CN208665536U - A kind of UAV Landing protective device - Google Patents
A kind of UAV Landing protective device Download PDFInfo
- Publication number
- CN208665536U CN208665536U CN201820905206.2U CN201820905206U CN208665536U CN 208665536 U CN208665536 U CN 208665536U CN 201820905206 U CN201820905206 U CN 201820905206U CN 208665536 U CN208665536 U CN 208665536U
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- air bag
- motor
- lifter plate
- equipment compartment
- signal
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Abstract
The utility model provides a kind of UAV Landing protective device; including equipment compartment, signal receiver, motor and buffer unit; buffer unit is arranged in equipment compartment lower region; buffer unit includes lifter plate, air bag and spring; lifter plate is parallel to being horizontally installed in lower region of partition; lifter plate is arranged on the side that equipment compartment is open in air bag, and spring is arranged on the lower surface of air bag；Signal receiver and motor are mounted in the top area of equipment compartment, and signal receiver and remote control equipment are wirelessly connected and receive the signal of remote control equipment transmission, and signal is sent motor by signal wire；Motor drives lifter plate to extend downwardly outside lower region according to signal, or drives lifter plate that close to partition, buffer unit is withdrawn in lower region upwards.The utility model can be landed by the air bag and spring of buffer unit for unmanned plane provides cushion effect, carries out safeguard protection to unmanned plane, extends the service life of unmanned plane.
Description
Technical field
The utility model relates generally to unmanned plane equipment technical field, and in particular to a kind of UAV Landing protective device.
Background technique
UAV is referred to as " unmanned plane ", and english abbreviation is " UAV ", manipulates nobody using radio robot
Machine carries out high altitude operation, such as is taken photo by plane etc. using unmanned plane, brings great convenience, but in unmanned plane landing
In the process, due to operating personnel's misoperation, the case where be easy to causeing unmanned plane to fall to damage unmanned plane, and current nothing
It is man-machine to be not provided with protective device, shorten the service life of unmanned plane, need thus one kind peace of the dropping control device to unmanned plane
It is protected entirely.
Utility model content
Technical problem to be solved in the utility model is in view of the deficiencies of the prior art, to provide a kind of UAV Landing guarantor
Protection unit.
The technical solution that the utility model solves above-mentioned technical problem is as follows: a kind of UAV Landing protective device, including
Equipment compartment, signal receiver, motor and buffer unit, the equipment compartment is the quadrangle box structure that bottom is equipped with opening, described
Equipment compartment passes through hanging in uav bottom and is located at the lower section of uav bottom picture pick-up device, parallel in the equipment compartment
It is equipped with partition in the opening, the equipment compartment is divided into top area and lower region by the partition；
The buffer unit is arranged in the lower region, and the buffer unit includes lifter plate, air bag and spring, institute
It states lifter plate and is parallel to being horizontally installed in the lower region of the partition, the bottom of the lifter plate is arranged in the air bag
In portion, the spring is arranged on the lower surface of the air bag；
The signal receiver and motor are mounted in the top area, and the signal receiver and motor pass through signal
Line connection, the signal receiver and remote control equipment are wirelessly connected and receive the signal of remote control equipment transmission, and pass through the letter
The signal is sent the motor by number line, is connected with telescopic rod on the output end of the motor, the middle part of the partition is equipped with
Through-hole, the telescopic rod pass through the through-hole and extend downwardly and be connected on the lifter plate far from one end of motor；
The signal drives the telescopic rod to stretch up and down to the motor based on the received, and drives the lifter plate downward
Stretch out outside the lower region, or drive the lifter plate upwards close to the partition, by the buffer unit withdraw it is described under
In layer region.
The beneficial effects of the utility model are: being equipped with equipment compartment in uav bottom, it is equipped with buffer unit in equipment compartment, is delayed
The air bag and spring for rushing component can land for unmanned plane provides cushion effect, carries out safeguard protection to unmanned plane, extends unmanned plane
Service life；Buffer unit is arranged on lifter plate, and liftable plate is when unmanned plane lands by buffer unit extending equipment storehouse
Buffer unit is retracted in lower region after the completion of landing by lifter plate, thus to buffer part by external carry out buffer protection
Part is protected.
Based on the above technical solution, the utility model can also do following improvement.
Further, the air bag is equipped with for the inflating port for air bag inflation, and the inflating port is arranged described
The middle part of air bag bottom.
Beneficial effect using above-mentioned further scheme is: when not in use, can be put the gas in air bag by inflating port
Out, air bag is protected.
Further, the spring is equipped with multiple, and the air bag is cuboid-type, and the multiple spring is arranged at equal intervals
On the lower surface of the air bag.
Beneficial effect using above-mentioned further scheme is: spring stress can be made uniform, improve more gentle cushion effect.
Further, for the connecting rod at least provided with three, at least described three connecting rods are distributed in the outer edge of the equipment compartment
Place, and it is removably attachable to the uav bottom.
Beneficial effect using above-mentioned further scheme is: connecting equipment compartment by more connecting rods and is able to maintain equipment compartment
Stress balance when not in use can disassemble more connecting rods from unmanned plane, convenient for storage.
Further, rubber pad is equipped between the spring and the air bag.
Beneficial effect using above-mentioned further scheme is: preventing spring excessive to gasbag pressure and punctures the feelings of air bag
Condition.
Further, it is equipped at the top area of the equipment compartment and exposes the top area or closed door body.
Beneficial effect using above-mentioned further scheme is: the equipment in top area easy to repair.
It further, further include battery, the battery is arranged in the top area of the equipment compartment, and passes through power supply
Line is connect with the signal receiver and motor respectively, provides electric power for it.
Detailed description of the invention
Fig. 1 is the overall structure diagram of UAV Landing protective device provided by the embodiment of the utility model；
Fig. 2 is the structural schematic diagram of equipment compartment provided by the embodiment of the utility model.
In attached drawing, the names of the parts represented by the respective symbols are as follows:
1, unmanned plane, 2, equipment compartment, 3, signal receiver, 4, motor, 5, partition, 6, lifter plate, 7, air bag, 8, spring,
9, telescopic rod, 10, battery, 201, connecting rod.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figs. 1-2, a kind of UAV Landing protective device, including equipment compartment 2, signal receiver 3, motor 4 are gentle
Component is rushed, the equipment compartment 2 is the quadrangle box structure equipped with opening, and the equipment compartment 2 is suspended on unmanned plane by connecting rod 201
1 bottom and the lower section for being located at 1 bottom picture pick-up device of unmanned plane, the opening is parallel in the equipment compartment 2 is equipped with partition 5,
The partition 5 divides the equipment compartment 2 for top area and lower region；
The buffer unit is arranged in the lower region, and the buffer unit includes lifter plate 6, air bag 7 and spring
8, the lifter plate 6 is parallel to being horizontally installed in the lower region of the partition 5, and the air bag 7 is arranged in the liter
On the bottom for dropping plate 6, the spring 8 is arranged on the lower surface of the air bag 7；
The signal receiver 3 and motor 4 are mounted in the top area, and the signal receiver 3 and motor 4 pass through
Signal wire connection, the signal receiver 3 is wirelessly connected with remote control equipment and receives the signal of remote control equipment transmission, and passes through institute
It states signal wire and the signal is sent into the motor 4, be connected with telescopic rod 9 on the output end of the motor 4, the partition 5
Middle part is equipped with through-hole, and the telescopic rod 9 passes through the through-hole and extend downwardly far from one end of motor 4 is connected to the lifter plate
On 6；
The signal drives about 9 telescopic rod to stretch to the motor 4 based on the received, and drives the lifter plate 6
It extends downwardly outside the lower region, or drives the lifter plate 6 upwards close to the partition 5, the buffer unit is withdrawn
In the lower region.
The motor 4 drives about 9 telescopic rod to stretch for the prior art, and one of driving method is telescopic rod 9
One end be connected on the output rod of motor 4, the motor 4 drives telescopic rod 9 to extend downwardly or be lifted up.
In above-described embodiment, it is equipped with equipment compartment in uav bottom, is equipped with buffer unit, the gas of buffer unit in equipment compartment
Capsule and spring can land for unmanned plane provides cushion effect, carries out safeguard protection to unmanned plane, extends the service life of unmanned plane；
Buffer unit is arranged on lifter plate, and liftable plate is buffered when unmanned plane lands by buffer unit extending equipment storehouse is external
Buffer unit is retracted in lower region after the completion of landing by lifter plate, to protect to buffer unit by protection.
When buffer unit is retracted in lower region, the edge of lower region be can be placed in plane.
Optionally, as an embodiment of the present invention, the air bag 7 is equipped with for filling for the air bag 7 inflation
The middle part of 7 bottom of air bag is arranged in port, the inflating port.
In above-described embodiment, when not in use, the gas in air bag can be released by inflating port, protect air bag, and be arranged
It is convenient for inflation at the middle part of air bag bottom.
Optionally, as an embodiment of the present invention, the spring 8 is equipped with multiple, and the air bag 7 is cuboid-type,
The multiple spring 8 is arranged on the lower surface of the air bag 7 at equal intervals.
In above-described embodiment, spring stress can be made uniform, improve more gentle cushion effect.
Preferably, there are four the spring 8 is set, four springs 8
Optionally, as an embodiment of the present invention, the connecting rod 201 is at least provided with three, at least described three companies
Bar 201 is distributed in the outer edge of the equipment compartment 2, and is removably attachable to 1 bottom of unmanned plane.
For example, the connecting rod 201 is equipped with four, four connecting rods 201 are located at the quadrangle of the equipment compartment 2, and
It is removably attachable to 1 bottom of unmanned plane；The quadrangle of the bottom of equipment compartment 2 is equipped with nut, four connecting rods 201 and institute
The nut for stating 1 bottom of unmanned plane corresponds, and is removably connect by screw thread with each nut.
For example, the connecting rod 201 is equipped with more, more connecting rods 201 are distributed as external comparatively dense, and middle part is diluter
It dredges；Such as, the connecting rod 201 is equipped with 9, wherein 6 outer edges that the equipment compartment 2 is arranged in round, 3 remaining
It is arranged at the close center of the equipment compartment 2.When unmanned plane, which tilts, to land, intensive connecting rod 201 can be reinforced to equipment
The protection in storehouse 2 reduces the impulse force to equipment compartment 2.
In above-described embodiment, the stress balance that equipment compartment is able to maintain equipment compartment is connected by four connecting rods, when not in use,
Four connecting rods can be disassembled from unmanned plane, convenient for storage.
Optionally, as an embodiment of the present invention, rubber pad is equipped between the spring 8 and the air bag 7.
In above-described embodiment, the case where preventing spring excessive to gasbag pressure and puncture air bag.
Optionally, as an embodiment of the present invention, it is equipped at the top area of the equipment compartment 2 by the top regions
Domain is exposed or closed door body.
Equipment in above-described embodiment, in top area easy to repair.
It optionally, as an embodiment of the present invention, further include battery 10, the setting of battery 10 is set described
It in the top area in standby storehouse 2, and is connect respectively with the signal receiver (3) and motor 4 by power supply line, provides electricity for it
Power.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (7)
1. a kind of UAV Landing protective device, which is characterized in that including equipment compartment (2), signal receiver (3), motor (4) and
Buffer unit, the equipment compartment (2) are the quadrangle box structure that bottom is equipped with opening, and the equipment compartment (2) passes through connecting rod (201)
It is suspended on unmanned plane (1) bottom and is located at the lower section of unmanned plane (1) bottom picture pick-up device, be parallel to institute in the equipment compartment (2)
That states opening is equipped with partition (5), and the equipment compartment (2) is divided into top area and lower region by the partition (5)；
The buffer unit is arranged in the lower region, and the buffer unit includes lifter plate (6), air bag (7) and spring
(8), the lifter plate (6) is parallel to being horizontally installed in the lower region of the partition (5), air bag (7) setting
On the bottom of the lifter plate (6), the spring (8) is arranged on the lower surface of the air bag (7)；
The signal receiver (3) and motor (4) are mounted in the top area, the signal receiver (3) and motor (4)
It being connected by signal wire, the signal receiver (3) and remote control equipment are wirelessly connected and receive the signal of remote control equipment transmission, and
The signal is sent into the motor (4) by the signal wire, is connected with telescopic rod (9) on the output end of the motor (4),
The middle part of the partition (5) is equipped with through-hole, and the telescopic rod (9) far from the one end of motor (4) passes through the through-hole and to downward
It stretches and is connected on the lifter plate (6)；
The signal drives the telescopic rod (9) to stretch up and down to the motor (4) based on the received, and drives the lifter plate
(6) it extends downwardly outside the lower region, or drives the lifter plate (6) upwards close to the partition (5), by the buffer part
Part is withdrawn in the lower region.
2. a kind of UAV Landing protective device according to claim 1, which is characterized in that the air bag (7) is equipped with
Inflating port for being inflated for the air bag (7), middle part of the inflating port setting in the air bag (7) bottom.
3. a kind of UAV Landing protective device according to claim 1, which is characterized in that the spring (8) is equipped with more
A, the air bag (7) is cuboid-type, and the multiple spring (8) is arranged on the lower surface of the air bag (7) at equal intervals.
4. a kind of UAV Landing protective device according to claim 1, which is characterized in that the connecting rod (201) is at least
Equipped with three, at least described three connecting rods (201) are distributed in the outer edge of the equipment compartment (2), and are removably attachable to
Unmanned plane (1) bottom.
5. a kind of UAV Landing protective device according to any one of claims 1 to 4, which is characterized in that the spring
(8) rubber pad is equipped between the air bag (7).
6. a kind of UAV Landing protective device according to any one of claims 1 to 4, which is characterized in that the equipment
It is equipped at the top area in storehouse (2) and exposes the top area or closed door body.
7. a kind of UAV Landing protective device according to any one of claims 1 to 4, which is characterized in that further include storing
Battery (10), the battery (10) are arranged in the top area of the equipment compartment (2), and by power supply line respectively with it is described
Signal receiver (3) and motor (4) connection, provide electric power for it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820905206.2U CN208665536U (en) | 2018-06-12 | 2018-06-12 | A kind of UAV Landing protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820905206.2U CN208665536U (en) | 2018-06-12 | 2018-06-12 | A kind of UAV Landing protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208665536U true CN208665536U (en) | 2019-03-29 |
Family
ID=65823833
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820905206.2U Active CN208665536U (en) | 2018-06-12 | 2018-06-12 | A kind of UAV Landing protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208665536U (en) |
-
2018
- 2018-06-12 CN CN201820905206.2U patent/CN208665536U/en active Active
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