CN214306298U - Small laser range radar support capable of being installed in multiple occasions - Google Patents

Small laser range radar support capable of being installed in multiple occasions Download PDF

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Publication number
CN214306298U
CN214306298U CN202120026026.9U CN202120026026U CN214306298U CN 214306298 U CN214306298 U CN 214306298U CN 202120026026 U CN202120026026 U CN 202120026026U CN 214306298 U CN214306298 U CN 214306298U
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China
Prior art keywords
ball
thin
landing leg
thick
ball hinge
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CN202120026026.9U
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Chinese (zh)
Inventor
张洁洁
朱荣海
董事
金马
梅晓辉
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Hefei Hagong Hot Air Balloon Digital Technology Co Ltd
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Hefei Hagong Hot Air Balloon Digital Technology Co Ltd
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Abstract

The utility model belongs to the technical field of radar supports, in particular to a small laser ranging radar support which can be installed in multiple occasions, comprising a cloud platform seat, a thin supporting leg, a thick supporting leg and a supporting leg, a plurality of thin supporting legs are uniformly distributed below the bottom of the cloud platform seat, the thin supporting legs are movably connected with the cloud platform seat, one end of each thin supporting leg is inserted into the corresponding thick supporting leg, the thin supporting legs and the thick supporting legs are positioned on the same straight line, the thin supporting legs and the thick supporting legs are in one-to-one correspondence, and the supporting legs are movably installed at the tail ends of the thick supporting legs, the small laser range radar bracket of the utility model has the advantages of simple structure, convenient operation, easy carrying, convenient maintenance and low manufacturing cost, the small laser ranging radar can be suitable for being installed and used under the conditions of multiple occasions, even can be used for installing and using other instruments, can ensure the stability of the instruments in use, and has wide application range.

Description

Small laser range radar support capable of being installed in multiple occasions
Technical Field
The utility model relates to a radar support technical field specifically is a small-size laser rangefinder radar support that can install in many occasions.
Background
Small-size laser rangefinder radar support is the necessary mechanism in installation of small-size laser rangefinder radar, the use, and small-size laser rangefinder radar support dominant effect provides the space that small-size laser rangefinder radar is fixed, the installation, provides condition and protection for small-size laser rangefinder radar's use.
Because the small laser ranging radar belongs to a precise instrument, certain requirements are required on installation and use. The small-size laser rangefinder radar installing support of tradition is according to the small-size laser rangefinder radar appearance design or the small-size laser rangefinder radar of direct mount and does not use the support, and this all has led to the installation of small-size laser rangefinder radar and has used can not full seat requirement.
Along with the continuous development of science and technology, the times of humanization come, the use of common sensors such as small laser ranging radar can be more and more frequent in the future, and the requirement of using can not be satisfied to traditional small laser ranging radar support and mounting means.
Also appear some small-size laser range radar installing supports that can protect small-size laser range radar device in the market at present, but the focus of most installing supports is put on the small-size laser range radar installation of vehicles such as car, does not consider the use of the middle-size and small-size laser range radar in other occasions in the real life, and these installing supports most are focused on the protection to small-size laser range radar, and neglected the stationarity of small-size laser range radar installation, adaptability.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a but small-size laser rangefinder radar support of many occasions installation to solve the problem that provides among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a small-size laser rangefinder radar support that can install in many occasions, includes cloud pedestal, thin landing leg, thick landing leg and supporting legs, the below evenly distributed of cloud pedestal bottom has a plurality of thin landing legs, thin landing leg and cloud platform seat swing joint, the inside of thick landing leg is inserted to the one end of thin landing leg, and thin landing leg and thick landing leg are located same straight line, thin landing leg and thick landing leg one-to-one, the terminal movable mounting of thick landing leg has the supporting legs.
Preferably, the holder comprises a holder, a base and four first connecting balls, the holder is arranged above the base, and the four first connecting balls are uniformly arranged along the periphery of the base.
Preferably, the thin leg includes first ball hinge, bracing piece, first well cavity pole and first through-hole, first ball hinge installs on the top of bracing piece, the end of bracing piece is connected with first well cavity pole, the one end that first well hole pole is close to the bracing piece is provided with first through-hole, first connecting ball inserts the inside of first ball hinge, and first connecting ball slides along first ball hinge is inside.
Preferably, thick landing leg includes flexible rotatory hasp, second cavity pole, second through-hole, damping shock absorber, branch and second ball hinge, the upper end at the second cavity pole is installed to flexible rotatory hasp, the one end that flexible rotatory hasp was kept away from to the second cavity pole is provided with the second through-hole, the end of pole is connected with the damping shock absorber in the second, the damping shock absorber is connected with second ball hinge through branch, the first cavity pole passes flexible rotatory hasp and inserts inside the second cavity pole, the inside screw thread that is provided with of flexible rotatory hasp, and the surface threaded connection of flexible rotatory hasp and first cavity pole.
Preferably, the supporting legs includes that the second connects ball, connecting rod, installation base and screw hole, the installation base is kept flat subaerial, the ball is connected through connecting rod and second in installation base upper end, and is provided with a plurality of screw holes along the upper surface of installation base, the second is connected inside the ball inserts the second ball hinge, and the second is connected the ball and is slided along the second ball hinge is inside.
Preferably, first connecting ball and second connecting ball are the spheroid, first ball hinge and second ball hinge's structure is the same, and first ball hinge and second ball hinge comprise a plurality of arc, and the lower extreme of a plurality of arc is connected, and the upper end of a plurality of arc is disconnected, the inside storing groove that forms of a plurality of arc, inside the spheroid inserted the storing inslot, the spheroid slided along storing inslot portion.
Compared with the prior art, the beneficial effects of the utility model are that: this small-size laser rangefinder radar support simple structure, convenient operation easily carries, the maintenance of being convenient for, low in manufacturing cost can adapt to the installation use of small-size laser rangefinder radar under the many occasions condition, can be used for the installation of other instruments even and use, and the stationarity when can guaranteeing the instrument use, application range is wider.
Drawings
Fig. 1 is a schematic overall structure diagram of the present invention;
FIG. 2 is a schematic structural view of the supporting leg of the present invention;
fig. 3 is a schematic structural view of the thin leg of the present invention;
fig. 4 is a schematic structural view of the thick leg of the present invention;
fig. 5 is a schematic structural diagram of the cloud platform of the present invention.
In the figure: 1. a cloud pedestal; 101. a holder; 102. a base; 103. a first connecting ball; 2. thin legs; 201. a first ball hinge; 202. a support bar; 203. a first hollow rod; 204. a first through hole; 3. thick supporting legs; 301. a telescopic rotary lock catch; 302. a second hollow shaft; 303. a damping shock absorber; 304. a second through hole; 305. a strut; 306. a second ball hinge; 4. supporting legs; 401. a second connecting ball; 402. a connecting rod; 403. installing a base; 404. and (4) screw holes.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; 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 according to specific situations by those skilled in the art.
Referring to fig. 1-5, the present invention provides a technical solution: the utility model provides a small-size laser rangefinder radar support that can install in many occasions, includes cloud platform seat 1, thin landing leg 2, thick landing leg 3 and supporting legs 4, the below evenly distributed of 1 bottom of cloud platform seat has a plurality of thin landing legs 2, thin landing leg 2 and 1 swing joint of cloud platform seat, the inside of thick landing leg 3 is inserted to the one end of thin landing leg 2, and thin landing leg 2 and thick landing leg 3 are located same straight line, thin landing leg 2 and thick landing leg 3 one-to-one, the terminal movable mounting of thick landing leg 3 has supporting legs 4.
Further, the cloud platform base 1 includes a cloud deck 101, a base 102, and four first connection balls 103, wherein the cloud deck 101 is installed above the base 102, and the four first connection balls 103 are uniformly arranged along the periphery of the base 102.
Further, the thin leg 2 includes a first ball hinge 201, a support rod 202, a first hollow rod 203 and a first through hole 204, the first ball hinge 201 is installed on the top end of the support rod 202, the end of the support rod 202 is connected with the first hollow rod 203, the first through hole 204 is arranged at one end of the first hollow rod 203 close to the support rod 202, the first connecting ball 103 is inserted into the first ball hinge 201, and the first connecting ball 103 slides along the inside of the first ball hinge 201.
Further, thick landing leg 3 is including flexible rotatory hasp 301, the second hollow pole 302, second through-hole 304, damping shock absorber 303, branch 305 and second ball hinge 306, flexible rotatory hasp 301 is installed in the upper end of second hollow pole 302, the second hollow pole 302 one end of keeping away from flexible rotatory hasp 301 is provided with second through-hole 304, the end of second hollow pole 302 is connected with damping shock absorber 303, damping shock absorber 303 is connected with second ball hinge 306 through branch 305, first hollow pole 203 passes flexible rotatory hasp 301 and inserts inside the second hollow pole 302, the inside screw thread that is provided with of flexible rotatory hasp 301, and the surface threaded connection of flexible rotatory hasp 301 and first hollow pole 203.
Further, supporting legs 4 include that the second connects ball 401, connecting rod 402, installation base 403 and screw hole 404, installation base 403 keeps flat subaerial, installation base 403 upper end is connected ball 401 through connecting rod 402 and second and is connected, and is provided with a plurality of screw holes 404 along the upper surface of installation base 403, second connection ball 401 inserts inside second ball hinge 306, and second connection ball 401 slides along second ball hinge 306 is inside.
Further, first connecting ball 103 is the spheroid with second connecting ball 401, first ball hinge 201 and second ball hinge 306's structure is the same, and first ball hinge 201 and second ball hinge 306 comprise a plurality of arc, and the lower extreme of a plurality of arc is connected, and the upper end of a plurality of arc is disconnected from, the inside storing groove that forms of a plurality of arc, inside the spheroid inserted the storing groove, the spheroid slided along storing inslot portion.
The working principle is as follows:
when in use, the length of the supporting leg and the posture of the supporting leg are adjusted according to different using occasions. When the length of the supporting leg is adjusted, firstly, the telescopic rotary lock catch 301 is rotated, the telescopic rotary lock catch 301 drives the thick supporting leg 3 to rotate, and as the telescopic rotary lock catch 301 is in threaded connection with the first hollow rod 203, the distance between the upper end of the first hollow rod 203 and the telescopic rotary lock catch 301 is adjusted, the distance between the lower end of the thick supporting leg 3 and the upper end of the thin supporting leg 2 is further adjusted, and further the length of the supporting leg is adjusted;
when adjusting the gesture of landing leg, because first ball hinge 201 and first connecting ball 103 swing joint, adjust the contained angle between thin landing leg 2 and the cloud platform seat 1 for the angle of the slope of thin landing leg 2 is different, then the inside position that second connecting ball 401 is located second ball hinge 306 is adjusted in the activity, make installation base 403 level place, be provided with screw hole 404 on installation base 403, accessible nail or bolt are fixed its position department of installing, guarantee the stability of installation.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides a but small-size laser rangefinder radar support of many occasions installation, includes cloud pedestal (1), thin landing leg (2), thick landing leg (3) and supporting legs (4), its characterized in that: cloud platform seat (1) bottom below evenly distributed has a plurality of thin landing legs (2), thin landing leg (2) and cloud platform seat (1) swing joint, the inside of thick landing leg (3) is inserted to the one end of thin landing leg (2), and thin landing leg (2) and thick landing leg (3) are located same straight line, thin landing leg (2) and thick landing leg (3) one-to-one, the terminal movable mounting of thick landing leg (3) has supporting legs (4).
2. The compact laser range radar bracket capable of being mounted in multiple occasions according to claim 1, wherein: cloud platform seat (1) includes cloud platform (101), base (102), four first connecting ball (103), cloud platform (101) are installed in base (102) top, have four first connecting ball (103) along the peripheral align to grid of base (102).
3. The compact laser range radar bracket capable of being mounted in multiple occasions according to claim 2, wherein: thin landing leg (2) include first ball hinge (201), bracing piece (202), first cavity pole (203) and first through-hole (204), the top at bracing piece (202) is installed in first ball hinge (201), the end and the first cavity pole (203) of bracing piece (202) are connected, the one end that first cavity pole (203) is close to bracing piece (202) is provided with first through-hole (204), the inside of first ball hinge (201) is inserted in first connecting ball (103), and first connecting ball (103) slide along first ball hinge (201) is inside.
4. A multiple-field-installable compact lidar mount according to claim 3, wherein: the thick supporting leg (3) comprises a telescopic rotating lock catch (301), a second hollow rod (302), a second through hole (304), a damping shock absorber (303), a supporting rod (305) and a second ball hinge (306), the telescopic rotary lock catch (301) is arranged at the upper end of the second hollow rod (302), a second through hole (304) is arranged at one end of the second hollow rod (302) far away from the telescopic rotary lock catch (301), the end of the second hollow rod (302) is connected to a damping shock absorber (303), the damping shock absorber (303) is connected with a second ball hinge (306) through a strut (305), the first hollow rod (203) penetrates through the telescopic rotary lock catch (301) to be inserted into the second hollow rod (302), the telescopic rotary lock catch (301) is internally provided with threads, and the telescopic rotary lock catch (301) is in threaded connection with the outer surface of the first hollow rod (203).
5. The compact laser range radar bracket capable of being mounted in multiple occasions according to claim 4, wherein: supporting legs (4) are including second connection ball (401), connecting rod (402), installation base (403) and screw hole (404), installation base (403) are kept flat subaerial, installation base (403) upper end is connected ball (401) through connecting rod (402) with the second and is provided with a plurality of screw holes (404) along the upper surface of installation base (403), inside second ball hinge (306) was inserted in second connection ball (401), and the second was connected ball (401) and is slided along second ball hinge (306) is inside.
6. The compact laser range radar bracket capable of being mounted in multiple occasions according to claim 5, wherein: first connecting ball (103) are the spheroid with second connecting ball (401), first ball hinge (201) and second ball hinge (306) the same structure, and first ball hinge (201) and second ball hinge (306) comprise a plurality of arc, and the lower extreme of a plurality of arc is connected, and the upper end of a plurality of arc is disconnected from, the inside storing groove that forms of a plurality of arc, inside the spheroid inserted the storing inslot, the spheroid slided along the storing inslot portion.
CN202120026026.9U 2021-01-06 2021-01-06 Small laser range radar support capable of being installed in multiple occasions Active CN214306298U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120026026.9U CN214306298U (en) 2021-01-06 2021-01-06 Small laser range radar support capable of being installed in multiple occasions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120026026.9U CN214306298U (en) 2021-01-06 2021-01-06 Small laser range radar support capable of being installed in multiple occasions

Publications (1)

Publication Number Publication Date
CN214306298U true CN214306298U (en) 2021-09-28

Family

ID=77822801

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120026026.9U Active CN214306298U (en) 2021-01-06 2021-01-06 Small laser range radar support capable of being installed in multiple occasions

Country Status (1)

Country Link
CN (1) CN214306298U (en)

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