CN111036992A - Unmanned aerial vehicle wing shaft fretwork equipment - Google Patents
Unmanned aerial vehicle wing shaft fretwork equipment Download PDFInfo
- Publication number
- CN111036992A CN111036992A CN201911375584.XA CN201911375584A CN111036992A CN 111036992 A CN111036992 A CN 111036992A CN 201911375584 A CN201911375584 A CN 201911375584A CN 111036992 A CN111036992 A CN 111036992A
- Authority
- CN
- China
- Prior art keywords
- rod
- hollow
- frame
- side wall
- unmanned aerial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23D—PLANING; SLOTTING; SHEARING; BROACHING; SAWING; FILING; SCRAPING; LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOT OTHERWISE PROVIDED FOR
- B23D79/00—Methods, machines, or devices not covered elsewhere, for working metal by removal of material
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention relates to the field of unmanned aerial vehicles, in particular to a wing shaft hollowing device of an unmanned aerial vehicle. The wing shafts of the unmanned aerial vehicles with different specifications can be fixed; the stability of the fixed wing shaft of the unmanned aerial vehicle can be improved; the wing shaft of the unmanned aerial vehicle can be symmetrically processed, so that the processing efficiency is conveniently improved; the processing position of the wing shaft of the unmanned aerial vehicle can be adjusted according to actual conditions. The inner end clamping rod is pushed to be separated from the hollowed boss, and then the hollowed upper frame is manually slid along the hollowed outer frame, so that the position of the hollowed cutter is changed, and further the position of the hollowed cutter can be adjusted; in order to adapt to the unmanned aerial vehicle wing shaft of different specifications, because of the unmanned aerial vehicle wing shaft's of different specifications gravity is different, and then make and bear the frame degree of moving down along the outer end chassis different, it is different along the inner compression degree that pushes away the spring of inner traveller compression through articulated post simultaneously.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to a wing shaft hollowing device of an unmanned aerial vehicle.
Background
Unmanned aerial vehicle wing axle fretwork equipment is the equipment commonly used in the unmanned aerial vehicle field, but general unmanned aerial vehicle wing axle fretwork equipment function is more single.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle wing shaft hollowing device which can fix unmanned aerial vehicle wing shafts with different specifications; the stability of the fixed wing shaft of the unmanned aerial vehicle can be improved; the wing shaft of the unmanned aerial vehicle can be symmetrically processed, so that the processing efficiency is conveniently improved; the processing position of the wing shaft of the unmanned aerial vehicle can be adjusted according to actual conditions.
The purpose of the invention is realized by the following technical scheme:
the utility model provides an unmanned aerial vehicle wing axle fretwork equipment, includes axle mount, horizontal balladeur train assembly, mount assembly, chassis assembly, fretwork assembly, the axle mount is connected with the chassis assembly, and horizontal balladeur train assembly is connected with the chassis assembly, and the mount assembly is connected with horizontal slide frame assembly, and the fretwork assembly is connected with horizontal slide frame assembly.
As a further optimization of the technical scheme, the unmanned aerial vehicle wing shaft hollowing device comprises a shaft fixing frame, an outer end bottom frame, a trapezoidal sliding groove, a bearing frame, a fixing rod, a hinge column, an inner end sliding column, an inner end pushing spring, a matching waist groove, a lower end sleeve and a side wall support, wherein the trapezoidal sliding groove is formed in the outer end bottom frame, the bearing frame is connected with the outer end bottom frame in a sliding mode, the side wall support is connected with the trapezoidal sliding groove in a sliding mode, the fixing rod is connected with the hinge column in a hinged mode, the hinge column is connected with the inner end sliding column in a sliding mode, the inner end sliding column is fixedly connected with the side wall support, the inner end pushing spring is connected with the inner end sliding column in a sleeved mode, the fixing rod is.
As a further optimization of the technical scheme, the invention relates to an unmanned aerial vehicle wing shaft hollowing device, the transverse sliding frame assembly comprises a transverse sliding frame body, a matching groove, a side wall hinge rod, an adjusting threaded rod, a hinge slider, a hinge connecting rod, a first clutch rod, a second clutch rod, a clutch rod limiting plate, a third clutch rod and a clutch rod push spring, the matching groove is formed in the transverse sliding frame body, the side wall hinge rod is hinged with the transverse sliding frame body, the adjusting threaded rod is rotatably connected with the side wall hinge rod, the hinge slider is slidably connected with the side wall hinge rod, the hinge slider is in threaded connection with the adjusting threaded rod, the hinge connecting rod is hinged with the hinge slider, the hinge connecting rod is hinged with the first clutch rod, the first clutch rod is fixedly connected with the second clutch rod, the second clutch rod is matched with the third clutch rod, the third clutch rod is slidably connected with the clutch rod limiting plate, the clutch rod push spring is arranged between the third clutch rod and the clutch rod, the lower end sleeve is connected with the matching groove in a matching way.
As a further optimization of the technical scheme, the invention relates to an unmanned aerial vehicle wing shaft hollowing device, wherein a fixing frame assembly comprises a fixing frame bottom plate, an input motor, an input belt, a rotating shaft I, a driving disc II, a support I, a support II, a side wall boss, a hollow groove, a clamping groove, a support III, a support IV, a driving disc III, a rotating shaft II, a driving disc IV, a meshing straight tooth I, a meshing straight tooth II, a meshing straight tooth III, a meshing straight tooth IV, a meshing straight tooth V, a middle end outer frame, a side wall clamping rod and a side wall clamping rod push spring, the input motor is fixedly connected with the fixing frame bottom plate, the input belt is connected with an output shaft of the input motor, the support I, the support II, the support III and the support IV are fixedly connected with the fixing frame bottom plate, the rotating shaft I is rotatably connected with the support II, the rotating shaft II is rotatably connected with the support III and the, a first driving disk, a second driving disk and a first rotating shaft are fixedly connected, a side wall boss is fixedly connected with a bottom plate of a fixing frame, a hollow groove is arranged on the side wall boss, a clamping groove is connected with the hollow groove, a first meshing straight tooth is matched and connected with a second rotating shaft, a second meshing straight tooth is matched and connected with the first rotating shaft, a first meshing straight tooth is in meshing transmission with the second meshing straight tooth, a first meshing straight tooth and a second meshing straight tooth are rotatably connected with an outer frame at the middle end, a third meshing straight tooth is matched and connected with the second rotating shaft, a fifth meshing straight tooth is matched and connected with the first rotating shaft, a third meshing straight tooth, a fourth meshing straight tooth and a fifth meshing transmission straight tooth, a side wall clamping rod is slidably connected with the outer frame at the middle end, a side wall clamping rod pushing spring is in sleeving connection with the side wall clamping rod, and pushing spring is arranged between the middle end and the side wall boss, the second rotating shaft is fixedly connected with the clutch lever limiting plate, and the input belt is connected with the first rotating shaft in a matched mode.
As a further optimization of the technical scheme, the unmanned aerial vehicle wing shaft hollowing equipment comprises an underframe base plate, an underframe rod I, an underframe rod II, a connecting belt II, a bevel gear shaft I, a transmission bevel gear I and a transmission bevel gear II, wherein the underframe rod I and the underframe rod II are fixedly connected with the underframe base plate, the connecting belt II is in matched connection with the bevel gear shaft I, the bevel gear shaft I is in rotary connection with the underframe rod II, the transmission bevel gear I is fixedly connected with the bevel gear shaft I, the transmission bevel gear II is in meshed transmission with the bevel gear shaft I, the transmission bevel gear II is fixedly connected with a lower end sleeve, the lower end sleeve is in rotary connection with the underframe rod I, the underframe base plate is fixedly connected with the underframe base plate, the clutch rod I is in matched connection with the connecting belt II, and the clutch rod I is in rotary connection with the underframe rod II.
According to the further optimization of the technical scheme, the unmanned aerial vehicle wing shaft hollowing equipment comprises a hollowed-out frame, a hollowed-out boss, a hollowed-out upper frame, a hollowed-out knife, a hollowed-out sleeve, a hollowed-out push spring, an inner end clamping rod, an inner side sliding column and an inner side sliding column sleeve spring, wherein the hollowed-out boss is fixedly connected with the hollowed-out frame, the hollowed-out upper frame is slidably connected with the hollowed-out frame, the hollowed-out sleeve is fixedly connected with the hollowed-out upper frame, the hollowed-out knife is slidably connected with the hollowed-out sleeve, the hollowed-out push spring is arranged between the hollowed-out knife and the hollowed-out upper frame, the inner side sliding column is fixedly connected with the hollowed-out upper frame, the inner side sliding column sleeve spring is connected with the inner side sliding column in a sleeved mode, the inner end clamping rod is slidably connected with the.
The unmanned aerial vehicle wing shaft hollowing equipment has the beneficial effects that:
according to the wing shaft hollowing device of the unmanned aerial vehicle, the inner end clamping rod is pushed to be separated from the hollowed boss, the hollowed upper frame is manually slid along the hollowed outer frame, the position of the hollowed cutter is changed, and the hollowed position is adjusted; in order to adapt to the unmanned aerial vehicle wing shaft of different specifications, because of the gravity difference of the unmanned aerial vehicle wing shaft of different specifications, and then make and bear the frame along the degree that the outer end chassis moved down different, it is different along the inner traveller compression inner compression degree that pushes away the spring simultaneously through articulated post, and then make the dead lever turn over a degree difference to the inboard unmanned aerial vehicle wing shaft of outer end chassis simultaneously, and then make the dead lever conveniently adapt to the different specifications.
Drawings
The invention is described in further detail below with reference to the accompanying drawings and specific embodiments.
FIG. 1 is a first general structural diagram of the present invention;
FIG. 2 is a second overall structural schematic of the present invention;
FIG. 3 is a third schematic view of the overall structure of the present invention;
FIG. 4 is a first schematic view of the shaft fixing bracket of the present invention;
FIG. 5 is a second schematic structural view of the shaft fixing bracket of the present invention;
FIG. 6 is a third schematic structural view of the shaft fixing bracket of the present invention;
FIG. 7 is a schematic view of the transverse carriage assembly configuration of the present invention;
FIG. 8 is a first schematic view of a first embodiment of a fastening frame assembly of the present invention;
FIG. 9 is a second schematic view of the fastening frame assembly of the present invention;
FIG. 10 is a schematic view of the undercarriage assembly of the present invention;
fig. 11 is a schematic structural diagram of the hollow-out assembly of the present invention.
In the figure: a shaft fixing frame 1; an outer end underframe 1-1; a trapezoidal chute 1-2; a carrier 1-3; fixing rods 1-4; hinge columns 1-5; inner end sliding columns 1-6; the inner end pushes springs 1-7; 1-8 of a waist groove; a lower end sleeve 1-9; 1-10 parts of side wall brackets; a transverse carriage assembly 2; a transverse carriage body 2-1; a matching groove 2-2; side wall hinge rods 2-3; adjusting the threaded rod 2-4; 2-5 of hinged slider; hinged connecting rods 2-6; 2-7 parts of a clutch lever I; 2-8 parts of a clutch lever II; 2-9 parts of a clutch lever limiting plate; 2-10 parts of a clutch lever; a clutch lever push spring 2-11; a holder assembly 3; a fixed frame bottom plate 3-1; inputting a motor 3-2; 3-3 of an input belt; 3-4 of a first rotating shaft; a first driving disc 3-5; a second driving disc 3-6; 3-7 of a first bracket; 3-8 parts of a second bracket; 3-9 parts of side wall bosses; 3-10 parts of hollow grooves; 3-11 parts of a clamping groove; 3-12 parts of a bracket III; bracket four 3-13; a third driving disc 3-14; 3-15 parts of a second rotating shaft; driving discs four 3 to 16; 3-17 of a first meshing straight tooth; meshing straight teeth II 3-18; meshing straight teeth III 3-19; meshing straight teeth four 3-20; 3-21 parts of meshing straight teeth; 3-22 of a middle-end outer frame; side wall clamping rods 3-23; 3-24 parts of side wall clamping rod push spring; a chassis assembly 4; a chassis base plate 4-1; 4-2 parts of a first bottom frame rod; 4-3 parts of a bottom frame rod II; a second connecting belt 4-4; 4-5 of a bevel gear shaft I; 4-6 of a transmission bevel gear I; 4-7 parts of a second transmission bevel gear; a hollow-out assembly 5; 5-1 of a hollow outer frame; 5-2 of hollowed-out bosses; 5-3, hollowing out the upper frame; 5-4 of a hollow knife; 5-5 of a hollow sleeve; 5-6 of a hollow push spring; 5-7 of an inner end clamping rod; 5-8 parts of inner sliding column; and 5-9 parts of inner sliding column sleeve spring.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The fixed connection in the device is realized by welding; fixing by means of thread fixing and the like, and using different fixing modes by combining different use environments; the rotary connection means that the bearing is arranged on the shaft in a drying mode, a spring retainer ring groove is formed in the shaft or the shaft hole, and the elastic retainer ring is clamped in the retainer ring groove to achieve axial fixation of the bearing and achieve rotation; the sliding connection refers to the connection through the sliding of the sliding block in the sliding groove or the guide rail, and the sliding groove or the guide rail is generally in a step shape, so that the sliding block is prevented from falling off in the sliding groove or the guide rail; the hinge is formed by a hinge; the pin shaft, the short shaft and other connecting parts are movably connected; the required sealing positions are sealed by sealing rings or O-shaped rings.
The first embodiment is as follows:
the embodiment is described below with reference to fig. 1 to 11, and an unmanned aerial vehicle wing shaft hollowing apparatus includes a shaft fixing frame 1, a transverse carriage assembly 2, a fixing frame assembly 3, a chassis assembly 4, and a hollowing assembly 5, where the shaft fixing frame 1 is connected to the chassis assembly 4, the transverse carriage assembly 2 is connected to the chassis assembly 4, the fixing frame assembly 3 is connected to the transverse carriage assembly 2, and the hollowing assembly 5 is connected to the transverse carriage assembly 2.
The second embodiment is as follows:
the following describes the present embodiment with reference to fig. 1 to 11, and the present embodiment further describes the first embodiment, where the shaft fixing frame 1 includes an outer end chassis 1-1, a trapezoidal sliding groove 1-2, a bearing frame 1-3, a fixing rod 1-4, a hinge post 1-5, an inner end sliding post 1-6, an inner end push spring 1-7, a matching waist groove 1-8, a lower end sleeve 1-9, and a side wall bracket 1-10, the trapezoidal sliding groove 1-2 is disposed on the outer end chassis 1-1, the bearing frame 1-3 is slidably connected with the outer end chassis 1-1, the side wall bracket 1-10 is slidably connected with the trapezoidal sliding groove 1-2, the fixing rod 1-4 is hingedly connected with the hinge post 1-5, the hinge post 1-5 is slidably connected with the inner end sliding post 1-6, the inner end sliding columns 1-6 are fixedly connected with the side wall supports 1-10, the inner end push springs 1-7 are connected with the inner end sliding columns 1-6 in a sleeved mode, the fixed rods 1-4 are hinged to the bearing frames 1-3, the lower end sleeves 1-9 are fixedly connected with the outer end underframe 1-1, and the matched waist grooves 1-8 are arranged on the fixed rods 1-4;
placing an unmanned aerial vehicle wing shaft needing hollow processing on a bearing frame 1-3, under the action of the gravity of the wing shaft of the unmanned aerial vehicle, pushing the bearing frame 1-3 to move downwards along an outer end chassis 1-1, simultaneously enabling a fixing rod 1-4 to be simultaneously folded inwards through the driving of the bearing frame 1-3, simultaneously enabling a side wall support 1-10 to simultaneously slide inwards along a trapezoidal sliding groove 1-2 through the driving of a hinge column 1-5, preventing the fixing rod 1-4 from being simultaneously folded inwards to generate functional interference, and further fixing the wing shaft of the unmanned aerial vehicle when the fixing rod 1-4 is in contact with the wing shaft of the unmanned aerial vehicle; in order to adapt to unmanned aerial vehicle wing shafts of different specifications, the degrees of downward movement of the bearing frame 1-3 along the outer end underframe 1-1 are different due to different gravity of the unmanned aerial vehicle wing shafts of different specifications, meanwhile, the compression degrees of the inner end push springs 1-7 compressed along the inner end sliding columns 1-6 through the hinge columns 1-5 are different, further, the folding degrees of the fixed rods 1-4 towards the inner sides of the outer end underframe 1-1 are different, and further, the fixed rods 1-4 are convenient to adapt to the unmanned aerial vehicle wing shafts of different specifications.
The third concrete implementation mode:
the following describes the present embodiment with reference to fig. 1-11, and the present embodiment further describes the first embodiment, where the transverse carriage assembly 2 includes a transverse carriage body 2-1, a mating groove 2-2, a side wall hinge rod 2-3, an adjusting threaded rod 2-4, a hinge slider 2-5, a hinge connecting rod 2-6, a clutch rod one 2-7, a clutch rod two 2-8, a clutch rod limit plate 2-9, a clutch rod three 2-10, and a clutch rod push spring 2-11, the mating groove 2-2 is disposed on the transverse carriage body 2-1, the side wall hinge rod 2-3 is hinged to the transverse carriage body 2-1, the adjusting threaded rod 2-4 is rotatably connected to the side wall hinge rod 2-3, the hinge slider 2-5 is slidably connected to the side wall hinge rod 2-3, the hinged slider 2-5 is in threaded connection with the adjusting threaded rod 2-4, the hinged connecting rod 2-6 is in hinged connection with the hinged slider 2-5, the hinged connecting rod 2-6 is in hinged connection with the clutch rod I2-7, the clutch rod I2-7 is fixedly connected with the clutch rod II 2-8, the clutch rod II 2-8 is in matched connection with the clutch rod III 2-10, the clutch rod III 2-10 is in sliding connection with the clutch rod limiting plate 2-9, the clutch rod push spring 2-11 is arranged between the clutch rod III 2-10 and the clutch rod limiting plate 2-9, and the lower end sleeve 1-9 is in matched connection with the matching groove 2-2.
The fourth concrete implementation mode:
the embodiment is described below with reference to fig. 1-11, and the embodiment will be further described, wherein the fixed frame assembly 3 includes a fixed frame bottom plate 3-1, an input motor 3-2, an input belt 3-3, a rotating shaft I3-4, a driving disc I3-5, a driving disc II 3-6, a bracket I3-7, a bracket II 3-8, a side wall boss 3-9, a hollow groove 3-10, a slot 3-11, a bracket III 3-12, a bracket IV 3-13, a driving disc III 3-14, a rotating shaft II 3-15, a driving disc IV 3-16, a meshing straight tooth I3-17, a meshing straight tooth II 3-18, a meshing straight tooth III 3-19, a meshing straight tooth IV 3-20, a meshing straight tooth IV 3-21, a middle end outer frame 3-22, a straight tooth C, Side wall clamping rods 3-23 and side wall clamping rod push springs 3-24, an input motor 3-2 is fixedly connected with a fixed frame bottom plate 3-1, an input belt 3-3 is connected with an output shaft of the input motor 3-2, a first bracket 3-7, a second bracket 3-8, a third bracket 3-12 and a fourth bracket 3-13 are fixedly connected with the fixed frame bottom plate 3-1, a first rotating shaft 3-4 is rotatably connected with the first bracket 3-7 and the second bracket 3-8, a second rotating shaft 3-15 is rotatably connected with the third bracket 3-12 and the fourth bracket 3-13, a third driving disk 3-14 and a fourth driving disk 3-16 are fixedly connected with the second rotating shaft 3-15, a first driving disk 3-5 and a second driving disk 3-6 are fixedly connected with the first rotating shaft 3-4, a side wall boss 3-9 is fixedly connected with the fixed frame bottom plate 3-1, the hollow-out grooves 3-10 are arranged on the side wall bosses 3-9, the clamping grooves 3-11 are connected with the hollow-out grooves 3-10, the first meshing straight teeth 3-17 are connected with the second rotating shafts 3-15 in a matching mode, the second meshing straight teeth 3-18 are connected with the first rotating shafts 3-4 in a matching mode, the first meshing straight teeth 3-17 are in meshing transmission with the second meshing straight teeth 3-18, the first meshing straight teeth 3-17 and the second meshing straight teeth 3-18 are in rotating connection with the middle end outer frames 3-22, the third meshing straight teeth 3-19 are connected with the second rotating shafts 3-15 in a matching mode, the fifth meshing straight teeth 3-21 are in matching connection with the first rotating shafts 3-4, the third meshing straight teeth 3-19, the fourth meshing straight teeth 3-20, the fifth meshing straight teeth 3-21 are in rotating connection with the middle end outer frames 3-22, the third meshing straight teeth 3-19 are in meshing transmission with the fourth meshing straight, the fourth meshing straight teeth 3-20 are in meshing transmission with the fifth meshing straight teeth 3-21, the side wall clamping rods 3-23 are in sliding connection with the middle-end outer frame 3-22, the side wall clamping rod push springs 3-24 are in sleeve connection with the side wall clamping rods 3-23, the side wall clamping rod push springs 3-24 are arranged between the middle-end outer frame 3-22 and the side wall bosses 3-9, the second rotating shafts 3-15 are fixedly connected with the clutch rod limiting plates 2-9, and the input belts 3-3 are in matching connection with the first rotating shafts 3-4.
The fifth concrete implementation mode:
the embodiment is described below with reference to fig. 1-11, and the embodiment further describes the first embodiment, where the underframe assembly 4 includes an underframe bottom plate 4-1, an underframe first 4-2, an underframe second 4-3, a connecting belt second 4-4, a bevel gear shaft first 4-5, a transmission bevel gear first 4-6, a transmission bevel gear second 4-7, the underframe first 4-2 and the underframe second 4-3 are fixedly connected with the underframe bottom plate 4-1, the connecting belt second 4-4 is connected with the bevel gear shaft first 4-5 in a matching manner, the bevel gear shaft first 4-5 is rotatably connected with the underframe second 4-3, the transmission bevel gear first 4-6 is fixedly connected with the bevel gear shaft first 4-5, the transmission bevel gear second 4-7 is in a meshing transmission with the bevel gear shaft first 4-5, the transmission bevel gear second 4-7 is fixedly connected with a lower end sleeve 1-9, the lower end sleeve 1-9 is rotationally connected with the first underframe rod 4-2, the fixed frame bottom plate 3-1 is fixedly connected with the bottom underframe bottom plate 4-1, the first clutch rod 2-7 is connected with the second connecting belt 4-4 in a matching way, and the first clutch rod 2-7 is rotationally connected with the second underframe rod 4-3.
The sixth specific implementation mode:
the following describes the present embodiment with reference to fig. 1-11, and the present embodiment further describes the first embodiment, wherein the hollow assembly 5 includes a hollow outer frame 5-1, a hollow boss 5-2, a hollow upper frame 5-3, a hollow knife 5-4, a hollow sleeve 5-5, a hollow push spring 5-6, an inner end clamping bar 5-7, an inner slide column 5-8, an inner slide column sleeve spring 5-9, a hollow boss 5-2 fixedly connected to the hollow outer frame 5-1, a hollow upper frame 5-3 slidably connected to the hollow outer frame 5-1, a hollow sleeve 5-5 fixedly connected to the hollow upper frame 5-3, a hollow knife 5-4 slidably connected to the hollow sleeve 5-5, a hollow push spring 5-6 disposed between the hollow knife 5-4 and the hollow upper frame 5-3, the inner side sliding column 5-8 is fixedly connected with the hollowed upper frame 5-3, the inner side sliding column sleeve spring 5-9 is connected with the inner side sliding column 5-8 in a sleeved mode, the inner end clamping rod 5-7 is connected with the inner side sliding column 5-8 in a sliding mode, the inner end clamping rod 5-7 is connected with the hollowed boss 5-2 in a matched mode, and the hollowed outer frame 5-1 is fixedly connected with the matching groove 2-2;
the position of the hollow can be adjusted according to actual conditions, the inner end clamping rod 5-7 is pushed manually, the inner end clamping rod 5-7 is separated from the hollow boss 5-2, the hollow upper frame 5-3 is slid manually along the hollow outer frame 5-1, the position of the hollow knife 5-4 is changed, and the position of the hollow can be adjusted.
The invention relates to an unmanned aerial vehicle wing shaft hollowing device, which has the working principle that:
when the unmanned aerial vehicle wing shaft fixing device is used, the unmanned aerial vehicle wing shaft needing hollowing processing is placed on the bearing frames 1-3, the bearing frames 1-3 are pushed to move downwards along the outer end underframe 1-1 under the action of the gravity of the unmanned aerial vehicle wing shaft, meanwhile, the fixing rods 1-4 are simultaneously turned inwards through the driving of the bearing frames 1-3, meanwhile, the side wall supports 1-10 are simultaneously slid inwards along the trapezoidal sliding grooves 1-2 through the driving of the hinge columns 1-5, the fixing rods 1-4 are prevented from being simultaneously turned inwards to generate functional interference, and when the fixing rods 1-4 are in contact with the unmanned aerial vehicle wing shaft, the fixing of the unmanned aerial vehicle wing shaft is further completed; in order to adapt to unmanned aerial vehicle wing shafts of different specifications, the degrees of downward movement of the bearing frame 1-3 along the outer end underframe 1-1 are different due to different gravity of the unmanned aerial vehicle wing shafts of different specifications, and meanwhile, the degrees of compression of the inner end push springs 1-7 compressed along the inner end sliding columns 1-6 through the hinge columns 1-5 are different, so that the fixed rods 1-4 are different in turnover degree towards the inner side of the outer end underframe 1-1 at the same time, and further the fixed rods 1-4 are convenient to adapt to the unmanned aerial vehicle wing shafts of different specifications; the input motor 3-2 is started, the first rotating shaft 3-4 is driven to rotate by the input belt 3-3, the first driving disk 3-5 and the second driving disk 3-6 are driven to rotate simultaneously, the initial position of the middle-end outer frame 3-22 is shown in figure 7, the second driving disk 3-6 is driven to rotate, simultaneously, the second driving disk 3-6 is in fit connection with the fifth meshing straight tooth 3-21 by the second driving disk 3-6, the fifth meshing straight tooth 3-21 is driven to rotate, the third meshing straight tooth 3-19 is driven to rotate by the fourth meshing straight tooth 3-20, the third meshing straight tooth 3-19 is in fit connection with the fourth driving disk 3-16, the second rotating shaft 3-15 is driven to rotate, the clutch lever limiting plate 2-9 is driven to rotate, and the second clutch lever 2-8 is in fit connection with the third clutch lever 2-10, the first clutch rod 2-7 is driven to rotate, the second hinge connecting rod 2-6 drives the second hinge slider 2-5 to move, the second hinge slider 2-5 drives the transverse sliding frame body 2-1 to move through the adjusting threaded rod 2-4, the matching groove 2-2 and the lower end sleeve 1-9 slide relative to one side of the lower end sleeve 1-9, the middle end outer frame 3-22 is manually pushed, the side wall clamping rod 3-23 is driven to slide along the hollow groove 3-10 through the middle end outer frame 3-22, the side wall clamping rod 3-23 is connected with the other clamping groove 3-11 in a matching way, the third meshing straight tooth 3-19 is separated from the fourth driving disk 3-16, and the third driving disk 3-14 is connected with the first meshing straight tooth 3-17 in a matching way, simultaneously, the second driving disk 3-6 is separated from the fifth meshing straight teeth 3-21, the second meshing straight teeth 3-18 are matched and connected with the first driving disk 3-5, when the second meshing straight teeth 3-18 drive the first meshing straight teeth 3-17 to rotate, the first meshing straight teeth 3-17 drive the third driving disk 3-14 to rotate, the second rotating shaft 3-15 is driven to rotate, the second rotating shaft 3-15 reversely rotates, the matching groove 2-2 and the lower end sleeve 1-9 relatively slide to the other side of the lower end sleeve 1-9 through the transmission relation, the hollow outer frame 5-1 is driven to move along with the transverse sliding frame body 2-1 through the driving of the transverse sliding frame body 2-1, when the matching groove 2-2 and the lower end sleeve 1-9 relatively slide to one side of the lower end sleeve 1-9, the method comprises the steps that a hollow knife 5-4 on a hollow outer frame 5-1 on one side of a transverse sliding frame body 2-1 is made to be in contact with an unmanned aerial vehicle wing shaft, machining is completed, when a matching groove 2-2 and a lower end sleeve 1-9 slide relatively towards the other side of the lower end sleeve 1-9, the hollow knife 5-4 on the hollow outer frame 5-1 on the other side of the transverse sliding frame body 2-1 is made to be in contact with the unmanned aerial vehicle wing shaft, machining is completed, and machining efficiency is improved conveniently; the position of the hollow can be adjusted according to actual conditions, the inner end clamping rod 5-7 is pushed manually, the inner end clamping rod 5-7 is separated from the hollow boss 5-2, the hollow upper frame 5-3 is slid manually along the hollow outer frame 5-1, the position of the hollow knife 5-4 is changed, and the position of the hollow can be adjusted.
Of course, the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and variations can be made by those skilled in the art within the spirit and scope of the present invention; modifying; and the addition or the replacement also belongs to the protection scope of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle wing axle fretwork equipment, includes axle mount (1), horizontal balladeur train assembly (2), mount assembly (3), chassis assembly (4), fretwork assembly (5), its characterized in that: the shaft fixing frame (1) is connected with the bottom frame assembly (4), the transverse sliding frame assembly (2) is connected with the bottom frame assembly (4), the fixing frame assembly (3) is connected with the transverse sliding frame assembly (2), and the hollow-out assembly (5) is connected with the transverse sliding frame assembly (2).
2. The unmanned aerial vehicle wing shaft hollowing out equipment of claim 1, wherein: the shaft fixing frame (1) comprises an outer end underframe (1-1), a trapezoid sliding chute (1-2), a bearing frame (1-3), a fixing rod (1-4), a hinged column (1-5), an inner end sliding column (1-6), an inner end push spring (1-7), a matching waist groove (1-8), a lower end sleeve (1-9) and a side wall support (1-10), wherein the trapezoid sliding chute (1-2) is arranged on the outer end underframe (1-1), the bearing frame (1-3) is in sliding connection with the outer end underframe (1-1), the side wall support (1-10) is in sliding connection with the trapezoid sliding chute (1-2), the fixing rod (1-4) is in hinged connection with the hinged column (1-5), the hinged column (1-5) is in sliding connection with the inner end sliding column (1-6), the inner end sliding columns (1-6) are fixedly connected with the side wall supports (1-10), the inner end push springs (1-7) are connected with the inner end sliding columns (1-6) in a sleeved mode, the fixed rods (1-4) are hinged to the bearing frames (1-3), the lower end sleeves (1-9) are fixedly connected with the outer end bottom frames (1-1), and the matching waist grooves (1-8) are arranged on the fixed rods (1-4).
3. The unmanned aerial vehicle wing shaft hollowing out equipment of claim 1, wherein: the transverse sliding frame assembly (2) comprises a transverse sliding frame body (2-1), a matching groove (2-2), a side wall hinge rod (2-3), an adjusting threaded rod (2-4), a hinge slider (2-5), a hinge connecting rod (2-6), a clutch rod I (2-7), a clutch rod II (2-8), a clutch rod limiting plate (2-9), a clutch rod III (2-10) and a clutch rod push spring (2-11), the matching groove (2-2) is arranged on the transverse sliding frame body (2-1), the side wall hinge rod (2-3) is hinged with the transverse sliding frame body (2-1), the adjusting threaded rod (2-4) is rotatably connected with the side wall hinge rod (2-3), the hinge slider (2-5) is slidably connected with the side wall hinge rod (2-3), the hinged slider (2-5) is in threaded connection with the adjusting threaded rod (2-4), the hinged connecting rod (2-6) is in hinged connection with the hinged slider (2-5), the hinged connecting rod (2-6) is in hinged connection with the clutch rod I (2-7), the clutch rod I (2-7) is fixedly connected with the clutch rod II (2-8), the clutch rod II (2-8) is in matched connection with the clutch rod III (2-10), the clutch rod III (2-10) is in sliding connection with the clutch rod limiting plate (2-9), the clutch rod push spring (2-11) is arranged between the clutch rod III (2-10) and the clutch rod limiting plate (2-9), and the lower end sleeve (1-9) is in matched connection with the matching groove (2-2).
4. The unmanned aerial vehicle wing shaft hollowing out equipment of claim 1, wherein: the fixing frame assembly (3) comprises a fixing frame bottom plate (3-1), an input motor (3-2), an input belt (3-3), a rotating shaft I (3-4), a driving disc I (3-5), a driving disc II (3-6), a bracket I (3-7), a bracket II (3-8), a side wall boss (3-9), a hollow groove (3-10), a clamping groove (3-11), a bracket III (3-12), a bracket IV (3-13), a driving disc III (3-14), a rotating shaft II (3-15), a driving disc IV (3-16), a meshing straight tooth I (3-17), a meshing straight tooth II (3-18), a meshing straight tooth III (3-19), a meshing straight tooth IV (3-20), a meshing straight tooth V (3-21) and a straight tooth I (3-17), Middle end outer frame (3-22), side wall clamping rod (3-23), side wall clamping rod push spring (3-24), input motor (3-2) is fixedly connected with fixed frame bottom plate (3-1), input belt (3-3) is connected with output shaft of input motor (3-2), support I (3-7), support II (3-8), support III (3-12), support IV (3-13) is fixedly connected with fixed frame bottom plate (3-1), rotary shaft I (3-4) is rotatably connected with support I (3-7), support II (3-8), rotary shaft II (3-15) is rotatably connected with support III (3-12), support IV (3-13), drive disk III (3-14), drive disk IV (3-16) is fixedly connected with rotary shaft II (3-15), a first driving disk (3-5), a second driving disk (3-6) and a first rotating shaft (3-4) are fixedly connected, a side wall boss (3-9) and a bottom plate (3-1) of a fixed frame are fixedly connected, hollow grooves (3-10) are arranged on the side wall boss (3-9), clamping grooves (3-11) are connected with the hollow grooves (3-10), a first meshing straight tooth (3-17) is connected with a second rotating shaft (3-15) in a matching way, a second meshing straight tooth (3-18) is connected with a first rotating shaft (3-4) in a matching way, the first meshing straight tooth (3-17) is in meshing transmission with a second meshing straight tooth (3-18), the first meshing straight tooth (3-17) and the second meshing straight tooth (3-18) are rotationally connected with a middle-end outer frame (3-22), a third meshing straight tooth (3-19) is connected with the second rotating shaft (3-15) in a matching way, five meshing straight teeth (3-21) are matched and connected with the first rotating shaft (3-4), three meshing straight teeth (3-19), four meshing straight teeth (3-20), five meshing straight teeth (3-21) are rotationally connected with the middle-end outer frame (3-22), three meshing straight teeth (3-19) are in meshing transmission with four meshing straight teeth (3-20), four meshing straight teeth (3-20) are in meshing transmission with five meshing straight teeth (3-21), side wall clamping rods (3-23) are in sliding connection with the middle-end outer frame (3-22), side wall clamping rod push springs (3-24) are in sleeved connection with the side wall clamping rods (3-23), the side wall clamping rod push springs (3-24) are arranged between the middle-end outer frame (3-22) and the side wall bosses (3-9), the second rotating shaft (3-15) is fixedly connected with clutch rod limiting plates (2-9), the input belt (3-3) is connected with the first rotating shaft (3-4) in a matching way.
5. The unmanned aerial vehicle wing shaft hollowing out equipment of claim 1, wherein: the underframe assembly (4) comprises an underframe bottom plate (4-1), an underframe rod I (4-2), an underframe rod II (4-3), a connecting belt II (4-4), a bevel gear shaft I (4-5), a transmission bevel gear I (4-6) and a transmission bevel gear II (4-7), wherein the underframe rod I (4-2), the underframe rod II (4-3) and the underframe bottom plate (4-1) are fixedly connected, the connecting belt II (4-4) is matched and connected with the bevel gear shaft I (4-5), the bevel gear shaft I (4-5) is rotatably connected with the underframe rod II (4-3), the transmission bevel gear I (4-6) is fixedly connected with the bevel gear shaft I (4-5), the transmission bevel gear II (4-7) is meshed and transmitted with the bevel gear shaft I (4-5), the transmission bevel gear II (4-7) is fixedly connected with a lower end sleeve (1-9), the lower end sleeve (1-9) is rotationally connected with the first underframe rod (4-2), the fixed frame bottom plate (3-1) is fixedly connected with the bottom underframe bottom plate (4-1), the first clutch rod (2-7) is connected with the second connecting belt (4-4) in a matching way, and the first clutch rod (2-7) is rotationally connected with the second underframe rod (4-3).
6. The unmanned aerial vehicle wing shaft hollowing out equipment of claim 1, wherein: the hollow assembly (5) comprises a hollow outer frame (5-1), a hollow boss (5-2), a hollow upper frame (5-3), a hollow knife (5-4), a hollow sleeve (5-5), a hollow push spring (5-6), an inner end clamping rod (5-7), an inner side sliding column (5-8) and an inner side sliding column sleeve spring (5-9), the hollow boss (5-2) is fixedly connected with the hollow outer frame (5-1), the hollow upper frame (5-3) is in sliding connection with the hollow outer frame (5-1), the hollow sleeve (5-5) is fixedly connected with the hollow upper frame (5-3), the hollow knife (5-4) is in sliding connection with the hollow sleeve (5-5), and the hollow push spring (5-6) is arranged between the hollow knife (5-4) and the hollow upper frame (5-3), the inner side sliding column (5-8) is fixedly connected with the hollowed upper frame (5-3), the inner side sliding column sleeve spring (5-9) is connected with the inner side sliding column (5-8) in a sleeved mode, the inner end clamping rod (5-7) is connected with the inner side sliding column (5-8) in a sliding mode, the inner end clamping rod (5-7) is connected with the hollowed boss (5-2) in a matched mode, and the hollowed outer frame (5-1) is fixedly connected with the matching groove (2-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911375584.XA CN111036992B (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle wing shaft fretwork equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911375584.XA CN111036992B (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle wing shaft fretwork equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111036992A true CN111036992A (en) | 2020-04-21 |
| CN111036992B CN111036992B (en) | 2021-06-22 |
Family
ID=70240595
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911375584.XA Active CN111036992B (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle wing shaft fretwork equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111036992B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111453317A (en) * | 2020-04-29 | 2020-07-28 | 于子江 | Intelligent carrying equipment |
| CN111498155A (en) * | 2020-04-29 | 2020-08-07 | 刘金友 | Medical capsule canning equipment |
| CN111974505A (en) * | 2020-08-13 | 2020-11-24 | 惠安县崇武镇婉云广告设计中心 | Construction waste treatment device |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070107541A1 (en) * | 2005-11-14 | 2007-05-17 | John Cannon | Low Horsepower Transmission |
| CN105215398A (en) * | 2015-09-29 | 2016-01-06 | 重庆盛镁镁业有限公司 | Circumference porous rotary work piece drilling equipment |
| CN105798351A (en) * | 2016-05-20 | 2016-07-27 | 湖州科达化工燃料有限公司 | Improved four-head drilling machine |
| CN206845808U (en) * | 2017-07-10 | 2018-01-05 | 三峡大学 | A kind of automatic reversing apparatus |
| CN207043370U (en) * | 2017-04-06 | 2018-02-27 | 安吉伟誉家具有限公司 | A kind of adaptive bench drill |
| CN109108384A (en) * | 2018-09-18 | 2019-01-01 | 张树林 | A kind of fixed cutting apparatus of factory |
| CN110014315A (en) * | 2019-05-16 | 2019-07-16 | 徐旭东 | A kind of self-centering self-locking jig of gravity |
| CN209552812U (en) * | 2018-12-29 | 2019-10-29 | 天津市金丞泰节能建材科技有限公司 | Turnover device is used in a kind of hollow hollowed-out board processing |
-
2019
- 2019-12-27 CN CN201911375584.XA patent/CN111036992B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070107541A1 (en) * | 2005-11-14 | 2007-05-17 | John Cannon | Low Horsepower Transmission |
| CN105215398A (en) * | 2015-09-29 | 2016-01-06 | 重庆盛镁镁业有限公司 | Circumference porous rotary work piece drilling equipment |
| CN105798351A (en) * | 2016-05-20 | 2016-07-27 | 湖州科达化工燃料有限公司 | Improved four-head drilling machine |
| CN207043370U (en) * | 2017-04-06 | 2018-02-27 | 安吉伟誉家具有限公司 | A kind of adaptive bench drill |
| CN206845808U (en) * | 2017-07-10 | 2018-01-05 | 三峡大学 | A kind of automatic reversing apparatus |
| CN109108384A (en) * | 2018-09-18 | 2019-01-01 | 张树林 | A kind of fixed cutting apparatus of factory |
| CN209552812U (en) * | 2018-12-29 | 2019-10-29 | 天津市金丞泰节能建材科技有限公司 | Turnover device is used in a kind of hollow hollowed-out board processing |
| CN110014315A (en) * | 2019-05-16 | 2019-07-16 | 徐旭东 | A kind of self-centering self-locking jig of gravity |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111453317A (en) * | 2020-04-29 | 2020-07-28 | 于子江 | Intelligent carrying equipment |
| CN111498155A (en) * | 2020-04-29 | 2020-08-07 | 刘金友 | Medical capsule canning equipment |
| CN111974505A (en) * | 2020-08-13 | 2020-11-24 | 惠安县崇武镇婉云广告设计中心 | Construction waste treatment device |
| CN111974505B (en) * | 2020-08-13 | 2022-08-05 | 台成环保科技股份有限公司 | Construction waste treatment device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111036992B (en) | 2021-06-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111036992B (en) | Unmanned aerial vehicle wing shaft fretwork equipment | |
| CN111619847B (en) | Sealing washer equipment for packing | |
| CN107972128B (en) | Bamboo wood toy processing is with rough plane device | |
| CN115179113B (en) | Novel polishing device for glass polishing disc | |
| CN213749116U (en) | Suspension fatigue test testing device | |
| CN113304804A (en) | Mineral secondary processing equipment | |
| CN112959415A (en) | Punching equipment of automobile tire V-belt model | |
| CN110587039B (en) | Industrial robot gear equipment | |
| CN112657405A (en) | Feed mixing device | |
| CN212468760U (en) | Organic-coated nano-aluminum-coated particle preparation auxiliary equipment | |
| CN110638583B (en) | Automatic wheelchair for pediatric rehabilitation | |
| CN113084263A (en) | Tube bore line processing device | |
| CN110576211A (en) | machining device for industrial robot main shaft | |
| CN112916103B (en) | Earphone charging box recovery equipment | |
| CN111590283A (en) | Inside fretwork equipment of engineering device | |
| CN216057152U (en) | Portable voice communication data analysis equipment | |
| CN111282648A (en) | Processing apparatus of waste material for building | |
| CN112172964A (en) | High-end equipment manufacturing and packaging equipment | |
| CN213064475U (en) | Safety damping device of sealing test bed | |
| CN205764969U (en) | A kind of arrangements for automotive doors side drilling equipment | |
| CN217918156U (en) | Connecting structure of semitrailer carriage | |
| CN112691750B (en) | Computer material recovery unit | |
| CN220515491U (en) | Drilling device for mechanical accessory production | |
| CN218225565U (en) | Planet carrier boring fixing tool | |
| CN214086513U (en) | Shopping platform is with transportation robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210527 Address after: 362000 No.50 Daxin north, Daxin village, Taozhou Township, Anxi County, Quanzhou City, Fujian Province Applicant after: Xu Qionghua Address before: 516830 Dajiang UAV, 103 Huancheng East Road, Longmen County, Huizhou City, Guangdong Province Applicant before: Yang Xiaojun |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |