Rotary insertion structure of land exploration flight node device

Abstract

The utility model discloses a rotary insertion structure of a land exploration flight node device, which comprises a cantilever support, a shell is arranged on the cantilever support, a rotor rotating mechanism is arranged on the cantilever support, a rotor mechanism is connected with the rotor rotating mechanism, a rotary insertion tail cone is arranged at the bottom of the shell, and the shell is connected with the rotary insertion tail cone. The land exploration flight node device is provided with the rotor wing rotating mechanism and the rotary insertion tail cone, so that the rotor wing mechanism rotates by an angle, the thrust angle of the rotor wing is changed, the rotor wing mechanism operates, the land exploration flight node device is pushed to rotate in situ, the rotary insertion tail cone is firstly and rapidly inserted into the ground in a rotary mode through rotary threads, and the land exploration flight node device is stably inserted into the ground in a rotary mode; the connection stability of the land exploration flight node device and the ground is improved, and the exploration data accuracy of the land exploration flight node device is further improved.

Description

Technical Field

[0001] The utility model belongs to the technical field of land exploration flight equipment, and in particular relates to a rotary plug structure of a land exploration flight node device. Background Art

[0002] The land exploration flight node device is a device used in the field of seismic exploration. It represents an important direction for the development of seismic acquisition technology. The emergence of the land exploration flight node device has greatly promoted the development of geophysical exploration, enabling it to transition from traditional wired acquisition to wireless acquisition mode, improving acquisition efficiency, and promoting the integration of wired and wireless modes of land exploration flight node acquisition equipment. It has played an important role in large-scale, high-density seismic exploration.

[0003] The existing land exploration flight node device cannot be inserted into the ground well when landing at the exploration site, resulting in poor stability of the land exploration flight node device and inaccurate exploration data of the land exploration flight node device. For this reason, we propose a rotary insertion structure for the land exploration flight node device. Utility Model Content

[0004] The purpose of the present utility model is to provide a rotary plug structure of a land exploration flight node device to solve the problems raised in the above background technology.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a rotary plug structure of a land exploration flight node device, comprising:

[0006] A cantilever bracket, wherein a shell is provided on the cantilever bracket;

[0007] a rotor rotation mechanism, the rotor rotation mechanism being arranged on the cantilever bracket;

[0008] a rotor mechanism connected to the rotor rotation mechanism;

[0009] The coccyx is rotated and inserted, and the coccyx is arranged at the bottom of the shell.

[0010] Preferably, the cantilever bracket includes a base and a cantilever, and a plurality of cantilevers are provided, and the plurality of cantilevers are arranged in a ring shape on the outer peripheral side of the base.

[0011] Preferably, the rotor rotation mechanism includes a rotating motor, a first bevel gear, a transmission shaft, a second bevel gear and a mounting seat;

[0012] The rotating motor is arranged in the base, and the first bevel gear is arranged at the output end of the rotating motor;

[0013] A rotating hole is provided in the cantilever, and the transmission shaft is rotatably arranged in the rotating hole. One end of the transmission shaft extends into the base and is provided with the second bevel gear, and the first bevel gear and the second bevel gear are meshed and connected;

[0014] The other end of the transmission shaft extends out of the transmission shaft and is provided with the mounting seat.

[0015] Preferably, the rotor mechanism is arranged on the mounting seat.

[0016] Preferably, the rotor mechanism includes a high-speed motor and a rotor;

[0017] The high-speed motor is arranged on the mounting seat, and the rotor is arranged on the output end of the high-speed motor.

[0018] Preferably, the rotating tail vertebra is fixed to the bottom of the shell through a connecting piece and bolts.

[0019] Preferably, the spiral insert tail vertebra is a conical structure, and the lower part of the spiral insert tail vertebra is provided with spiral patterns.

[0020] Compared with the prior art, the beneficial effects of the present invention are:

[0021] 1. The utility model is provided with a rotor rotation mechanism and a rotary plug tail vertebra. When in use, the rotating motor drives the first bevel gear to rotate, so that the first bevel gear and the second bevel gear engage and rotate, driving the transmission shaft to rotate in the rotating hole in the cantilever, and then driving the mounting seat to rotate, so that the rotor mechanism rotates the angle, realizing the change of the rotor thrust angle. The operation of the rotor mechanism drives the land exploration flight node device to rotate in situ, so that the rotary plug tail vertebra is first quickly rotated into the ground through the spiral pattern, so that the land exploration flight node device is firmly rotated into the ground, thereby improving the connection stability between the land exploration flight node device and the ground, and thereby improving the accuracy of the exploration data of the land exploration flight node device. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 This is a schematic diagram of the overall three-dimensional structure of the utility model;

[0023] Figure 2 This is a schematic diagram of the overall three-dimensional structure of the utility model;

[0024] Figure 3 It is a schematic cross-sectional structural diagram of the present utility model.

[0025] In the figure: 1. Cantilever bracket; 101. Base; 102. Cantilever; 103. Rotary hole; 2. Housing; 3. Rotor rotating mechanism; 301. Rotating motor; 302. First bevel gear; 303. Transmission shaft; 304. Second bevel gear; 305. Mounting seat; 4. Rotor mechanism; 401. High-speed motor; 402. Rotor; 5. Rotary tail cone; 501. Connecting piece; 502. Rotary pattern. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0027] See also Figure 1-Figure 3 The rotary plug structure of the land exploration flight node device provided by the utility model includes:

[0028] A cantilever support 1 is provided with a housing 2, and the cantilever support 1 includes a base 101 and a cantilever 102. Four cantilever arms 102 are provided, and the four cantilever arms 102 are arranged in a ring shape on the outer periphery of the base 101;

[0029] The rotor rotation mechanism 3 is arranged on the cantilever bracket 1 and includes a rotating motor 301, a first bevel gear 302, a transmission shaft 303, a second bevel gear 304 and a mounting base 305. The rotating motor 301 is arranged in the base 101, and the first bevel gear 302 is arranged at the output end of the rotating motor 301. A rotating hole 103 is opened in the cantilever 102, and the transmission shaft 303 is rotatably arranged in the rotating hole 103. One end of the transmission shaft 303 extends into the base 101 and is provided with the second bevel gear 304. The first bevel gear 302 and the second bevel gear 304 are meshed and connected. The other end of the transmission shaft 303 extends outside the transmission shaft 303 and is provided with a mounting base 305.

[0030] Rotor mechanism 4, which is connected to rotor rotation mechanism 3 and is disposed on mounting base 305, includes a high-speed motor 401 and rotors 402; high-speed motor 401 is disposed on mounting base 305, and rotors 402 are disposed on the output end of high-speed motor 401;

[0031] The spiral plug-in tail vertebra 5 is arranged at the bottom of the shell 2 and is fixed to the bottom of the shell 2 by a connecting piece 501 and bolts. The spiral plug-in tail vertebra 5 is a conical structure, and a spiral pattern 502 is provided at the lower part of the spiral plug-in tail vertebra 5 to facilitate screwing into the ground.

[0032] The present invention is provided with a rotor rotation mechanism 3 and a rotary tail vertebra 5. When in use, the rotating motor 301 drives the first bevel gear 302 to rotate, so that the first bevel gear 302 and the second bevel gear 304 engage and rotate, driving the transmission shaft 303 to rotate in the rotating hole 103 in the cantilever 102, and then driving the mounting seat 305 to rotate, so that the rotor mechanism 4 rotates the angle, realizing the change of the rotor thrust angle. The operation of the rotor mechanism pushes the land exploration flight node device to rotate in situ, so that the rotary tail vertebra 5 is first quickly rotated into the ground through the spiral pattern 502, so that the land exploration flight node device is firmly rotated into the ground, thereby improving the connection stability between the land exploration flight node device and the ground, and thereby improving the accuracy of the exploration data of the land exploration flight node device.

[0033] In summary, the method for using the rotary insertion structure of the land exploration flight node device provided in this embodiment is as follows: when rotating and inserting into the ground, the rotating motor 301 drives the first bevel gear 302 to rotate, causing the first bevel gear 302 and the second bevel gear 304 to engage and rotate, driving the transmission shaft 303 to rotate in the rotating hole 103 in the cantilever 102, and then driving the mounting seat 305 to rotate, causing the rotor mechanism 4 to rotate an angle, thereby achieving a change in the rotor thrust angle. The rotor mechanism operates, driving the land exploration flight node device to rotate in place, so that the rotary insertion tail cone 5 is first quickly rotated into the ground through the spiral pattern 502;

[0034] When rotating out of the ground, the rotating motor 301 drives the first bevel gear 302 to rotate, so that the first bevel gear 302 and the second bevel gear 304 engage and rotate, driving the transmission shaft 303 to rotate in the rotating hole 103 in the cantilever 102, and then driving the mounting seat 305 to rotate, so that the rotor mechanism 4 rotates the angle, realizing the change of the rotor thrust angle. The rotor mechanism runs, pushing the land exploration flight node device to rotate in place, so that the rotary tail vertebra 5 first rotates out of the ground quickly through the spiral pattern 502.

[0035] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A rotary plug structure of a land exploration flight node device, characterized in that: include, A cantilever bracket (1), wherein a housing (2) is provided on the cantilever bracket (1); A rotor rotation mechanism (3), the rotor rotation mechanism (3) being arranged on the cantilever bracket (1); A rotor mechanism (4), the rotor mechanism (4) being connected to the rotor rotation mechanism (3); A rotating tail vertebra (5) is provided at the bottom of the housing (2).

2. The rotary plug structure of the land exploration flight node device according to claim 1, characterized in that: The cantilever bracket (1) comprises a base (101) and a cantilever (102), wherein a plurality of cantilever arms (102) are provided, and the plurality of cantilever arms (102) are arranged in a ring shape on the outer peripheral side of the base (101).

3. The rotary plug structure of the land exploration flight node device according to claim 2, characterized in that: The rotor rotation mechanism (3) comprises a rotating motor (301), a first bevel gear (302), a transmission shaft (303), a second bevel gear (304) and a mounting seat (305); The rotating motor (301) is arranged in the base (101), and the first bevel gear (302) is arranged at the output end of the rotating motor (301); A rotating hole (103) is provided in the cantilever (102), and the transmission shaft (303) is rotatably disposed in the rotating hole (103). One end of the transmission shaft (303) extends into the base (101) and is provided with the second bevel gear (304). The first bevel gear (302) and the second bevel gear (304) are meshed and connected. The other end of the transmission shaft (303) extends out of the transmission shaft (303) and is provided with the mounting seat (305).

4. The rotary plug structure of the land exploration flight node device according to claim 3, characterized in that: The rotor mechanism (4) is arranged on the mounting seat (305).

5. The rotary plug structure of the land exploration flight node device according to claim 4, characterized in that: The rotor mechanism (4) comprises a high-speed motor (401) and a rotor (402); The high-speed motor (401) is arranged on the mounting seat (305), and the rotor (402) is arranged on the output end of the high-speed motor (401).

6. The rotary plug structure of the land exploration flight node device according to claim 1, characterized in that: The rotating tail vertebra (5) is fixed to the bottom of the housing (2) via a connecting piece (501) and bolts.

7. The rotary plug structure of the land exploration flight node device according to claim 1, characterized in that: The spiral insert tail vertebra (5) is a conical structure, and a spiral pattern (502) is provided on the lower part of the spiral insert tail vertebra (5).

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