CN212861838U - Can conveniently dismantle unmanned aerial vehicle of wing - Google Patents
Can conveniently dismantle unmanned aerial vehicle of wing Download PDFInfo
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- CN212861838U CN212861838U CN202021965663.4U CN202021965663U CN212861838U CN 212861838 U CN212861838 U CN 212861838U CN 202021965663 U CN202021965663 U CN 202021965663U CN 212861838 U CN212861838 U CN 212861838U
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Abstract
The utility model discloses an unmanned aerial vehicle that can conveniently dismantle wing, including the battery installation cover, the lower terminal surface sliding connection of battery installation cover has the main part mounting bracket, the both sides of main part mounting bracket all are provided with the side warning light, the lower terminal surface of main part mounting bracket is provided with the image acquisition head, the equal fixed mounting in four end angles of main part mounting bracket has the fixed connection arm, the up end fixed mounting of fixed connection arm has the angle locating plate, the inboard sliding connection of fixed connection arm has the wing, the inboard sliding connection of wing one end has the locating lever, the outside of locating lever bottom is provided with two first supporting spring, one of them the latch segment is installed to first supporting spring's bottom, the other end fixed mounting of wing has the motor cabinet. The utility model discloses a carry out fixed connection to wing and horn, be convenient for disassemble wing and horn, and then overhaul more convenient, and be convenient for adjust the horn angle, it is more convenient to debug.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle technical field specifically is an unmanned aerial vehicle that can conveniently dismantle wing.
Background
Along with the rapid development of social economy, unmanned aerial vehicles are used more and more, unmanned aerial vehicles are short unmanned aerial vehicles, and are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices; unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned dirigible, unmanned helicopter, unmanned many rotor crafts, unmanned parachute-wing aircraft etc. unmanned aerial vehicle's use technical requirement also is lower and lower.
However, in the use process of the existing unmanned aerial vehicle, the wings and the horn are inconvenient to disassemble, so that the trouble of maintenance and replacement is caused, the horn is inconvenient to adjust, and the debugging is inconvenient; therefore, the existing requirements are not met, and the unmanned aircraft with the conveniently detachable wings is provided for the unmanned aircraft.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a can conveniently dismantle unmanned aerial vehicle of wing to in solving the current unmanned aerial vehicle use that proposes in the above-mentioned background art, be not convenient for disassemble wing and horn, cause to overhaul and change troublesome, and be not convenient for adjust the horn, debug inconvenient scheduling problem.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with conveniently detachable wings comprises a battery mounting cover, wherein the lower end surface of the battery mounting cover is connected with a main body mounting frame in a sliding way, side warning lamps are arranged on two sides of the main body mounting frame, an image collecting head is arranged on the lower end face of the main body mounting frame, the four end corners of the main body mounting frame are fixedly provided with fixed connecting arms, the upper end surfaces of the fixed connecting arms are fixedly provided with angle positioning plates, the inner side of the fixed connecting arm is connected with a wing in a sliding way, the inner side of one end of the wing is connected with a positioning rod in a sliding way, the outer side of the bottom end of the positioning rod is provided with two first supporting springs, the bottom end of one of the first supporting springs is provided with a locking block, the other end of the wing is fixedly provided with a motor base, the motor transmission gear is arranged on the inner side of the motor base, and the propeller is installed on one side of the motor transmission gear.
Preferably, the fixed connecting sleeve is fixedly mounted at four end corners of the lower end face of the main body mounting frame, a second supporting spring is arranged on the inner side of the fixed connecting sleeve, and a supporting foot block is fixedly mounted on the outer side of the bottom end of the second supporting spring.
Preferably, the one end and the main part mounting bracket welded fastening of fixed link arm, the inboard of fixed link arm one end all is provided with the locating hole with the one end of wing, the inboard of locating hole is provided with the check lock pole, the fixed link arm passes through the check lock pole with the wing and is connected.
Preferably, the angle locating plate passes through the screw connection to be fixed at the up end of fixed connection arm, the up end of angle locating plate is provided with the equidistance locating hole, the bottom of locating lever runs through the inboard that equidistance locating hole and wing extended to the latch segment respectively, the wing passes through first supporting spring with the latch segment and is connected fixedly, the latch segment passes through the nut with the locating lever and is connected fixedly.
Preferably, the up end of main part mounting bracket is provided with the spout, the both sides of battery installation cover all extend to the inboard of spout, the both ends of battery installation cover are all fixed through the joint with the main part mounting bracket.
Preferably, the motor is arranged on the inner side of the motor base, the motor transmission gear is fixedly connected to the outer side of the upper end of the motor through a flat key, the bottom end of the propeller is connected with the motor base through a bearing, and the propeller is connected with the motor transmission gear through a gear.
Preferably, the fixed connecting sleeve is fixedly connected with the main body mounting frame through a screw, the fixed connecting sleeve is connected with the supporting foot block through a second supporting spring, and threads are arranged on the outer side of the upper end of the supporting foot block and the inner side of the bottom end of the fixed connecting sleeve.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses a both ends of battery installation cover all are fixed through the joint with the main part mounting bracket for dismantle through the battery installation cover and can change the battery, be convenient for protect and install the battery, the fixed connection arm passes through the check lock lever with the wing and is connected, and then can fix the wing and the definite of angle through the check lock lever, adjust the wing through the angle relative to the fixed connection arm, and then confirm the angle through the check lock lever, be convenient for wholly debug the position of propeller and wing;
2. the utility model discloses a to the dismouting of location member can disassemble wing and screw, be convenient for overhaul the operation to the motor cabinet, and first supporting spring plays the cushioning effect to the wing, the outside of supporting foot piece upper end all is provided with the screw thread with the inboard of fixed connection cover bottom, separates and then realizes the supporting foot piece to wholly support and the shock attenuation through fixed connection cover and supporting foot piece, uses safelyr.
Drawings
Fig. 1 is a schematic overall structure diagram of the present invention;
fig. 2 is a top view of the whole of the present invention;
fig. 3 is a schematic view of a partial cross-sectional structure of the wing of the present invention;
fig. 4 is a schematic view of a partial structure of the main body mounting frame of the present invention.
In the figure: 1. a motor base; 2. a propeller; 3. an airfoil; 4. an angle positioning plate; 5. a fixed connecting arm; 6. a main body mounting frame; 7. a side warning light; 8. a battery mounting cover; 9. a motor transmission gear; 10. positioning a rod; 11. a first support spring; 12. a locking block; 13. an image pick-up head; 14. fixing the connecting sleeve; 15. a second support spring; 16. and a supporting foot block.
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.
Referring to fig. 1 to 4, the present invention provides an embodiment: an unmanned aerial vehicle with conveniently detachable wings comprises a battery mounting cover 8, wherein the lower end surface of the battery mounting cover 8 is connected with a main body mounting frame 6 in a sliding manner, two ends of the battery mounting cover 8 and the main body mounting frame 6 are fixed in a clamping manner, batteries can be replaced by detaching through the battery mounting cover 8, the batteries are protected and mounted conveniently, side warning lamps 7 are arranged on two sides of the main body mounting frame 6, an image acquisition head 13 is arranged on the lower end surface of the main body mounting frame 6, fixed connecting arms 5 are fixedly arranged on four end corners of the main body mounting frame 6, an angle positioning plate 4 is fixedly arranged on the upper end surface of each fixed connecting arm 5, wings 3 are slidably connected to the inner sides of the fixed connecting arms 5, positioning rods 10 are slidably connected to the inner sides of one ends of the wings 3, the angles of the wings 3 relative to the fixed connecting arms 5 are adjusted, and the, be convenient for wholly debug the operation to the position of screw 2 and wing 3, the outside of locating lever 10 bottom is provided with two first supporting spring 11, latch segment 12 is installed to the bottom of one of them first supporting spring 11, the other end fixed mounting of wing 3 has motor cabinet 1, the inboard of motor cabinet 1 is provided with motor drive gear 9, screw 2 is installed to one side of motor drive gear 9, wholly through carrying out fixed connection to wing 3 and horn, be convenient for disassemble wing 3 and horn, and then it is more convenient to overhaul, and be convenient for adjust the horn angle, it is more convenient to debug.
Further, fixed connection sleeves 14 are fixedly installed at four end corners of the lower end face of the main body installation frame 6, second support springs 15 are arranged on the inner sides of the fixed connection sleeves 14, and support foot blocks 16 are fixedly installed on the outer sides of the bottom ends of the second support springs 15.
Through adopting above-mentioned technical scheme, separate through fixed connection cover 14 and supporting foot piece 16, be convenient for support the whole through supporting foot piece 16.
Furthermore, one end of the fixed connecting arm 5 is welded and fixed with the main body mounting frame 6, the inner side of one end of the fixed connecting arm 5 and one end of the wing 3 are both provided with a positioning hole, the inner side of the positioning hole is provided with a locking rod, and the fixed connecting arm 5 is connected with the wing 3 through the locking rod.
Through adopting above-mentioned technical scheme, can fix and the definite of angle to wing 3 through the check lock pole.
Furthermore, the angle positioning plate 4 is fixed on the upper end face of the fixed connecting arm 5 through screw connection, the upper end face of the angle positioning plate 4 is provided with equidistant positioning holes, the bottom end of the positioning rod 10 penetrates through the equidistant positioning holes and the inner sides of the wings 3 extending to the locking blocks 12 respectively, the wings 3 are connected with the locking blocks 12 through first supporting springs 11, and the locking blocks 12 are connected and fixed with the positioning rod 10 through nuts.
By adopting the technical scheme, the angle of the wing 3 relative to the fixed connecting arm 5 is adjusted, and then the angle is determined through the positioning rod 10, so that the whole debugging operation on the positions of the propeller 2 and the wing 3 is facilitated.
Further, the up end of main part mounting bracket 6 is provided with the spout, and the both sides of battery installation cover 8 all extend to the inboard of spout, and the both ends of battery installation cover 8 are all fixed through the joint with main part mounting bracket 6.
Through adopting above-mentioned technical scheme, can change the battery to dismantling through battery installation cover 8, be convenient for protect and install the battery.
Further, a motor is arranged on the inner side of the motor base 1, a motor transmission gear 9 is fixedly connected to the outer side of the upper end of the motor through a flat key, the bottom end of the propeller 2 is connected with the motor base 1 through a bearing, and the propeller 2 is connected with the motor transmission gear 9 through a gear.
Through adopting above-mentioned technical scheme, be convenient for carry out the dismouting and overhaul the motor to motor drive gear 9.
Further, the fixed connecting sleeve 14 is fixedly connected with the main body mounting frame 6 through screws, the fixed connecting sleeve 14 is connected with the supporting foot block 16 through the second supporting spring 15, and threads are arranged on the outer side of the upper end of the supporting foot block 16 and the inner side of the bottom end of the fixed connecting sleeve 14.
Through adopting above-mentioned technical scheme, connect through second supporting spring 15, be convenient for cushion whole.
The working principle is as follows: when the device is used, whether the functions of all parts are intact is checked, a sliding groove is arranged on the upper end face of a main body mounting frame 6, two sides of a battery mounting cover 8 extend to the inner side of the sliding groove, two ends of the battery mounting cover 8 are fixed with the main body mounting frame 6 in a clamping mode, so that the battery can be replaced by disassembling the battery mounting cover 8, the battery is protected and mounted conveniently, positioning holes are formed in the inner side of one end of a fixed connecting arm 5 and one end of a wing 3, a locking rod is arranged on the inner side of each positioning hole, the fixed connecting arm 5 is connected with the wing 3 through the locking rod, the wing 3 can be fixed and the angle can be determined through the locking rod, equidistant positioning holes are formed in the upper end face of an angle positioning plate 4, the bottom end of a positioning rod 10 penetrates through the equidistant positioning holes and the wing 3 to extend to the inner side of a locking block 12 respectively, further, the angle is determined by the positioning rod 10, so that the position of the propeller 2 and the wing 3 can be conveniently debugged and operated integrally, the wing 3 is connected with the locking block 12 through the first supporting spring 11, the locking block 12 is fixedly connected with the positioning rod 10 through a nut, the wing 3 and the propeller 2 can be disassembled by disassembling and assembling the positioning rod 10, the maintenance and operation of the motor base 1 are convenient, the first supporting spring 11 has a damping effect on the wing 3, the fixed connecting sleeves 14 are fixedly installed at four corners of the bottom end of the main body mounting frame 6, the fixed connecting sleeves 14 are connected with the supporting foot blocks 16 through the second supporting springs 15, wherein the outer sides of the upper ends of the supporting foot blocks 16 and the inner sides of the bottom ends of the fixed connecting sleeves 14 are provided with threads, so that the fixed connecting sleeves 14 are fixedly connected through the supporting foot blocks 16 through the threads, and further the whole body can be placed and supported through the, the supporting foot blocks 16 are integrally supported and damped by separating the fixed connecting sleeves 14 from the supporting foot blocks 16, so that the use is safer.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented 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.
Claims (7)
1. The utility model provides a can conveniently dismantle unmanned aerial vehicle of wing, includes battery installation cover, its characterized in that: the lower terminal surface sliding connection of battery installation cover has the main part mounting bracket, the both sides of main part mounting bracket all are provided with the side warning light, the lower terminal surface of main part mounting bracket is provided with the image acquisition head, the equal fixed mounting in four end angles of main part mounting bracket has fixed connection arm, fixed connection arm's up end fixed mounting has the angle locating plate, fixed connection arm's inboard sliding connection has the wing, the inboard sliding connection of wing one end has the locating lever, the outside of locating lever bottom is provided with two first supporting spring, one of them the latch segment is installed to first supporting spring's bottom, the other end fixed mounting of wing has the motor cabinet, the inboard of motor cabinet is provided with motor drive gear, the screw is installed to motor drive gear's one side.
2. The unmanned aerial vehicle with the detachable wings, according to claim 1, wherein: the fixed connecting sleeve is fixedly mounted at four end corners of the lower end face of the main body mounting frame, a second supporting spring is arranged on the inner side of the fixed connecting sleeve, and a supporting foot block is fixedly mounted on the outer side of the bottom end of the second supporting spring.
3. The unmanned aerial vehicle with the detachable wings, according to claim 1, wherein: one end of the fixed connecting arm is welded and fixed with the main body mounting frame, the inner side of one end of the fixed connecting arm and one end of the wing are both provided with a positioning hole, the inner side of the positioning hole is provided with a locking rod, and the fixed connecting arm is connected with the wing through the locking rod.
4. The unmanned aerial vehicle with the detachable wings, according to claim 1, wherein: the angle locating plate passes through the screw connection to be fixed at the up end of fixed connection arm, the up end of angle locating plate is provided with the equidistance locating hole, the bottom of locating lever runs through the inboard that equidistance locating hole and wing extended to the latch segment respectively, the wing passes through a supporting spring with the latch segment and is connected, the latch segment passes through the nut with the locating lever and is connected fixedly.
5. The unmanned aerial vehicle with the detachable wings, according to claim 1, wherein: the up end of main part mounting bracket is provided with the spout, the both sides of battery installation cover all extend to the inboard of spout, the both ends of battery installation cover all are fixed through the joint with the main part mounting bracket.
6. The unmanned aerial vehicle with the detachable wings, according to claim 1, wherein: the motor is arranged on the inner side of the motor base, the motor transmission gear is fixedly connected to the outer side of the upper end of the motor through a flat key, the bottom end of the propeller is connected with the motor base through a bearing, and the propeller is connected with the motor transmission gear through a gear.
7. The unmanned aerial vehicle with the detachable wings, according to claim 2, wherein: the fixed connecting sleeve is fixedly connected with the main body mounting frame through screws, the fixed connecting sleeve is connected with the supporting foot blocks through second supporting springs, and threads are arranged on the outer side of the upper ends of the supporting foot blocks and the inner side of the bottom end of the fixed connecting sleeve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021965663.4U CN212861838U (en) | 2020-09-10 | 2020-09-10 | Can conveniently dismantle unmanned aerial vehicle of wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021965663.4U CN212861838U (en) | 2020-09-10 | 2020-09-10 | Can conveniently dismantle unmanned aerial vehicle of wing |
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| Publication Number | Publication Date |
|---|---|
| CN212861838U true CN212861838U (en) | 2021-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202021965663.4U Active CN212861838U (en) | 2020-09-10 | 2020-09-10 | Can conveniently dismantle unmanned aerial vehicle of wing |
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| CN (1) | CN212861838U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114701638A (en) * | 2022-03-07 | 2022-07-05 | 上海立鑫安防工程有限公司 | Unmanned aerial vehicle for security protection convenient to it is folding |
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2020
- 2020-09-10 CN CN202021965663.4U patent/CN212861838U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114701638A (en) * | 2022-03-07 | 2022-07-05 | 上海立鑫安防工程有限公司 | Unmanned aerial vehicle for security protection convenient to it is folding |
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