CN211731849U - Unmanned aerial vehicle recovery unit - Google Patents
Unmanned aerial vehicle recovery unit Download PDFInfo
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- CN211731849U CN211731849U CN201922358639.8U CN201922358639U CN211731849U CN 211731849 U CN211731849 U CN 211731849U CN 201922358639 U CN201922358639 U CN 201922358639U CN 211731849 U CN211731849 U CN 211731849U
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Abstract
The utility model provides an unmanned aerial vehicle recovery unit, include: a support assembly; one end of the main arm is connected with the supporting component; the upper cross rod component is connected with the other end of the main arm; the lower cross bar assembly comprises a lower cross bar and a centering connecting piece connected with one end of the lower cross bar, and the centering connecting piece is connected with two opposite sides of the supporting assembly, so that the lower cross bar and the upper cross bar are always positioned on the same vertical plane; wherein, the sheer pole subassembly is located the below of entablature pole for cooperate in order to inject the recovery space that is used for retrieving unmanned aerial vehicle with last sheer pole. This unmanned aerial vehicle recovery unit sets up the centering connecting piece rather than linking to each other through the one end at the sheer pole, and the centering connecting piece links to each other with the relative both sides of supporting component, makes sheer pole and last horizontal pole be in on same perpendicular all the time, has reduced unmanned aerial vehicle recovery unit and has leaded to the risk of sheer pole or last horizontal pole damage because of receiving unmanned aerial vehicle's great impact force, has improved unmanned aerial vehicle recovery unit's stability, has improved unmanned aerial vehicle recovery unit's life.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle retrieves technical field, particularly, relates to an unmanned aerial vehicle recovery unit.
Background
The recovery unit is an important functional system of the unmanned aerial vehicle. Unmanned aerial vehicle's recovery mode includes that the undercarriage rollout lands and retrieves, parachutes and retrieves, skyhook retrieves, interception net retrieves etc. and wherein the skyhook is retrieved the mode and has efficient, work preparation time is short, retrieve the place and require lowly, no matter can both use on the platform of space tension such as land or naval vessel. Unmanned aerial vehicle recovery unit of skyhook recovery mode is an unmanned aerial vehicle recovery space that is provided jointly by last horizontal pole subassembly and sheer pole subassembly. Present sheer pole subassembly form has lug connection on whole car landing leg or install on the revolving stage, together rotatory with the revolving stage, but sheer pole subassembly and last horizontal pole subassembly are often can not be in the centering state all the time when retrieving unmanned aerial vehicle owing to receive the effect of transverse force, sheer pole subassembly and last horizontal pole subassembly can not be in same vertical face all the time promptly, the sheer pole and last horizontal pole atress unstable when unmanned aerial vehicle is retrieved to unmanned aerial vehicle recovery unit, this kind of condition easily leads to the damage of sheer pole subassembly and last horizontal pole subassembly, recovery unit's life has been shortened in the intangible.
SUMMERY OF THE UTILITY MODEL
In order to solve at least one of the above technical problem, the utility model aims to provide an unmanned aerial vehicle recovery unit.
In order to achieve the above object, the technical scheme of the utility model provides an unmanned aerial vehicle recovery unit, include: a support assembly; the main arm is connected with the supporting component at one end; the upper cross rod component is connected with the other end of the main arm; the lower cross bar assembly comprises a lower cross bar and a centering connecting piece connected with one end of the lower cross bar, and the centering connecting piece is connected with two opposite sides of the supporting assembly, so that the lower cross bar and the upper cross bar are always positioned on the same vertical surface; wherein, the sheer pole subassembly is located the below of entablature pole for cooperate with the entablature pole in order to inject the recovery space that is used for retrieving unmanned aerial vehicle.
The utility model provides an unmanned aerial vehicle recovery unit, set up the centering connecting piece rather than linking to each other through the one end at the sheer pole, the centering connecting piece links to each other with the relative both sides of supporting component, play to neutralization limiting displacement, thus, when utilizing sheer pole subassembly and last horizontal pole subassembly when retrieving unmanned aerial vehicle device, the sheer pole is in on same perpendicular with last horizontal pole all the time, the risk of unmanned aerial vehicle recovery unit because of receiving the damage of unmanned aerial vehicle's great impact force and leading to sheer pole or last horizontal pole has been reduced, the stability of unmanned aerial vehicle recovery unit when retrieving unmanned aerial vehicle has been improved, unmanned aerial vehicle recovery unit's life has been improved.
Particularly, the utility model provides an unmanned aerial vehicle recovery unit, including supporting component, main arm, upper horizontal pole subassembly and sheer pole subassembly, wherein, the one end of main arm links to each other with the supporting component, the one end of upper horizontal pole subassembly links to each other with the other end of main arm, the sheer pole subassembly includes sheer pole and the centering connecting piece that links to each other with the one end of sheer pole, the centering connecting piece is through linking to each other with the relative both sides of supporting component, thereby play the risk that the sheer pole takes place the skew relatively supporting component because of receiving the transverse force, and make sheer pole and upper horizontal pole subassembly can be in the same vertical plane all the time, sheer pole subassembly and upper horizontal pole subassembly keep good centering nature, the circumstances that lower horizontal pole subassembly and upper horizontal pole subassembly lead to the fact the damage because of receiving the impact force of unmanned aerial vehicle great when retrieving unmanned aerial vehicle has been reduced takes place, the stability of unmanned aerial vehicle recovery unit when retrieving unmanned aerial vehicle has been guaranteed.
Additionally, the utility model provides an unmanned aerial vehicle recovery unit among the above-mentioned technical scheme can also have following additional technical characteristics:
in the above technical solution, the centering connecting member includes a first connecting arm and a second connecting arm, one end of the first connecting arm and one end of the second connecting arm are both connected to the lower cross bar and are obliquely arranged relative to the length direction of the lower cross bar, and the other end of the first connecting arm and the other end of the second connecting arm are respectively hinged to two opposite sides of the supporting assembly, so that the other end of the lower cross bar can rotate up and down relative to the supporting assembly; and/or, the centering connecting piece include one end with the coaxial first linking arm and the one end that link to each other of one end of sheer pole with the other end of first linking arm links to each other and is relative second linking arm, the third linking arm that the length direction slope of first linking arm set up, the other end of second linking arm with the other end of third linking arm respectively with the relative both sides of supporting component are articulated mutually, so that the other end of sheer pole can be relative the supporting component rotates from top to bottom.
The centering connecting piece includes two linking arms, include first linking arm and second linking arm promptly, the one end of first linking arm and the one end of second linking arm all link to each other with the sheer pole and the length direction slope setting of relative sheer pole, the centering connecting piece wholly is the V type promptly, the other end through with first linking arm and second linking arm is articulated mutually with the relative both sides of supporting component respectively, thereby make the sheer pole can keep good centering nature with last sheer pole subassembly, make the other end of sheer pole can support component tilting relatively simultaneously, unmanned aerial vehicle's span space has been increased to pivoted sheer pole from top to bottom, help reducing the length of main arm, thereby be favorable to reducing unmanned aerial vehicle recovery unit's whole weight.
Centering connecting piece includes three linking arm, including first linking arm promptly, second linking arm and third linking arm, the one end and the sheer pole of first linking arm are coaxial continuous, the one end of second linking arm and third linking arm links to each other with the other end of first linking arm, and the length direction slope design of the relative first linking arm of second linking arm and third linking arm, centering connecting piece wholly is the Y type promptly, it is articulated mutually with the relative both sides of supporting component through the other end with second linking arm and third linking arm, thereby make the sheer pole can keep good centering nature with last horizontal pole component, make the other end of sheer pole can support component tilting relatively simultaneously, but the sheer pole of tilting has increased unmanned aerial vehicle's span space, help reducing the length of main arm, thereby be favorable to reducing unmanned aerial vehicle recovery unit's whole weight.
It is worth mentioning that the centering connecting piece can be integrally formed with the bottom rail, and can also be fixedly connected with the bottom rail through the connecting piece.
In any of the above technical solutions, the support assembly includes a first connecting support and a second connecting support disposed at opposite sides thereof, and the centering connection member is hinged to the first connecting support and the second connecting support, respectively.
The supporting component comprises two connecting supports, namely a first connecting support and a second connecting support which are arranged on two opposite sides of the supporting component, the centering connecting piece is hinged to the first connecting support and the second connecting support respectively, so that the connection between the centering connecting piece and the supporting component is facilitated, the stability of the connection between the centering connecting piece and the supporting component is improved, and the use stability of a product is improved.
In the above technical solution, the positions where the centering connecting piece is hinged to the first connecting support and the second connecting support are provided with first connecting holes, the first connecting support and the second connecting support are both provided with second connecting holes, and a pin is inserted into the first connecting holes and the second connecting holes, so that the centering connecting piece is hinged to the first connecting support and the second connecting support respectively.
The first connecting hole is formed in the position, hinged to the first connecting support and the second connecting support, of the centering connecting piece, the second connecting hole is formed in the first connecting support and the second connecting support, and when the centering connecting piece is assembled with the first connecting support and the second connecting support, the pin shaft only needs to penetrate through the first connecting hole and the second connecting hole.
In the above technical solution, unmanned aerial vehicle recovery unit still includes: the two pin shaft baffles are respectively connected with the first connecting support and the second connecting support through bolts and are used for fixing the pin shafts; the hinge pin comprises a first connecting support and a second connecting support, wherein one end of the hinge pin is provided with a groove, and a hinge pin baffle is embedded in the groove to limit the hinge pin to rotate relative to the first connecting support or the second connecting support.
Unmanned aerial vehicle recovery unit still includes two round pin axle baffles, two round pin axle baffles respectively with first connection support and second connection support bolted connection, it is comparatively reliable to connect, through the recess that sets up at the one end of round pin axle and round pin axle baffle looks adaptation, and inlay the round pin axle baffle and establish in the recess, thereby can prevent effectively that the relative first connection support of round pin axle or second from connecting the support and taking place to rotate, guaranteed that centering connecting piece is connected reliability and stability that the support is connected with first connection support and second.
In any of the above solutions, the bottom rail assembly further comprises: the roller assembly comprises a roller arranged at one end of the lower cross rod far away from the supporting assembly and a roller bracket used for fixing the roller, and the roller is used for supporting the upper cross rod in the process that the main arm rotates to ascend or descend relative to the supporting assembly so as to assist the upper cross rod to unfold or retract.
Unmanned aerial vehicle recovery unit is still including setting up the gyro wheel of the one end of keeping away from supporting component at the sheer pole, and the gyro wheel can rotate the in-process that rises or descend and hold up last horizontal pole subassembly at the relative supporting component of main arm, plays the supporting role, and when going up horizontal pole subassembly and gyro wheel sliding connection, helps reducing the frictional force when the relative sheer pole of entablature moves, is convenient for realize going up the expansion and the recovery of horizontal pole subassembly.
In the above technical solution, the support assembly includes: the centering connecting piece and the main arm are hinged with the rotary table welding body, and the rotary table welding body horizontally rotates relative to the rotary support so as to drive the lower cross rod and the main arm to rotate relative to the rotary support.
Supporting component supports and rotates the revolving stage welding body of being connected including the gyration, and centering connecting piece and main arm all are articulated mutually with the revolving stage welding body, and the revolving stage welding body supports the level through relative gyration and rotates to can drive sheer pole and main arm, drive the entablature through the main arm and rotate simultaneously, the unmanned aerial vehicle recovery unit of being convenient for can rotate according to the wind direction and retrieve unmanned aerial vehicle with quick.
In any one of the above technical solutions, the unmanned aerial vehicle recovery device further includes: the first driving mechanism comprises an oil cylinder base and a first pitching oil cylinder, wherein the oil cylinder base is connected with the bottom of the supporting component, one end of the first pitching oil cylinder is connected with the oil cylinder base, the other end of the first pitching oil cylinder is connected with the lower side of the lower cross rod, and the lower cross rod is driven to rotate up and down relative to the supporting component.
Unmanned aerial vehicle recovery unit is still including being used for driving the first actuating mechanism of sheer pole subassembly tilting, and first actuating mechanism includes that hydro-cylinder base and one end that link to each other with the bottom of supporting component link to each other with hydro-cylinder base, and the other end links to each other with the downside of sheer pole first every single move hydro-cylinder, and first every single move hydro-cylinder is through the relative supporting component tilting of drive sheer pole to can rationally adjust the size of the recovery area between sheer pole and the last horizontal pole, with convenient recovery to unmanned aerial vehicle.
In any one of the above technical solutions, the unmanned aerial vehicle recovery device further includes: and the second driving mechanism comprises a second pitching oil cylinder of which one end is connected with the oil cylinder base, and the other end of the second pitching oil cylinder is connected with the lower side of the main arm so as to drive the main arm to rotate up and down relative to the supporting component.
Unmanned aerial vehicle recovery unit is still including being used for driving main arm tilting's second actuating mechanism, and second actuating mechanism includes that one end links to each other with the hydro-cylinder base, and the second every single move hydro-cylinder that the other end links to each other with the downside of main arm, and second every single move hydro-cylinder is through the relative supporting component tilting of drive main arm to in the expansion or the recovery of last horizontal pole subassembly, improved the efficiency that last horizontal pole subassembly expanded or retrieved.
In any of the above solutions, the main arm is a foldable member or a telescopic member; and/or the upper cross bar is a foldable piece or a telescopic piece; and/or the lower cross bar is a foldable piece or a telescopic piece.
The main arm is collapsible piece or extensible member, therefore its length is adjusted to the folding or flexible mode of accessible to distance between regulation entablature pole subassembly and the sheer pole subassembly, thereby rationally adjust unmanned aerial vehicle and retrieve regional size and ensure to retrieve unmanned aerial vehicle.
Go up the horizontal pole subassembly and be foldable piece or extensible member, consequently go up the horizontal pole subassembly and can adjust its length that expandes through folding or flexible mode to satisfy the requirement to unmanned aerial vehicle recovery area size.
The sheer pole subassembly is collapsible or scalable piece, therefore the sheer pole subassembly can adjust its length of expanding through folding or flexible mode to satisfy the requirement to unmanned aerial vehicle recovery area size.
Additional aspects and advantages of the invention will be set forth in part in the description which follows, or may be learned by practice of the invention.
Drawings
The above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a schematic perspective view of a recovery device of an unmanned aerial vehicle according to some embodiments of the present invention;
fig. 2 is a schematic view of a partial structure of a recovery device of an unmanned aerial vehicle according to some embodiments of the present invention;
fig. 3 is a schematic perspective view of a bottom rail assembly according to some embodiments of the present invention.
Wherein, the correspondence between the reference numbers and the component names in fig. 1 to 3 is:
1 unmanned aerial vehicle recovery unit, 101 revolving stage welded body, 102 slewing support, 103 first connecting support, 20 main arms, 30 entablature pole components, 40 bottom rail components, 401 bottom rail, 402 centering connecting piece, 403 roller components, 4031 roller, 4032 roller support, 50 first actuating mechanism, 501 cylinder base, 502 first pitch cylinder, 60 second pitch cylinder, 70 round pin axles, 80 round pin axle baffles.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention more clearly understood, the present invention will be described in further detail with reference to the accompanying drawings and detailed description. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the scope of the present invention is not limited by the specific embodiments disclosed below.
An unmanned aerial vehicle recovery device according to some embodiments of the present invention is described below with reference to fig. 1 to 3.
As shown in fig. 1 and fig. 2, the embodiment of the utility model provides an unmanned aerial vehicle recovery unit 1, include: a support assembly, a main arm 20, an upper crossbar assembly 30, and a lower crossbar 40; one end of the main arm 20 is connected to the support member; the upper cross bar assembly 30 is connected to the other end of the main arm 20; the lower cross bar 40 comprises a lower cross bar 401 and a centering connecting piece 402 connected with one end of the lower cross bar 401, the centering connecting piece 402 is connected with two opposite sides of the support assembly, so that the lower cross bar 401 and the upper cross bar are always positioned on the same vertical plane; wherein, sheer pole 40 is located the below of entablature for cooperate with the entablature in order to inject the recovery space that is used for retrieving unmanned aerial vehicle.
The utility model provides an unmanned aerial vehicle recovery unit 1, through the one end setting at sheer pole 401 rather than the centering connecting piece 402 that links to each other, centering connecting piece 402 links to each other with supporting component's relative both sides, play centering and limiting displacement, thus, when utilizing sheer pole 40 and last horizontal pole subassembly 30 when retrieving unmanned aerial vehicle device, sheer pole 401 and last horizontal pole are in on same perpendicular all the time, the risk of unmanned aerial vehicle recovery unit 1 because of receiving the damage of unmanned aerial vehicle's great impact force and leading to sheer pole 401 or last horizontal pole has been reduced, the stability of unmanned aerial vehicle recovery unit 1 when retrieving unmanned aerial vehicle has been improved, the life of unmanned aerial vehicle recovery unit 1 has been improved.
Specifically, the utility model provides an unmanned aerial vehicle recovery unit 1, including supporting component, main arm 20, upper horizontal pole assembly 30 and sheer pole 40, wherein, the one end of main arm 20 links to each other with the supporting component, the one end of upper horizontal pole assembly 30 links to each other with the other end of main arm 20, sheer pole 40 includes sheer pole 401 and centering connecting piece 402 that links to each other with the one end of sheer pole 401, centering connecting piece 402 is through linking to each other with the relative both sides of supporting component, thereby play the risk that relative supporting component of limiting sheer pole 401 because of receiving the transverse force takes place to squint, and make sheer pole 401 and upper horizontal pole assembly 30 can be in the same vertical plane all the time, sheer pole 40 and upper horizontal pole assembly 30 keep good centering, the circumstances that sheer pole 40 and upper horizontal pole assembly 30 lead to the fact the damage because of receiving the impact force of unmanned aerial vehicle great when retrieving unmanned aerial vehicle has been reduced and has occurred, thereby, the stability of unmanned aerial vehicle recovery unit 1 when retrieving unmanned aerial vehicle has been guaranteed.
The specific structure of the recovery device 1 for unmanned aerial vehicle provided by the present application is described in detail below with reference to some embodiments.
Example one
Centering connecting piece 402 includes first linking arm and second linking arm, and the one end of first linking arm and the one end of second linking arm all link to each other with sheer pole 401 and relative sheer pole 401's length direction slope sets up, and the other end of first linking arm and the other end of second linking arm are articulated mutually with the relative both sides of supporting component respectively to make sheer pole 401's the other end support component tilting relatively.
Centering connecting piece 402 includes two linking arms, including first linking arm and second linking arm promptly, the one end of first linking arm and the one end of second linking arm all link to each other with sheer pole 401 and relative sheer pole 401's length direction slope sets up, centering connecting piece 402 is whole to be the V type promptly, the other end through with first linking arm and second linking arm is articulated mutually with the relative both sides of supporting component respectively, thereby make sheer pole 401 can keep good centering nature with last horizontal pole subassembly 30, make sheer pole 401's the other end can support component tilting relatively simultaneously, but tilting's sheer pole 401 has increased unmanned aerial vehicle's span space, help reducing the length of main arm 20, thereby be favorable to reducing unmanned aerial vehicle recovery unit 1's whole weight.
Example two
The difference from the first embodiment is that: the centering connecting piece 402 includes a first connecting arm having one end coaxially connected to one end of the bottom rail 401, and a second connecting arm and a third connecting arm having one end connected to the other end of the first connecting arm and inclined with respect to the length direction of the first connecting arm, and the other end of the second connecting arm and the other end of the third connecting arm are respectively hinged to opposite sides of the supporting assembly, so that the other end of the bottom rail 401 can rotate up and down with respect to the supporting assembly, as shown in fig. 1 and 2.
The centering connecting piece 402 comprises three connecting arms, namely a first connecting arm, a second connecting arm and a third connecting arm, wherein one end of the first connecting arm is coaxially connected with the lower cross bar 401, one ends of the second connecting arm and the third connecting arm are connected with the other end of the first connecting arm, the second connecting arm and the third connecting arm are obliquely designed relative to the length direction of the first connecting arm, i.e., the centering linkage 402 is generally Y-shaped, by hinging the other ends of the second and third link arms to opposite sides of the support assembly, so that the lower cross bar 401 can maintain good alignment with the upper cross bar assembly 30, while the other end of the lower cross bar 401 can be rotated up and down with respect to the support assembly, the sheer pole 401 that can rotate from top to bottom has increased unmanned aerial vehicle's span space, helps reducing the length of main arm 20 to be favorable to reducing unmanned aerial vehicle recovery unit 1's whole weight.
It should be noted that the centering connection member 402 may be integrally formed with the bottom rail 401, or may be fixedly connected to the bottom rail 401 through a connection member.
Specifically, the support assembly comprises a first connection seat 103 and a second connection seat arranged on opposite sides thereof, and the centering connection piece 402 is hinged to the first connection seat 103 and the second connection seat, respectively, as shown in fig. 1 and 2.
The supporting component comprises two connecting supports, namely a first connecting support 103 and a second connecting support which are arranged on two opposite sides of the supporting component, the centering connecting piece 402 is hinged to the first connecting support 103 and the second connecting support respectively, so that the connection between the centering connecting piece 402 and the supporting component is facilitated, the stability of the connection between the centering connecting piece 402 and the supporting component is improved, and the use stability of a product is improved.
Further, the parts of the centering connection member 402 hinged to the first connection support 103 and the second connection support are provided with first connection holes, the first connection support 103 and the second connection support are provided with second connection holes, and the pin 70 is inserted into the first connection hole and the second connection hole, so that the centering connection member 402 is hinged to the first connection support 103 and the second connection support respectively.
The first connecting hole is formed in the position, hinged to the first connecting support 103 and the second connecting support, of the centering connecting piece 402, the second connecting hole is formed in the first connecting support 103 and the second connecting support, when the centering connecting piece 402 is assembled with the first connecting support 103 and the second connecting support, the pin shaft 70 only needs to penetrate through the first connecting hole and the second connecting hole, the connecting mode is convenient, the assembling difficulty is reduced, and the assembling efficiency of the centering connecting piece 402 and the first connecting support 103 and the second connecting support is improved.
EXAMPLE III
The difference from the first embodiment or the second embodiment is that: on the basis of embodiment one or embodiment two, further, unmanned aerial vehicle recovery unit 1 still includes: the two pin shaft baffles 80 are respectively connected with the first connecting support 103 and the second connecting support through bolts and used for fixing the pin shaft 70; wherein, one end of the pin 70 is provided with a groove, and the pin baffle 80 is embedded in the groove to limit the pin 70 to rotate relative to the first connecting support 103 or the second connecting support, as shown in fig. 1 and 2.
Unmanned aerial vehicle recovery unit 1 still includes two round pin axle baffles 80, two round pin axle baffles 80 are connected support bolted connection with first connection support 103 and second respectively, it is comparatively reliable to connect, through the recess that sets up and round pin axle baffle 80 looks adaptation in the one end of round pin axle 70, and inlay round pin axle baffle 80 and establish in the recess, thereby can prevent effectively that round pin axle 70 from taking place to rotate for first connection support 103 or second connection support relatively, the reliability and the stability that centering connecting piece 402 is connected with first connection support 103 and second connection support have been guaranteed.
Example four
The difference from the third embodiment is that: on the basis of the third embodiment, further, the lower cross bar 40 further includes: the roller assembly 403 includes a roller 4031 disposed at an end of the lower cross bar 401 away from the support assembly and a roller support 4032 for fixing the roller 4031, wherein the roller 4031 is used for supporting the upper cross bar during the rotation of the main arm 20 to raise or lower relative to the support assembly to assist the upper cross bar to be unfolded or retracted, as shown in fig. 1 and 3.
Unmanned aerial vehicle recovery unit 1 is still including setting up the gyro wheel 4031 of keeping away from the one end of supporting component at bottom end rail 401, and gyro wheel 4031 can rotate the in-process that rises or descend at main arm 20 relative supporting component and hold up last horizontal pole subassembly 30, plays the supporting role, and when going up horizontal pole subassembly 30 and gyro wheel 4031 sliding connection, helps reducing the relative bottom end rail 401 friction when moving of top end rail, is convenient for realize going up the expansion and the recovery of horizontal pole subassembly 30.
Specifically, the support assembly includes: the centering connector 402 and the main arm 20 are hinged to the rotating table welded body 101, and the rotating table welded body 101 horizontally rotates relative to the rotating support 102 to drive the lower cross bar 401 and the main arm 20 to rotate relative to the rotating support, as shown in fig. 1 and 2.
Supporting component includes that the gyration is supported 102 and is rotated the revolving stage welded body 101 of being connected with gyration support 102, and centering connecting piece 402 and main arm 20 all are articulated mutually with revolving stage welded body 101, and revolving stage welded body 101 supports 102 level through relative gyration and rotates to can drive sheer pole 401 and main arm 20, drive the sheer pole through main arm 20 and rotate simultaneously, be convenient for unmanned aerial vehicle recovery unit 1 can rotate according to the wind direction with quick recovery unmanned aerial vehicle.
EXAMPLE five
The difference from the fourth embodiment is that: on the basis of the fourth embodiment, further, unmanned aerial vehicle recovery unit 1 still includes: the first driving mechanism 50 includes a cylinder base 501 connected to the bottom of the support assembly and a first pitch cylinder 502 having one end connected to the cylinder base 501, and the other end of the first pitch cylinder 502 is connected to the lower side of the bottom rail 401 to drive the bottom rail 401 to rotate up and down relative to the support assembly, as shown in fig. 1 and 2.
Unmanned aerial vehicle recovery unit 1 is still including being used for driving first actuating mechanism 50 of sheer pole 40 upper and lower pivoted, first actuating mechanism 50 includes that cylinder base 501 and one end that link to each other with supporting component's bottom link to each other with cylinder base 501, the other end links to each other with sheer pole 401's downside first every single move hydro-cylinder 502, first every single move hydro-cylinder 502 rotates from top to bottom through the relative supporting component of drive sheer pole 401, thereby can rationally adjust the size of the recovery region between sheer pole 401 and the last horizontal pole, in order to make things convenient for the recovery to unmanned aerial vehicle.
EXAMPLE six
The difference from the fifth embodiment is that: on the basis of the fifth embodiment, further, unmanned aerial vehicle recovery unit 1 still includes: and a second driving mechanism including a second pitch cylinder 60 having one end connected to the cylinder base 501, and the other end of the second pitch cylinder 60 being connected to the lower side of the main arm 20 to drive the main arm 20 to rotate up and down with respect to the support assembly, as shown in fig. 1 and 2.
The unmanned aerial vehicle recovery device 1 further comprises a second driving mechanism used for driving the main arm 20 to rotate up and down, the second driving mechanism comprises a second pitching oil cylinder 60, one end of the second pitching oil cylinder is connected with the oil cylinder base 501, the other end of the second pitching oil cylinder is connected with the lower side of the main arm 20, the second pitching oil cylinder 60 rotates up and down relative to the supporting component through driving the main arm 20, so that the upper transverse rod component 30 can be unfolded or recovered conveniently, and the unfolding or recovery efficiency of the upper transverse rod component 30 is improved.
Further, the main arm 20 is a foldable member or a retractable member.
Further, the upper cross bar is a foldable piece or a telescopic piece.
Go up horizontal pole subassembly 30 and be collapsible piece or extensible member, consequently go up horizontal pole subassembly 30 and can adjust its length that expandes through folding or flexible mode to satisfy the requirement to unmanned aerial vehicle recovery area size.
Further, the bottom rail 401 is a foldable or retractable member.
The sheer pole 40 is collapsible or extensible, therefore the sheer pole 40 can adjust its length of expanding through folding or flexible mode to satisfy the requirement to unmanned aerial vehicle recovery area size.
The specific structure and the working principle of the recovery device for unmanned aerial vehicles provided by the present application are described in detail below with reference to a specific embodiment.
As shown in fig. 1 to 3, the utility model provides an unmanned aerial vehicle recovery unit fixes at the base or arranges on two types of chassis, and the concrete position of relative automobile body is unlimited. Unmanned aerial vehicle recovery unit mainly comprises revolving stage (being supporting component), main arm, entablature, sheer pole, centering connecting piece, first every single move hydro-cylinder, second every single move hydro-cylinder, auxiliary roller etc..
This unmanned aerial vehicle recovery unit 1's the state of withdrawing is when being in unoperated state promptly, and the entablature side is put in the side position of main arm, and the main arm is 0 degree contained angle with the horizontal plane, and entablature and sheer pole all are horizontal position with the main arm. The auxiliary roller is positioned at the tail end of the lower cross bar. The lower cross rod is hinged on the rotary table through a centering connecting piece, and the upper cross rod is hinged on the arm head of the main arm. The oil cylinder is a variable amplitude oil cylinder of the main arm, and two ends of the oil cylinder are connected with the main arm and the rotary table, so that variable-angle pitching motion of the main arm on a vertical plane can be realized. The oil cylinder is a pitching oil cylinder of the lower cross rod, and the variable-angle pitching motion of the lower cross rod on a vertical plane can be realized.
The lower cross rod is located below the main arm and fixed together with the rotary table, and the rotary table comprises a rotary table welding body, supports on the left side and the right side (namely a first connecting support and a second connecting support), a bottom pitching oil cylinder support (namely an oil cylinder base 501) and a rotary support. The lower cross rod assembly is connected with the left and right connecting supports of the rotating table welding body through a pin shaft and a pin shaft baffle, and the pitching oil cylinder, the oil cylinder pin shaft and the baffle are connected below the lower cross rod structure. The rollers and the roller supports are arranged at the ends of the lower cross rod, so that the upper cross rod can be assisted to be recovered. The main arm is connected the variable amplitude hydro-cylinder through round pin axle and baffle, thereby it changes unmanned aerial vehicle's direction is retrieved to reach whole car along with the wind direction change to go on the bus through slewing bearing degree gyration, need not to carry out the moving of whole car. The up-down amplitude of the angle of the bottom rail is achieved by the extension and contraction of the pitching cylinder (i.e. the first pitching cylinder 502).
Through the structure and the recovery method of the lower cross rod of the recovery device of the unmanned aerial vehicle, the rotary table can be structurally guaranteed to rotate by 360 degrees, the main arm can realize telescopic pitching, the lower cross rod 40 can keep good centering performance with the upper cross rod assembly, the lower cross rod can rotate together with the rotary table and expand the recovery space of the unmanned aerial vehicle, the upper cross rod can be recovered through the roller assemblies at the end parts of the lower cross rods, the upper cross rod assembly does not need to be additionally provided with a hydraulic oil cylinder, the upper cross rod assembly can be unfolded and folded through a hydraulic winch or an electric winch and the like, and the recovery device has good.
To sum up, the utility model provides an unmanned aerial vehicle recovery unit, through the one end setting at the sheer pole rather than the centering connecting piece that links to each other, the centering connecting piece links to each other with supporting component's relative both sides, play centering and limiting displacement, thus, when utilizing sheer pole and last horizontal pole subassembly when retrieving unmanned aerial vehicle device, the sheer pole is in same perpendicular with last horizontal pole all the time, the risk of unmanned aerial vehicle recovery unit because of receiving the damage of unmanned aerial vehicle's great impact force and leading to sheer pole or last horizontal pole has been reduced, the stability of unmanned aerial vehicle recovery unit when retrieving unmanned aerial vehicle has been improved, unmanned aerial vehicle recovery unit's life has been improved.
In the present application, the terms "first", "second", "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance; the term "plurality" means two or more unless expressly limited otherwise. The terms "mounted," "connected," "fixed," and the like are to be construed broadly, and for example, "connected" may be a fixed connection, a removable connection, or an integral connection; "coupled" may be direct or indirect through an intermediary. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the description of the present invention, it should be understood that the terms "upper", "lower", "left", "right", "front", "back", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or unit indicated must have a specific direction, be constructed and operated in a specific orientation, and therefore, should not be construed as limiting the present invention.
In the description of the present specification, the description of the terms "one embodiment," "some embodiments," "specific embodiments," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle recovery unit, its characterized in that includes:
a support assembly;
the main arm is connected with the supporting component at one end;
the upper cross rod component is connected with the other end of the main arm;
the lower cross bar assembly comprises a lower cross bar and a centering connecting piece connected with one end of the lower cross bar, and the centering connecting piece is connected with two opposite sides of the supporting assembly, so that the lower cross bar and the upper cross bar are always positioned on the same vertical surface;
wherein, the sheer pole subassembly is located the below of entablature pole for cooperate with the entablature pole in order to inject the recovery space that is used for retrieving unmanned aerial vehicle.
2. Unmanned aerial vehicle recovery device of claim 1,
the centering connecting piece comprises a first connecting arm and a second connecting arm, one end of the first connecting arm and one end of the second connecting arm are both connected with the lower cross rod and are obliquely arranged relative to the length direction of the lower cross rod, and the other end of the first connecting arm and the other end of the second connecting arm are respectively hinged with two opposite sides of the supporting component, so that the other end of the lower cross rod can rotate up and down relative to the supporting component; and/or
Centering connecting piece include one end with the coaxial first linking arm and the one end that links to each other of one end of sheer pole with the other end of first linking arm links to each other and is relative second linking arm, the third linking arm that the length direction slope of first linking arm set up, the other end of second linking arm with the other end of third linking arm respectively with the relative both sides of supporting component are articulated mutually, so that the other end of sheer pole can be relative the supporting component rotates from top to bottom.
3. Unmanned aerial vehicle recovery apparatus of claim 1 or 2,
the supporting component comprises a first connecting support and a second connecting support which are arranged on two opposite sides of the supporting component, and the centering connecting piece is hinged with the first connecting support and the second connecting support respectively.
4. Unmanned aerial vehicle recovery apparatus of claim 3,
the part of the centering connecting piece, which is hinged with the first connecting support and the second connecting support, is provided with a first connecting hole, the first connecting support and the second connecting support are both provided with second connecting holes, and a pin shaft is inserted into the first connecting hole and the second connecting hole, so that the centering connecting piece is respectively hinged with the first connecting support and the second connecting support.
5. The unmanned aerial vehicle recovery device of claim 4, further comprising:
the two pin shaft baffles are respectively connected with the first connecting support and the second connecting support through bolts and are used for fixing the pin shafts;
the hinge pin comprises a first connecting support and a second connecting support, wherein one end of the hinge pin is provided with a groove, and a hinge pin baffle is embedded in the groove to limit the hinge pin to rotate relative to the first connecting support or the second connecting support.
6. The unmanned aerial vehicle recovery device of claim 1 or 2, wherein the bottom rail assembly further comprises:
the roller assembly comprises a roller arranged at one end of the lower cross rod far away from the supporting assembly and a roller bracket used for fixing the roller, and the roller is used for supporting the upper cross rod in the process that the main arm rotates to ascend or descend relative to the supporting assembly so as to assist the upper cross rod to unfold or retract.
7. Unmanned aerial vehicle recovery apparatus of claim 1 or 2,
the support assembly includes: the centering connecting piece and the main arm are hinged with the rotary table welding body, and the rotary table welding body horizontally rotates relative to the rotary support so as to drive the lower cross rod and the main arm to rotate relative to the rotary support.
8. The unmanned aerial vehicle recovery device of claim 1 or 2, further comprising:
the first driving mechanism comprises an oil cylinder base and a first pitching oil cylinder, wherein the oil cylinder base is connected with the bottom of the supporting component, one end of the first pitching oil cylinder is connected with the oil cylinder base, the other end of the first pitching oil cylinder is connected with the lower side of the lower cross rod, and the lower cross rod is driven to rotate up and down relative to the supporting component.
9. The unmanned aerial vehicle recovery device of claim 8, further comprising:
and the second driving mechanism comprises a second pitching oil cylinder of which one end is connected with the oil cylinder base, and the other end of the second pitching oil cylinder is connected with the lower side of the main arm so as to drive the main arm to rotate up and down relative to the supporting component.
10. Unmanned aerial vehicle recovery apparatus of claim 1 or 2,
the main arm is a foldable part or a telescopic part; and/or
The upper cross rod component is a foldable part or a telescopic part; and/or
The lower cross bar assembly is a foldable member or a telescopic member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922358639.8U CN211731849U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle recovery unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922358639.8U CN211731849U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle recovery unit |
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| Publication Number | Publication Date |
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| CN211731849U true CN211731849U (en) | 2020-10-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922358639.8U Withdrawn - After Issue CN211731849U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle recovery unit |
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| CN (1) | CN211731849U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979713A (en) * | 2019-12-25 | 2020-04-10 | 三一汽车制造有限公司 | Unmanned aerial vehicle recovery unit |
-
2019
- 2019-12-25 CN CN201922358639.8U patent/CN211731849U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979713A (en) * | 2019-12-25 | 2020-04-10 | 三一汽车制造有限公司 | Unmanned aerial vehicle recovery unit |
| CN110979713B (en) * | 2019-12-25 | 2023-04-07 | 湖南省地面无人装备工程研究中心有限责任公司 | Unmanned aerial vehicle recovery unit |
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