CN214524445U - Air cylinder buffer device of unmanned airport - Google Patents
Air cylinder buffer device of unmanned airport Download PDFInfo
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- CN214524445U CN214524445U CN202023251771.8U CN202023251771U CN214524445U CN 214524445 U CN214524445 U CN 214524445U CN 202023251771 U CN202023251771 U CN 202023251771U CN 214524445 U CN214524445 U CN 214524445U
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Abstract
The utility model particularly discloses a cylinder buffer at unmanned airport, include: the middle part of the rack is provided with an installation cavity; the first partition plate and the first air cylinder are fixed on the inner wall of the rack and are in driving connection with the first partition plate, and the first partition plate transversely crosses the installation cavity and can move back and forth; the second air cylinder is fixed on the inner wall of the rack and is in driving connection with the second partition plate, the second partition plate transversely crosses the installation cavity and can do reciprocating movement in the same direction as the first partition plate, and the first air cylinder and the second air cylinder are located on different planes. The utility model discloses a cylinder buffer structural reliability is strong, simple structure, and the precision of operation is stronger and the smoothness nature is higher.
Description
Technical Field
The utility model relates to an unmanned airport technical field, concretely relates to cylinder buffer at unmanned airport.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like. The drone needs to be parked back into the prepared airport after use.
However, the cylinder buffer device of the existing unmanned airport has low control precision, great mutual operation influence and low stability.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome prior art not enough, provide a cylinder buffer at unmanned airport.
The utility model discloses the above-mentioned problem that will solve is through following technical scheme in order to realize:
a cylinder cushion apparatus for an unmanned aerial vehicle, comprising: the middle part of the frame 1 is provided with an installation cavity; the first partition plate and the first air cylinder are fixed on the inner wall of the rack and are in driving connection with the first partition plate, and the first partition plate transversely crosses the installation cavity and can move back and forth; the second air cylinder is fixed on the inner wall of the rack and is in driving connection with the second partition plate, the second partition plate transversely crosses the installation cavity and can do reciprocating movement in the same direction as the first partition plate, and the first air cylinder and the second air cylinder are located on different planes.
Preferably, the frame comprises two support structures, the support structures being arranged side by side and the mounting cavity being formed between the support structures.
Preferably, the supporting structure comprises a transverse bracket and a longitudinal bracket, and the two longitudinal brackets are selected and fixed at the left end and the right end of the transverse bracket respectively.
Preferably, at least two transverse supports are selected, at least one placing cavity is formed between the transverse supports, and the first air cylinder and the second air cylinder are fixed on the upper side and the lower side of the same placing cavity or fixed in different placing cavities.
Preferably, the first partition plate is movably connected to the first air cylinder through a first splicing assembly, and the second partition plate is movably connected to the second air cylinder through a second splicing assembly.
Preferably, the first splicing assembly comprises a first arc plate, a first supporting straight plate and a first splicing buckle, two ends of the first arc plate are respectively and fixedly connected with the top of the first supporting straight plate and the side end of the first partition plate, the bottom of the first supporting straight plate is connected with one end of the first splicing buckle, and the first splicing buckle is connected to the telescopic shaft of the first cylinder in a buckling manner; the first arc plate, the first supporting straight plate and the first splicing buckle form a Z-shaped structure.
Preferably, the second splicing assembly comprises a second arc plate, a second supporting straight plate and a second splicing buckle, two ends of the second arc plate are respectively and fixedly connected with the top of the second supporting straight plate and the side end of the second partition plate, the bottom of the second supporting straight plate is connected with one end of the second splicing buckle, and the second splicing buckle is connected to the telescopic shaft of the second cylinder in a buckling manner; the second arc plate, the second supporting straight plate and the second splicing buckle form a Z-shaped structure.
Preferably, the second supporting straight plate and the first supporting straight plate are movably connected to the side end of the rack through a sliding rail assembly.
Preferably, the slide rail assembly comprises a first slide block, a second slide block and a guide rail, the guide rail is fixed at the inner side end of the rack, one side surface of the first slide block is fixedly connected with the first support straight plate, and the other side end of one side surface of the first slide block is slidably connected to the guide rail; and one side surface of the second sliding block is fixedly connected with the second supporting straight plate, and the other side of the second sliding block is connected on the guide rail in a sliding manner.
Preferably, the guide rail is an I-shaped slide rail.
Has the advantages that: after the structure of the utility model is adopted, the first and the second air cylinders respectively drive the first and the second clapboards to do the transverse reciprocating movement, so that the respective baffle separation processes can be ensured not to be influenced, and the working efficiency and the convenience of disassembly, maintenance and repair are improved; meanwhile, the first cylinder and the second cylinder which are arranged on different planes can avoid mutual influence in the operation process, and the order and the fluency of operation are guaranteed; besides, the structure has strong reliability and lower processing cost.
Drawings
Fig. 1 is a schematic structural diagram of a cylinder buffer device of an unmanned airport according to the present invention.
Fig. 2 is a schematic structural diagram of a part of a cylinder buffer device of an unmanned airport according to the present invention.
FIGS. 1-2: 1-a frame; 11-a transverse bracket; 111-a first placement cavity; 112-a second placement cavity; 12-a longitudinal scaffold; 2-a first separator; 3-a first cylinder; 4-a second separator; 5-a second cylinder; 61-a first arc plate; 63-a first supporting straight plate; 64-a first splice buckle; 71-a first slider; 72-a second slider; 73-a guide rail; 81-a second arc plate; 82-a second supporting straight plate; 83-second splice clasp.
Detailed Description
The present invention will be described in further detail with reference to the following drawings and specific examples, which are not intended to limit the present invention in any manner.
The directional designations of "front", "rear", "left" and "right" described in this specification are determined according to the schematic drawings used in this specification.
As shown in fig. 1-2, a cylinder buffer apparatus for an unmanned aerial vehicle includes: the device comprises a rack 1, wherein a mounting cavity is formed in the middle of the rack 1; a first partition plate 2 and a first air cylinder 3, wherein the first air cylinder 3 is fixed on the inner wall of the frame 1 and is in driving connection with the first partition plate 2, and the first partition plate 2 spans the installation cavity and can move back and forth; the second partition plate 4 and the second air cylinder 5, the second air cylinder 5 is fixed on the inner wall of the frame 1 and is in driving connection with the second partition plate 4, the second partition plate 4 crosses the installation cavity and can do reciprocating movement in the same direction as the first partition plate 2, and the first air cylinder 3 and the second air cylinder 5 are in different planes.
The first and second air cylinders respectively drive the first and second partition plates to transversely reciprocate, so that the respective blocking and separating processes are not influenced, and the working efficiency and the convenience of disassembly, overhaul and maintenance are improved; simultaneously, the first cylinder and the second cylinder which are arranged on different planes can avoid mutual influence in the operation process, and the orderliness and the fluency of operation are guaranteed.
Specifically, the frame 1 includes two support structures, the support structures are distributed side by side and the installation cavity is formed between the support structures, and the stability of the partition board and the cylinder installation is guaranteed through the support of the left and right double pivots.
The supporting structure comprises a transverse bracket 11 and a longitudinal bracket 12, wherein the two longitudinal brackets 12 are selected and fixed at the left end and the right end of the transverse bracket 11 respectively;
it can be understood that two transverse supports 11 are selected and distributed side by side, a second placing cavity 112 is formed between the transverse supports 11, the first air cylinder 3 and the second air cylinder 5 are respectively fixed at the upper end and the lower end of the second placing cavity 112, and the operation fluency of each operation process can be further ensured by separately placing the upper end and the lower end of the first air cylinder 3 and the upper end and the lower end of the second air cylinder 5.
It can also be understood that three transverse supports 11 are selected and distributed side by side, a first placing cavity 111 and a second placing cavity 112 are formed between the transverse supports 11, and the first cylinder 3 and the second cylinder 5 are respectively located on the inner walls of the first placing cavity 111 and the second placing cavity 112.
Specifically, the first partition plate 2 is movably connected to the first cylinder 3 through a first splicing assembly, and the second partition plate 4 is movably connected to the second cylinder 5 through a second splicing assembly.
It can be understood that the first splicing assembly comprises a first arc plate 61, a first supporting straight plate 63 and a first splicing buckle 64, two ends of the first arc plate 61 are respectively and fixedly connected with the top of the first supporting straight plate 63 and the side end of the first partition plate 2, the bottom of the first supporting straight plate 63 is connected with one end of the first splicing buckle 64, and the first splicing buckle 64 is connected to the telescopic shaft of the first cylinder 3 in a buckling manner; the first arc plate 61, the first straight supporting plate 63 and the first splicing buckle 64 form a Z-shaped structure; the first splicing assembly with the Z-shaped structure can guarantee the stability of the support, and meanwhile, the installation space can be saved.
It can also be understood that the second splicing assembly comprises a second arc plate 81, a second supporting straight plate 82 and a second splicing buckle 83, two ends of the second arc plate 81 are respectively and fixedly connected with the top of the second supporting straight plate 82 and the side end of the second partition plate 4, the bottom of the second supporting straight plate 82 is connected with one end of the second splicing buckle 83, and the second splicing buckle 83 is connected to the telescopic shaft of the second cylinder 5 in a buckling manner; the second arc plate 81, the second supporting straight plate 82 and the second splicing buckle 83 form a Z-shaped structure; the first splicing assembly with the Z-shaped structure can guarantee the stability of the support, and meanwhile, the installation space can be saved.
Specifically, the second supporting straight plate 82 and the first supporting straight plate 63 are movably connected to the side end of the frame 1 through a slide rail assembly. The operation stability of the first and second partition plates can be further ensured through the sliding rail assembly.
It can be understood that the slide rail assembly comprises a first slide block 71, a second slide block 72 and a guide rail 73, the guide rail 73 is fixed at the inner end of the side end of the frame 1, one side surface of the first slide block 71 is fixedly connected with the first support straight plate 63, and the other side end of one side surface of the first slide block 71 is slidably connected on the guide rail 73; one side surface of the second sliding block 72 is fixedly connected with the second straight supporting plate 82, and the other side of the second sliding block 72 is slidably connected to the guide rail 73.
It will also be appreciated that the rails 73 are I-shaped rails.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (10)
1. A cylinder buffer device for an unmanned aerial vehicle, comprising:
the middle part of the rack is provided with an installation cavity;
the first partition plate and the first air cylinder are fixed on the inner wall of the rack and are in driving connection with the first partition plate, and the first partition plate transversely crosses the installation cavity and can move back and forth;
the second air cylinder is fixed on the inner wall of the rack and is in driving connection with the second partition plate, the second partition plate transversely crosses the installation cavity and can do reciprocating movement in the same direction as the first partition plate, and the first air cylinder and the second air cylinder are located on different planes.
2. The cylinder cushion system for an unmanned airport of claim 1, wherein the frame comprises two support structures, the support structures being arranged side-by-side and forming the mounting cavity therebetween.
3. The cylinder buffer device at the unmanned airport according to claim 2, wherein the support structure comprises two lateral brackets and two longitudinal brackets fixed at the left and right ends of the lateral brackets.
4. The cylinder buffer device for the unmanned airport according to claim 3, wherein at least two transverse brackets are selected, at least one placing cavity is formed between the transverse brackets, and the first cylinder and the second cylinder are fixed on the upper side and the lower side of the same placing cavity or the first cylinder and the second cylinder are fixed in different placing cavities.
5. The cylinder cushion system for an unmanned airport of claim 1, wherein said first bulkhead is movably connected to said first cylinder by a first splice assembly and said second bulkhead is movably connected to said second cylinder by a second splice assembly.
6. The cylinder buffer device for the unmanned airport according to claim 5, wherein the first splicing assembly comprises a first arc plate, a first straight supporting plate and a first splicing buckle, two ends of the first arc plate are fixedly connected with the top of the first straight supporting plate and the side end of the first partition plate respectively, the bottom of the first straight supporting plate is connected with one end of the first splicing buckle, and the first splicing buckle is connected to the telescopic shaft of the first cylinder in a buckling manner; the first arc plate, the first supporting straight plate and the first splicing buckle form a Z-shaped structure.
7. The cylinder buffer device for the unmanned airport according to claim 5, wherein the second splicing assembly comprises a second arc plate, a second straight supporting plate and a second splicing buckle, two ends of the second arc plate are respectively and fixedly connected with the top of the second straight supporting plate and the side end of the second partition plate, the bottom of the second straight supporting plate is connected with one end of the second splicing buckle, and the second splicing buckle is connected to the telescopic shaft of the second cylinder in a buckling manner; the second arc plate, the second supporting straight plate and the second splicing buckle form a Z-shaped structure.
8. The cylinder buffer device for the unmanned airport according to claim 7, wherein the second straight supporting plate and the first straight supporting plate are movably connected to the side end of the frame through a sliding rail assembly.
9. The cylinder buffer device for the unmanned aerial vehicle as claimed in claim 8, wherein the rail assembly comprises a first sliding block, a second sliding block and a guide rail, the guide rail is fixed at an inner side end of a side end of the frame, a side surface of the first sliding block is fixedly connected with the first support straight plate, and another side end of a side surface of the first sliding block is slidably connected with the guide rail; and one side surface of the second sliding block is fixedly connected with the second supporting straight plate, and the other side of the second sliding block is connected on the guide rail in a sliding manner.
10. The cylinder buffer device for the unmanned aerial vehicle as claimed in claim 9, wherein the rail is an i-shaped rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023251771.8U CN214524445U (en) | 2020-12-29 | 2020-12-29 | Air cylinder buffer device of unmanned airport |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023251771.8U CN214524445U (en) | 2020-12-29 | 2020-12-29 | Air cylinder buffer device of unmanned airport |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214524445U true CN214524445U (en) | 2021-10-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023251771.8U Active CN214524445U (en) | 2020-12-29 | 2020-12-29 | Air cylinder buffer device of unmanned airport |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214524445U (en) |
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2020
- 2020-12-29 CN CN202023251771.8U patent/CN214524445U/en active Active
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