CN214474628U

CN214474628U - Airborne signal control module

Info

Publication number: CN214474628U
Application number: CN202120515310.2U
Authority: CN
Inventors: 严小龙
Original assignee: Shaanxi Star Electronic Technology Co ltd
Current assignee: Shaanxi Star Electronic Technology Co ltd
Priority date: 2021-03-11
Filing date: 2021-03-11
Publication date: 2021-10-22
Anticipated expiration: 2031-03-11

Abstract

The utility model relates to an airborne signal control module technical field just discloses an airborne signal control module, including PMKD, articulated seat has been seted up in PMKD's front, the positive fixedly connected with mount pad of articulated seat, the location mounting groove has been seted up in the front of mount pad, two the equal sliding connection in mount pad left and right sides has the inserted bar. The utility model discloses a, through articulated seat of fixed connection and damping spring between PMKD and mount pad, can articulate and the shock attenuation, can play better shock attenuation cushioning effect to airborne signal control module main part, the ability of device shock attenuation buffering has been increased, the inserted link can receive the promotion effect of elastic tension piece, the joint piece of messenger's inserted link other end installation, but joint to the inside of fixed slot, and then make airborne signal control module main part can stable mounting in the front of mount pad, thereby can be convenient carry out the dismouting, it is better to make the device reach shock attenuation stability, and change convenient effect.

Description

Airborne signal control module

Technical Field

The utility model relates to an airborne signal control module technical field specifically is an airborne signal control module.

Background

An unmanned aircraft, abbreviated as "unmanned aerial vehicle" in english and abbreviated as "UAV", is an unmanned aircraft operated by a radio remote control device and a self-contained program control device, or is autonomously operated by an onboard computer, either completely or intermittently; wherein airborne signal control module is the important component device who connects ground and unmanned aerial vehicle. Airborne equipment measures, handles, transmission, demonstration and the equipment of control to various information, instruction and manipulation in the aircraft flight, and wherein airborne signal control module plays the effect to unmanned aerial vehicle control and monitoring, but in the in-service use process, airborne signal control module's installation location ability is not good enough, probably because the vibrations take place during the unmanned aerial vehicle flight, cause its internal component to damage, and damage the back and change inconveniently, for this we propose an airborne signal control module and solve above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The not enough to prior art, the utility model provides an airborne signal control module, it is better to possess shock attenuation stability, and changes advantages such as facility, and the shock attenuation protective capacities who has solved control module is not good enough, easily takes place to damage, and changes the problem convenient inadequately relatively.

(II) technical scheme

For realizing that above-mentioned shock attenuation stability is better, and change convenient purpose, the utility model provides a following technical scheme: an airborne signal control module comprises a fixed bottom plate, wherein the front surface of the fixed bottom plate is provided with a hinged seat, the front surface of the hinged seat is fixedly connected with a mounting seat, the front surface of the mounting seat is provided with a positioning mounting groove, the left side and the right side of the two mounting seats are respectively connected with an inserting rod in a sliding manner, one opposite side of the two inserting rods is respectively connected to the inside of the positioning mounting groove in a sliding manner, one opposite side of the two inserting rods is respectively and fixedly connected with an elastic stretching piece, one opposite side of the two elastic stretching pieces is fixedly connected with the mounting seat, the front surface of the mounting seat is provided with an airborne signal control module main body, the back surface of the airborne signal control module main body is fixedly provided with a mounting block, the left side and the right side of the mounting block are respectively provided with a fixing groove, one opposite side of the two elastic stretching pieces is respectively and fixedly connected with a clamping block, one opposite side of the two clamping blocks extends and is clamped to the inside of the fixing grooves, damping springs which are uniformly distributed are fixedly connected between the hinged base and the mounting base.

Preferably, the hinge base comprises a positioning cylinder and a hinge ball, the back of the positioning cylinder is fixedly connected with the front of the fixing base plate, the front of the hinge ball is fixedly connected with the back of the mounting base, and the back of the hinge ball extends and is hinged to the inner side of the positioning cylinder.

Preferably, the left side and the right side of the mounting seat are both provided with mounting pipes, and the two insertion rods are respectively connected to the inner end surfaces of the two mounting pipes in a sliding manner.

Preferably, the inside of positioning installation groove is provided with a plurality of evenly distributed's extrusion spring, the equal fixedly connected with flexure strip in front and the back of extrusion spring, two one side that the flexure strip carried on the back mutually contacts with positioning installation groove and installation piece respectively.

Preferably, the two elastic stretching pieces comprise control springs and elastic plates, one sides of the two elastic plates, which are back to back, are fixedly connected with the two plug rods respectively, the two control springs are sleeved on the two plug rods, and two sides of each control spring are fixedly connected with the mounting seat and the elastic plates respectively.

Preferably, two equal fixedly connected with in one side that the elastic plate carried on the back mutually grips the handle, two equal fixedly connected with in one side that the handle carried on the back mutually grips the buckle.

Preferably, the front view cross section of location mounting groove and installation piece is equilateral hexagon, location mounting groove and installation piece looks adaptation.

Compared with the prior art, the utility model provides an airborne signal control module possesses following beneficial effect:

install articulated seat through the front at PMKD, make the mount pad can articulate with PMKD, and install damping spring between PMKD and the mount pad, thereby can play better shock attenuation cushioning effect to airborne signal control module main part, the ability of device shock attenuation buffering has been increased, the inserted link can receive the promotion effect of elastic tension piece, the joint piece that makes the installation of the inserted link other end, but joint to the inside of fixed slot, and then make airborne signal control module main part can stable mounting in the front of mount pad, thereby the dismouting of carrying on that can be convenient, it is better to make the device reach shock attenuation stability, and change convenient effect.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic top view of the connection structure of the mounting seat and the positioning mounting groove of the present invention;

fig. 3 is an enlarged schematic view of a point a in the structure diagram of the present invention;

fig. 4 is a schematic front view of the section of the connection structure of the positioning installation groove and the installation block.

In the figure: 1. fixing the bottom plate; 2. a hinged seat; 201. a positioning cylinder; 202. hinging the ball; 3. a mounting seat; 4. positioning the mounting groove; 5. a plug rod; 6. an elastic tension member; 601. a control spring; 602. an elastic plate; 7. an airborne signal control module main body; 8. mounting blocks; 9. fixing grooves; 10. a clamping block; 11. a damping spring; 12. installing a pipe; 13. a compression spring; 14. an elastic sheet; 15. a grip handle; 16. connecting the retaining ring.

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.

Referring to fig. 1-4, an airborne signal control module comprises a fixed base plate 1, a hinge seat 2 is disposed on the front side of the fixed base plate 1, a mounting seat 3 is fixedly connected to the front side of the hinge seat 2, a positioning mounting groove 4 is disposed on the front side of the mounting seat 3, insertion rods 5 are slidably connected to the left and right sides of the two mounting seats 3, opposite sides of the two insertion rods 5 are slidably connected to the inside of the positioning mounting groove 4, elastic stretching members 6 are fixedly connected to opposite sides of the two insertion rods 5, opposite sides of the two elastic stretching members 6 are fixedly connected to the mounting seat 3, an airborne signal control module main body 7 is disposed on the front side of the mounting seat 3, a mounting block 8 is fixedly mounted on the back side of the airborne signal control module main body 7, fixing grooves 9 are disposed on the left and right sides of the mounting block 8, and a clamping block 10 is fixedly connected to opposite sides of the two elastic stretching members 6, one sides of the two clamping blocks 10 opposite to each other extend and are clamped into the fixing grooves 9 respectively, and damping springs 11 which are uniformly distributed are fixedly connected between the hinge seat 2 and the mounting seat 3;

in this embodiment, install articulated seat 2 through the front at PMKD 1, make mount pad 3 can articulate with PMKD 1, and install damping spring 11 between PMKD 1 and the mount pad 3, thereby can play better shock attenuation cushioning effect to airborne signal control module main part 7, the ability of device shock attenuation buffering has been increased, peg graft pole 5 can receive the promotion effect of elastic tension piece 6, make the joint piece 10 of 5 other end installations of peg pole, can joint to the inside of fixed slot 9, and then make airborne signal control module main part 7 can stable installation in the front of mount pad 3, thereby the dismouting of carrying on that can be convenient, it is better to make the device reach shock attenuation stability, and change convenient effect.

Further, the hinge base 2 comprises a positioning cylinder 201 and a hinge ball 202, the back surface of the positioning cylinder 201 is fixedly connected with the front surface of the fixed base plate 1, the front surface of the hinge ball 202 is fixedly connected with the back surface of the mounting base 3, and the back surface of the hinge ball 202 extends and is hinged to the inner side of the positioning cylinder 201;

in this embodiment, including a location section of thick bamboo 201 and articulated ball 202 through setting up articulated seat 2, a location section of thick bamboo 201 can play articulated location effect to articulated ball 202, and then makes the articulated location between PMKD 1 and the mount pad 3 comparatively stable, increases the practicality of device.

Furthermore, the left side and the right side of the mounting seat 3 are both provided with mounting pipes 12, and the two insertion rods 5 are respectively connected with the inner end surfaces of the two mounting pipes 12 in a sliding manner;

in this embodiment, the installation pipes 12 are installed on the left side and the right side of the installation base 3, so that the insertion rod 5 is not easily abraded when sliding in a left-right displacement manner, and the positioning anti-abrasion capability of the installation pipes 12 is stable.

Furthermore, a plurality of uniformly distributed extrusion springs 13 are arranged inside the positioning installation groove 4, the front and the back of each extrusion spring 13 are fixedly connected with elastic pieces 14, and the opposite sides of the two elastic pieces 14 are respectively contacted with the positioning installation groove 4 and the installation block 8;

in this embodiment, through being provided with a plurality of evenly distributed's extrusion spring 13 in the inside of location mounting groove 4, when installation piece 8 pegs graft to the inside of location mounting groove 4, can play the extrusion positioning effect to installation piece 8 by extrusion spring 13 cooperation flexure strip 14 to make installation piece 8 can stabilize the joint in the inside of location mounting groove 4, increased the practicality of device.

Further, each of the two elastic stretching members 6 comprises a control spring 601 and an elastic plate 602, wherein one side of each of the two elastic plates 602, which is opposite to the other side, is fixedly connected with the two insertion rods 5, the two control springs 601 are sleeved on the two insertion rods 5, and two sides of each of the control springs 601 are fixedly connected with the mounting base 3 and the elastic plate 602;

in this embodiment, through setting up that elastic stretching member 6 all includes control spring 601 and elastic plate 602, control spring 601 can pull peg rod 5, makes peg rod 5 have elastic pushing action, and after installation piece 8 pegged graft to location mounting groove 4 in, control spring 601 can pull and be close to installation piece 8 from peg rod 5, and then makes joint piece 10 can extrude the inside of pegging graft to fixed slot 9, has increased the practicality of device.

Furthermore, the opposite sides of the two elastic plates 602 are fixedly connected with holding handles 15, and the opposite sides of the two holding handles 15 are fixedly connected with connecting snap rings 16;

in this embodiment, through the equal fixedly connected with in the one side that the elastic plate 602 carried on the back mutually and gripping handle 15, the user can grasp and grip handle 15 to pulling peg 5, the joint piece 10 of the peg 5 other end can break away from installation piece 8, and then makes the dismouting of airborne signal control module main part 7 all more convenient, has increased the practicality of device.

Furthermore, the front sections of the positioning installation groove 4 and the installation block 8 are equilateral hexagons, and the positioning installation groove 4 is matched with the installation block 8;

in this embodiment, be equilateral hexagon through the front view cross-section that sets up location mounting groove 4 and installation piece 8, make installation piece 8 stable installation in the inside of location mounting groove 4, comparatively stable when making the installation of airborne signal control module main part 7, increased the stability of device.

It should be noted that each device in the present application is a common device in the market, and can be selected according to the requirement when in specific use, and the circuit connection relationship of each device all belongs to a simple series and parallel connection circuit, and there is no innovation point in the circuit connection, and those skilled in the art can easily implement the circuit connection, and belong to the prior art, and are not described again.

The working principle is as follows: the front surface of the fixed base plate 1 is provided with the hinge seat 2, so that the mounting seat 3 can be hinged with the fixed base plate 1, the damping spring 11 is arranged between the fixed base plate 1 and the mounting seat 3, after the airborne signal control module main body 7 is arranged on the mounting seat 3, the mounting seat 3 can play a good damping and buffering role for the airborne signal control module main body 7, the damping and buffering capacity of the device is increased, the back surface of the airborne signal control module main body 7 is provided with the mounting block 8 which can be inserted into the positioning mounting groove 4, the inserting rod 5 can be pushed by the elastic stretching piece 6, so that the clamping block 10 arranged at the other end of the inserting rod 5 can be clamped into the fixing groove 9, the airborne signal control module main body 7 can be stably arranged on the front surface of the mounting seat 3, when the holding handle 15 is held, the clamping block 10 can be pulled to be separated from the fixing groove 9, and the device is convenient to disassemble, finally, the device has the advantages of good damping stability and convenient replacement, and the problems that the damping protection capability of the control module is not good enough, the control module is easy to damage, and the control module is not convenient to replace are solved.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

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

1. An airborne signal control module, includes PMKD (1), its characterized in that: the front of the fixed base plate (1) is provided with a hinged seat (2), the front of the hinged seat (2) is fixedly connected with a mounting seat (3), the front of the mounting seat (3) is provided with a positioning mounting groove (4), the left side and the right side of the two mounting seats (3) are both connected with insertion rods (5) in a sliding manner, one opposite sides of the two insertion rods (5) are respectively connected to the inside of the positioning mounting groove (4) in a sliding manner, one opposite sides of the two insertion rods (5) are both fixedly connected with elastic stretching pieces (6), one opposite sides of the two elastic stretching pieces (6) are fixedly connected with the mounting seat (3), the front of the mounting seat (3) is provided with an airborne signal control module main body (7), the back of the airborne signal control module main body (7) is fixedly provided with a mounting block (8), the left side and the right side of the mounting block (8) are both provided with fixing grooves (9), two equal fixedly connected with joint piece (10) in one side that elasticity tensioning member (6) is relative, two the inside of joint to fixed slot (9) is extended respectively and joint to one side that joint piece (10) is relative, fixedly connected with evenly distributed's damping spring (11) between articulated seat (2) and mount pad (3).

2. The airborne signal control module of claim 1, wherein: the hinge base (2) comprises a positioning cylinder (201) and a hinge ball (202), the back surface of the positioning cylinder (201) is fixedly connected with the front surface of the fixed base plate (1), the front surface of the hinge ball (202) is fixedly connected with the back surface of the mounting base (3), and the back surface of the hinge ball (202) extends and is hinged to the inner side of the positioning cylinder (201).

3. The airborne signal control module of claim 1, wherein: the left side and the right side of the mounting seat (3) are provided with mounting pipes (12), and the two insertion rods (5) are respectively connected to the inner end faces of the two mounting pipes (12) in a sliding manner.

4. The airborne signal control module of claim 1, wherein: the inside of location mounting groove (4) is provided with a plurality of evenly distributed's extrusion spring (13), the front of extrusion spring (13) and the equal fixedly connected with flexure strip (14) in the back, two one side that flexure strip (14) carried on the back mutually contacts with location mounting groove (4) and installation piece (8) respectively.

5. The airborne signal control module of claim 1, wherein: two elasticity tensile piece (6) all include control spring (601) and elastic plate (602), two one side that elastic plate (602) carried on the back respectively with two peg graft pole (5) fixed connection, two control spring (601) cover is located on two peg graft poles (5), the both sides of control spring (601) respectively with mount pad (3) and elastic plate (602) fixed connection.

6. The airborne signal control module of claim 5, wherein: two equal fixedly connected with in one side that elastic plate (602) carried on the back mutually grips handle (15), two equal fixedly connected with in one side that grips handle (15) carried on the back mutually connects buckle (16).

7. The airborne signal control module of claim 1, wherein: the front-view section of the positioning installation groove (4) and the installation block (8) is an equilateral hexagon, and the positioning installation groove (4) is matched with the installation block (8).