CN215155722U - Unmanned aerial vehicle flies mounting structure of accuse subassembly - Google Patents
Unmanned aerial vehicle flies mounting structure of accuse subassembly Download PDFInfo
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- CN215155722U CN215155722U CN202121663949.1U CN202121663949U CN215155722U CN 215155722 U CN215155722 U CN 215155722U CN 202121663949 U CN202121663949 U CN 202121663949U CN 215155722 U CN215155722 U CN 215155722U
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- connecting rod
- flight control
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 32
- 239000003822 epoxy resin Substances 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 claims description 2
- 229920000647 polyepoxide Polymers 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 10
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000009471 action Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000004593 Epoxy Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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Abstract
The utility model provides an unmanned aerial vehicle flies mounting structure of accuse subassembly, including flying to control the subassembly, the mounting plate, mounting plate and standing groove, the standing groove has been seted up in the middle of the mounting plate upper end surface, mounting base upper end surface left side and right side all are fixed with a side board, two side boards all have seted up the spread groove to one side inwards, each mounting plate all is fixed with two connecting rods two to one side outwards, the other end of connecting rod one is fixed in the spread groove of side board, be connected with connecting spring between spread groove and the mounting plate, connecting spring cup joints on connecting rod one and connecting rod two, flying to control the subassembly and place in the standing groove of seting up in the middle of the mounting plate upper end surface; compared with the prior art, the utility model discloses following beneficial effect has: the quick and accurate positioning and installation of the flight control assembly are realized, the flow of batch assembly production of the unmanned aerial vehicle is simplified, the efficiency of mass production is improved, and the flight control assembly can be protected to a certain extent.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, in particular to unmanned aerial vehicle flies mounting structure of accuse subassembly.
Background
The flight control module (hereinafter, referred to as flight control module) is an important subsystem in the unmanned aerial vehicle system, and its main function is to measure state information such as flight attitude of the unmanned aerial vehicle and control the flight of the unmanned aerial vehicle in real time. In order to ensure the accuracy of measurement, after the unmanned aerial vehicle is provided with the flight control module, the calibration and calibration of the flight control module must be carried out firstly. At present, only two mounting modes of gluing and thread fixing are available for commercial flight control modules. The adhesive mounting scheme has low reliability, while the thread fixing mounting scheme improves the reliability, but still cannot ensure the positioning precision of the flight control module in the mass production and assembly process. Therefore, there is a need for a mounting structure for a drone flight control assembly to address this problem.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art exists, the utility model aims at providing an unmanned aerial vehicle flies mounting structure who controls subassembly to solve the problem that provides in the above-mentioned background art.
The utility model discloses a following technical scheme realizes: an installation structure of a flight control assembly of an unmanned aerial vehicle comprises the flight control assembly, an installation bottom plate, a fastening plate and a placing groove, a placing groove is arranged in the middle of the upper end surface of the mounting bottom plate, a side edge plate is fixed on each of the left side and the right side of the upper end surface of the mounting bottom plate, a connecting groove is arranged on each of the inward sides of the two side edge plates, two connecting rods II are fixed on each of the outward sides of the fastening plates, a sliding groove is arranged in the second connecting rod, the first connecting rod is arranged in the sliding groove, the other end of the first connecting rod is fixed in the connecting groove of the side plate, the connecting spring is connected between the connecting groove and the fastening plate, the connecting spring is sleeved on the first connecting rod and the second connecting rod, a through hole is formed in one side of the side plate facing outwards, the pull rope penetrates through the through hole, the other end of the pull rope is fixed to the fastening plate, and the flight control assembly is placed in a placing groove formed in the middle of the upper end surface of the mounting base plate.
In a preferred embodiment, the first connecting rod, the second connecting rod, the sliding groove and the connecting spring form a telescopic mechanism.
As a preferred embodiment, the limiting ring is fixed at one end of a sliding groove arranged in the connecting rod i, and the depth of the sliding groove is greater than the length of the connecting rod i.
In a preferred embodiment, the fixing groove is opened on an inward side of the fastening plate, the gasket is disposed in the fixing groove, the gasket is bonded in the fixing groove by epoxy resin, and the gasket is made of rubber.
In a preferred embodiment, the height of the connecting slot is greater than the height of the fastening plate.
As a preferred embodiment, four corners of the upper end of the mounting bottom plate are respectively provided with a connecting hole.
In a preferred embodiment, the width of the placement groove formed in the middle of the upper end surface of the mounting base plate is larger than the width of the flight control assembly.
After the technical scheme is adopted, the beneficial effects of the utility model are that: simple structure through mounting plate, side board and the spread groove that sets up, has realized flying quick accurate positioning and the installation of accuse subassembly, has simplified unmanned aerial vehicle batch assembly production's flow, has improved mass production's efficiency, through the gasket that sets up, can play certain guard action to flying the accuse subassembly.
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, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 is the utility model relates to an unmanned aerial vehicle flies the structure schematic diagram of mounting structure's of accuse subassembly mounting panel.
Fig. 2 is the utility model relates to an unmanned aerial vehicle flies mounting structure of accuse subassembly and overlooks the schematic diagram.
Fig. 3 is the utility model relates to an unmanned aerial vehicle flies section schematic diagram of connecting rod two of mounting structure of accuse subassembly.
In the figure, 1-flight control assembly, 2-installation bottom plate, 3-connecting rod I, 4-pull rope, 5-connecting rod II, 6-connecting spring, 7-side plate, 8-connecting groove, 9-fastening plate, 10-gasket, 11-placing groove, 12-limiting ring and 13-sliding groove.
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 efforts belong to the protection scope of the present invention.
Referring to fig. 1, fig. 2 and fig. 3, the present invention provides a technical solution: an installation structure of an unmanned aerial vehicle flight control assembly comprises a flight control assembly 1, an installation bottom plate 2, fastening plates 9 and a placement groove 11, the placement groove 11 is formed in the middle of the upper end surface of the installation bottom plate 2, side plates 7 are fixed on the left side and the right side of the upper end surface of the installation bottom plate 2, connecting grooves 8 are formed in inward sides of the two side plates 7, two connecting rods II 5 are fixed on outward sides of the fastening plates 9, sliding grooves 13 are formed in the connecting rods II 5, the connecting rods I3 are arranged in the sliding grooves 13, the other ends of the connecting rods I3 are fixed in the connecting grooves 8 of the side plates 7, connecting springs 6 are connected between the connecting grooves 8 and the fastening plates 9, the connecting springs 6 are sleeved on the connecting rods I3 and the connecting rods II 5, through holes are formed in outward sides of the side plates 7, a pull rope 4 penetrates through the through holes, and the other ends of the pull ropes 4 are fixed on the fastening plates 9, the flight control assembly 1 is placed in a placing groove 11 formed in the middle of the upper end surface of the mounting base plate 2.
Connecting rod 3, connecting rod two 5, spout 13 and coupling spring 6 constitute a telescopic machanism, can draw mounting plate 9 to spread in the groove 8 to the convenience is placed flight control subassembly 1 in spread groove 8.
The limiting ring 12 is fixed at one end of the connecting rod I3, which is arranged in the sliding groove 13 in the connecting rod II 5, the connecting rod I3 cannot be separated from the sliding groove 13, and the depth of the sliding groove 13 is greater than the length of the connecting rod I3.
The fixing groove is opened in the inboard one side of mounting plate 9, and gasket 10 sets up in the fixing groove, and gasket 10 glues in the fixing groove through epoxy, and the material of gasket 10 is a rubber.
The height of spread groove 8 is greater than the height of mounting plate 9, is convenient for mounting plate 9 to draw to spread the inslot 8 to it places flight control subassembly 1 in spread groove 8 to be convenient.
Connecting holes have all been seted up at four edges on 2 upper ends of mounting plate, are convenient for fix mounting plate 2 on unmanned aerial vehicle.
The width of the placing groove 11 formed in the middle of the upper end surface of the mounting base plate 2 is larger than that of the flight control assembly 1, so that the flight control assembly 1 is conveniently placed in the connecting groove 8.
As an embodiment of the present invention: in practical use, the mounting base plate 2 is connected to the unmanned aerial vehicle through four connecting holes and bolts, the pull rope 4 is pulled towards the outside, at the moment, under the action of the pull rope 4, the fastening plate 9 moves towards the connecting groove 8, the connecting rod I3 contracts into the sliding groove 13 of the connecting rod II 5, the connecting spring 6 is in a compressed state, after the two fastening plates 9 are pulled to the maximum, the flight control assembly 1 is placed in the connecting groove 8 formed in the mounting base plate 2, the two pull ropes 4 are loosened, the connecting spring 6 rebounds outwards, the fastening plate 9 returns to the original position under the action of the connecting spring 6, so that the flight control assembly 1 in the connecting groove 8 is fixed, a certain buffering effect can be achieved through the arranged gasket 10, a certain protection effect can be achieved on the flight control assembly 1, and the rapid and accurate positioning and installation of the flight control assembly 1 are achieved, the flow of unmanned aerial vehicle batch assembly production is simplified, and the efficiency of mass production is improved.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle flies mounting structure of accuse subassembly, includes to fly accuse subassembly (1), mounting plate (2), mounting plate (9) and standing groove (12), its characterized in that: a placing groove (12) is formed in the middle of the upper end surface of the mounting bottom plate (2), a side plate (7) is fixed on each of the left side and the right side of the upper end surface of the mounting bottom plate (2), a connecting groove (8) is formed in each of the inward sides of the two side plates (7), two connecting rods (5) are fixed on each of the outward sides of the fastening plates (9), a sliding groove (13) is formed in each of the connecting rods (5), a connecting rod I (3) is arranged in each of the sliding grooves (13), the other end of each connecting rod I (3) is fixed in each of the connecting grooves (8) of the side plates (7), a connecting spring (6) is connected between each connecting groove (8) and each fastening plate (9), each connecting spring (6) is sleeved on each of the connecting rods I (3) and each connecting rod II (5), and a through hole is formed in each outward side plate (7), the pull rope (4) penetrates through the through hole, the other end of the pull rope (4) is fixed on the fastening plate (9), and the flight control assembly (1) is placed in a placing groove (12) formed in the middle of the upper end surface of the mounting base plate (2).
2. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: the first connecting rod (3), the second connecting rod (5), the sliding groove (13) and the connecting spring (6) form a telescopic mechanism.
3. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: one end of the sliding groove (13) in the connecting rod II (5) is arranged in the connecting rod I (3), a limiting ring is fixed at one end, and the length of the connecting rod I (3) is smaller than the depth of the sliding groove (13).
4. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: the fixing groove is formed in one inward side of the fastening plate (9), a gasket (10) is arranged in the fixing groove, the gasket (10) is bonded in the fixing groove through epoxy resin, and the gasket (10) is made of rubber.
5. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: the height of the fastening plate (9) is smaller than that of the connecting groove (8).
6. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: connecting holes are formed in four corners of the upper end of the mounting bottom plate (2).
7. The mounting structure of unmanned aerial vehicle flight control subassembly of claim 1, characterized in that: the width of a placing groove (12) formed in the middle of the upper end surface of the mounting base plate (2) is larger than that of the flight control assembly (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121663949.1U CN215155722U (en) | 2021-07-21 | 2021-07-21 | Unmanned aerial vehicle flies mounting structure of accuse subassembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121663949.1U CN215155722U (en) | 2021-07-21 | 2021-07-21 | Unmanned aerial vehicle flies mounting structure of accuse subassembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215155722U true CN215155722U (en) | 2021-12-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121663949.1U Active CN215155722U (en) | 2021-07-21 | 2021-07-21 | Unmanned aerial vehicle flies mounting structure of accuse subassembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215155722U (en) |
-
2021
- 2021-07-21 CN CN202121663949.1U patent/CN215155722U/en active Active
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