CN214296419U - Integral type unmanned aerial vehicle frame - Google Patents
Integral type unmanned aerial vehicle frame Download PDFInfo
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- CN214296419U CN214296419U CN202120327751.XU CN202120327751U CN214296419U CN 214296419 U CN214296419 U CN 214296419U CN 202120327751 U CN202120327751 U CN 202120327751U CN 214296419 U CN214296419 U CN 214296419U
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Abstract
The utility model provides an integrated unmanned aerial vehicle frame; including the frame body, the bottom integrated into one piece of frame body has the mounting bracket, open one side of mounting bracket has the mounting hole, the homogeneous body shaping all around of frame body has the expansion board, one side integrated into one piece of expansion board has the connecting rod, the installation pole is installed through the bolt in one side of connecting rod, the one end integrated into one piece of installation pole has the installation shell, open at the top of installation shell has the mounting groove, the inside integrated into one piece of frame body has the fixed block, open the bottom of fixed block has thread groove one, open the bottom of mounting bracket has thread groove two, supporting mechanism is installed through the bolt in the bottom of mounting bracket, supporting mechanism is including the connecting plate, the bottom welding of connecting plate has the supporting leg. The utility model discloses prevent that the unmanned aerial vehicle frame from taking place to warp and the great phenomenon of deviation that the equipment part too leads to when using, improve the stability that the unmanned aerial vehicle frame used, improve the convenience to the installation of circuit board for unmanned aerial vehicle, be convenient for give off the heat that the circuit board produced.
Description
Technical Field
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to an integral type unmanned aerial vehicle frame.
Background
Along with the continuous development and the progress of scientific and technological, the unmanned aerial vehicle technique is also at quick development and maturity, and most unmanned aerial vehicle's frame forms for distributed equipment at present for can take place the deviation phenomenon when the equipment unmanned aerial vehicle frame, can discount greatly when leading to unmanned aerial vehicle to use.
Unmanned aerial vehicle support among the prior art has following problem: the unmanned aerial vehicle frame takes place to warp easily when using, and the great phenomenon of deviation can be produced to too many assembling parts simultaneously, leads to the stability of unmanned aerial vehicle frame use relatively poor, and it is not convenient relatively to the circuit board installation for unmanned aerial vehicle, is not convenient for give off the heat that the circuit board produced simultaneously.
Therefore, it is desirable to design an integrated drone frame to solve the above problems.
Disclosure of Invention
The utility model aims to overcome prior art's not enough unmanned aerial vehicle frame and take place to warp easily when using, the great phenomenon of deviation can be produced to too many of equipment parts simultaneously, leads to the relatively poor shortcoming of stability of unmanned aerial vehicle frame use, adapts to reality needs, provides an integral type unmanned aerial vehicle frame.
In order to realize the utility model discloses a purpose, the utility model discloses the technical scheme who adopts does:
the utility model provides an integral type unmanned aerial vehicle frame, includes the frame body, the bottom integrated into one piece of frame body has the mounting bracket, open one side of mounting bracket has the mounting hole, the homogeneous integrated into one piece all around of frame body has the expansion board, one side integrated into one piece of expansion board has the connecting rod, the installation pole is installed through the bolt to one side of connecting rod, the one end integrated into one piece of installation pole has the installation shell, open at the top of installation shell has the mounting groove, the inside integrated into one piece of frame body has the fixed block, open the bottom of fixed block has thread groove one, open the bottom of mounting bracket has thread groove two, the supporting mechanism is installed through the bolt in the bottom of mounting bracket, the supporting mechanism is including the connecting plate, the bottom welding of connecting plate has the supporting leg.
One end of the connecting rod is integrally formed with a first flange, and the other end of the mounting rod is integrally formed with a second flange.
One side of the first flange plate is provided with a first fixing hole, and one side of the second flange plate is provided with a second fixing hole.
One side of the first flange plate is provided with an inserting hole, one side of the second flange plate is provided with an inserting rod, and the inserting rod is inserted in the inserting hole.
The bottom welding of supporting leg has the bottom plate, the bottom of bottom plate is provided with the blotter.
The bottom of mounting bracket is opened there is the joint groove, the top integrated into one piece of connecting plate has the joint piece, and the inside in joint groove is pegged graft to the joint piece.
The bottom of the connecting plate is provided with a connecting hole, and the bottom of the connecting plate is provided with a sinking groove.
The beneficial effects of the utility model reside in that:
(1) this design utilizes frame body, mounting bracket, expansion board and connecting rod, and frame body, mounting bracket, expansion board and connecting rod are the integrated into one piece structure, prevent that the unmanned aerial vehicle frame from taking place to warp when using and the great phenomenon of deviation that the equipment part too leads to, improve the stability that the unmanned aerial vehicle frame used.
(2) This design utilizes fixed block and thread groove one, and the thread groove one is convenient for the circuit board to pass through the bolt and installs in the inside of frame body, improves the convenience to the installation of circuit board for unmanned aerial vehicle, and the fixed block enables to install this internal circuit board of frame and the inner wall of frame body and produces certain distance, is convenient for give off the heat that the circuit board produced.
(3) This design utilizes ring flange, inserted link and spliced eye, adopts ring flange one and ring flange two to connect connecting rod and installation pole, is convenient for to the equipment of connecting rod and installation pole, and the spliced pole is pegged graft in the inside of spliced eye, not only is convenient for to the concatenation between two ring flanges, improves the stability that connecting rod and installation pole are connected simultaneously.
(4) This design utilizes joint piece, joint groove and thread groove two, and the joint piece can the joint in the inside in joint groove, is convenient for play the positioning action when supporting mechanism installs in the bottom of mounting bracket, improves equipment unmanned aerial vehicle's efficiency, and bolt through-connection downthehole and screw thread can be with supporting mechanism fixed mounting in the bottom of mounting bracket in the inside of thread groove two.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present design;
FIG. 2 is a schematic diagram of the interior of the structure of the present design;
FIG. 3 is a schematic view of the mounting structure of the present design;
fig. 4 is a schematic view of the supporting frame of the present design.
In the figure: 1 frame body, 2 mounting brackets, 3 mounting holes, 4 supporting mechanisms, 5 expansion plates, 6 connecting rods, 7 mounting rods, 8 mounting shells, 9 mounting grooves, 10 fixing blocks, 11 thread groove I, 12 flange plate I, 13 fixing hole I, 14 flange plate II, 15 fixing hole II, 16 plug holes, 17 plug rods, 18 connecting plates, 19 supporting legs, 20 bottom plates, 21 cushion pads, 22 clamping blocks, 23 clamping grooves, 24 thread groove II, 25 connecting holes and 26 sinking grooves.
Detailed Description
The invention will be further described with reference to the following figures and examples:
an integrated unmanned aerial vehicle frame, see fig. 1 to 4, including a frame body 1, a mounting frame 2 is integrally formed at the bottom of the frame body 1, a mounting hole 3 is opened at one side of the mounting frame 2, an expansion plate 5 is integrally formed around the frame body 1, the expansion plate 5 increases the contact area of a connecting rod 6 and the frame body 1, and improves the stability of the connecting rod 6 when in use, a connecting rod 6 is integrally formed at one side of the expansion plate 5, the frame body 1, the mounting frame 2, the expansion plate 5 and the connecting rod 6 are all of an integrally formed structure, so as to prevent the unmanned aerial vehicle frame from deforming and having a large deviation caused by too many assembling parts when in use, a mounting rod 7 is installed at one side of the connecting rod 6 through a bolt, the mounting rod 7 increases the length of the connecting rod 6, so as to facilitate the retraction of an unmanned aerial vehicle, a mounting shell 8 is integrally formed at one end of the mounting rod 7, a mounting groove 9 is opened at the top of the mounting shell 8, the mounting groove 9 is used for mounting the coreless fan, a fixing block 10 is integrally formed in the rack body 1, the fixing block 10 enables a circuit board mounted in the rack body 1 to be away from the inner wall of the rack body 1 to facilitate dissipation of heat generated by the circuit board, a first thread groove 11 is formed in the bottom of the fixing block 10 and facilitates the circuit board to be mounted in the rack body 1 through bolts, convenience in mounting the circuit board for the unmanned aerial vehicle is improved, a second thread groove 24 is formed in the bottom of the mounting rack 2, the bolts penetrate through the connecting holes 25 and are threaded inside the second thread groove 24, the supporting mechanism 4 can be fixedly mounted at the bottom of the mounting rack 2, the supporting mechanism 4 is mounted at the bottom of the mounting rack 2 through bolts, the supporting mechanism 4 comprises a connecting plate 18, the connecting plate 18 facilitates connection of the supporting mechanism 4 and the mounting rack 2, and supporting legs 19 are welded at the bottom of the connecting plate 18, the supporting legs 19 are used for supporting the unmanned aerial vehicle frame.
Furthermore, in the design, one end of the connecting rod 6 is integrally formed with a first flange 12, the other end of the mounting rod 7 is integrally formed with a second flange 14, and the first flange 12 and the second flange 14 are adopted to connect the connecting rod 6 and the mounting rod 7, so that the connecting rod 6 and the mounting rod 7 can be conveniently assembled.
Furthermore, in the design, one side of the first flange plate 12 is provided with a first fixing hole 13, one side of the second flange plate 14 is provided with a second fixing hole 15, and bolts penetrate through the first fixing hole 13 and the second fixing hole 15 to fix the first flange plate 12 and the second flange plate 14.
Furthermore, in the design, one side of the first flange plate 12 is provided with an inserting hole 16, one side of the second flange plate 14 is provided with an inserting rod 17, and the inserting rod 17 is inserted in the inserting hole 16, so that the two flange plates can be spliced conveniently, and the connection stability of the connecting rod 6 and the mounting rod 7 is improved.
Further, in this design, the bottom welding of supporting leg 19 has bottom plate 20, and bottom plate 20 has increased the area of contact of supporting leg 19 with ground, and the bottom of bottom plate 20 is provided with blotter 21, and blotter 21 can play the cushioning effect to when unmanned aerial vehicle contacts ground.
Further, in this design, the bottom of mounting bracket 2 is opened there is joint groove 23, and the top integrated into one piece of connecting plate 18 has joint piece 22, and joint piece 22 pegs graft in the inside of joint groove 23, is convenient for play the positioning action when the bottom at mounting bracket 2 is installed at supporting mechanism 4, improves equipment unmanned aerial vehicle's efficiency.
Furthermore, in the design, the bottom of the connecting plate 18 is provided with a connecting hole 25, a bolt penetrates through the connecting hole 25 and is threaded inside the second thread groove 24, the supporting mechanism 4 can be fixedly installed at the bottom of the installation frame 2, the bottom of the connecting plate 18 is provided with a sinking groove 26, the bolt can be immersed in the sinking groove 26, and the attractiveness of the installation connecting plate 18 after installation is improved.
To sum up the utility model discloses a theory of operation does: when in use, the frame body 1, the mounting frame 2, the expansion plate 5 and the connecting rod 6 are of an integrally formed structure, the phenomenon that the unmanned aerial vehicle frame is deformed and the deviation caused by too many assembling parts is large when in use can be prevented, the stability of the unmanned aerial vehicle frame in use is improved, the circuit board is convenient to be mounted inside the frame body 1 through the bolt by adopting the first thread groove 11, the convenience of mounting the circuit board for the unmanned aerial vehicle is improved, the fixed block 10 can enable the circuit board mounted in the frame body 1 to generate a certain distance with the inner wall of the frame body 1, the heat generated by the circuit board is convenient to be dissipated, the clamping block 22 is clamped inside the clamping groove 23, the positioning effect is convenient to be realized when the supporting mechanism 4 is mounted at the bottom of the mounting frame 2, the efficiency of assembling the unmanned aerial vehicle is improved, the bolt penetrates through the connecting hole 25 and the thread is arranged inside the second thread groove 24, the supporting mechanism 4 can be fixedly mounted at the bottom of the mounting frame 2, connecting rod 6 and installation pole 7 pass through the bolt and the flange dish is connected, adopt flange dish one 12 and two 14 connecting rod 6 of flange dish and installation pole 7, be convenient for to connecting rod 6 and installation pole 7's equipment, peg graft in 16 inside of spliced eye, not only be convenient for to the concatenation between two flange dishes, improve the stability that connecting rod 6 and installation pole 7 are connected simultaneously, install the interior at mounting groove 9 with the coreless fan, later with the power supply line welding of coreless fan on the circuit board.
The embodiment of the present invention discloses a preferred embodiment, but not limited thereto, and those skilled in the art can easily understand the spirit of the present invention according to the above embodiment, and make different extensions and changes, but do not depart from the spirit of the present invention, all of which are within the protection scope of the present invention.
Claims (7)
1. The utility model provides an integral type unmanned aerial vehicle frame, includes frame body (1), its characterized in that, the bottom integrated into one piece of frame body (1) has mounting bracket (2), open one side of mounting bracket (2) has mounting hole (3), all integrated into one piece all around of frame body (1) has expansion board (5), one side integrated into one piece of expansion board (5) has connecting rod (6), install installation pole (7) through the bolt in one side of connecting rod (6), the one end integrated into one piece of installation pole (7) has installation shell (8), open at the top of installation shell (8) has mounting groove (9), the inside integrated into one piece of frame body (1) has fixed block (10), open the bottom of fixed block (10) has thread groove one (11), open the bottom of mounting bracket (2) has thread groove two (24), supporting mechanism (4) is installed through the bolt in the bottom of mounting bracket (2), the supporting mechanism (4) comprises a connecting plate (18), and supporting legs (19) are welded at the bottom of the connecting plate (18).
2. The integrated drone airframe of claim 1 wherein: one end of the connecting rod (6) is integrally formed with a first flange (12), and the other end of the mounting rod (7) is integrally formed with a second flange (14).
3. The integrated drone airframe of claim 2 wherein: one side of the first flange plate (12) is provided with a first fixing hole (13), and one side of the second flange plate (14) is provided with a second fixing hole (15).
4. The integrated drone airframe of claim 2 wherein: one side of the first flange plate (12) is provided with an inserting hole (16), one side of the second flange plate (14) is provided with an inserting rod (17), and the inserting rod (17) is inserted in the inserting hole (16).
5. The integrated drone airframe of claim 1 wherein: the bottom of the supporting leg (19) is welded with a bottom plate (20), and the bottom of the bottom plate (20) is provided with a cushion pad (21).
6. The integrated drone airframe of claim 1 wherein: the bottom of mounting bracket (2) is opened there is joint groove (23), the top integrated into one piece of connecting plate (18) has joint piece (22), and joint piece (22) pegs graft in the inside in joint groove (23).
7. The integrated drone airframe of claim 1 wherein: the bottom of the connecting plate (18) is provided with a connecting hole (25), and the bottom of the connecting plate (18) is provided with a sinking groove (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120327751.XU CN214296419U (en) | 2021-02-03 | 2021-02-03 | Integral type unmanned aerial vehicle frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120327751.XU CN214296419U (en) | 2021-02-03 | 2021-02-03 | Integral type unmanned aerial vehicle frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214296419U true CN214296419U (en) | 2021-09-28 |
Family
ID=77833293
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120327751.XU Active CN214296419U (en) | 2021-02-03 | 2021-02-03 | Integral type unmanned aerial vehicle frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214296419U (en) |
-
2021
- 2021-02-03 CN CN202120327751.XU patent/CN214296419U/en active Active
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