CN210284654U - Unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and launches recovery car - Google Patents
Unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and launches recovery car Download PDFInfo
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- CN210284654U CN210284654U CN201920780447.3U CN201920780447U CN210284654U CN 210284654 U CN210284654 U CN 210284654U CN 201920780447 U CN201920780447 U CN 201920780447U CN 210284654 U CN210284654 U CN 210284654U
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Abstract
The utility model provides an unmanned aerial vehicle ejection system, an unmanned aerial vehicle ejection recovery system and an ejection recovery vehicle, which relate to the technical field of unmanned aerial vehicle lifting equipment, wherein the unmanned aerial vehicle ejection system comprises an installation part, a driving device and an ejection device; the ejection device is hinged with the mounting piece; the driving device is used for driving the ejection device to rotate around a hinge point between the ejection device and the mounting part, so that the mounting area of the ejection device can move upwards or downwards. When unmanned aerial vehicle is got in the dress, can utilize drive arrangement to drive ejection device's installation region up or remove down to adjust the distance between ejection device's the installation region and the ground, make the workman can get unmanned aerial vehicle in subaerial installation region dress to ejection device, need not to board on the installed part or use the loop wheel machine, easy and simple to handle, work efficiency is higher.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle rises and falls equipment technique and specifically relates to an unmanned aerial vehicle launches system, an unmanned aerial vehicle launches recovery system to and an unmanned aerial vehicle launches recovery car.
Background
The unmanned aerial vehicle needs the assistance of an ejection system and a recovery system in the ejection and recovery processes. At present, an ejection system and a recovery system are mostly respectively installed on different trailer chassis, and are inconvenient to transport and poor in maneuverability.
In order to solve the problems, some manufacturers integrate an ejection system and a recovery system on the same trailer chassis to form an unmanned aerial vehicle ejection recovery vehicle. The trailer chassis can transport the ejection system and the recovery system simultaneously, and the transportation is convenient and the mobility is high.
Because the ejection system is fixed on the platform on trailer chassis, when adorning unmanned aerial vehicle on the ejection system or taking off from the ejection system, need the manual work to climb on trailer chassis platform and adorn unmanned aerial vehicle or utilize small-size arm crane to assist to lift by crane unmanned aerial vehicle and adorn and get, the process of adorning and getting unmanned aerial vehicle is loaded down with trivial details, and the operation is inconvenient.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and unmanned aerial vehicle launches recovery car to the unmanned aerial vehicle who solves among the prior art launches recovery car dress and gets the inconvenient technical problem of unmanned aerial vehicle.
The utility model provides an unmanned aerial vehicle ejection system, which comprises an installation part, a driving device and an ejection device;
the ejection device is hinged with the mounting piece;
the driving device is used for driving the ejection device to rotate around a hinge point between the ejection device and the mounting part, so that the mounting area of the ejection device can move upwards or downwards.
Further, a first rotating mechanism is arranged on the mounting piece;
the first rotating mechanism can rotate around the rotating axis of the first rotating mechanism relative to the mounting piece, and the ejection device is hinged to the first rotating mechanism.
Further, the ejection device comprises an underframe, an ejection track and an ejection trolley;
the ejection pulley is arranged on the ejection track in a sliding mode, the ejection track is fixed on the underframe, and the underframe is hinged to the first rotating mechanism.
Further, the driving device is a telescopic driving device;
one end of the telescopic driving device is hinged with the ejection device, and the other end of the driving device is hinged with the first rotating mechanism.
The utility model aims at providing an unmanned aerial vehicle launches recovery system still, including the skyhook recovery system and the utility model provides an unmanned aerial vehicle launches the system, the setting of skyhook recovery system is in on the installed part.
Further, a second swing mechanism is arranged on the mounting part; the second slewing mechanism can rotate around the slewing axis of the second slewing mechanism relative to the mounting part, and the skyhook recovery system is arranged on the second slewing mechanism.
Further, the hook recovery system comprises a main arm frame, an upper cross rod assembly, a lower cross rod assembly and a recovery rope assembly;
one end of the main arm support is hinged with the second swing mechanism, and the other end of the main arm support is hinged with the upper cross rod assembly; the lower cross rod assembly is hinged to the second swing mechanism, and the recovery rope assembly is connected with the upper cross rod assembly and the lower cross rod assembly through pulleys respectively.
Further, the hook recovery system and the ejection device are arranged on the mounting piece diagonally.
The utility model also aims to provide an unmanned aerial vehicle ejection recovery vehicle, which comprises a chassis and the unmanned aerial vehicle ejection system or the unmanned aerial vehicle ejection recovery system provided by the utility model; the mounting piece is arranged on the chassis.
Further, the unmanned aerial vehicle ejection recovery vehicle also comprises a plurality of leveling support legs; the plurality of leveling legs are respectively arranged at the corners of the mounting piece.
The utility model provides an unmanned aerial vehicle ejection system, which comprises an installation part, a driving device and an ejection device; the ejection device is hinged with the mounting piece; the driving device is used for driving the ejection device to rotate around a hinge point between the ejection device and the mounting part, so that the mounting area of the ejection device can move upwards or downwards. When unmanned aerial vehicle is got in the dress, can utilize drive arrangement to drive ejection device's installation region up or remove down to adjust the distance between ejection device's the installation region and the ground, make the workman can get unmanned aerial vehicle in subaerial installation region dress to ejection device, need not to board on the installed part or use the loop wheel machine, easy and simple to handle, work efficiency is higher.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the technical solutions in the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a first schematic structural view (transportation state) of an unmanned aerial vehicle ejection recovery vehicle provided by an embodiment of the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle ejection recovery vehicle provided in an embodiment of the present invention, i.e., a second structural diagram (a state in which the hook recovery system is deployed and the ejection device is deployed);
fig. 3 is a schematic structural diagram three (the state of the inclination angle of the ejection device) of the unmanned aerial vehicle ejection recovery vehicle provided by the embodiment of the present invention;
fig. 4 is a schematic view of an included angle between an ejection guide rail and a horizontal plane and an installation height in the unmanned aerial vehicle ejection recovery vehicle provided by the embodiment of the invention;
fig. 5 is a schematic structural diagram of a hook recovery system in an unmanned aerial vehicle ejection recovery vehicle provided by an embodiment of the present invention;
fig. 6 is a schematic diagram of the unmanned aerial vehicle ejection and recovery range of the unmanned aerial vehicle ejection recovery vehicle provided by the embodiment of the present invention;
fig. 7 is a schematic structural diagram of a chassis in the unmanned aerial vehicle ejection recovery vehicle provided by the embodiment of the utility model.
Icon: 1-a chassis; 11-class II chassis; 12-a chassis platform; 13-leveling legs; 14-recovering the power system; 2-a hook recovery system; 21-main arm support; 22-an upper traverse bar assembly; 23-a lower cross bar assembly; 24-retrieving the rope assembly; 25-a rotating tower; 3-ejection means; 31-a rotating base; 32-a chassis; 33-an ejection track; 34-ejection trolley; 35-hydraulic cylinder.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. 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.
In the description of the present invention, it should be noted that, as the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. appear, the indicated orientation or positional relationship thereof is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, but does not indicate or imply that the indicated device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like, as may be used herein, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Wherein the terms "first position" and "second position" are two different positions.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The utility model provides an unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and unmanned aerial vehicle launches recovery car, and it is right to give a plurality of embodiments below the utility model provides an unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and unmanned aerial vehicle launches recovery car and carries out detailed description.
Example 1
The ejection system of the unmanned aerial vehicle provided by the embodiment, as shown in fig. 1 to 7, includes a mounting member, a driving device, and an ejection device 3; the ejection device 3 is hinged with the mounting piece; the driving device is used for driving the ejection device 3 to rotate around a hinge point between the ejection device and the mounting part, so that the mounting area of the ejection device 3 can move upwards or downwards.
When the driving device drives the ejection device 3 to rotate towards or away from the mounting part, the mounting area of the ejection device 3 can be driven to move towards or away from the ground, so that the distance between the mounting area of the ejection device 3 and the ground can be adjusted.
When the unmanned aerial vehicle needs to be installed, as shown in fig. 4, the driving device is utilized to drive the installation area of the ejection device 3 to move towards the ground, the minimum included angle between the installation area of the ejection device 3 and the horizontal plane is continuously increased until the minimum included angle reaches a, after the installation area of the ejection device 3 moves to a distance H from the ground, the height is convenient for a worker to install the unmanned aerial vehicle on the ground, the driving device stops working, the ejection device 3 is fixed at the position, and the worker can install the unmanned aerial vehicle on the installation area of the ejection device 3 on the ground; after the unmanned aerial vehicle installation finishes, utilize drive arrangement to drive the installation region of jettison device 3 and keep away from ground and remove, when the installation region of jettison device 3 removed and personally submits suitable angle with the level, satisfied unmanned aerial vehicle transmission angle this moment, drive arrangement stop work, jettison device 3 fixes in this position, and unmanned aerial vehicle can launch.
When unmanned aerial vehicle is taken off to needs, the installation region that utilizes drive arrangement to drive jettison device 3 moves towards ground, jettison device 3's installation region and the continuous increase of minimum contained angle of horizontal plane, reach A until minimum contained angle, jettison device 3's installation region remove to with ground apart from the H after, this highly be convenient for workman takes off unmanned aerial vehicle on ground, drive arrangement stop work, jettison device 3 fixes in this position, the workman can take off unmanned aerial vehicle on subaerial installation region from jettison device 3.
The unmanned aerial vehicle ejection system that this embodiment provided, when the unmanned aerial vehicle was got in the dress, can utilize drive arrangement to drive the installation region of jettison device 3 up or move down to adjust the distance between the installation region of jettison device 3 and the ground, make the workman can get unmanned aerial vehicle in the installation region dress of subaerial to jettison device 3, need not to board the installed part or use the loop wheel machine, easy and simple to handle, work efficiency is higher. In addition, drive arrangement can also help unmanned aerial vehicle to adjust transmission angle, increases the convenience.
Moreover, compared with the unmanned aerial vehicle ejection system provided with a crane for installing and taking the unmanned aerial vehicle in the prior art, the unmanned aerial vehicle ejection system provided by the embodiment is additionally provided with a driving device, the crane is not required to be arranged, the driving device is relative to the crane, the structure is simple, the cost is low, the occupied space is small, the complexity of the unmanned aerial vehicle ejection system can be simplified, the cost is reduced, and the available space is enlarged.
Wherein, the installed part can be the mounting platform, also can be arbitrary suitable form such as mounting bracket. The driving device may be a hydraulic cylinder 35 (driven by hydraulic oil), or may be any suitable form such as an electric motor (driven by a generator or mains electricity).
The mounting piece is arranged at a suitable position above the ground, the ejection device 3 is hinged with the mounting piece, and when the ejection device 3 rotates towards the mounting piece (towards the ground), in order to prevent the mounting piece from blocking the ejection device 3 and causing the mounting area on the ejection device 3 not to move towards the ground, the following embodiments can be adopted:
for example: the middle part of the ejection device 3 is hinged with the edge area of the mounting part, one end of the ejection device 3 extends out of the mounting part, the mounting area of the ejection device 3 is positioned at one end of the ejection device 3, which extends out of the mounting part, and the mounting area of the ejection device 3 can move towards or away from the ground without being blocked by the mounting part under the driving of the driving device;
or the middle part of the ejection device 3 is hinged with the middle part of the mounting part, the mounting area of the ejection device 3 is positioned at one end of the ejection device 3, the mounting part is provided with an opening, the opening is positioned in the area near the lower part of one end of the ejection device 3, and when the mounting area of the ejection device 3 moves towards or away from the ground, the mounting area of the ejection device 3 can pass through the opening, so that the mounting part is prevented from blocking the ejection device 3.
Further, a first rotating mechanism is arranged on the mounting piece; the first swivel mechanism can rotate about its swivel axis relative to the mounting, and the ejector 3 is articulated with the first swivel mechanism.
Wherein, first slewing mechanism can include first rotating member and first gyration drive arrangement, and first rotating member can be for rotating base 31 or revolving rack etc. arbitrary suitable form, and first rotating member rotates with the installed part to be connected, and first rotating member can rotate for the installed part around the axis of first rotating member.
The first rotation driving device can be a rotation driving device such as an electric motor or a hydraulic motor, and an output shaft of the electric motor or the hydraulic motor is coaxially arranged with the first rotation member and fixedly connected with the first rotation member.
Through setting up first slewing mechanism, can drive jettison device 3 and rotate around the axis of first slewing mechanism to change the orientation of jettison device 3 in the horizontal plane, can carry out unmanned aerial vehicle in the wide range and launch, and when the wind direction changes, can quick adjustment launch the direction, reduce the removal of installed part.
In addition, through setting up first slewing mechanism, can be when the transportation, after jetter 3 contracts to non-operating condition, rotate jetter 3 to the primary importance, make jetter 3 all be located the region at installed part place, perhaps most be located the region at installed part place, reduce the volume that jetter 3 stretches out the installed part, can be convenient for transport. When the unmanned aerial vehicle needs to be ejected, the ejection device 3 is rotated to a proper ejection position by using the first rotating mechanism.
Specifically, the ejector 3 includes a chassis 32, an ejector rail 33, and an ejector trolley 34; the ejection trolley 34 is arranged on the ejection track 33 in a sliding mode, the ejection track 33 is fixed on the base frame 32, and the base frame 32 is hinged to the first rotating mechanism.
When the unmanned aerial vehicle is loaded or unloaded, the unmanned aerial vehicle needs to be installed on the ejection trolley 34 or taken down from the ejection trolley 34.
The procedure for mounting the drone to the launch trolley 34 is as follows:
as shown in fig. 1 to 2, in an initial state, the extending direction of the ejection device 3 is parallel to the length direction of the mounting member, the first rotation mechanism is used to drive the ejection device 3 to rotate until one end of the ejection device 3 extends out of the mounting member (at this time, the extending direction of the ejection device 3 is substantially parallel to the width direction of the mounting member), the ejection track 33 is unfolded, the ejection trolley 34 is pulled to one end of the ejection track 33, the driving device is used to drive the chassis to tilt, thereby driving the ejection track 33 to tilt, the minimum included angle between the ejection track 33 and the horizontal plane is increased, the ejection trolley 34 moves towards the ground continuously until the ejection trolley 34 on one end of the ejection track 33 moves to a position suitable for the ground, a worker installs the unmanned aerial vehicle on the ejection trolley 34 on the ground, after the installation, the driving device is used to drive the ejection trolley 34 on the ejection track, the minimum included angle between the ejection track 33 and the horizontal plane is reduced until the emission angle required by the unmanned aerial vehicle is reached, and then the unmanned aerial vehicle can be emitted.
Drive arrangement can be for rotary drive device such as motor or hydraulic motor, for example drive arrangement is the motor, and jettison device 3 is equipped with the mount pad including the installation axle on the installed part, and the installation axle is articulated with the mount pad, and the output shaft of motor and the coaxial setting and fixed connection of installation axle can drive jettison device 3 and rotate towards or keep away from the installed part.
Or the driving device is a telescopic driving device; one end of the telescopic driving device is hinged with the ejection device 3, and the other end of the driving device is hinged with the first rotating mechanism.
The driving device may be a hydraulic cylinder 35, or may be any suitable type such as an electric push rod or an air cylinder.
Specifically, the driving device is a hydraulic cylinder 35, one end of the hydraulic cylinder 35 is hinged to the underframe, and the other end of the hydraulic cylinder 35 is hinged to the rotating base 31.
The unmanned aerial vehicle that this embodiment provided launches recovery system, including the unmanned aerial vehicle that this embodiment provided launch system and sky hook recovery system 2, sky hook recovery system 2 sets up on the installed part.
It hook recovery system 2 can block, retrieve unmanned aerial vehicle, and it hook recovery system 2 can fixed connection on the installed part, also can rotate to connect on the installed part.
Preferably, a second swing mechanism is arranged on the mounting part; the second swing mechanism is rotatable about its swing axis relative to the mounting, and the skyhook recovery system 2 is disposed on the second swing mechanism.
The second rotating mechanism may include a second rotating member and a second rotating driving device, the second rotating member may be in any suitable form such as a rotating tower 25 or a rotating frame, the second rotating member is rotatably connected to the mounting member, and the second rotating member is capable of rotating around an axis of the second rotating member relative to the mounting member.
The second rotary driving device can be a rotary driving device such as an electric motor or a hydraulic motor, and an output shaft of the electric motor or the hydraulic motor is coaxially arranged with the second rotary member and fixedly connected with the second rotary member.
Through setting up second rotation mechanism, can drive skyhook recovery system 2 and rotate around second rotation mechanism's axis to change the orientation of skyhook recovery system 2 in the horizontal plane, can carry out unmanned aerial vehicle in the wide range and retrieve, and when the wind direction changes, can quick adjustment retrieve the direction, reduce the removal of installed part.
In addition, through setting up the second rotation mechanism, can be during the transportation, after the skyhook recovery system 2 contracts to non-operating condition, rotate skyhook recovery system 2 to the primary importance, make the whole region that is located the installed part of skyhook recovery system 2, perhaps most be located the region at installed part place, reduce the volume that the skyhook recovery system 2 stretches out the installed part, can be convenient for transport. When the unmanned aerial vehicle needs to be ejected, the second swing mechanism is used for rotating the hook recovery system 2 to a proper recovery position.
The hook recovery system 2 may be fixedly connected to the second swing mechanism, or may be hinged to the second swing mechanism.
Further, the hook recovery system 2 comprises a main arm frame 21, an upper cross rod assembly 22, a lower cross rod assembly 23 and a recovery rope assembly 24; one end of the main arm support 21 is hinged with the rotary tower 25, and the other end of the main arm support 21 is hinged with the upper cross rod assembly 22; the lower cross bar assembly 23 is hinged with a revolving tower 25, and the recovery rope assembly 24 is respectively connected with the upper cross bar assembly 22 and the lower cross bar assembly 23 through pulleys.
After the top hook recovery system 2 is unfolded, the main arm frame 21, the upper cross rod assembly 22, the lower cross rod assembly 23 and the recovery rope assembly 24 are locked at appropriate positions to form a bow-shaped structure for stopping and recovering the unmanned aerial vehicle, the main arm frame 21 rotates along with the rotating tower 25, and the upper cross rod assembly 22, the lower cross rod assembly 23 and the recovery rope assembly 24 can rotate along with the main arm frame 21.
Because jettison device 3 and skyhook recovery system 2 all can rotate alone, in order to avoid jettison device 3 and skyhook recovery system 2 to influence each other, when launching unmanned aerial vehicle, can utilize first slewing mechanism to rotate skyhook recovery system 2 to suitable position, reserve suitable space for launching unmanned aerial vehicle, when retrieving unmanned aerial vehicle, can utilize second slewing mechanism to rotate jettison device 3 to suitable position, reserve suitable space for retrieving unmanned aerial vehicle. As shown in fig. 6, the launch range C and the recovery range B of the drone can be determined according to the size of the drone.
Further, the skyhook recovery system 2 is located diagonally to the launch system on the mount.
The skyhook recovery system 2 and the launching system are arranged in a staggered mode, the range of ejection and recovery angles is enlarged, limited space can be utilized as far as possible, and the structure is simplified.
For example, when the hook recovery system 2 is applied to a vehicle, the mounting member is a chassis platform 12 on a class ii chassis 11, the hook recovery system 2 may be disposed on one side behind a cab (schematically illustrated as the left side in fig. 1 to 7), and the ejector 3 may be disposed on the other side of a vehicle tail (schematically illustrated as the right side in fig. 1 to 7).
The unmanned aerial vehicle ejection system that this embodiment provided, when the unmanned aerial vehicle was got in the dress, can utilize drive arrangement to drive the installation region of jettison device 3 up or move down to adjust the distance between the installation region of jettison device 3 and the ground, make the workman can get unmanned aerial vehicle in the installation region dress of subaerial to jettison device 3, need not to board the installed part or use the loop wheel machine, easy and simple to handle, work efficiency is higher. In addition, drive arrangement can also help unmanned aerial vehicle to adjust the transmission angle. Moreover, the unmanned aerial vehicle ejection system that this embodiment provided uses the loop wheel machine to load and get unmanned aerial vehicle's unmanned aerial vehicle ejection system among the prior art, simple structure and cost are lower to usable space is great.
Example 2
The unmanned aerial vehicle ejection recovery vehicle provided by the embodiment comprises a chassis 1 and the unmanned aerial vehicle ejection system or the unmanned aerial vehicle ejection recovery system provided by the embodiment 1; the mounting is provided on the chassis 1.
The chassis 1 may include a first type chassis, a second type chassis 11, and any other suitable form. The mounting member may be fixed to the chassis 1 by a fastener or may be welded to the chassis 1.
In this embodiment, the mounting member is a chassis platform 12, and the chassis platform 12 is connected to the girder of the second type chassis 11 by bolts.
When unmanned aerial vehicle is got in needs dress, can utilize drive arrangement to drive jettison device 3 and keep away from the installed part and rotate, make jettison device 3 for the installed part slope, when the mounting point of jettison device 3 removed to the distance that is fit for with ground distance, the workman can subaerial get unmanned aerial vehicle to the mounting point dress of jettison device 3. According to the unmanned aerial vehicle ejection recovery vehicle, a worker can mount and dismount the unmanned aerial vehicle when standing on the ground, mounting pieces do not need to be mounted or a crane does not need to be used, and the operation is simple and convenient; and moreover, a crane is not needed, the structure is simple, the cost is low, and the available space is larger.
Further, the unmanned aerial vehicle ejection recovery vehicle also comprises a plurality of leveling support legs 13; a plurality of leveling legs 13 are provided at the corners of the mounting member, respectively.
Specifically, four leveling legs 13 are respectively mounted at four corners of the chassis platform 12, and are used for leveling the chassis platform 12 and the entire vehicle.
In addition, the chassis 1 further comprises a recovery power system 14, the recovery power system 14 comprises a power take-off port mounted oil pump on a transmission of the second-type chassis 11, a hydraulic power source is provided for driving components such as a driving device and the hook recovery system 2 which need to be driven by hydraulic power, and a generator is mounted on the chassis 1 or the chassis platform 12, and power is provided for components such as the ejection device 3 which need to be driven by electric power.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle ejection system is characterized by comprising a mounting part, a driving device and an ejection device (3);
the ejection device (3) is hinged with the mounting piece;
the driving device is used for driving the ejection device (3) to rotate around a hinge point between the ejection device and the mounting piece, so that the mounting area of the ejection device (3) can move upwards or downwards.
2. The unmanned aerial vehicle ejection system of claim 1, wherein the mounting member has a first swivel mechanism disposed thereon;
the first rotating mechanism can rotate around the rotating axis of the first rotating mechanism relative to the mounting piece, and the ejection device (3) is hinged with the first rotating mechanism.
3. The unmanned aerial vehicle ejection system of claim 2, wherein the ejection device (3) comprises a chassis (32), an ejection track (33) and an ejection trolley (34);
the ejection trolley (34) is arranged on the ejection track (33) in a sliding mode, the ejection track (33) is fixed to the base frame (32), and the base frame (32) is hinged to the first rotating mechanism.
4. The unmanned aerial vehicle ejection system of claim 2, wherein the drive is a telescopic drive;
one end of the telescopic driving device is hinged with the ejection device (3), and the other end of the driving device is hinged with the first rotating mechanism.
5. An unmanned aerial vehicle ejection recovery system, comprising a hook recovery system (2) and the unmanned aerial vehicle ejection system of any one of claims 1-4, the hook recovery system (2) being disposed on the mount.
6. The unmanned aerial vehicle catapult recovery system of claim 5, wherein the mounting member is provided with a second swing mechanism; the second slewing mechanism can rotate around the slewing axis of the second slewing mechanism relative to the mounting part, and the skyhook recovery system (2) is arranged on the second slewing mechanism.
7. The unmanned aerial vehicle catapult recovery system of claim 6, wherein the hook recovery system (2) comprises a main boom (21), an upper crossbar assembly (22), a lower crossbar assembly (23), and a recovery rope assembly (24);
one end of the main arm support (21) is hinged with the second swing mechanism, and the other end of the main arm support (21) is hinged with the upper transverse rod assembly (22); the lower cross rod assembly (23) is hinged to the second swing mechanism, and the recovery rope assembly (24) is respectively connected with the upper cross rod assembly (22) and the lower cross rod assembly (23) through pulleys.
8. The unmanned aerial vehicle catapult recovery system of any one of claims 5 to 7, wherein the hook recovery system (2) is disposed on the mount diagonally to the catapult (3).
9. An unmanned aerial vehicle ejection recovery vehicle, characterized by comprising a chassis (1) and the unmanned aerial vehicle ejection system of any one of claims 1-4 or the unmanned aerial vehicle ejection recovery system of any one of claims 5-8; the mounting piece is arranged on the chassis (1).
10. The drone launch recovery vehicle of claim 9, further comprising a plurality of leveling legs (13); the leveling legs (13) are respectively arranged at the corners of the mounting piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920780447.3U CN210284654U (en) | 2019-05-27 | 2019-05-27 | Unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and launches recovery car |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920780447.3U CN210284654U (en) | 2019-05-27 | 2019-05-27 | Unmanned aerial vehicle launches system, unmanned aerial vehicle launches recovery system and launches recovery car |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111762332A (en) * | 2020-07-09 | 2020-10-13 | 四川航天烽火伺服控制技术有限公司 | Fixed wing unmanned aerial vehicle friction disc power consumption rope hook recovery unit |
| CN113280679A (en) * | 2021-06-30 | 2021-08-20 | 四川航天烽火伺服控制技术有限公司 | Ejection test system, method and capture device |
| CN114167882A (en) * | 2021-12-02 | 2022-03-11 | 海丰通航科技有限公司 | Unmanned aerial vehicle offshore recovery system and method |
-
2019
- 2019-05-27 CN CN201920780447.3U patent/CN210284654U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111762332A (en) * | 2020-07-09 | 2020-10-13 | 四川航天烽火伺服控制技术有限公司 | Fixed wing unmanned aerial vehicle friction disc power consumption rope hook recovery unit |
| CN113280679A (en) * | 2021-06-30 | 2021-08-20 | 四川航天烽火伺服控制技术有限公司 | Ejection test system, method and capture device |
| CN113280679B (en) * | 2021-06-30 | 2023-08-25 | 四川航天烽火伺服控制技术有限公司 | Ejection testing system and method |
| CN114167882A (en) * | 2021-12-02 | 2022-03-11 | 海丰通航科技有限公司 | Unmanned aerial vehicle offshore recovery system and method |
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221102 Address after: 413062 Floor 3, No. 1 Factory Building, Sany Zhongyang Industrial Park, East New District, Yuxiangshan Street, Yiyang City, Hunan Province (101, Shiba Village, Henglongqiao Town) Patentee after: Hunan Province Ground Unmanned Equipment Engineering Research Center Co.,Ltd. Address before: 410000 Sanyi Industrial City, Jingkai District, Changsha City, Hunan Province Patentee before: Sany Automobile Manufacturing Co.,Ltd. |