proof cable cutting ferrule (24)
The right part of awl point (1) presses the left part of connector (5) to be threaded with the hole, and the left part of awl pinnacle cover (4) is positioned at awl point (1) and press between the connector (5) in the hole, and the right part of awl pinnacle cover (4) is enclosed within the hole and presses on the left part of connector (5);
The left part of sidewall sealing drum (12) is enclosed within the right part that connector (5) is pressed in the hole, and the left part of sidewall sealing drum (12) and hole are pressed between the connector (5) and be provided with first positioning retainer ring (8) and an O RunddichtringO (9); The left part of sidewall friction tube (7) is enclosed within on the right part of awl pinnacle cover (4), and the right part of sidewall friction tube (7) is enclosed within on the left part of supporting casing (18), and sidewall sealing drum (12) is positioned at sidewall friction tube (7); The right part of sidewall sealing drum (12) is enclosed within the right part of hollow fore-set (10), the left part of hollow fore-set (10) is positioned at sidewall sealing drum (12), is provided with the 3rd O RunddichtringO (16) and second positioning retainer ring (17) between the right part of the right part of sidewall sealing drum (12) and hollow fore-set (10); The hole presses the right part of connector (5) to be threaded with the left part of hollow fore-set (10); The right part of hollow fore-set (10) is threaded with the left part of supporting casing (18); Be provided with awl sharp sensor installation cavity (28), sidewall fore-set installation cavity between hollow fore-set (10) and the sidewall sealing drum (12), bore sharp sensor installation cavity (28) and be positioned at the left side of sidewall fore-set installation cavity, bore awl sharp sensor (11) is installed in the sharp sensor installation cavity (28), bore sharp sensor (11) and paste on the hollow fore-set (10), hollow fore-set (10) is linked to each other with aviation socket (21) by lead; Sidewall fore-set (15) is installed in the sidewall fore-set installation cavity, be provided with the 2nd O RunddichtringO (13) between sidewall fore-set (15) and the hollow fore-set (10), the 2nd O RunddichtringO (13) is positioned at the left side of the 4th aperture (30), surround sidewall sensor installation cavity (32) between sidewall fore-set (15) and the sidewall sealing drum (12), be provided with sidewall sensor (14) in the sidewall sensor installation cavity (32), sidewall sensor (14) sticks on the sidewall fore-set (15), and sidewall sensor (14) is linked to each other with aviation socket (21) by lead; Be provided with first through hole (29) in the hollow fore-set (10), sidewall fore-set (15) is provided with the 4th aperture (30), hollow fore-set (10) is provided with the 5th aperture (31), the 5th aperture (31) is connected with first through hole (29), and the 4th aperture (30) is connected with the 5th aperture (31), sidewall sensor installation cavity (32) respectively; Support in the casing (18) and be provided with second through hole (33), second through hole (33) is connected with first through hole (29), the right part that supports casing (18) is threaded with the left part of sealing casing (22), is provided with the 4th O RunddichtringO (19) between the right part of the left end of sealing casing (22) and support casing (18); Air plug adpting flange (20), aviation socket (21) all are positioned at sealing casing (22), air plug adpting flange (20) is connected by bolt with the right-hand member that supports casing (18), aviation socket (21) is threaded with air plug adpting flange (20), aviation socket (21) links to each other with shielded multiconductor cable (23), the outer water-proof cable cutting ferrule (24) that is with of shielded multiconductor cable (23), water-proof cable cutting ferrule (24) is threaded with the right part of sealing casing (22).
2. a kind of static sounding probe according to claim 1, it is characterized in that: the right part of described awl point (1) and hole are pressed the left part of connector (5) to be threaded and one are bored sharp connector (2), the left part of boring sharp connector (2) is threaded with the right part of awl point (1), boring the right part of sharp connector (2) presses the left part of connector (5) to be threaded with the hole, the right part of awl point (1) is with permeable circle (3), permeable circle (3) is positioned between awl point (1) and the awl pinnacle cover (4), and the left part of awl pinnacle cover (4) is enclosed within on the sharp connector of awl (2); Permeable circle (3) is the loose structure of even compact, the right part of awl point (1) is provided with second aperture (25), bore sharp connector (2) and be provided with the 3rd aperture (26), the hole is pressed in the connector (5) and is provided with hole pressure sensor installing hole (27), first aperture is connected with second aperture (25), second aperture (25) is connected with the 3rd aperture (26), the 3rd aperture (26) is connected with hole pressure sensor installing hole (27), hole pressure sensor (6) is positioned at hole pressure sensor installing hole (27), hole pressure sensor (6) is linked to each other with aviation socket (21) by lead, and first through hole (29) is connected with hole pressure sensor installing hole (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202817480U CN201738295U (en) | 2010-08-03 | 2010-08-03 | Probe for cone penetration test |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202817480U CN201738295U (en) | 2010-08-03 | 2010-08-03 | Probe for cone penetration test |
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|---|---|
| CN201738295U true CN201738295U (en) | 2011-02-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2010202817480U Expired - Lifetime CN201738295U (en) | 2010-08-03 | 2010-08-03 | Probe for cone penetration test |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102518106A (en) * | 2011-12-13 | 2012-06-27 | 东南大学 | Method for determining the lateral earth pressure based on the multi-functional piezocone penetration test probe |
| CN102900064A (en) * | 2012-11-14 | 2013-01-30 | 安徽华电工程咨询设计有限公司 | Micro static force penetrometer |
| WO2015024310A1 (en) | 2013-08-22 | 2015-02-26 | 中交第三航务工程勘察设计院有限公司 | Shipborne truss combined in-situ testing platform |
| CN105403336A (en) * | 2015-12-16 | 2016-03-16 | 东南大学 | Miniaturized full-bridge sounding test probe |
| CN105804040A (en) * | 2016-05-05 | 2016-07-27 | 中国能源建设集团江苏省电力设计院有限公司 | Minitype double-bridge probe for static cone penetration tests |
| CN106759215A (en) * | 2016-12-02 | 2017-05-31 | 东南大学 | A kind of multifunction digital seismic wave hole pressure touching methods test system |
| CN109541180A (en) * | 2018-12-06 | 2019-03-29 | 青岛海洋地质研究所 | A kind of dedicated static sounding probe of hydrate reservoir |
| CN114277757A (en) * | 2021-12-17 | 2022-04-05 | 中国计量大学 | Mechanical structure of multi-variable ring column hole pressure static sounding probe for one-rod measurement of soft and hard soil layers |
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2010
- 2010-08-03 CN CN2010202817480U patent/CN201738295U/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102518106A (en) * | 2011-12-13 | 2012-06-27 | 东南大学 | Method for determining the lateral earth pressure based on the multi-functional piezocone penetration test probe |
| CN102900064A (en) * | 2012-11-14 | 2013-01-30 | 安徽华电工程咨询设计有限公司 | Micro static force penetrometer |
| CN102900064B (en) * | 2012-11-14 | 2014-10-29 | 安徽华电工程咨询设计有限公司 | Micro static force penetrometer |
| WO2015024310A1 (en) | 2013-08-22 | 2015-02-26 | 中交第三航务工程勘察设计院有限公司 | Shipborne truss combined in-situ testing platform |
| CN105403336A (en) * | 2015-12-16 | 2016-03-16 | 东南大学 | Miniaturized full-bridge sounding test probe |
| CN105403336B (en) * | 2015-12-16 | 2018-06-12 | 东南大学 | A kind of miniature full-bridge feeler inspection probe |
| CN105804040A (en) * | 2016-05-05 | 2016-07-27 | 中国能源建设集团江苏省电力设计院有限公司 | Minitype double-bridge probe for static cone penetration tests |
| CN106759215A (en) * | 2016-12-02 | 2017-05-31 | 东南大学 | A kind of multifunction digital seismic wave hole pressure touching methods test system |
| CN106759215B (en) * | 2016-12-02 | 2019-03-05 | 东南大学 | A kind of multifunction digital seismic wave hole pressure touching methods test macro |
| CN109541180A (en) * | 2018-12-06 | 2019-03-29 | 青岛海洋地质研究所 | A kind of dedicated static sounding probe of hydrate reservoir |
| CN114277757A (en) * | 2021-12-17 | 2022-04-05 | 中国计量大学 | Mechanical structure of multi-variable ring column hole pressure static sounding probe for one-rod measurement of soft and hard soil layers |
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