CN217022907U - Unmanned aerial vehicle twin-engine installs base structure convenient to dismantle - Google Patents
Unmanned aerial vehicle twin-engine installs base structure convenient to dismantle Download PDFInfo
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- CN217022907U CN217022907U CN202220651201.8U CN202220651201U CN217022907U CN 217022907 U CN217022907 U CN 217022907U CN 202220651201 U CN202220651201 U CN 202220651201U CN 217022907 U CN217022907 U CN 217022907U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses a conveniently-detachable unmanned aerial vehicle double-engine mounting base structure which comprises an unmanned aerial vehicle body, an engine left side placing mechanism, a fixing mechanism, an adjusting mechanism, a body mechanism and an engine right side placing mechanism, wherein the engine left side placing mechanism is located on the left side inside the unmanned aerial vehicle body, the fixing mechanism is located above the engine left side placing mechanism, the adjusting mechanism is located on the right side of the upper end of the engine left side placing mechanism, and the body mechanism is located in the middle of the upper end of the engine left side placing mechanism. This unmanned aerial vehicle twin-engine installation base structure convenient to dismantle, through setting up unable adjustment base, when the installation engine body, can fix engine body and unable adjustment base, install unable adjustment base in the inside of unmanned aerial vehicle body again, increase the convenience of engine body at unmanned aerial vehicle body internally mounted, the engine body and the dismantlement of unmanned aerial vehicle body of also being convenient for simultaneously.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a conveniently-detachable double-engine mounting base structure of an unmanned aerial vehicle.
Background
The engine is a machine capable of converting other forms of energy into mechanical energy and is a whole set of power output equipment, including speed changing gears, engines, transmission shafts and the like, and the engine which is most commonly used in life is an engine used on an automobile.
In the prior art, because of the importance of the engine, when the installation, mostly weld the engine in unmanned aerial vehicle's inside, this kind of welding mode is very firm in use, but not convenient to dismantle, especially when overhauing more troublesome.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model aims to provide a conveniently-detachable double-engine mounting base structure of an unmanned aerial vehicle, and aims to solve the problems that in the prior art, due to the importance of engines, most of the engines are welded inside the unmanned aerial vehicle during mounting, and although the welding mode is very firm in use, the disassembly is inconvenient, and particularly the maintenance is more troublesome.
(II) technical scheme
In order to achieve the purpose, the utility model provides the following technical scheme: an unmanned aerial vehicle twin-engine mounting base structure convenient to disassemble comprises an unmanned aerial vehicle body, an engine left side placing mechanism, a fixing mechanism, an adjusting mechanism, a body mechanism and an engine right side placing mechanism, wherein the engine left side placing mechanism is positioned on the left side inside the unmanned aerial vehicle body, the fixing mechanism is positioned above the engine left side placing mechanism, the adjusting mechanism is positioned on the right side of the upper end of the engine left side placing mechanism, the body mechanism is positioned in the middle of the upper end of the engine left side placing mechanism, the engine right side placing mechanism is positioned on the right side inside the unmanned aerial vehicle body, the fixing mechanism comprises a handrail, a fixing bolt, a handle, a limiting block and a fixing plate, the fixing bolt is movably mounted inside the handrail, the handle is fixedly arranged on the outer side of the upper end of the fixing bolt, the limiting block is fixedly mounted in the middle of the fixing bolt and positioned below the handrail, the fixing plate is movably installed in the middle of the fixing bolt and located below the limiting block.
Preferably, the engine left side placing mechanism is including unable adjustment base, mounting groove one, fixed orifices, mounting hole and built-in groove, mounting groove one is fixed to be set up in the left side of unable adjustment base upper end, the fixed left side that sets up at the middle part of unable adjustment base upper end and lie in mounting groove one of fixed orifices, the fixed avris that sets up in unable adjustment base upper end of mounting hole, the fixed inside that sets up in unable adjustment base right-hand member top of built-in groove through setting up unable adjustment base, when installing the engine body, can fix engine body and unable adjustment base well, installs the inside at the unmanned aerial vehicle body with unable adjustment base again, increases the convenience of engine body at unmanned aerial vehicle body internally mounted, and the engine body and the dismantlement of unmanned aerial vehicle body of also being convenient for simultaneously.
Preferably, guiding mechanism is including adjusting bottom plate, mounting groove two, fixed part and telescopic link, two fixed settings on the right side of adjusting the bottom plate upper end of mounting groove, fixed part fixed mounting is at the avris of adjusting the bottom plate upper end, telescopic link fixed mounting is at the left end of adjusting the bottom plate, through setting up the telescopic link, when installing engine body, will adjust the outside that the bottom plate released unable adjustment base through the telescopic link for mounting groove two and mounting groove one's space is enlarged, places unable adjustment bottom plate at mounting groove two and mounting groove one, will adjust the bottom plate and draw close unable adjustment base by the telescopic link again, makes unable adjustment bottom plate tightly block in mounting groove two and mounting groove one's inside, can not take place to rock.
Preferably, body mechanism is including PMKD, engine body, draw-in groove and fixed screw, engine body fixed mounting is in PMKD's upper end, the draw-in groove is fixed to be set up in PMKD's upper end and is located the outside of engine body, the fixed inside that sets up at PMKD and run through the draw-in groove of fixed screw increases the fastness of PMKD and unable adjustment base installation through setting up the draw-in groove.
Preferably, handrail and unable adjustment base fixed connection, fixing bolt is the inside of symmetric distribution in the handrail, the handle is a straight line structure, the fixed orifices is the middle part of symmetric distribution in unable adjustment base upper end, the mounting hole is the avris of symmetric distribution in unable adjustment base upper end, sets up the handle into a straight line structure, and it is more convenient when the dismouting the device of being convenient for.
Preferably, guiding mechanism and unable adjustment base fixed connection, mounting groove two and mounting groove one are the isostructure, fixed part and fixed establishment are the isostructure, the outside end fixed mounting of telescopic link sets up mounting groove two and mounting groove one to the isostructure in the inside of built-in groove, and both combine to form the notch and form all-round parcel to PMKD, and it is more fixed when making the PMKD installation.
Preferably, PMKD is located the upper end of mounting groove two and mounting groove one, the draw-in groove is symmetric distribution in PMKD's upper end, draw-in groove and PMKD looks adaptation, fixed screw and fixed orifices are the isostructure, fixed screw and fixing bolt looks adaptation are the isostructure with fixed screw and fixed orifices, and fixed screw and fixing bolt looks adaptation simultaneously, when fixed to PMKD, make fixing bolt from last to running through fixed screw down tightly link together PMKD and unable adjustment base.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the unmanned aerial vehicle double-engine mounting base structure convenient to disassemble, the engine body and the fixing base can be well fixed by arranging the fixing base when the engine body is mounted, and then the fixing base is mounted inside the unmanned aerial vehicle body, so that the convenience of mounting the engine body inside the unmanned aerial vehicle body is increased, and the engine body and the unmanned aerial vehicle body can be conveniently disassembled;
2. according to the conveniently-disassembled unmanned aerial vehicle dual-engine mounting base structure, when an engine body is mounted, the adjusting bottom plate is pushed out of the outer side of the fixing base through the telescopic rod, so that the space between the mounting groove II and the mounting groove I is enlarged, the fixing bottom plate is placed in the mounting groove II and the mounting groove I, and then the adjusting bottom plate is pulled close to the fixing base through the telescopic rod, so that the fixing bottom plate is tightly clamped in the mounting groove II and the mounting groove I, and the shaking cannot occur;
3. this unmanned aerial vehicle twin-engine installation base structure convenient to dismantle is through being the equivalent structure with fixed screw and fixed orifices, and fixed screw and fixing bolt looks adaptation simultaneously when fixed to PMKD, make fixing bolt from last to running through the fixed screw down tightly link together PMKD and unable adjustment base.
Drawings
FIG. 1 is a schematic top view of the present invention;
FIG. 2 is a schematic perspective view of a left placement mechanism of the engine of the present invention;
FIG. 3 is a schematic side view of the mechanism of the main body of the present invention;
FIG. 4 is a schematic cross-sectional view of a fixing mechanism according to the present invention;
FIG. 5 is a schematic cross-sectional view of an adjusting mechanism according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a mechanism is placed on the left side of the engine; 201. a fixed base; 202. a first mounting groove; 203. a fixing hole; 204. mounting holes; 205. a built-in groove; 3. a fixing mechanism; 301. a handrail; 302. fixing the bolt; 303. a handle; 304. a limiting block; 305. a fixing plate; 4. an adjustment mechanism; 401. adjusting the bottom plate; 402. a second mounting groove; 403. a fixing member; 404. a telescopic rod; 5. a body mechanism; 501. fixing a bottom plate; 502. an engine body; 503. a card slot; 504. fixing screw holes; 6. the engine right side is placed the mechanism.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without making any creative effort based on the embodiments in the present invention, belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a conveniently-detachable unmanned aerial vehicle dual-engine mounting base structure comprises an unmanned aerial vehicle body 1, an engine left side placing mechanism 2, a fixing mechanism 3, an adjusting mechanism 4, a body mechanism 5 and an engine right side placing mechanism 6, wherein the engine left side placing mechanism 2 is positioned on the left side inside the unmanned aerial vehicle body 1, the fixing mechanism 3 is positioned above the engine left side placing mechanism 2, the adjusting mechanism 4 is positioned on the right side of the upper end of the engine left side placing mechanism 2, the body mechanism 5 is positioned in the middle of the upper end of the engine left side placing mechanism 2, the engine right side placing mechanism 6 is positioned on the right side inside the unmanned aerial vehicle body 1, the fixing mechanism 3 comprises a handrail 301, a fixing bolt 302, a handle 303, a limiting block 304 and a fixing plate 305, the fixing bolt 302 is movably mounted inside the handrail 301, the handle 303 is fixedly arranged on the outer side of the fixing bolt 302, the limiting block 304 is fixedly mounted in the middle of the upper end of the fixing bolt 302 and positioned below the handrail 301, the fixing plate 305 is movably installed in the middle of the fixing bolt 302 and below the limiting block 304.
The engine left placing mechanism 2 comprises a fixed base 201, a first mounting groove 202, a first fixing hole 203, a mounting hole 204 and a built-in groove 205, the first mounting groove 202 is fixedly arranged on the left side of the upper end of the fixed base 201, the first fixing hole 203 is fixedly arranged in the middle of the upper end of the fixed base 201 and located on the left side of the first mounting groove 202, the mounting hole 204 is fixedly arranged on the lateral side of the upper end of the fixed base 201, the built-in groove 205 is fixedly arranged inside the upper portion of the right end of the fixed base 201, through the arrangement of the fixed base 201, when the engine body 502 is mounted, the engine body 502 and the fixed base 201 can be fixed well, the fixed base 201 is mounted inside the unmanned aerial vehicle body 1, the convenience of mounting the engine body 502 inside the unmanned aerial vehicle body 1 is improved, and meanwhile the engine body 502 and the unmanned aerial vehicle body 1 can be conveniently detached; the adjusting mechanism 4 comprises an adjusting bottom plate 401, a second mounting groove 402, a fixing part 403 and an expansion link 404, the second mounting groove 402 is fixedly arranged on the right side of the upper end of the adjusting bottom plate 401, the fixing part 403 is fixedly arranged on the side of the upper end of the adjusting bottom plate 401, the expansion link 404 is fixedly arranged on the left end of the adjusting bottom plate 401, and by arranging the expansion link 404, when the engine body 502 is mounted, the adjusting bottom plate 401 is pushed out of the outer side of the fixing base 201 through the expansion link 404, so that the space between the second mounting groove 402 and the first mounting groove 202 is enlarged, the fixing bottom plate 501 is placed in the second mounting groove 402 and the first mounting groove 202, and the adjusting bottom plate 401 is pulled close to the fixing base 201 through the expansion link 404, so that the fixing bottom plate 501 is tightly clamped in the second mounting groove 402 and the first mounting groove 202, and cannot shake; the body mechanism 5 comprises a fixed bottom plate 501, an engine body 502, a clamping groove 503 and a fixed screw hole 504, wherein the engine body 502 is fixedly arranged at the upper end of the fixed bottom plate 501, the clamping groove 503 is fixedly arranged at the upper end of the fixed bottom plate 501 and positioned at the outer side of the engine body 502, the fixed screw hole 504 is fixedly arranged in the fixed bottom plate 501 and penetrates through the clamping groove 503, and the firmness of installation of the fixed bottom plate 501 and the fixed base 201 is improved by arranging the clamping groove 503.
The handrail 301 is fixedly connected with the fixed base 201, the fixing bolts 302 are symmetrically distributed in the handrail 301, the handle 303 is in a linear structure, the fixing holes 203 are symmetrically distributed in the middle of the upper end of the fixed base 201, the mounting holes 204 are symmetrically distributed on the side edge of the upper end of the fixed base 201, and the handle 303 is arranged in a linear structure, so that the device is convenient to disassemble and assemble; the adjusting mechanism 4 is fixedly connected with the fixed base 201, the mounting groove II 402 and the mounting groove I202 are of the same structure, the fixing part 403 and the fixing mechanism 3 are of the same structure, the outer end of the telescopic rod 404 is fixedly mounted inside the built-in groove 205, the mounting groove II 402 and the mounting groove I202 are of the same structure, and the mounting groove II 402 and the mounting groove I202 are combined to form a notch to wrap the fixed base plate 501 in an all-dimensional mode, so that the fixed base plate 501 is more fixed during mounting; the PMKD 501 is located the upper end of mounting groove two 402 and mounting groove 202, the draw-in groove 503 is the upper end of symmetric distribution in PMKD 501, draw-in groove 503 and fixed plate 305 looks adaptation, fixed screw 504 and fixed orifices 203 are the equivalent structure, fixed screw 504 and fixing bolt 302 looks adaptation, be the equivalent structure with fixed screw 504 and fixed orifices 203, fixed screw 504 and fixing bolt 302 looks adaptation simultaneously, when fixed to PMKD 501, make fixing bolt 302 from last to running through fixed screw 504 from bottom tightly link together PMKD 501 and unable adjustment base 201.
The working principle is as follows: the technical scheme of the utility model is that an unmanned aerial vehicle double-engine mounting base structure convenient to disassemble is characterized in that a first mounting groove 202 is arranged at the upper end of a fixed base 201, a second mounting groove 402 is arranged at the upper end of an adjusting bottom plate 401, when an engine body 502 is mounted, the adjusting bottom plate 401 is pushed out of the outer side of the fixed base 201 through the arrangement of a telescopic rod 404, so that the space between the second mounting groove 402 and the first mounting groove 202 is enlarged, the fixed bottom plate 501 is placed in the second mounting groove 402 and the first mounting groove 202, the adjusting bottom plate 401 is pulled close to the fixed base 201 through the telescopic rod 404, the fixed bottom plate 501 is tightly clamped in the second mounting groove 402 and the first mounting groove 202 and cannot shake, when the engine body 502 is mounted in the unmanned aerial vehicle body 1, the engine body 502 and the fixed base 201 can be fixed, then the fixed base 201 is mounted in the unmanned aerial vehicle body 1, and the convenience of mounting the engine body 502 in the unmanned aerial vehicle body 1 is improved, also be convenient for simultaneously engine body 502 and unmanned aerial vehicle body 1 dismantle, each part of the device complements each other to it is more convenient in the handling to make engine body 502 dismantle in unmanned aerial vehicle body 1 through setting up handrail 301.
Finally, it should be noted that the above-mentioned contents are only used for illustrating the technical solutions of the present invention, and do not limit the protection scope of the present invention, and those skilled in the art can make simple modifications or equivalent substitutions on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle twin engine installation base structure convenient to dismantle, includes that unmanned aerial vehicle body (1), engine left side place mechanism (2), fixed establishment (3), guiding mechanism (4), body mechanism (5) and engine right side place mechanism (6), its characterized in that: the left engine side placing mechanism (2) is located on the left side of the inside of the unmanned aerial vehicle body (1), the fixing mechanism (3) is located above the left engine side placing mechanism (2), the adjusting mechanism (4) is located on the right side of the upper end of the left engine side placing mechanism (2), the body mechanism (5) is located in the middle of the upper end of the left engine side placing mechanism (2), the right engine side placing mechanism (6) is located on the right side of the inside of the unmanned aerial vehicle body (1), the fixing mechanism (3) comprises a handrail (301), a fixing bolt (302), a handle (303), a limiting block (304) and a fixing plate (305), the fixing bolt (302) is movably mounted inside the handrail (301), the handle (303) is fixedly arranged on the outer side of the fixing bolt (302), and the limiting block (304) is fixedly mounted in the middle of the upper end of the fixing bolt (302) and located below the handrail (301), the fixing plate (305) is movably arranged in the middle of the fixing bolt (302) and is positioned below the limiting block (304).
2. The unmanned aerial vehicle twin-engine installation base structure convenient to dismantle of claim 1, characterized in that: the engine left side is placed mechanism (2) including unable adjustment base (201), mounting groove (202), fixed orifices (203), mounting hole (204) and built-in groove (205), the fixed left side that sets up in unable adjustment base (201) upper end of mounting groove (202), the fixed middle part that sets up in unable adjustment base (201) upper end of fixed orifices (203) is located the left side of mounting groove (202), the avris of the fixed setting in unable adjustment base (201) upper end of mounting hole (204), the fixed inside that sets up in unable adjustment base (201) right-hand member top of built-in groove (205).
3. The unmanned aerial vehicle twin engine installation base structure convenient to dismantle of claim 2, characterized in that: adjustment mechanism (4) are including adjusting bottom plate (401), mounting groove two (402), fixed part (403) and telescopic link (404), mounting groove two (402) are fixed to be set up on the right side of adjusting bottom plate (401) upper end, fixed part (403) fixed mounting is at the avris of adjusting bottom plate (401) upper end, telescopic link (404) fixed mounting is at the left end of adjusting bottom plate (401).
4. The unmanned aerial vehicle twin engine installation base structure convenient to dismantle of claim 3, characterized in that: the engine body mechanism (5) comprises a fixed bottom plate (501), an engine body (502), a clamping groove (503) and a fixed screw hole (504), wherein the engine body (502) is fixedly arranged at the upper end of the fixed bottom plate (501), the clamping groove (503) is fixedly arranged at the upper end of the fixed bottom plate (501) and positioned at the outer side of the engine body (502), and the fixed screw hole (504) is fixedly arranged in the fixed bottom plate (501) and penetrates through the clamping groove (503).
5. The unmanned aerial vehicle twin engine installation base structure convenient to dismantle of claim 4, characterized in that: handrail (301) and unable adjustment base (201) fixed connection, fixing bolt (302) are symmetric distribution in the inside of handrail (301), handle (303) are the straight line structure, fixed orifices (203) are symmetric distribution in the middle part of unable adjustment base (201) upper end, mounting hole (204) are the avris of symmetric distribution in unable adjustment base (201) upper end.
6. The unmanned aerial vehicle twin-engine installation base structure convenient to dismantle of claim 5, characterized in that: the adjusting mechanism (4) is fixedly connected with the fixed base (201), the mounting groove II (402) and the mounting groove I (202) are of the same structure, the fixing part (403) and the fixing mechanism (3) are of the same structure, and the outer end of the telescopic rod (404) is fixedly mounted inside the built-in groove (205).
7. The unmanned aerial vehicle twin-engine installation base structure convenient to dismantle of claim 6, characterized in that: the fixed bottom plate (501) is located the upper end of mounting groove two (402) and mounting groove one (202), draw-in groove (503) are the upper end of symmetric distribution in fixed bottom plate (501), draw-in groove (503) and fixed plate (305) looks adaptation, fixed screw (504) and fixed orifices (203) are the equivalent structure, fixed screw (504) and fixing bolt (302) looks adaptation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220651201.8U CN217022907U (en) | 2022-03-24 | 2022-03-24 | Unmanned aerial vehicle twin-engine installs base structure convenient to dismantle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220651201.8U CN217022907U (en) | 2022-03-24 | 2022-03-24 | Unmanned aerial vehicle twin-engine installs base structure convenient to dismantle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217022907U true CN217022907U (en) | 2022-07-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220651201.8U Active CN217022907U (en) | 2022-03-24 | 2022-03-24 | Unmanned aerial vehicle twin-engine installs base structure convenient to dismantle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217022907U (en) |
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- 2022-03-24 CN CN202220651201.8U patent/CN217022907U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221013 Address after: No. 117, Group 8, Zhengfei Village, Goudun Town, Funing County, Yancheng City, Jiangsu Province, 224433 Patentee after: Chen Haifeng Patentee after: Wu Jun Address before: 450000 Taishan Road, Longhu Town, Xinzheng City, Zhengzhou City, Henan Province Patentee before: ZHENGZHOU YABO INTELLIGENT TECHNOLOGY CO.,LTD. |
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230301 Address after: 450000 Henan Electromechanical Vocational College, Taishan Road, Longhu Town, Xinzheng City, Zhengzhou City, Henan Province Patentee after: ZHENGZHOU YABO INTELLIGENT TECHNOLOGY CO.,LTD. Address before: No. 117, Group 8, Zhengfei Village, Goudun Town, Funing County, Yancheng City, Jiangsu Province, 224433 Patentee before: Chen Haifeng Patentee before: Wu Jun |
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| TR01 | Transfer of patent right |