CN209795851U - Auxiliary landing lighting device for unmanned aerial vehicle - Google Patents
Auxiliary landing lighting device for unmanned aerial vehicle Download PDFInfo
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- CN209795851U CN209795851U CN201920593036.3U CN201920593036U CN209795851U CN 209795851 U CN209795851 U CN 209795851U CN 201920593036 U CN201920593036 U CN 201920593036U CN 209795851 U CN209795851 U CN 209795851U
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Abstract
The utility model discloses an unmanned aerial vehicle is with supplementary descending lighting fixture, including shell, circuit board, profection lamp and apron, the profection lamp passes through screw fixed mounting in the bottom of shell, fixed mounting has switch on the shell, the circuit board passes through screw fixed mounting in the shell, the circuit board has distance sensor through electric wire electric connection, the circuit board has the lithium cell through electric wire electric connection, the lithium cell passes through electric wire and switch electric connection, distance sensor passes through electric wire and profection lamp electric connection, the apron passes through screw and shell fixed connection. The utility model discloses can let the driver drive when unmanned aerial vehicle descends at night safe accurate finding the descending position of settlement, avoid the driver because night light is not enough and the vision is poor and lead to the descending position fuzzy inaccurate, avoided falling the machine, exploding the quick-witted accident because of the aircraft descends and causes inaccurately.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to supplementary descending lighting fixture for unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Most self of current unmanned aerial vehicle does not have supplementary landing light, when the flight was descended at night, because of the weak and driver's of ambient light vision difference, the accurate position of very difficult definite landing to lead to the inaccurate accident that causes the break of aircraft descending.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is with supplementary descending lighting fixture can let the driver drive the descending position of safe accurate finding settlement when unmanned aerial vehicle descends at night, has avoided the driver because night light is not enough and the vision is poor and lead to the descending position fuzzy inaccurate, has avoided falling the machine, the fried accident because of the aircraft descends inaccurate and causes to solve the problem of proposing among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
The utility model provides an unmanned aerial vehicle is with supplementary descending lighting fixture, includes shell, circuit board, profection lamp and apron, the profection lamp passes through screw fixed mounting in the bottom of shell, fixed mounting has switch on the shell, the circuit board passes through screw fixed mounting in the shell, the circuit board has distance sensor through electric wire electric connection, the circuit board has the lithium cell through electric wire electric connection, the lithium cell passes through electric wire and switch electric connection, distance sensor passes through electric wire and profection lamp electric connection, the apron passes through screw and shell fixed connection.
Preferably, the lateral part fixedly connected with damping axle sleeve of shell, the inside rotation of damping axle sleeve installs the damping pivot, the one end fixedly connected with protecting crust of damping pivot, switch is located the inside of protecting crust, the protecting crust sets up to the plastics protecting crust.
Preferably, the bottom of the outer shell is fixedly connected with a dust cover, the projection lamp is located inside the dust cover, and the projection lamp is an LED projection lamp.
Preferably, the lithium battery is configured as a rechargeable lithium battery.
Preferably, the sensing end of the distance sensor penetrates through the bottom of the shell and is perpendicular to the ground.
Preferably, the inside fixed mounting of shell has the battery mount pad, lithium cell fixed mounting has seted up the through-hole in the inside of battery mount pad on the shell, the through-hole is just to the electric mortiser that charges of lithium cell.
Compared with the prior art, the beneficial effects of the utility model are that:
1. through the use of distance sensor and profection lamp, can let the descending position of setting for of safe accurate finding of operating personnel when driving unmanned aerial vehicle to descend night, avoided the driver because night light is not enough and the vision is poor and lead to the descending position fuzzy inaccurate, avoided falling machine, the fried accident because of the aircraft descends inaccurate and causes.
2. Through switch and lithium cell series connection, can be when the daytime, through closing switch, make distance sensor stop work, can reduce the working strength of lithium cell, improve life.
Drawings
fig. 1 is an exploded view of the present invention;
FIG. 2 is a side view of the protective shell of the present invention;
Fig. 3 is a bottom view of the dust cover of the present invention;
Fig. 4 is a block diagram of the power switch of the present invention.
In the figure: 1. a housing; 2. a circuit board; 3. a projection lamp; 4. a cover plate; 5. a screw; 6. a power switch; 7. a distance sensor; 8. a lithium battery; 9. a dust cover; 10. a damping shaft sleeve; 11. a damping rotating shaft; 12. a protective shell; 13. a storage battery mounting seat; 14. and a through hole.
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 work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution:
the utility model provides an unmanned aerial vehicle is with supplementary descending lighting fixture, includes shell 1, circuit board 2, profection lamp 3 and apron 4, profection lamp 3 passes through 5 fixed mounting of screw in the bottom of shell 1, fixed mounting has switch 6 on the shell 1, circuit board 2 passes through 5 fixed mounting of screw in shell 1, circuit board 2 has distance sensor 7 through electric wire electric connection, distance sensor 7's the biggest inductive distance sets up to two meters, circuit board 2 has lithium cell 8 through electric wire electric connection, lithium cell 8 passes through electric wire and 6 electric connection of switch, distance sensor 7 passes through electric wire and 3 electric connection of profection lamp, apron 4 passes through screw 5 and 1 fixed connection of shell.
Further, lateral part fixedly connected with damping axle sleeve 10 of shell 1, damping pivot 11 is installed in the inside rotation of damping axle sleeve 10, the one end fixedly connected with protecting crust 12 of damping pivot 11, switch 6 is located the inside of protecting crust 12, protecting crust 12 sets up to the plastics protecting crust, through the setting of damping pivot 11 and damping axle sleeve 10, can make things convenient for opening and closing of protecting crust 12, can protect switch 6 to in driving, can prevent that protecting crust 12 from rocking.
Further, the bottom fixedly connected with dust cover 9 of shell 1, profection lamp 3 is located the inside of dust cover 9, and profection lamp 3 sets up to the LED profection lamp, through the use of dust cover 9, can carry out dustproof protection to profection lamp 3, can improve the life of profection lamp 3.
further, the lithium battery 8 is set as a rechargeable lithium battery, so that resource waste can be reduced, and environmental pollution is reduced.
Furthermore, the sensing end of the distance sensor 7 penetrates through the bottom of the shell 1 and is vertically arranged with the ground, so that the normal use of the distance sensor 7 can be ensured.
Further, the inside fixed mounting of shell 1 has battery mount pad 13, lithium cell 8 fixed mounting has seted up through-hole 14 in the inside of battery mount pad 13 on shell 1, through-hole 14 is just to lithium cell 8's charging socket, can make things convenient for lithium cell 8's installation fixed to can make things convenient for lithium cell 8 to charge.
The structure principle is as follows: before flying, checking the electric quantity of the lithium battery 8, installing the lithium battery 8 at the bottom of the airplane to be flown after the electric quantity is sufficient, starting the power switch 6, placing the airplane, lighting the projection lamp 3, and after the projection lamp leaves the ground for two meters after flying, sensing the height of the projection lamp 3 which is separated from the ground for two meters by the distance sensor 7 on the circuit board 2 to turn off the projection lamp; when the aircraft flies to land for two meters, the distance sensor 7 senses that the projection lamp 3 is automatically turned on when the aircraft flies to the ground for two meters, and irradiates the ground right below the aircraft, so that an operator can see the landing position condition clearly, can land safely or not, and the risk of collision and falling of the aircraft is avoided.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. the utility model provides an unmanned aerial vehicle is with supplementary descending lighting fixture, includes shell (1), circuit board (2), profection lamp (3) and apron (4), its characterized in that: profection lamp (3) are through screw (5) fixed mounting in the bottom of shell (1), fixed mounting has switch (6) on shell (1), circuit board (2) are through screw (5) fixed mounting in shell (1), circuit board (2) have distance sensor (7) through electric wire electric connection, circuit board (2) have lithium cell (8) through electric wire electric connection, lithium cell (8) are through electric wire and switch (6) electric connection, distance sensor (7) are through electric wire and profection lamp (3) electric connection, apron (4) are through screw (5) and shell (1) fixed connection.
2. An auxiliary landing light device for unmanned aerial vehicle according to claim 1, characterized in that: lateral part fixedly connected with damping axle sleeve (10) of shell (1), damping pivot (11) are installed in the inside rotation of damping axle sleeve (10), the one end fixedly connected with protecting crust (12) of damping pivot (11), switch (6) are located the inside of protecting crust (12), protecting crust (12) set up to the plastics protecting crust.
3. An auxiliary landing light device for unmanned aerial vehicle according to claim 1, characterized in that: the bottom fixedly connected with dust cover (9) of shell (1), profection lamp (3) are located the inside of dust cover (9), and profection lamp (3) set up to the LED profection lamp.
4. An auxiliary landing light device for unmanned aerial vehicle according to claim 1, characterized in that: the lithium battery (8) is configured as a rechargeable lithium battery.
5. An auxiliary landing light device for unmanned aerial vehicle according to claim 1, characterized in that: the induction end of the distance sensor (7) penetrates through the bottom of the shell (1) and is perpendicular to the ground.
6. An auxiliary landing light device for unmanned aerial vehicle according to claim 1, characterized in that: the inside fixed mounting of shell (1) has battery mount pad (13), lithium cell (8) fixed mounting has seted up through-hole (14) in the inside of battery mount pad (13) on shell (1), through-hole (14) are just to the charging socket of lithium cell (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920593036.3U CN209795851U (en) | 2019-04-28 | 2019-04-28 | Auxiliary landing lighting device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920593036.3U CN209795851U (en) | 2019-04-28 | 2019-04-28 | Auxiliary landing lighting device for unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN209795851U true CN209795851U (en) | 2019-12-17 |
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| CN201920593036.3U Active CN209795851U (en) | 2019-04-28 | 2019-04-28 | Auxiliary landing lighting device for unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591130A (en) * | 2020-12-07 | 2021-04-02 | 吉林化工学院 | Aircraft landing indicating device and using method thereof |
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2019
- 2019-04-28 CN CN201920593036.3U patent/CN209795851U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591130A (en) * | 2020-12-07 | 2021-04-02 | 吉林化工学院 | Aircraft landing indicating device and using method thereof |
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