CN203666997U - Automatic circulating launching and recovery device of unmanned aerial vehicle - Google Patents
Automatic circulating launching and recovery device of unmanned aerial vehicle Download PDFInfo
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- CN203666997U CN203666997U CN201320889304.9U CN201320889304U CN203666997U CN 203666997 U CN203666997 U CN 203666997U CN 201320889304 U CN201320889304 U CN 201320889304U CN 203666997 U CN203666997 U CN 203666997U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle systems, and particularly relates to an automatic circulating launching and recovery device of an unmanned aerial vehicle, and. The device can achieve launce and takeoff, net recovery, posture adjustment and intermediate transport of the unmanned aerial vehicle. The device solves the launch and recovery problems of the unmanned aerial vehicle in unattended or severe environment, and therefore the automation degree of the unmanned aerial vehicle system is improved. The device comprises a catapult, a recovery mechanism and a posture adjusting and transport mechanism. The catapult comprises a supporting mechanism, a launch sliding rail mechanism and an unmanned aerial vehicle loader. The supporting mechanism comprises a tripod and a fixed hinge supporting base. The launch sliding rail mechanism comprises a linear guide rail, a spring, a rope, a fixed pulley block, a sliding rail supporting plate and a drive mechanism. The drive mechanism comprises a first drive motor, a wheel shaft, a magnetic switch, a belt wheel and a belt. The posture adjusting and transport mechanism comprises a posture adjusting mechanism, a first-level transmission mechanism and a second-level transmission mechanism.
Description
Technical field
The utility model belongs to Unmanned Aircraft Systems (UAS) technical field, particularly relate to a kind of unmanned plane from major cycle transmitting, regenerative apparatus, comprise unmanned plane catapult-assisted take-off, hit that net reclaims, attitude adjustment and intermediate transport.
Background technology
Current, the development of China's Unmanned Aircraft Systems (UAS) has entered a new stage, and transmitting is day by day ripe with the mode reclaiming, increasingly extensive in the application of national defence and civil area.
The transmitting of unmanned plane directly affects reliability, manoevreability, Local Adaptation and the viability of Unmanned Aircraft Systems (UAS), is difficulty and the key link the most during unmanned plane uses.The recovery of unmanned plane is that unmanned plane recycles fully to realize the prerequisite of its value.Can, but unmanned plane is prone to accident in removal process, consequence be serious, reclaim safely and reliably and become the important indicator of evaluating unmanned plane performance.
Transmitting and the regenerative apparatus of China's Unmanned Aircraft Systems (UAS) are separated from each other at present, and the transmitting cycle is longer, and organic efficiency is lower, and whole process need people's participation, so, wait under harsh environment high and cold, and it is very difficult that the transmitting of unmanned plane and removal process will become.
Utility model content
The problem existing for prior art, the utility model provide a kind of unmanned plane from major cycle transmitting, regenerative apparatus, in order to solve transmitting and the recovery problem of unmanned plane under unmanned or harsh environment, thereby further promote the degree of automation of Unmanned Aircraft Systems (UAS).
To achieve these goals, the utility model adopts following technical scheme: a kind of unmanned plane from major cycle transmitting, regenerative apparatus, comprise elastic force ejection mechanism, recovering mechanism, attitude adjustment and connecting gear; Elastic force ejection mechanism comprises supporting mechanism, launches sliding track mechanism and unmanned plane carrier, supporting mechanism is made up of tripod and fixed-hinged support, launch sliding track mechanism and be made up of several line slideways, spring, rope, fixed pulley group, slide rail stay bearing plate and driver train, tripod, fixed-hinged support are hinged with the two ends of slide rail stay bearing plate respectively; The two ends of line slideway are arranged on the end face of slide rail stay bearing plate, bottom at slide rail stay bearing plate is provided with spring, one end of spring is fixed on the bottom of the near end of slide rail stay bearing plate, the other end is connected with rope, rope is connected with unmanned plane carrier by fixed pulley group, and fixed pulley group is fixed on holding of slide rail stay bearing plate far awayly, and unmanned plane carrier is arranged on the top of slide rail stay bearing plate, on unmanned plane carrier, be fixed with linear bearing, linear bearing coordinates one by one with line slideway; Driver train is made up of the first drive motor, wheel shaft, magnet-switch, belt wheel and belt, and wheel shaft is separately fixed at the two ends of the end face of slide rail stay bearing plate, and the wheel shaft that is arranged on one end of slide rail stay bearing plate is connected with the output shaft of the first drive motor; On wheel shaft, be provided with belt wheel, between belt wheel corresponding to the two ends of slide rail stay bearing plate, be provided with belt; Magnet-switch is made up of first, second magnetic sheet, and the first magnetic sheet is fixed on lower floor's belt, and the second magnetic sheet is fixed on unmanned plane carrier; Described attitude adjustment and connecting gear comprise attitude-adjusting system, one-level connecting gear and secondary connecting gear; Attitude-adjusting system is by landing plate, baffle plate, the second firm banking and stretch out bar and form, and landing plate is fixed on the second firm banking, and baffle plate is separately fixed at the both sides of landing plate, is provided with and stretches out bar in the front end both sides of landing plate; One-level connecting gear is arranged on the front of attitude-adjusting system, one-level connecting gear is made up of the first lifter, the 3rd firm banking, the second drive motor, rotating disk, swinging strut and connecting panel, the first lifter is arranged on the both sides of the 3rd firm banking, connecting panel is fixed on the first lifter slide block, on connecting panel, be fixed with the second drive motor, above connecting panel, be provided with rotating disk, rotating disk is fixedly connected with the output shaft of the second drive motor, on rotating disk, be fixed with swinging strut, swinging strut is arranged on the front lower place of stretching out bar of attitude-adjusting system; Secondary connecting gear is arranged on the front of one-level connecting gear, secondary connecting gear is made up of the second lifter, the 4th firm banking and hook, the second lifter is arranged on the both sides of the 4th firm banking, the setting that is inclined upwardly of the front end of the second lifter, and hook is arranged on the second lifter slide block; Described elastic force ejection mechanism is arranged on one-level, secondary connecting gear place, is provided with recovering mechanism at the rear portion of described attitude-adjusting system.
Bottom at described slide rail stay bearing plate is provided with spring shell, and described spring is arranged on spring shell inside, and described tripod and spring shell are hinged.
Described fixed pulley group is made up of upper and lower fixed pulley, upper fixed pulley is arranged on the top of holding of slide rail stay bearing plate far awayly, lower fixed pulley is arranged on the bottom of holding of slide rail stay bearing plate far awayly, and described rope is connected with unmanned plane carrier by lower fixed pulley, upper fixed pulley successively.
Described unmanned plane carrier is made up of vehicle body, elastic reset hook and loading plate lid, is provided with elastic reset hook in body structure both sides, is provided with loading plate lid at body rear end; Described rope is connected with the vehicle body of unmanned plane carrier, is fixed with linear bearing at the body bottom of unmanned plane carrier, and belt is arranged on the top of the body bottom of unmanned plane carrier, and the second magnetic sheet is fixed on the body bottom of unmanned plane carrier.
Two ends at described slide rail stay bearing plate are fixed with adjustment block, and described wheel shaft is fixed in adjustment block.
Far away end at described line slideway is provided with damper.
The inverted trapezoidal flat board that described landing plate is the downward-sloping placement of front end, the rear end width of landing plate is greater than the front end width of landing plate, and the front end width of landing plate be less than unmanned plane length, be greater than the width of unmanned plane.
The height of described baffle plate is 1/2nd of unmanned plane thickness.
Described recovering mechanism forms by hitting net recovering mechanism, the first firm banking and adjust bar, hit net recovering mechanism and be arranged on the top of the first firm banking, the top of adjust bar is connected with the catch net that hits net recovering mechanism by connection lead, and the bottom of adjust bar is connected with the pipe link that hits net recovering mechanism by connection lead.
The beneficial effects of the utility model:
The utility model has been realized unmanned plane from major cycle transmitting, the overall process that reclaims, and the transmitting cycle is short, and organic efficiency is high, can unmanned, and compact conformation, easy for installation.
Brief description of the drawings
Fig. 1 is the structural representation from major cycle transmitting, regenerative apparatus of unmanned plane of the present utility model;
Fig. 2 is the structural representation of the elastic force ejection mechanism after dismounting tripod of the present utility model and tripod head;
Fig. 3 is the lateral plan that the Fig. 2 after tripod and tripod head is installed;
Fig. 4 is the back view of Fig. 2;
Fig. 5 is the structural representation of the recovering mechanism after dismounting the first firm banking of the present utility model;
Fig. 6 is the structural representation of attitude-adjusting system of the present utility model;
Fig. 7 is the structural representation of one-level connecting gear of the present utility model;
Fig. 8 is the structural representation of secondary connecting gear of the present utility model;
In figure, the two circle of 1--hook extension spring, 2--spring shell, 3--slide rail stay bearing plate, the short optical axis of 4--, the short optical axis bearing of 5--, 6--steel rope, 7-upper fixed pulley, 8-lower fixed pulley, 9--unmanned plane carrier, 10--elastic reset hook, 11--loading plate lid, 12--the second strong magnetic piece, 13-magnet button, 14-linear bearing, 15--line slideway, 16--bearing, 17--damper, 18--damper bearing, 19--damper top board, 20--motor support plate, the 21-the first drive motor, the output shaft of 22--the first drive motor, 23--coupler, the 24-the first cog belt wheel shaft, 25-clutch shaft bearing seat, 26--the first profile of tooth belt wheel, the 27-the first adjustment block, the 28-the second cog belt wheel shaft, 29--the second profile of tooth belt wheel, 30--the second bearing seat, the 31-the second adjustment block, 32--cog belt, 33--the first strong magnetic piece, 34--fixed-hinged support, 35--axle sleeve, 36--tripod, 37--tripod head, 38--hits net recovering mechanism, 39--the first linear bearing, 40--catch net, 41--fishing line, 42--adjust bar, 43--pipe link, the 44-the second linear bearing, the 45-the first firm banking, 46--landing plate, 47-stretch out bar, the 48-the second firm banking, 49--baffle plate, the 50-the three firm banking, the 51-the first lifter, the 52-the first lifter slide block, 53--connecting panel, the 54-the second drive motor, the output shaft of 55--the second drive motor, 56--rotating disk, 57--swinging strut, the 58-the four firm banking, the 59-the second lifter, the 60-the second lifter slide block, 61--hook, 62-vehicle body.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
As shown in Fig. 1～Fig. 8, a kind of unmanned plane from major cycle transmitting, regenerative apparatus, comprise coaxial elastic force ejection mechanism of arranging, recovering mechanism, attitude adjustment and connecting gear, elastic force ejection mechanism comprises supporting mechanism, launches sliding track mechanism and unmanned plane carrier, and supporting mechanism is made up of the fixed-hinged support 34 of adjustable for height tripod 36 and pair of parallel setting, and the height of tripod 36 is higher than the height of fixed-hinged support 34, launching sliding track mechanism is made up of left and right line slideway 15, slide rail stay bearing plate 3, two round hook extension spring 1, steel rope 6, the spring shell 2 with through hole, driver train and upper and lower fixed pulley, fixed-hinged support 34 is hinged with the bottom of the near end of slide rail stay bearing plate 3, and fixed-hinged support 34 forms revolute pair by axle sleeve 35 and the circular hole that is arranged on slide rail stay bearing plate 3 bottoms, the top of tripod 36 is hinged by far away the bottom of holding of tripod head 37 and spring shell 2, spring shell 2 is fixed on the bottom of slide rail stay bearing plate 3, one circle hook of two round hook extension springs 1 is enclosed within on short optical axis 4 through the through hole of spring shell 2, short optical axis 4 is fixed on the bottom of the near end of slide rail stay bearing plate 3 by short optical axis bearing 5, another circle hook of two round hook extension springs 1 is connected with steel rope 6, steel rope 6 is by lower fixed pulley 8, upper fixed pulley 7 is connected with the bottom of unmanned plane carrier 9, described upper fixed pulley 7 is arranged on the top of holding of slide rail stay bearing plate 3 far awayly, lower fixed pulley 8 is arranged on the bottom of holding of slide rail stay bearing plate 3 far awayly, described unmanned plane carrier 9 is similar to a dolly, unmanned plane carrier 9 is made up of vehicle body 62, elastic reset hook 10 and loading plate lid 11, be provided with elastic reset hook 10 in the vehicle body 62 front end both sides of unmanned plane carrier 9, unmanned plane can hang on elastic reset hook 10 by trammel beam, vehicle body 62 rear ends at unmanned plane carrier 9 are provided with loading plate lid 11, can change angle to adjust the attitude of launching of unmanned plane, unmanned plane carrier 9 is arranged on the top of slide rail stay bearing plate 3, in the vehicle body 62 bottom symmetries of unmanned plane carrier 3, be parallelly fixed with left and right linear bearing 14, left and right linear bearing 14 matches with left and right line slideway 15 respectively, and unmanned plane carrier 9 can be moved up and down along left and right line slideway 15, in the time that unmanned plane carrier 9 moves downward along left and right line slideway 15, two round hook extension springs 1 extend, in the time that two round hook extension springs 1 shrink under restoring force effect, drive unmanned plane carrier 9 along the quick upward movement of left and right line slideway 15, now, the unmanned plane hanging on unmanned plane carrier 9 will obtain ejection energy requirement, left, right line slideway 15 is round bar, its two ends are fixed on the end face of slide rail stay bearing plate 3 by bearing 16 respectively, driver train is by the first drive motor 21, the first cog belt wheel shaft 24, the second cog belt wheel shaft 28, magnet-switch, the first profile of tooth belt wheel 26, the second profile of tooth belt wheel 29 and cog belt 32 form, the first cog belt wheel shaft 24, the second cog belt wheel shaft 28 is respectively by clutch shaft bearing seat 25, the second bearing seat 30 is fixed on the two ends of slide rail stay bearing plate 3, the first cog belt wheel shaft 24 is connected by coupler 23 with the output shaft 22 of the first drive motor, the first drive motor 21 is fixed on the side of slide rail stay bearing plate 3 by motor support plate 20, the first drive motor 21 provides power for the utility model device, on the first cog belt wheel shaft 24, be provided with two the first profile of tooth belt wheels 26, on the second cog belt wheel shaft 28, be provided with two the second profile of tooth belt wheels 29, between first, second profile of tooth belt wheel of correspondence, be provided with cog belt 32, cog belt 32 is arranged on the top of vehicle body 62 bottoms of unmanned plane carrier 9, and cog belt 32 can be connected with vehicle body 62 bottoms of unmanned plane carrier 9 by magnet-switch, first, second cog belt wheel shaft, cog belt 32 and first, second cog belt wheel form the tape transport of two groups of parallel connections, magnet-switch is made up of first, second strong magnetic piece, and the first strong magnetic piece 33 is bolted on the lower surface of lower floor's cog belt 32, does synchronous reciprocating motion with cog belt 32, the second strong magnetic piece 12 is fixed on vehicle body 62 bottom surfaces of unmanned plane carrier 9 by magnet button 13, in the time that the pulling force of two round hook extension springs 1 equals the attractive force of magnet-switch, magnet-switch triggers, described attitude adjustment and connecting gear comprise attitude-adjusting system, one-level connecting gear and secondary connecting gear, attitude-adjusting system is by landing plate 46, baffle plate 49, the second firm banking 48 and stretch out bar 47 and form, and landing plate 46 is fixed on the second firm banking 48, and baffle plate 49 is separately fixed at the both sides of landing plate 46, is provided with and stretches out bar 47 in the front end both sides of landing plate 46, one-level connecting gear is arranged on the front of attitude-adjusting system, one-level connecting gear is made up of two the first lifters 51, the 3rd firm banking 50, the second drive motor 54, rotating disk 56, two swinging struts 57 and connecting panel 53, the both sides that two the first lifters 51 are parallel, be symmetricly set on the 3rd firm banking 50, two the first lifters 51 are as line slideway, in order to realize the linear transmission of unmanned plane, connecting panel 53 is horizontally fixed on two the first lifter slide blocks 52, be fixed with the second drive motor 54 in the bottom centre of connecting panel 53, above connecting panel 53, be provided with rotating disk 56, rotating disk 56 is fixedly connected with by pin with the output shaft 55 of the second drive motor, the second drive motor 54 can drive rotating disk 56 to do 180 ° of rotations, in order to adjust the front and rear direction of unmanned plane, be fixed with two symmetrical swinging struts 57 at the top of rotating disk 56, swinging strut 57 is arranged on the front lower place of stretching out bar 47 of attitude-adjusting system, ensure that unmanned plane slides on swinging strut 57 by stretching out bar 47, secondary connecting gear is arranged on the front of one-level connecting gear, secondary connecting gear is made up of two the second lifters 59, the 4th firm banking 58 and two hooks 61, the both sides that two the second lifters 59 are parallel, be symmetricly set on the 4th firm banking 58, the rear portion of two the second lifters 59 is arranged on the front upper place of the first lifter 51 of one-level connecting gear, swinging strut 57 lower than one-level connecting gear, the second lifter 59 is as line slideway, in order to realize the linear transmission of unmanned plane, the setting that is inclined upwardly of the front end of the second lifter 59, two hooks 61 are separately positioned on the inner side of two the second lifter slide blocks 60, and the spacing of two hooks 61 is less than the length of unmanned plane trammel beam, when the second lifter slide block 60 is during at stroke top, its height is a little less than the swinging strut 57 of one-level connecting gear, advancing in process of the second lifter slide block 60, hook 61 hooks the trammel beam of getting unmanned plane, and unmanned plane is come on secondary connecting gear, when the second lifter slide block 60 is during at end of travel, the trammel beam of unmanned plane presses down the elastic reset hook 10 of unmanned plane carrier 9 front ends and enters unmanned plane carrier 9, prepares emission process next time, the near end of described elastic force ejection mechanism is arranged between two the first lifters 51 of one-level connecting gear, and lower than the height of the first lifter 51, holding between two the second lifters 59 that are arranged on secondary connecting gear of elastic force ejection mechanism far awayly, and higher than the height of the second lifter 59, be provided with recovering mechanism at described attitude-adjusting system rear portion.
Be fixed with respectively first, second adjustment block of plastics at the two ends of described slide rail stay bearing plate 3, clutch shaft bearing seat 25 is fixed in the first adjustment block 27, and the second bearing seat 30 is fixed in the second adjustment block 31.
Far away end at described line slideway 15 is provided with damper 17, and damper 17 is fixed on slide rail stay bearing plate 3 by damper bearing 18 and damper top board 19, the shock and vibration that bring when reducing unmanned plane transmitting.
The model that described damper 17 adopts is: AD2525-5.
Described recovering mechanism is made up of the adjust bar 42 that hits net recovering mechanism 38, the first firm banking 45 and have a through hole, hit net recovering mechanism 38 and be fixed on the top of the first firm banking 45, fishing line 41 one end are connected with the catch net 40 that hits net recovering mechanism 38, and fishing line 4 other ends are connected with the pipe link 43 that hits net recovering mechanism 38 through the through hole of adjust bar 42; Travel forward in process at the first linear bearing 39 and the second linear bearing 44 that hit net recovering mechanism 38, fishing line 41 can be strained gradually, and mention catch net 40, and play the effect that regulates catch net 40 shapes, facilitate unmanned plane to fall on landing plate 46 from catch net 40.
It is described that what hit that net recovering mechanism 38 adopts is that application number is 201320039180.5 Chinese patent " a kind of two-freedom net collision recovery device of unmanned aerial vehicle ".
Described landing plate 46 is the inverted trapezoidal flat board of the downward-sloping placement of front end, the rear end width of landing plate 46 is greater than landing plate 46 front end width, the flat funnel that likeness in form is cut open, and the front end width of landing plate 46 be less than unmanned plane length, be greater than the width of unmanned plane, described in stretch out bar 47 and be arranged on landing plate 46 front end both sides; In the time that unmanned plane is anchored on landing plate 46 by catch net 40, unmanned plane can glide along landing plate 46 under the effect of gravity, because landing plate 46 is inverted trapezoidal wide at the top and narrow at the bottom, in downslide process, the head of unmanned plane, wing can be subject to the restriction of baffle plate 49, under the combined action of gravity and baffle plate 49, the angle of the axis of unmanned plane and the utility model device axis diminishes gradually, finally overlaps, then skidded off by the bar 47 that stretches out of landing plate 46, and slide to one-level connecting gear.
The height of described baffle plate 49 is 1/2nd of unmanned plane thickness, and unmanned plane carries out attitude adjustment under the double action of baffle plate 49 and gravity.
What described first, second lifter adopted is all that model is the electric glass lifter for automobile of east wind sky dragon 6104010-C0101.
Below in conjunction with brief description of the drawings use procedure of the present utility model:
As shown in Fig. 1～Fig. 8, when unmanned plane is finished the work while flying back, the rotating mechanism and the adjusting angle mechanism that hit net regenerative apparatus 38 move simultaneously, and the block mechanism that makes to hit net regenerative apparatus 38 stops after the orientation of interception unmanned plane and angle in being applicable to, and waits for that unmanned aerial vehicle net reclaims; When completing, hits after net unmanned plane, can hang on the catch net 40 that hits net regenerative apparatus 38, now, rotating mechanism first moves, the position that faces attitude-adjusting system is got back to by the mechanism that makes to block, and then adjusting angle mechanism moves to smallest limit position, and block mechanism is detained, unmanned plane is fallen on the landing plate 46 of attitude-adjusting system, and the front of unmanned plane or reverse side are upward; When unmanned plane departs from after block mechanism, rotating mechanism first resets, and then adjusting angle mechanism resets.
When unmanned plane is fallen on the landing plate 46 of attitude-adjusting system, can glide along landing plate 46, under the effect of baffle plate 49, unmanned plane carries out attitude adjustment simultaneously, its axis gradually with device dead in line; When the trammel beam of unmanned plane slides into while stretching out on bar 47, under the effect of gravity, unmanned plane carries out attitude adjustment again, and its fuselage is perpendicular to the ground, and then, unmanned plane skids off and stretches out bar 47, falls on the swinging strut 57 of one-level connecting gear.The first lifter 51 of one-level connecting gear starts, the first lifter slide block 52 in sliding process to unmanned plane (one side of unmanned plane scribbles special color) towards judging, if positive leading, rotating disk 56 meetings Rotate 180 ° under the driving of the second drive motor 54, makes the reverse side of unmanned plane forward.Then, one-level connecting gear continues to transmit unmanned plane, until the trammel beam of unmanned plane is come hook 61 fronts of secondary connecting gear, the second lifter slide block 60 of secondary connecting gear starts to travel forward from stroke top; In the process of travelling forward, hook 61 can hook the trammel beam of getting unmanned plane, and unmanned plane is moved on secondary connecting gear, and one-level connecting gear resets simultaneously; When the second lifter slide block 60 moves to end of travel, the trammel beam of unmanned plane is depressed the elastic reset hook 10 of unmanned plane carrier 9 front ends, and hangs on elastic reset hook 10, and secondary connecting gear is out of service, and secondary connecting gear resets simultaneously; The first strong magnetic piece 33 on cog belt 32 starts to approach the second strong magnetic piece 12 on unmanned plane carrier 9, until first, second strong magnetic piece adhesive, unmanned plane enters accurate emission state.
Receive and take off after assignment instructions when unmanned plane, the first drive motor 21 of elastic force ejection mechanism is started working, by the magnetic attracting force of the second strong magnetic piece 12 and the first strong magnetic piece 33, hauling unmanned plane carrier 9 moves backward, now, two round hook extension springs 1 are stressed to be extended gradually, the pulling force of unmanned plane carrier 9 is also increased gradually, in the time that this pulling force equals the magnetic attracting force of first, second strong magnetic piece, first, second strong magnetic piece separates, and unmanned plane carrier 9 is advanced fast along line slideway 15 under the elastic-restoring force effect of two round hook extension springs 1; In the time that unmanned plane carrier 9 is come end of travel, under the effect of damper 17, reduce speed now, finally stop, and unmanned plane obtains the required initial velocity that takes off, eject forward along the direction that is inclined upwardly, unmanned plane has been launched.
Claims (9)
- Unmanned plane from major cycle transmitting, a regenerative apparatus, it is characterized in that comprising elastic force ejection mechanism, recovering mechanism, attitude adjustment and connecting gear; Elastic force ejection mechanism comprises supporting mechanism, launches sliding track mechanism and unmanned plane carrier, supporting mechanism is made up of tripod and fixed-hinged support, launch sliding track mechanism and be made up of several line slideways, spring, rope, fixed pulley group, slide rail stay bearing plate and driver train, tripod, fixed-hinged support are hinged with the two ends of slide rail stay bearing plate respectively; The two ends of line slideway are arranged on the end face of slide rail stay bearing plate, bottom at slide rail stay bearing plate is provided with spring, one end of spring is fixed on the bottom of the near end of slide rail stay bearing plate, the other end is connected with rope, rope is connected with unmanned plane carrier by fixed pulley group, and fixed pulley group is fixed on holding of slide rail stay bearing plate far awayly, and unmanned plane carrier is arranged on the top of slide rail stay bearing plate, on unmanned plane carrier, be fixed with linear bearing, linear bearing coordinates one by one with line slideway; Driver train is made up of the first drive motor, wheel shaft, magnet-switch, belt wheel and belt, and wheel shaft is separately fixed at the two ends of the end face of slide rail stay bearing plate, and the wheel shaft that is arranged on one end of slide rail stay bearing plate is connected with the output shaft of the first drive motor; On wheel shaft, be provided with belt wheel, between belt wheel corresponding to the two ends of slide rail stay bearing plate, be provided with belt; Magnet-switch is made up of first, second magnetic sheet, and the first magnetic sheet is fixed on lower floor's belt, and the second magnetic sheet is fixed on unmanned plane carrier; Described attitude adjustment and connecting gear comprise attitude-adjusting system, one-level connecting gear and secondary connecting gear; Attitude-adjusting system is by landing plate, baffle plate, the second firm banking and stretch out bar and form, and landing plate is fixed on the second firm banking, and baffle plate is separately fixed at the both sides of landing plate, is provided with and stretches out bar in the front end both sides of landing plate; One-level connecting gear is arranged on the front of attitude-adjusting system, one-level connecting gear is made up of the first lifter, the 3rd firm banking, the second drive motor, rotating disk, swinging strut and connecting panel, the first lifter is arranged on the both sides of the 3rd firm banking, connecting panel is fixed on the first lifter slide block, on connecting panel, be fixed with the second drive motor, above connecting panel, be provided with rotating disk, rotating disk is fixedly connected with the output shaft of the second drive motor, on rotating disk, be fixed with swinging strut, swinging strut is arranged on the front lower place of stretching out bar of attitude-adjusting system; Secondary connecting gear is arranged on the front of one-level connecting gear, secondary connecting gear is made up of the second lifter, the 4th firm banking and hook, the second lifter is arranged on the both sides of the 4th firm banking, the setting that is inclined upwardly of the front end of the second lifter, and hook is arranged on the second lifter slide block; Described elastic force ejection mechanism is arranged on one-level, secondary connecting gear place, is provided with recovering mechanism at the rear portion of described attitude-adjusting system.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that being provided with spring shell in the bottom of described slide rail stay bearing plate, described spring is arranged on spring shell inside, described tripod and spring shell are hinged.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that described fixed pulley group is made up of upper and lower fixed pulley, upper fixed pulley is arranged on the top of holding of slide rail stay bearing plate far awayly, lower fixed pulley is arranged on the bottom of holding of slide rail stay bearing plate far awayly, and described rope is connected with unmanned plane carrier by lower fixed pulley, upper fixed pulley successively.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that described unmanned plane carrier is made up of vehicle body, elastic reset hook and loading plate lid, be provided with elastic reset hook in body structure both sides, be provided with loading plate lid at body rear end; Described rope is connected with vehicle body, is fixed with linear bearing at body bottom, and belt is arranged on the top of body bottom, and the second magnetic sheet is fixed on body bottom.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that being fixed with adjustment block at the two ends of described slide rail stay bearing plate, described wheel shaft is fixed in adjustment block.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that being provided with damper far away the end of described line slideway.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that the inverted trapezoidal flat board that described landing plate is the downward-sloping placement of front end, the rear end width of landing plate is greater than the front end width of landing plate, and the front end width of landing plate be less than unmanned plane length, be greater than the width of unmanned plane.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, the height that it is characterized in that described baffle plate is 1/2nd of unmanned plane thickness.
- Unmanned plane according to claim 1 from major cycle transmitting, regenerative apparatus, it is characterized in that described recovering mechanism forms by hitting net recovering mechanism, the first firm banking and adjust bar, hit net recovering mechanism and be arranged on the top of the first firm banking, the top of adjust bar is connected with the catch net that hits net recovering mechanism by connection lead, and the bottom of adjust bar is connected with the pipe link that hits net recovering mechanism by connection lead.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201320889304.9U CN203666997U (en) | 2013-12-31 | 2013-12-31 | Automatic circulating launching and recovery device of unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320889304.9U CN203666997U (en) | 2013-12-31 | 2013-12-31 | Automatic circulating launching and recovery device of unmanned aerial vehicle |
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| CN201320889304.9U Expired - Fee Related CN203666997U (en) | 2013-12-31 | 2013-12-31 | Automatic circulating launching and recovery device of unmanned aerial vehicle |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103693206A (en) * | 2013-12-31 | 2014-04-02 | 东北大学 | Autonomous circular launching and landing device for unmanned aerial vehicle |
| CN105109685A (en) * | 2015-09-29 | 2015-12-02 | 东北大学 | Launch and withdraw device of unmanned aerial vehicle and method for launch and withdraw device |
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
| CN106681357A (en) * | 2017-01-11 | 2017-05-17 | 深圳市元征科技股份有限公司 | Unmanned aerial vehicle backpack and method and system for controlling unmanned aerial vehicle on basis of unmanned aerial vehicle backpack |
| CN108382288A (en) * | 2018-03-02 | 2018-08-10 | 西安天博机电科技有限公司 | A kind of integral type R-T unit for unmanned plane |
| CN109502042A (en) * | 2018-11-26 | 2019-03-22 | 南京林业大学 | A kind of unmanned plane acquisition equipment |
| CN115489749A (en) * | 2022-11-16 | 2022-12-20 | 成都航空职业技术学院 | Fixed wing unmanned aerial vehicle launches take-off and land integrated system |
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2013
- 2013-12-31 CN CN201320889304.9U patent/CN203666997U/en not_active Expired - Fee Related
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| CN103693206A (en) * | 2013-12-31 | 2014-04-02 | 东北大学 | Autonomous circular launching and landing device for unmanned aerial vehicle |
| CN103693206B (en) * | 2013-12-31 | 2015-11-04 | 东北大学 | A kind of spontaneous circulation of unmanned plane is launched, regenerative apparatus |
| CN105109685A (en) * | 2015-09-29 | 2015-12-02 | 东北大学 | Launch and withdraw device of unmanned aerial vehicle and method for launch and withdraw device |
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
| CN106681357A (en) * | 2017-01-11 | 2017-05-17 | 深圳市元征科技股份有限公司 | Unmanned aerial vehicle backpack and method and system for controlling unmanned aerial vehicle on basis of unmanned aerial vehicle backpack |
| CN108382288A (en) * | 2018-03-02 | 2018-08-10 | 西安天博机电科技有限公司 | A kind of integral type R-T unit for unmanned plane |
| CN109502042A (en) * | 2018-11-26 | 2019-03-22 | 南京林业大学 | A kind of unmanned plane acquisition equipment |
| CN115489749A (en) * | 2022-11-16 | 2022-12-20 | 成都航空职业技术学院 | Fixed wing unmanned aerial vehicle launches take-off and land integrated system |
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