Monitoring radar

Abstract

The utility model discloses a monitoring radar which comprises a mounting seat, a machine body, a connecting piece, a shell and a probe. The body is connected with the mounting seat, the shell sleeves the probe, and the connecting piece is used for connecting the body with the shell; adjusting insertion holes are formed in the corresponding positions of the probe and the shell, and the multiple insertion holes are distributed in an arc shape, so that the monitoring angle of the probe in the vertical direction can be adjusted; a limiting jack is arranged at the joint of the connecting piece and the shell, and when the shell is connected with the connecting piece, a limiting piece penetrates through the limiting jack to be connected with the adjusting jack to adjust the monitoring angle of the probe in the vertical direction. The machine body is connected with the mounting base through a gear mechanism which is used for driving the machine body to rotate. Therefore, all-directional monitoring in the vertical direction and the horizontal direction can be achieved, multi-angle long-distance scanning extraction of tiny deformation and displacement information of the earth surface is conducted, and long-term or temporary stability monitoring of various slopes, geologic bodies and major projects is achieved.

Description

TECHNICAL FIELD

[0001] The utility model relates to radar technical field, specifically is a kind of monitoring radar. BACKGROUND

[0002] Radar application covers multiple fields, and it is an indispensable monitoring device in environmental monitoring, and the present application is suitable for monitoring in various environments, including: mine side slope long-term monitoring, mine collapse temporary monitoring, geological disaster hidden danger point long-term monitoring, tailing dam long-term monitoring and other environments.

[0003] At present, in prior art, disaster point environment is not the same, potential multiple point and multiple area hidden danger develop continuously, radar coverage area is not large enough, resulting in not accurate enough monitoring.

[0004] Therefore, the present application can realize the multi-angle long-distance scanning extraction of surface micro-deformation displacement information, realize the long-term or temporary stability monitoring of various slopes, geological bodies and major projects. UTILITY MODEL CONTENT

[0005] In order to solve the problems of disaster point environment in prior art, potential multiple point and multiple area hidden danger develop continuously, radar coverage area is not large enough, resulting in not accurate enough monitoring,

[0006] One purpose of the utility model is to provide a multi-angle long-distance scanning extraction of surface micro-deformation displacement information, to realize the long-term or temporary stability monitoring of various slopes, geological bodies and major projects.

[0007] The utility model realizes the following technical scheme:

[0008] The utility model provides a kind of monitoring radar provided by first aspect embodiment of the utility model, comprising: mounting seat, fuselage, connecting piece and probe;

[0009] The mounting seat is connected with the fuselage;

[0010] The front end of the fuselage is provided with connecting piece;

[0011] The connecting piece includes support and U-shaped frame;U-shaped frame is connected with support;The support is connected with one end of the fuselage, and the U-shaped frame is hingedly connected with the probe, and the probe can swing along the hinge connection;

[0012] The probe has a shell;

[0013] A plurality of adjusting insertion holes are provided on the shell, and the plurality of insertion holes are distributed in arc shape;

[0014] A plurality of limiting insertion holes are provided at the connecting piece and the shell connection, the limiting insertion hole corresponds with adjusting insertion hole, and limiting member is arranged on the limiting insertion hole;

[0015] When the shell is connected with the connecting piece, the limiting piece is connected with an adjusting hole through the limiting hole, and the swing angle of the probe is locked;

[0016] The mounting seat has a gear mechanism, and the mounting seat is connected with the fuselage through the gear mechanism.

[0017] Preferably, the gear mechanism comprises a first gear, a second gear and a motor.

[0018] The first gear is fixedly connected to a first connecting rod, and the first connecting rod is fixedly connected to the motor in the mounting seat.

[0019] The second gear is fixedly connected to a second connecting rod, and the second connecting rod is connected to a mounting plate.

[0020] The tooth surfaces of the first gear and the second gear are vertically engaged.

[0021] Preferably, a controller for controlling the start of the motor is arranged in the mounting seat.

[0022] Preferably, the first gear and the second gear are helical gears.

[0023] Preferably, a through hole is arranged on the bracket, the through hole is an oblong through hole, the bracket has a trapezoidal top structure, and the outer contour of the bracket gradually decreases from one end of the fuselage.

[0024] Preferably, the limiting piece is a bolt or a pin.

[0025] Preferably, the mounting seat, the fuselage, the connecting piece and the shell are made of stainless steel.

[0026] Preferably, the surfaces of the mounting seat, the fuselage, the connecting piece and the shell are covered with fluorocarbon paint.

[0027] Preferably, the outer shape of the fuselage has a trapezoidal top structure.

[0028] Preferably, the outer shape of the shell has a trapezoidal top structure.

[0029] Compared with the prior art, the utility model has the beneficial effects as follows:

[0030] The monitoring radar comprises a mounting base, a body, a probe, a shell and a connecting piece. The mounting base is connected with the body; the front end of the body is provided with the connecting piece; the connecting piece comprises a support and a U-shaped frame; one end of the support is connected with the body, and the U-shaped frame is hingedly connected with the probe, and the probe can swing along the hinge connection; the probe has the shell; a plurality of adjusting insertion holes are arranged on the shell in an arc shape; a plurality of limiting insertion holes are arranged at the connecting piece and the shell, the limiting insertion holes correspond to the adjusting insertion holes, and a limiting piece is arranged on the limiting insertion hole; when the shell is connected with the connecting piece, the limiting piece is connected with one adjusting insertion hole through the limiting insertion hole, and the swing angle of the probe is locked; the mounting base has a gear mechanism, the mounting base is connected with the body through the gear mechanism, and the gear mechanism is used for driving the body to rotate.

[0031] Therefore, the monitoring radar can realize omnidirectional monitoring in vertical and horizontal directions, multi-angle remote scanning and extraction of surface micro-deformation displacement information, and long-term or temporary stability monitoring of various slopes, geological bodies and major projects. BRIEF DESCRIPTION OF DRAWINGS

[0032] In order to more clearly illustrate the specific embodiments of the present application or the technical solutions in the prior art, the drawings used in the specific embodiments or the prior art description will be briefly introduced.

[0033] In all the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, each element or part is not necessarily drawn according to the actual scale.

[0034] Figure 1 A monitoring radar structure schematic view of the present application;

[0035] Figure 2 A monitoring radar shell partial schematic view of the present application;

[0036] Figure 3 A gear mechanism structure schematic view of the monitoring radar of the present application;

[0037] Explanation of the reference numerals:

[0038] 1-mounting base, 2-body, 3-connecting piece, 4-shell, 5-probe, 6-limiting piece, 101-first gear, 102-first connecting rod, 201-second gear, 202-second connecting rod, 203-mounting plate, 301-limiting insertion hole, 302-through hole, 303-U-shaped frame, 304-support, 401-adjusting insertion hole DETAILED DESCRIPTION

[0039] In order to more clearly understand the above-mentioned objectives, features and advantages of the present invention, the present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0040] The preferred embodiments of the present invention are described below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described herein are only used to illustrate and explain the present invention and are not used to limit the specific embodiments of the present invention.

[0041] like Figures 1 to 2 As shown, the monitoring radar provided by the embodiment of the first aspect of the present utility model includes: a mounting base 1, a fuselage 2, a connecting part 3 and a probe 5.

[0042] Specifically, it includes: a mounting base 1, a fuselage 2, a connecting member 3 and a probe 5; the mounting base 1 is connected to the fuselage 2; a connecting member 3 is provided at the front end of the fuselage 2, the connecting member 3 includes a bracket 304 and a U-shaped frame 303, and the U-shaped frame 303 is connected to the bracket 304; the bracket 304 is connected to the fuselage 2 at one end, and the U-shaped frame 303 is hingedly connected to the probe 5, and the probe 5 can swing along the hinge connection; a shell 4 matching the shape of the probe 5 is provided on the probe 5; an adjustment socket 401 is provided on the shell 4, and multiple sockets are distributed in an arc shape, which can adjust the monitoring angle of the probe 5, and multiple limit sockets 301 are provided at the connection between the connecting member 3 and the shell 4, the limit socket 301 corresponds to the adjustment socket 401, and a limit member 6 is passed through the limit socket 301.

[0043] When the housing 4 is connected to the U-shaped frame 303 , the limiting member 6 passes through the limiting socket 301 and is connected to an adjustment socket 401 , thereby locking the swing angle of the probe 5 . The limiting member 6 in this embodiment is a latch.

[0044] The mounting base 1 has a gear mechanism, and the mounting base 1 is connected to the body 2 via the gear mechanism, and the gear mechanism is used to drive the body 2 to rotate.

[0045] like Figure 1 As shown, the fuselage 2 and the shell 4 have a trapezoidal top structure. The trapezoidal top structure has a greater inclination, is less likely to accumulate rainwater, dust and other debris, and is easier to clean and maintain.

[0046] The bracket 304 of the connecting member 3 has a trapezoidal top structure, and the outer contour of the bracket 304 gradually decreases from the fuselage 2 to one end of the U-shaped frame 303.

[0047] The bracket 304 of the connector 3 is provided with a through hole 302 , which is used to reduce its own weight and filter rainwater and sand.

[0048] It is understandable that if Figure 2As shown, the adjusting jack 401 is adjusted to be consistent with the limiting jack 301, and then the limiting piece 6 is inserted into the limiting jack 301 to connect with the adjusting jack 401, and the direction monitored by the probe 5 is adjusted by adjusting the adjusting jack 401.

[0049] As shown, the gear mechanism comprises a first gear 101, a second gear 201 and a motor, and in the embodiment, the first gear 101 and the second gear 201 are helical gears. Figure 3 The first gear 101 is fixedly connected to the first connecting rod 102, the first connecting rod 102 is fixedly connected to the motor inside the mounting seat 1, the second gear 201 is fixedly connected to the second connecting rod 202, the second connecting rod is connected to the mounting plate 203, and the mounting plate 203 is connected to the fuselage 2.

[0050] In the above embodiment, the control board is arranged inside the mounting seat 1 for controlling the starting of the motor, the motor inside the mounting seat 1 can be started by opening the power switch connected to the mounting seat 1 through the control board, the motor drives the first connecting rod 102 to drive the first gear 101, the tooth surfaces of the first gear 101 and the second gear 201 are vertically engaged, the first gear 101 rotates around the first connecting rod 102 while driving the second gear 201 to rotate, and the second gear 201 drives the second connecting rod 202 to rotate to realize automatic rotation of the fuselage 2.

[0051] Similarly, when the motor is not started, the second connecting rod 202 drives the second gear 201 to rotate in cooperation with the first gear 101 when the fuselage 2 is rotated, so that manual adjustment of the monitoring and scanning of the radar can be realized.

[0052] In the embodiment, the mounting seat 1, the fuselage 2, the connecting piece 3 and the shell 4 in the monitoring radar are made of stainless steel, and the surfaces of the mounting seat 1, the fuselage 2, the connecting piece 3 and the shell 4 are covered with fluorocarbon paint, which plays a role of rust prevention, corrosion prevention and prolonging service life.

[0053] The above is only a preferred embodiment of the present application, and does not limit the present application in any form, so any modification, equivalent change and modification of the above embodiment according to the technical essence of the present application still belongs to the scope of the technical scheme of the present application.

Claims

1. A monitoring radar, characterized in that: include: A mounting seat (1); the mounting seat (1) is connected to the fuselage (2); A fuselage (2); a connecting member (3) is provided at the front end of the fuselage (2); A connecting member (3); the connecting member (3) includes a bracket (304) and a U-shaped frame (303), the U-shaped frame (303) being connected to the bracket (304); one end of the bracket (304) is connected to the fuselage (2), the U-shaped frame (303) is hingedly connected to the probe (5), and the probe (5) can swing along the hinge connection; A probe (5); the probe (5) has a housing (4); The housing (4) is provided with a plurality of adjustment sockets (401), and the plurality of sockets are distributed in an arc shape; A plurality of limiting jacks (301) are provided at the connection between the connecting member (3) and the housing (4), the limiting jacks (301) correspond to the adjustment jacks (401), and limiting members (6) are provided on the limiting jacks (301); When the housing (4) is connected to the connecting member (3), the limiting member (6) passes through the limiting socket (301) and is connected to an adjustment socket (401), thereby locking the swing angle of the probe (5); The mounting seat (1) has a gear mechanism, and the mounting seat (1) is connected to the fuselage (2) via the gear mechanism, and the gear mechanism is used to drive the fuselage (2) to rotate.

2. A monitoring radar according to claim 1, characterized in that: The gear mechanism comprises a first gear (101), a second gear (201) and a motor; The first gear (101) is fixedly connected to a first connecting rod (102), and the first connecting rod (102) is fixedly connected to a motor inside the mounting base (1); The second gear (201) is fixedly connected to a second connecting rod (202), the second connecting rod (202) is connected to a mounting plate (203), and the mounting plate (203) is connected to the fuselage (2); The tooth surfaces of the first gear (101) and the second gear (201) are vertically meshed.

3. A monitoring radar according to claim 2, characterized in that: A controller for controlling the start-up of the motor is arranged inside the mounting seat (1).

4. The monitoring radar according to claim 2, characterized in that: The first gear (101) and the second gear (201) are helical gears.

5. The monitoring radar according to claim 1, characterized in that: The bracket (304) is provided with a through hole (302), the through hole (302) is an oblong through hole, the bracket (304) has a trapezoidal top structure, and the outer contour of the bracket (304) gradually decreases from one end of the fuselage (2) to the other end.

6. The monitoring radar according to claim 1, characterized in that: The limiting member (6) is a latch or a bolt.

7. The monitoring radar according to claim 1, characterized in that: The mounting seat (1), the body (2), the connecting piece (3) and the outer shell (4) are made of stainless steel.

8. The monitoring radar according to claim 7, characterized in that: The surfaces of the mounting seat (1), the body (2), the connecting piece (3) and the outer shell (4) are covered with fluorocarbon paint.

9. The monitoring radar according to claim 1, characterized in that: The outer shape of the fuselage (2) has a trapezoidal top structure.

10. The monitoring radar according to claim 1, characterized in that: The outer shape of the housing (4) has a trapezoidal top structure.

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