CN215066976U

CN215066976U - Satellite time service remote wireless phase checking instrument

Info

Publication number: CN215066976U
Application number: CN202121531908.7U
Authority: CN
Inventors: 曹震
Original assignee: Nanjing Shennan Boling Power Technology Co ltd
Current assignee: Nanjing Shennan Boling Power Technology Co ltd
Priority date: 2021-07-07
Filing date: 2021-07-07
Publication date: 2021-12-07
Anticipated expiration: 2031-07-07

Abstract

The utility model discloses a long-range wireless nuclear phase appearance of satellite time service, including putting the under casing, accomodating shell and insulator spindle, the internally mounted of putting the under casing has the accomodating shell, and the one end of putting the under casing articulates there is the case top cap of putting, and the lateral wall fixedly connected with antiskid structure of host computer, the one end of accomodating the shell top is provided with the insulator spindle, and one side of insulator spindle lateral wall sets up first mounting structure. The utility model discloses a be provided with bearing structure, because the inside in the groove of accomodating is all accomodate with the bracing piece to the pivot seat, make this structure can hide when not using and accomodate at the long-range wireless nuclear phase appearance of satellite time service and can not occupy great space, make the bracing piece can fix a position at the fixed orifices distributed position after the pivot seat is inside to be rotated under the effect of fixed orifices and second spring bayonet lock simultaneously, so that this long-range wireless nuclear phase appearance of satellite time service keeps the stable putting of level, realized putting the stability of this long-range wireless nuclear phase appearance of satellite time service.

Description

Satellite time service remote wireless phase checking instrument

Technical Field

The utility model relates to a power grid measuring equipment technical field, in particular to long-range wireless nuclear phase appearance of satellite time service.

Background

The satellite time service remote wireless phase detector is used as a measuring device for remote phase detection and switch cabinet electricity-getting induction point phase detection, and mainly aims at high-voltage power grid to perform high-voltage electricity testing, phase sequence detection, grid frequency measurement and other related operations, so that the satellite time service remote wireless phase detector has relatively high specialty;

therefore, a multifunctional satellite time service remote wireless phase checking instrument is disclosed in a patent specification with the publication number of CN209992582U, the technical field of the phase checking instrument is related, the satellite time service remote wireless phase checking instrument in the prior art is composed of two boxes, the two boxes are connected through a hinge, and when the satellite time service remote wireless phase checking instrument is placed, the two boxes are placed on the same level, so that the problem that a large area needs to be occupied is solved. The telescopic device comprises a lower box, a telescopic frame, an upper box, a bolt, a telescopic rod, a movable pipe, a bolt and a bolt, wherein the telescopic frame is arranged on two sides of the inner part of the lower box, the upper end of the telescopic frame is provided with an upper box, the inner part of the telescopic frame comprises a fixed pipe, the upper end of the fixed pipe is embedded with the movable pipe, the upper end of the movable pipe is connected with the movable rod, the lower end of the front side of the movable pipe is provided with an insertion hole, the bolt is placed in the lower box, the telescopic rod is arranged in the upper box, the movable rod is fixedly connected with the upper box, the diameter of the movable rod is equal to the inner diameter of the movable pipe, the movable rod is in sliding connection with the movable pipe, and the movable pipe is in sliding connection with the fixed pipe;

although the satellite time service remote wireless nuclear phase instrument can keep stable in the using process, more parts are complex to install, and the complicated operation has great influence on the construction efficiency of electric power operation in the electric power action.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model aims at providing a long-range wireless nuclear phase appearance of satellite time service for solve the long-range wireless nuclear phase appearance of current satellite time service and put the defect of difficulty.

(II) contents of utility model

In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides a long-range wireless nuclear phase appearance of satellite time service, is including putting the under casing, accomodate shell and insulator spindle, the internally mounted who puts the under casing has accomodate the shell, the one end of putting the under casing articulates there is puts the case top cap, the bottom of putting the under casing is provided with bearing structure, bearing structure is including accomodating groove, pivot seat, fixed orifices, bracing piece and second spring bayonet lock, accomodate the inside of groove setting and putting the under casing bottom, accomodate one side fixedly connected with pivot seat of inslot portion, the inside of pivot seat is provided with the fixed orifices, one side of accomodating the shell top is provided with receiver, receiver's lateral wall fixedly connected with antiskid structure, the opposite side on receiver casing top is provided with the transmitter, the one end on receiver casing top is provided with the insulator spindle, one side of insulator spindle lateral wall sets up first mounting structure.

Preferably, the anti-slip structure comprises a fitting block, a rubber pad and an anti-slip block, one end of the fitting block is fixedly connected with one end of the receiving host, the bottom end of the receiving host is fixedly connected with the rubber pad, and the bottom end of the rubber pad is fixedly connected with the anti-slip block.

Preferably, the attaching blocks are symmetrically distributed about a vertical center line of the receiving host, and the anti-skid blocks are distributed at equal intervals at the bottom end of the rubber pad.

Preferably, the mounting structure comprises an elastic groove, a first spring bayonet lock and a positioning hole, the elastic groove is arranged in one side of the insulating rod, the first spring bayonet lock is arranged in the elastic groove, and the positioning hole is formed in the outer side wall of the emitter.

Preferably, the elastic groove is elastically connected with the inside of the first spring bayonet lock, and the positioning holes are annularly distributed in the outer side wall of the emitter.

Preferably, the inner side of the rotating shaft seat is rotatably connected with a supporting rod, and a second spring clamping pin is arranged on one side inside the supporting rod.

Preferably, be the rotating-structure between pivot seat and the bracing piece inside, the fixed orifices is provided with two sets ofly in the inside of pivot seat, and both be ninety degrees contained angle between the fixed orifices inside.

(III) advantageous effects

The utility model provides a pair of long-range wireless nuclear phase appearance of satellite time service, its advantage lies in: by arranging the supporting structure, the rotating shaft seat and the supporting rod are both accommodated in the accommodating groove, so that the structure can be hidden and accommodated when the satellite time service remote wireless phase checking instrument is not used, and does not occupy a large space, and meanwhile, the supporting rod can be positioned at the distribution position of the fixing hole after rotating in the rotating shaft seat under the action of the fixing hole and the second spring clamping pin, so that the satellite time service remote wireless phase checking instrument keeps horizontal and stable arrangement, and stable arrangement of the satellite time service remote wireless phase checking instrument is realized;

by arranging the anti-skidding structure, when the receiving host is used for setting data parameters of the satellite time service remote wireless phase checking instrument, the palm of an operator holds the receiving host and enables fingers to be attached to the attaching blocks, at the moment, the anti-skidding blocks are in contact with the palm of the operator, and meanwhile, the friction force between the anti-skidding blocks and the palm of the operator is increased, so that the receiving host is not easy to fall off, and the anti-skidding characteristic of the receiving host is improved;

through being provided with mounting structure, because a plurality of elasticity grooves of inside annular distribution of insulator spindle lateral wall one end, when inserting mounting structure lateral wall one end with the transmitter, first spring bayonet lock can contract to elasticity inslot portion under self elastic action to pop out in locating hole position department, and make first spring bayonet lock and locating hole block, fix the transmitter with this, realized the convenient installation to the transmitter.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic top view of the present invention;

fig. 2 is a schematic front view of the cross-sectional structure of the present invention;

FIG. 3 is a schematic front view of the anti-slip structure of the present invention;

fig. 4 is a schematic view of the mounting structure of the present invention;

fig. 5 is a schematic view of a front view partial section structure of the mounting structure of the present invention;

fig. 6 is an enlarged partial cross-sectional view of the point a in fig. 2 according to the present invention.

In the figure: 1. placing a bottom box; 2. a housing case; 3. receiving a host; 4. an anti-slip structure; 401. fitting blocks; 402. a rubber pad; 403. anti-skid blocks; 5. a transmitter; 6. an insulating rod; 7. a mounting structure; 701. an elastic groove; 702. a first spring bayonet; 703. positioning holes; 8. a top cover of the placing box; 9. a support structure; 901. a receiving groove; 902. a rotating shaft seat; 903. a fixing hole; 904. a support bar; 905. and the second spring is clamped with a pin.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-6, the utility model provides a satellite time service remote wireless nuclear phase instrument, which comprises a bottom case 1, a receiving case 2 and an insulating rod 6, wherein the receiving case 2 is installed inside the bottom case 1, one end of the bottom case 1 is hinged with a top cover 8, one side of the top end of the receiving case 2 is provided with a host 3, the other side of the top end of the receiving case 2 is provided with a transmitter 5, one end of the top end of the receiving case 2 is provided with the insulating rod 6, the outer side wall of the host 3 is fixedly connected with an anti-skid structure 4, the anti-skid structure 4 comprises an adhering block 401, a rubber pad 402 and an anti-skid block 403, one end of the adhering block 401 is fixedly connected with one end of the host 3, the bottom end of the host 3 is fixedly connected with the rubber pad 402, the bottom end of the rubber pad 402 is fixedly connected with the anti-skid block 403, the adhering blocks 401 are symmetrically distributed about the vertical central line of the host 3, the anti-skid blocks 403 are distributed at equal intervals at the bottom end of the rubber pad 402, so that the friction force between the anti-skid blocks 403 and the palm of an operator is increased;

specifically, as shown in fig. 1 and 3, when using this structure, first, when the palm of the operator holds the receiving host 3 to set parameters, the fingers of the operator are attached to the attaching block 401, and meanwhile, the palm of the operator is closely attached to the anti-slip block 403, so that the friction between the palm of the operator and the receiving host 3 is increased, and thus the risk of dropping the receiving host 3 during use is reduced;

a head mounting structure 7 is arranged on one side of the outer side wall of the insulating rod 6, the mounting structure 7 comprises an elastic groove 701, a first spring bayonet lock 702 and a positioning hole 703, the elastic groove 701 is arranged in the inner side of one side of the insulating rod 6, the first spring bayonet lock 702 is arranged in the elastic groove 701, the positioning hole 703 is arranged in the outer side wall of the emitter 5, the elastic groove 701 is elastically connected with the inner part of the first spring bayonet lock 702, and the positioning holes 703 are annularly distributed in the inner part of the outer side wall of the emitter 5, so that the connection between the emitter 5 and the insulating rod 6 is more stable;

specifically, as shown in fig. 1, 4 and 5, when the structure is used, firstly, because the elastic groove 701 is annularly distributed on one side of the outer side wall of the insulating rod 6, and the first spring bayonet lock 702 has a larger elastic force, when the emitter 5 is inserted into one end of the insulating rod 6, the first spring bayonet lock 702 retracts inside the elastic groove 701 under the action of the elastic force of the first spring bayonet lock 702, and pops out at the position of the positioning hole 703 to enable the first spring bayonet lock 702 to be clamped with the positioning hole 703, so that the emitter 5 and the insulating rod 6 are stably installed;

the bottom end of the placing bottom box 1 is provided with a supporting structure 9, the supporting structure 9 comprises a containing groove 901, a rotating shaft seat 902, a fixing hole 903, a supporting rod 904 and a second spring clamping pin 905, the containing groove 901 is arranged in the bottom end of the placing bottom box 1, one side in the containing groove 901 is fixedly connected with the rotating shaft seat 902, the fixing hole 903 is arranged in the rotating shaft seat 902, the inner side of the rotating shaft seat 902 is rotatably connected with the supporting rod 904, one side in the supporting rod 904 is provided with a second spring clamping pin 905, a rotating structure is formed between the rotating shaft seat 902 and the inside of the supporting rod 904, two groups of fixing holes 903 are arranged in the rotating shaft seat 902, and a ninety-degree included angle is formed between the fixing holes 903 in the rotating shaft seat 902, so that the supporting rod 904 can be fixed after being rotated;

specifically, as shown in fig. 1, 2 and 6, when using this structure, firstly, because the rotating shaft seat 902 and the support rod 904 are a rotating structure, when using the satellite time service remote wireless phase checking instrument, the second spring clamp 905 can be engaged with the fixing hole 903 by rotating the support rod 904, so as to rotate the support rod 904 and then fix the support rod 904, so that the bottom placing box 1 can be horizontally placed, and the satellite time service remote wireless phase checking instrument can be rapidly installed and used.

The working principle is as follows: when the device is used, firstly, the satellite time service remote wireless phase detector is carried to a designated area for power grid detection, then the supporting rod 904 in the accommodating groove 901 is pulled to enable the rotating shaft seat 902 and the supporting rod 904 to rotate, then the rotating supporting rod 904 rotates ninety degrees, the second spring clamping pin 905 is inserted into the fixing hole 903 under the action of the elastic force of the second spring clamping pin 905 to fix the position of the supporting rod 904, so that the supporting rod 904 rotates to enable the supporting rod 904 to support the bottom placing box 1, and then internal equipment of the satellite time service remote wireless phase detector is installed;

secondly, inserting one side of the outer side wall of the insulating rod 6 into the emitter 5, enabling the first spring bayonet lock 702 to retract into the elastic groove 701 under the action of self elastic force, and after the insulating rod 6 is inserted into the deepest part in the emitter 5, the first spring bayonet lock 702 is ejected out under the action of self elastic force and inserted into the positioning hole 703, so that the emitter 5 and the insulating rod 6 are connected and form a whole for subsequent use;

finally, an operator takes the receiving host 3 to set parameters of the satellite time service remote wireless phase checking instrument, fingers of the operator are attached to the positions of the attachment blocks 401 on the two sides of the anti-skidding structure 4 at the moment, a palm of the operator is attached to the anti-skidding blocks 403, the anti-skidding blocks 403 are arranged at the bottom end of the rubber pad 402, friction between the palm of the operator and the receiving host 3 is increased, the operator holds the receiving host 3 to set the parameters, then the satellite time service remote wireless phase checking instrument is used for detection, and finally the use work of the satellite time service remote wireless phase checking instrument is completed.

The above-described embodiments of the apparatus are merely illustrative, and the units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment. One of ordinary skill in the art can understand and implement it without inventive effort.

Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention in its corresponding aspects.

Claims

1. The utility model provides a long-range wireless nuclear phase appearance of satellite time service, is including putting bottom case (1), containing shell (2) and insulator spindle (6), its characterized in that: a containing shell (2) is arranged inside the placing bottom box (1), a placing box top cover (8) is hinged to one end of the placing bottom box (1), a supporting structure (9) is arranged at the bottom end of the placing bottom box (1), the supporting structure (9) comprises a containing groove (901), a rotating shaft seat (902), a fixing hole (903), a supporting rod (904) and a second spring clamping pin (905), the containing groove (901) is arranged inside the bottom end of the placing bottom box (1), one side inside the containing groove (901) is fixedly connected with the rotating shaft seat (902), and the fixing hole (903) is formed inside the rotating shaft seat (902);

a receiving host (3) is arranged on one side of the top end of the receiving shell (2), an anti-skid structure (4) is fixedly connected to the outer side wall of the receiving host (3), a transmitter (5) is arranged on the other side of the top end of the receiving shell (2), and an insulating rod (6) is arranged at one end of the top end of the receiving shell (2);

and a head mounting structure (7) is arranged on one side of the outer side wall of the insulating rod (6).

2. The satellite time service remote wireless phase checking instrument according to claim 1, characterized in that: the anti-skid structure (4) comprises an attaching block (401), a rubber pad (402) and an anti-skid block (403), one end of the attaching block (401) is fixedly connected with one end of the receiving host (3), the bottom end of the receiving host (3) is fixedly connected with the rubber pad (402), and the bottom end of the rubber pad (402) is fixedly connected with the anti-skid block (403).

3. The satellite time service remote wireless phase checking instrument according to claim 2, characterized in that: the sticking blocks (401) are symmetrically distributed about the vertical center line of the receiving host (3), and the anti-skidding blocks (403) are distributed at equal intervals at the bottom end of the rubber pad (402).

4. The satellite time service remote wireless phase checking instrument according to claim 1, characterized in that: the mounting structure (7) comprises an elastic groove (701), a first spring bayonet lock (702) and a positioning hole (703), the elastic groove (701) is arranged in one side of the insulating rod (6), the first spring bayonet lock (702) is arranged in the elastic groove (701), and the positioning hole (703) is arranged in the outer side wall of the emitter (5).

5. The satellite time service remote wireless phase checking instrument according to claim 4, characterized in that: the elastic groove (701) is elastically connected with the inside of the first spring clamping pin (702), and the positioning holes (703) are annularly distributed in the outer side wall of the emitter (5).

6. The satellite time service remote wireless phase checking instrument according to claim 1, characterized in that: the inboard of pivot seat (902) is rotated and is connected with bracing piece (904), one side of bracing piece (904) inside is provided with second spring bayonet lock (905).

7. The satellite time service remote wireless phase checking instrument according to claim 1, characterized in that: the rotating shaft seat (902) and the supporting rod (904) are of a rotating structure, two groups of fixing holes (903) are arranged in the rotating shaft seat (902), and the fixing holes (903) form ninety-degree included angles between the insides of the fixing holes (903).