CN212401589U - Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof - Google Patents
Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof Download PDFInfo
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- CN212401589U CN212401589U CN202020819282.9U CN202020819282U CN212401589U CN 212401589 U CN212401589 U CN 212401589U CN 202020819282 U CN202020819282 U CN 202020819282U CN 212401589 U CN212401589 U CN 212401589U
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Abstract
The utility model discloses an unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof. Relate to unmanned aerial vehicle take-off technical field. The problem that the requirement on an unmanned aerial vehicle launching site is high and the takeoff speed is slow can be solved. Unmanned aerial vehicle cluster transmitter includes unmanned aerial vehicle emitter, and unmanned aerial vehicle emitter cluster sets up on the launcher. Unmanned aerial vehicle emitter includes launching tube, boosting piston and power component. The boosting piston is arranged inside the launching tube in a sliding mode. The power assembly is arranged on one side of the launching tube and used for driving the boosting piston to slide. Unmanned aerial vehicle jets out along the launching tube under the promotion of boosting piston and accomplishes taking off, has solved unmanned aerial vehicle like this and has taken off and has required high to the place, the slow problem of take-off speed. Unmanned aerial vehicle cluster transmitter sets up the unmanned aerial vehicle emitter cluster on the launcher, arranges a plurality of unmanned aerial vehicle emitters together, can realize unmanned aerial vehicle cluster transmission, and emission efficiency is higher.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle take-off technical field, in particular to unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof.
Background
Along with scientific and technological development, unmanned aerial vehicle technique rapidly develops and popularizes, no matter military or civilian unmanned aerial vehicle all has very big progress, by the wide application in each trade, small-size unmanned aerial vehicle is by wide application in military investigation, aerial photography, remote control toy etc.. At present, however, the take-off modes of small and medium-sized unmanned aerial vehicles in the market mainly include ground running, hand throwing, vertical take-off and landing, rocket boosting and the like; these take-off modes require high, the take-off speed is slow to the place, inconvenient unmanned aerial vehicle transportation, complex operation, require high to the user, the accident appears easily.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve one of the technical problem that exists among the prior art at least, provide an unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof, can solve the problem that unmanned aerial vehicle transmission place requires higher and take-off speed is slower.
According to a first aspect of the present invention, there is provided an unmanned aerial vehicle launching device, comprising a launching tube; the boosting piston is arranged inside the launching barrel in a sliding mode; and the power assembly is arranged on one side of the launching tube and used for driving the boosting piston to slide.
The utility model discloses at least, include following beneficial effect: unmanned aerial vehicle emitter includes launching tube, boosting piston and power component. Pack into the launching tube with the boosting piston, put into unmanned aerial vehicle again, aerify to power component, when treating that the inside atmospheric pressure of boosting power component reaches the default, release the boosting piston, unmanned aerial vehicle jets out along the launching tube under the promotion of boosting piston and accomplishes taking off, has solved unmanned aerial vehicle like this and has taken off and has required height to the place, the slow problem of the speed of taking off.
According to the utility model discloses unmanned aerial vehicle emitter of first aspect, the boosting piston includes the piston body; and the push rod is arranged on the piston body and can be in contact with the unmanned aerial vehicle. The push rod can assist fixed unmanned aerial vehicle, makes unmanned aerial vehicle remain stable in the launching tube.
According to the utility model discloses first aspect unmanned aerial vehicle emitter, the push rod is a plurality of, and is a plurality of be provided with the holder between the push rod, be provided with first leading pulley on the holder, first leading pulley pastes on the wall in the launching tube. The retainer can keep the push rod stable, and the combination of the first guide pulley and the retainer can keep the boosting piston stable when moving in the launching tube.
According to the utility model discloses the first aspect unmanned aerial vehicle emitter, first guide way has been seted up on the piston body, the launching tube is inside be provided with can with first guide way complex guide rail, the guide rail is followed launching tube axial extension, the piston body can be followed the guide rail is in slide in the launching tube. The guide rail is matched with the first guide groove to ensure that the piston does not rotate when moving in the launching tube.
The unmanned aerial vehicle launcher according to the first aspect of the present invention further comprises a piston lock, wherein the piston lock comprises a locking shaft, and is fixed at the bottom of the boosting piston through a locking shaft seat; the lock seat is fixed at the bottom of the launching barrel; the unlocking steering engine is fixed on the lock seat; the first lock piece is arranged on the lock seat in a freely rotating mode, and a first unlocking strip and a first claw are arranged on the first lock piece; the second locking plate is arranged on the lock seat in a free rotating mode and provided with an arc groove and a second claw; the unlocking steering engine can stir the first unlocking bar to enable the first lock piece to rotate; the first claw can be hooked and locked with the second claw; the locking shaft can be accommodated in the arc groove.
According to the utility model discloses unmanned aerial vehicle emitter of first aspect, the power component includes the gas receiver; the charging connector is arranged at one end of the air storage cylinder; and the regulating valve is arranged at the bottom of the launching tube and communicated with the inflating nozzle through a connecting tube.
According to the utility model discloses first aspect unmanned aerial vehicle emitter, still include the lift piece, lift piece bottom is provided with the second leading pulley, lift piece lower part is provided with the second guide way, the second guide way cover is established on the guide rail, the lift piece can be followed the guide rail slides.
The unmanned aerial vehicle launcher according to the first aspect of the present invention further comprises a cushion damper, wherein the cushion damper comprises a cylinder; the telescopic rod is movably arranged in the cylinder barrel in a penetrating way; and the spring is arranged inside the cylinder barrel, one end of the spring is connected with the telescopic rod, and the other end of the spring is connected with the cylinder barrel.
According to the utility model discloses the second aspect provides an unmanned aerial vehicle cluster transmitter, include the utility model discloses the first aspect unmanned aerial vehicle emitter still include the launching cradle, it is a plurality of unmanned aerial vehicle emitter sets up on the launching cradle.
Has the advantages that: the utility model discloses arrange a plurality of above-mentioned unmanned aerial vehicle emitter together, can realize the transmission of unmanned aerial vehicle cluster, emission efficiency is higher, equally, and the place when having reduced unmanned aerial vehicle transmission requires, has promoted unmanned aerial vehicle's emission rate by a wide margin. Arrange a plurality of unmanned aerial vehicle emitter together, can realize unmanned aerial vehicle cluster transmission, the emission efficiency is higher.
Drawings
The present invention will be further described with reference to the accompanying drawings and examples;
fig. 1 is a schematic structural diagram of a cluster transmitter of an unmanned aerial vehicle according to a preferred embodiment of the present invention;
fig. 2 is a schematic structural diagram of the unmanned aerial vehicle cluster transmitter according to the preferred embodiment of the present invention;
fig. 3 is a schematic structural view of the launching device of the unmanned aerial vehicle according to the preferred embodiment of the present invention;
FIG. 4 is a view of FIG. 3 with the emission cartridge wall hidden;
FIG. 5 is an enlarged view of a portion A of FIG. 4;
FIG. 6 is a view of FIG. 5 with the booster piston hidden;
FIG. 7 is a schematic view of a piston lock according to a preferred embodiment of the present invention;
FIG. 8 is a view of FIG. 7 with the locking shaft and locking shaft seat hidden;
FIG. 9 is a schematic view of the locking shaft and the locking shaft seat according to the preferred embodiment of the present invention;
fig. 10 is a cross-sectional view of the launching device of the unmanned aerial vehicle according to the preferred embodiment of the present invention;
FIG. 11 is a schematic structural view of a lift block according to a preferred embodiment of the present invention;
fig. 12 is a schematic structural view of a cushion damper according to a preferred embodiment of the present invention.
Detailed Description
This section will describe in detail the embodiments of the present invention, preferred embodiments of the present invention are shown in the attached drawings, which are used to supplement the description of the text part of the specification with figures, so that one can intuitively and vividly understand each technical feature and the whole technical solution of the present invention, but they cannot be understood as the limitation of the protection scope of the present invention.
In the description of the present invention, it should be understood that the orientation or positional relationship indicated with respect to the orientation description, such as up, down, front, rear, left, right, etc., is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the description of the present invention, a plurality of means are one or more, a plurality of means are two or more, and the terms greater than, less than, exceeding, etc. are understood as not including the number, and the terms greater than, less than, within, etc. are understood as including the number. If the first and second are described for the purpose of distinguishing technical features, they are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.
In the description of the present invention, unless there is an explicit limitation, the words such as setting, installation, connection, etc. should be understood in a broad sense, and those skilled in the art can reasonably determine the specific meanings of the above words in combination with the specific contents of the technical solution.
Referring to fig. 1-2, unmanned aerial vehicle cluster transmitter includes unmanned aerial vehicle emitter, still includes launcher 70, and a plurality of unmanned aerial vehicle emitters set up on launcher 70.
Unmanned aerial vehicle cluster transmitter can realize many planes and launch simultaneously, improves transmission density. As shown in fig. 1-2, is a 24 drone cluster transmitter. Fig. 1 is a schematic diagram of a 24-joint drone cluster transmitter launching drone.
Referring to fig. 1 to 5, the drone launching device includes a launch canister 10, a boost piston 20, and a power assembly 30. The booster piston 20 is slidably disposed inside the launch barrel 10. The power assembly 30 is disposed at one side of the launch barrel 10 for driving the boosting piston 20 to slide.
The booster piston 20 includes a piston body 21 and a push rod 22. The push rod 22 is arranged on the piston body 21 and can be in contact with the drone. The push rods 22 are plural, and a retainer 24 is provided between the push rods 22. The holder 24 is provided with a first guide pulley 25. The first guide pulley 25 is attached to the inner wall of the launch barrel 10.
The piston body 21 is provided with a first guide groove 25, and the launching tube 10 is internally provided with a guide rail 13 which can be matched with the first guide groove 25. The guide rail 13 extends axially along the launch barrel 10 and the piston body 21 is slidable along the guide rail 13 within the launch barrel 10. The push rods 22 can assist in securing the drone. The holder 24 can support the push rod 22. The first guide pulley 23 stabilizes the booster piston 20 in its movement.
The power assembly 30 includes an air reservoir 31, an air charging nozzle 32, and a regulating valve 33. The charging connector 32 is provided at one end of the air cylinder 31. The regulating valve 33 is provided at the bottom of the launch barrel 10 and is communicated with the charging nozzle 32 through a connecting pipe 34.
Referring to fig. 6-9, the drone launching device further includes a piston lock 40. The piston lock 40 includes a locking shaft 41, a locking shaft seat 42, a locking seat 43, an unlocking steering gear 44, a first locking piece 45, and a second locking piece 46. The locking shaft 41 is fixed to the bottom of the booster piston 20 by a locking shaft seat 42. The lock holder 43 is fixed to the bottom of the launch barrel 10. The unlocking steering gear 44 is fixed on the lock seat 43. The first lock piece 45 is freely rotatably provided on the lock holder 43. The first locking piece 45 is provided with a first unlocking strip 451 and a first claw 452. The second locking piece 46 is freely rotatably provided on the lock case 43. The second locking piece 46 is provided with a second claw 461 and a circular arc groove 462. The unlocking steering engine 44 can toggle the first unlocking strip 451 to enable the first locking piece 45 to rotate; the first claw 452 can hook and lock with the second claw 461; the locking shaft 41 may be received in the arcuate slot 462.
When the piston lock 40 is locked, the locking shaft 41 fixed at the bottom of the boosting piston 20 is locked in the arc groove 462 of the second locking piece 46, and the second locking piece 46 is driven to rotate, so that the second claw 461 is hooked and locked with the first claw 452. When the piston lock 40 is unlocked, the unlocking steering engine 44 drives the first unlocking strip 451 to rotate the first locking plate 45, so that the first hook 452 and the second hook 461 are unhooked, then the second hook 46 is loosened, and the boosting piston 20 drives the locking shaft 41 to be separated from the piston lock 40 under the driving of air pressure.
Referring to fig. 10 to 11, the launching device of the unmanned aerial vehicle further includes a lifting block 50, and a second guide pulley 51 is disposed at the bottom of the lifting block 50. The lifting block 50 is provided with a second guide groove 52 at the lower part, and the second guide groove 52 is sleeved on the guide rail 13. The lift block 50 is slidable along the guide rail 13.
Referring to fig. 12, the cushion damper 60 includes a cylinder 61, an expansion link 62, and a spring 63. The telescopic rod 62 is movably arranged in the cylinder 61 in a penetrating way. The spring 63 is disposed inside the cylinder 61, and has one end connected to the telescopic rod 62 and the other end connected to the cylinder 61. It will be appreciated that the spring 62 is disposed inside the cylinder 61, and the connection between the spring 62 and the cylinder 61 is the inner bottom surface of the cylinder 61.
Before taking off and launching, the unmanned aerial vehicle is folded, and the unmanned aerial vehicle and the boosting piston 20 are put into the launching tube 10 together with the lifting block 50 along the guide rail 13 of the launching tube 10. The boosting piston 20 is provided with a push rod 22 for supporting the unmanned aerial vehicle. First guide pulley on boosting piston 20 and second guide pulley 51 on lifting block 50 make things convenient for unmanned aerial vehicle to slide along guide rail 13. Boosting piston 20 arrives launch barrel 10 bottom, and piston lock 40 locks piston body 21, and unmanned aerial vehicle accomplishes fixedly. The air cylinder 31 is inflated by the inflator 32 to a set pressure. And finishing the preparation work before the unmanned aerial vehicle is launched.
During takeoff and launching, the pressure applied to the piston is adjusted to reach a preset value by adjusting the adjusting valve 33 at the bottom of the launching tube 10. The unlocking steering engine 44 is started, the piston lock 40 is unlocked, and the piston body 21 pushes the unmanned aerial vehicle to fly out of the launching tube 10 under the action of air pressure. Be provided with guide rail 13 in the launching barrel 10, can prevent that unmanned aerial vehicle from rolling over at the launching process, make unmanned aerial vehicle along predetermineeing the steady departure of direction. And finishing the launching work.
The launching tube 10 is provided with a buffer damper 60 which can stop the piston body 21 from flying out of the tube, so that the next launching is facilitated. The unmanned aerial vehicle lifts block 50 outside along with unmanned aerial vehicle departure launching tube 10, relies on gravity and unmanned aerial vehicle separation outside launching tube 10, and the back is picked up for subsequent use to the transmission is accomplished.
The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art.
Claims (9)
1. Unmanned aerial vehicle emitter, its characterized in that includes:
a launch canister (10);
a boosting piston (20) slidably disposed inside the launch barrel (10); and
and the power assembly (30) is arranged on one side of the launching tube (10) and is used for driving the boosting piston (20) to slide.
2. The unmanned aerial vehicle transmitting device of claim 1, wherein: the boosting piston (20) comprises
A piston body (21); and
and the push rod (22) is arranged on the piston body (21) and can be in contact with the unmanned aerial vehicle.
3. Unmanned aerial vehicle emitter according to claim 2, characterized in that: the launching tube is characterized in that the number of the push rods (22) is multiple, a retainer (24) is arranged between the push rods (22), a first guide pulley (23) is arranged on the retainer (24), and the first guide pulley (23) is attached to the inner wall of the launching tube (10).
4. Unmanned aerial vehicle emitter according to claim 2, characterized in that: the launching device is characterized in that a first guide groove (25) is formed in the piston body (21), a guide rail (13) capable of being matched with the first guide groove (25) is arranged in the launching tube (10), the guide rail (13) extends along the axial direction of the launching tube (10), and the piston body (21) can slide in the launching tube (10) along the guide rail (13).
5. The unmanned aerial vehicle transmitting device of claim 1, wherein: further comprising a piston lock (40), the piston lock (40) comprising
The locking shaft (41) is fixed at the bottom of the boosting piston (20) through a locking shaft seat (42);
the lock seat (43) is fixed at the bottom of the launching barrel (10);
an unlocking steering engine (44) fixed on the lock seat (43);
the first locking piece (45) is freely and rotatably arranged on the lock seat (43), and a first unlocking strip (451) and a first claw (452) are arranged on the first locking piece (45); and
the second locking plate (46) is arranged on the lock seat (43) in a freely rotating way, and an arc groove (462) and a second claw (461) are arranged on the second locking plate (46);
the unlocking steering engine (44) can pull the first unlocking strip (451) to enable the first locking piece (45) to rotate; the first claw (452) can be hooked and locked with the second claw (461); the locking shaft (41) is receivable in the arcuate slot (462).
6. The unmanned aerial vehicle transmitting device of claim 1, wherein: the power assembly (30) comprises
An air cylinder (31);
the charging connector (32) is arranged at one end of the air storage cylinder (31); and
the adjusting valve (33) is arranged at the bottom of the launching tube (10) and is communicated with the inflating nozzle (32) through a connecting tube (34).
7. Unmanned aerial vehicle emitter unit of claim 4, characterized in that: still include lifting block (50), lifting block (50) bottom is provided with second leading pulley (51), lifting block (50) lower part is provided with second guide way (52), second guide way (52) cover is established on guide rail (13), lifting block (50) can be followed guide rail (13) slide.
8. The unmanned aerial vehicle transmitting device of claim 1, wherein: also comprises a buffer damper (60), wherein the buffer damper (60) comprises
A cylinder (61);
the telescopic rod (62) is movably arranged in the cylinder barrel (61) in a penetrating way; and
and the spring (63) is arranged inside the cylinder barrel (61), one end of the spring is connected with the telescopic rod (62), and the other end of the spring is connected with the cylinder barrel (61).
9. Drone cluster launcher, characterized in that it comprises a plurality of drone launchers according to any one of claims 1 to 8, and further comprises a launcher (70), on which a plurality of said drone launchers are arranged (70).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020819282.9U CN212401589U (en) | 2020-05-15 | 2020-05-15 | Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202020819282.9U CN212401589U (en) | 2020-05-15 | 2020-05-15 | Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof |
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| CN212401589U true CN212401589U (en) | 2021-01-26 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572798A (en) * | 2020-05-15 | 2020-08-25 | 珠海天晴航空航天科技有限公司 | Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof |
| CN113815887A (en) * | 2021-11-03 | 2021-12-21 | 沈阳天晴航空航天科技有限公司 | Quick aerial launching box device |
| CN115675905A (en) * | 2022-09-30 | 2023-02-03 | 中国船舶重工集团公司第七一三研究所 | Folding wing unmanned aerial vehicle cluster type launching and recycling system |
-
2020
- 2020-05-15 CN CN202020819282.9U patent/CN212401589U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572798A (en) * | 2020-05-15 | 2020-08-25 | 珠海天晴航空航天科技有限公司 | Unmanned aerial vehicle emitter and unmanned aerial vehicle cluster transmitter thereof |
| CN113815887A (en) * | 2021-11-03 | 2021-12-21 | 沈阳天晴航空航天科技有限公司 | Quick aerial launching box device |
| CN115675905A (en) * | 2022-09-30 | 2023-02-03 | 中国船舶重工集团公司第七一三研究所 | Folding wing unmanned aerial vehicle cluster type launching and recycling system |
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