CN206125461U - Gate is adorned behind aircraft, unload work platform - Google Patents
Gate is adorned behind aircraft, unload work platform Download PDFInfo
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- CN206125461U CN206125461U CN201620933101.9U CN201620933101U CN206125461U CN 206125461 U CN206125461 U CN 206125461U CN 201620933101 U CN201620933101 U CN 201620933101U CN 206125461 U CN206125461 U CN 206125461U
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Abstract
The utility model discloses a gate is adorned behind aircraft, unload work platform, main including transferring appearance platform and bracket assembly, transfer the appearance platform including the AGV dolly, platform base and a plurality of posture adjusting mechanisms that assemble in proper order, the height -adjustable of AGV dolly, posture adjusting mechanisms liftable and horizontal migration, bracket assembly connect be used for placing the aircraft in posture adjusting mechanisms's upper end after the gate, bracket assembly can rotate around each posture adjusting mechanisms's upper end. Realize the location of work platform position and the adjustment of height through the AGV dolly, planar motion and elevating movement cooperation through each posture adjusting mechanisms of connecting on the platform base realize work platform upper end bracket assembly angular adjustment and front and back angular adjustment about to realize the roll upset and the every single move upset at back gate, smooth installation and the dismantlement that realizes the back gate. Whole installation and the process of dismantlement staff's dependent manual operation is little. The roll upset and the every single move upset at back gate are all gone on through the work platform automation, and the structural performance at later gate can not be influenced.
Description
Technical field
This utility model is related to a kind of installation and removal equipment at gate after aircraft, and in particular to gate after a kind of aircraft
Loading, unloading work platformses.
Background technology
Generally, rear gate overall dimensions are about 4180 × 3078mm or so, weight 384.5Kg, and loading end is smooth flying
Machine lead-covering.Periphery design has hollow sealing rubber strip band.Afterwards gate is connected at hinge 2 with fuselage, and type of attachment is single ears
Joint, connecting hole version is strip hole.General assembly big part docking after the completion of need dismounting after gate, carry out system install adjust
Examination.Due to rear gate transverse design size, to compare side crossbeam aperture design size big.So, rear gate is removing and installing process
Rollover is required to, is that gate is installed after satisfaction, then rear gate needs laterally to overturn.At present after general assembly the dismounting at gate mainly according to
By hanging, upset relies primarily on personnel's counterweight, and single ears joint docking is promoted by least 4 people and helped, and stability is excessively poor,
When often result in rear gate periphery hollow seal rubber strip and damage and scrap, the serious quality problems such as construction machine is damaged.
Utility model content
The purpose of this utility model is to provide a kind of work that substantially can automatically mount and dismount gate after aircraft to put down
Platform, using gate after the work platformses installation and removal structural behaviour at gate after aircraft is not affected.
Loading, unloading work platformses in gate after this aircraft that this utility model is provided, mainly include posture adjustment platform and bracket group
Part, posture adjustment platform includes AGV dollies, platform base and some pose_adjusters for assembling successively, and the height adjustable of AGV dollies is adjusted
Appearance mechanism liftable and move horizontally, carriage assembly is connected to the upper end of pose_adjuster to be used to place gate after aircraft, bracket group
Part can be rotated around the upper end of each pose_adjuster.
The AGV dollies, mainly including rectangle frame, four groups of road wheels and its driving means, deployable and folding liter
Come down to a lower group the power set of part, lifting assembly, four groups of road wheels and its driving means are installed on rectangle frame by support respectively
Four corners outside, lifting assembly includes linkage and the rectangular slab of its upper end, and power set are arranged in rectangle frame and square
Between shape plate, linkage launches when power set promote rectangular slab to rise, when power set drive non-rectangle plate to decline, connecting rod
Mechanism folds draws in.Power set using two heavily loaded Electrohydraulic push rods, by two heavily loaded Electrohydraulic push rods be arranged in rectangle frame and
On the length direction median plane of rectangular slab；The surrounding of AGV dollies is disposed with the soft of noncontact obstacle detection and software self diagnosis
Emergency stop device.
The platform base includes the frame body of the cuboid surrounded by square tube and is connected to the rectangular of frame body corner
The link of the bodily form；Frame body is connected to the upside of the rectangular slab, and its upper frame upper surface laying walkway board, its surrounding is connected with
Guard rail and coaming plate；The upper end of link is stretched out in outside walkway board, section of stretching out surrounding closures；Link has higher connection
Two kinds of frame and relatively low link, they are respectively arranged two vertex angle parts of longitudinal direction in frame body, and the upper end of each link connects respectively
Rectangular mounting plate is connected to, there are two pieces of bar blocks being longitudinally arranged along frame body on rectangular mounting plate, have rectangle between two bar blocks
Hole.Telescopic ladder is connected with the underframe of frame body.
The pose_adjuster has four sets of the first pose_adjuster to the 4th pose_adjuster, often covers pose_adjuster flat including two groups
Longitudinal line slideway, two groups of horizontal line slideways being arranged in parallel and a screw lift that row is arranged；Longitudinal line slideway
It is fixed in the bar blocks, two ends are connected with end plate, are fixed on rectangular mounting plate on the downside of end plate；On longitudinal line slideway
Slide block be connected with sliding panel, horizontal line slideway is connected in parallel on sliding panel, on sliding panel correspondence two horizontal line slideways
Between have rectangular opening；Screw lift is connected as a single entity by installing plate with the slide block on horizontal line slideway, screw lift
Shaft lower end passes through from the rectangular opening of sliding panel and rectangular mounting plate, and the upper end of the screw mandrel of shaft upper end connection is connected with ball
Head, its power set adopt servomotor.
First pose_adjuster is connected on one of them higher link, and also including two servomotors, they divide
Vertical and horizontal ball screw is not connected with by diaphragm type servo shaft coupling and forms vertical and horizontal driving means respectively, longitudinal direction
Nut on ball screw is connected as a single entity by nut seat with the sliding panel, and the nut on transverse ball lead screw passes through nut seat
It is connected as a single entity with the installing plate of the screw lift, the rotary motion of longitudinal ball screw drives screw mandrel lifting by sliding panel
Machine is moved horizontally along longitudinal line slideway, the rotational movement screw lift of transverse ball lead screw transversely line slideway water
Translation is dynamic.
Second pose_adjuster is connected on another higher link, and also including a servomotor, it is by thin
Membrane type servo shaft coupling is connected with longitudinal ball screw and forms longitudinal driving device, and the nut on longitudinal ball screw passes through nut
Seat is connected as a single entity with the sliding panel, and the rotary motion of longitudinal ball screw drives screw lift straight along longitudinal direction by sliding panel
Line guide rail is moved horizontally.
3rd pose_adjuster is connected on one of them relatively low link, and with first pose_adjuster platform is located at
Longitudinal two ends of base frames support body, the 3rd pose_adjuster also includes a servomotor, and it is connected by diaphragm type servo shaft coupling
It is connected to transverse ball lead screw and forms lateral driver device, the nut on transverse ball lead screw is lifted by nut seat with the screw mandrel
The installing plate of machine is connected as a single entity, and the rotational movement screw lift of transverse ball lead screw transversely move by line slideway level
It is dynamic.
The carriage assembly includes bracket, connecting seat, adpting flange, ball cup and the locating piece of rectangle, and bracket is by side
The rectangle support body that pipe is surrounded, connecting seat is arranged at the downside of rectangle support body, and adpting flange and ball cup are sequentially connected to connecting seat
Downside, locating piece is connected in the slotted hole on bracket by connecting screw rod and locking nut；The ball of screw lift screw mandrel
Head can be rotated in ball cup connection, ball cup around bulb.There is a divider longitudinal one end of bracket, the inner side of divider and bracket
Horizontal skeleton upper surface posts rubber strip.
This utility model realizes the positioning of work-table position and the adjustment of height by AGV dollies, by platform base
The plane motion of each pose_adjuster of upper connection and elevating movement coordinate the left and right angle for realizing work platformses upper end carriage assembly
Adjustment and front and rear angles adjustment, so as to the rolling flip at gate after realizing and pitching overturn, after smoothly realizing the installation at gate and
Dismounting.The manual operation of whole installation and removal process staff seldom, need to only fix rear gate and bracket and and aircraft
Main body is connected.The rolling flip at gate and pitching upset afterwards is all carried out automatically by work platformses, later gate knot
Structure performance will not be impacted.
Description of the drawings
Fig. 1 is the structural representation of this utility model one embodiment.
Fig. 2 is the left view schematic diagram of Fig. 1.
Fig. 3 is the axle geodesic structure schematic diagram of the present embodiment.
Fig. 4 is the structural representation that AGV dollies lift state in Fig. 1.
Fig. 5 is the axle side structure schematic diagram of posture adjustment platform base in Fig. 1.
Fig. 6 is the configuration schematic diagram of the first pose_adjuster in Fig. 1.
Fig. 7 is the configuration schematic diagram of the second pose_adjuster in Fig. 1.
Fig. 8 is the configuration schematic diagram of the 3rd pose_adjuster in Fig. 1.
Fig. 9 is the configuration schematic diagram of the 4th pose_adjuster in Fig. 1.
Figure 10 is the configuration schematic diagram of carriage assembly in Fig. 1.
Specific embodiment
As shown in Figures 1 to 4, loading, unloading work platformses in gate after this aircraft that the present embodiment is provided, mainly including posture adjustment
Platform and carriage assembly, posture adjustment platform includes that the AGV dollies 1 for assembling successively, the pose_adjuster 3, second of platform base 2 and first are adjusted
Appearance mechanism 4, the 3rd pose_adjuster 5 and the 4th pose_adjuster 6, carriage assembly 7 is connected to the upper end of each pose_adjuster, big after aircraft
Door 8 is fixed on bracket group valency 7.
As shown in Figures 1 to 4, AGV dollies 1 mainly include 11, four groups of road wheels of rectangle frame and its driving means 12, rise
The heavily loaded Electrohydraulic push rod 14 of part 13, two of coming down to a lower group.Rectangle frame 11 is surrounded by square tube, and four groups of road wheels and its driving means 12 are distinguished
Four corners outside of rectangle frame 11 is installed on by support.Lifting assembly 13 includes linkage 131 and is attached to
The rectangular slab 132 at end, two heavily loaded Electrohydraulic push rods 14 are arranged in the length direction median plane of rectangle frame 11 and rectangular slab 132
On.Linkage 131 launches when heavily loaded Electrohydraulic push rod 14 promotes rectangular slab 132 to rise, and heavily loaded Electrohydraulic push rod 14 drives rectangular slab
During 132 decline, linkage 131 is folded and drawn in.Road wheel and its driving means 12 make whole AGV dollies 1 can any direction move
Dynamic, Arbitrary Rotation.The height adjustment of whole work platformses is realized by heavily loaded Electrohydraulic push rod 14 and lifting assembly 13, heavily loaded
When by 132 jacking of rectangular slab, platform base 2 and pose_adjuster and carriage assembly 7 rise Electrohydraulic push rod 14 simultaneously.
After AGV dollies are assembled, in its surrounding arrangement noncontact obstacle detection and the soft jerk dress of software self diagnosis
Put -- manual scram button, to play a part of anticollision and jerk.
As shown in figure 5, platform base 2 includes the frame body 21 of the cuboid surrounded by square tube and is connected to frame body four
The link of the cuboid at angle.Link is divided into two higher links 22 and two relatively low links 23, higher and relatively low
Link is respectively arranged two vertex angle parts of longitudinal direction in frame body 21, and the upper end of each link has horizontally disposed rectangle to install
Plate JXB, the both sides of rectangular mounting plate have been longitudinally arranged bar blocks TXB along frame body 21, two bar blocks of correspondence on rectangular mounting plate
Between have rectangular opening.
As shown in Figures 1 to 5, frame body 21 be formed around guard rail and coaming plate, upper surface are equipped with walkway board.Respectively connect
Connect frame and stretch out the surrounding of walkway board section and be equipped with coaming plate.Telescopic ladder TZ, ladder TZ are connected with the underframe of frame body 21
Positioned at the longitudinal middle part of frame body 21.
As shown in Figures 1 to 5, four pose_adjusters have identical structure also to have different structure, connect on two higher links
What is connect is the first pose_adjuster 3 and the 3rd pose_adjuster 5, and what is connected on relatively low link is the second pose_adjuster 4 and the 4th tune
Appearance mechanism 6, wherein the first pose_adjuster 3 and the second pose_adjuster 4 are located at the side of the longitudinal direction of frame body 21, the 3rd pose_adjuster 5
With the opposite side that the 4th pose_adjuster 6 is located at the longitudinal direction of frame body 21.
As shown in Figures 6 to 9, each pose_adjuster is put down including two groups of longitudinal line slideway ZXDG being arranged in parallel, two groups
The horizontal line slideway HXDG and a screw lift SGSJ of row arrangement.Longitudinal line slideway ZXDG and horizontal line slideway
The two ends of HXDG are connected with end plate DB, are connected to two on line slideway ZXDG and horizontal line slideway HXDG longitudinally in each
Slide block HK.Slide block HK on longitudinal line slideway ZXDG is connected with sliding panel HDB, and horizontal line slideway HXDG passes through sliding panel
Strip connecting plate on HDB is connected, and has rectangular opening between two horizontal line slideway HXDG of correspondence on sliding panel HDB.Screw mandrel
Elevator SGSJ is connected as a single entity by installing plate AZB with the slide block HK on horizontal line slideway HXDG, screw lift SGSJ's
Shaft lower end passes through from the rectangular opening of sliding panel and rectangular mounting plate, and the upper end of the screw mandrel of shaft upper end connection is connected with bulb
QT.Screw lift SGSJ is driven using servomotor SFDJ.
As shown in fig. 6, the first pose_adjuster 3 also includes two servomotor SFDJ, they pass through respectively diaphragm type servo
Shaft coupling LZJ is connected with longitudinal ball screw ZXSG and transverse ball lead screw HXSG forms respectively vertical and horizontal driving means.
Nut LM on longitudinal ball screw ZXSG is connected as a single entity by nut seat LMZ with sliding panel HDB.On transverse ball lead screw HXSG
Nut LM be connected as a single entity with the installing plate of screw lift SGSJ by nut seat LMZ.Longitudinal ball screw and horizontal ball
Screw mandrel is also associated with bearing and bearing block ZCZ, bearing block be individually fixed on rectangular mounting plate and sliding panel on.Longitudinal ball wire
The rotary motion of bar drives screw lift to move horizontally along longitudinal line slideway by sliding panel, the rotation of transverse ball lead screw
Motion drives screw lift, and transversely line slideway is moved horizontally, to adjust the plan-position of screw lift.
As shown in fig. 7, the second pose_adjuster 4 also includes a servomotor SFDJ, it passes through diaphragm type servo shaft coupling
LZJ is connected with longitudinal ball screw ZXSG and forms longitudinal driving device, and the nut LM on longitudinal ball screw ZXSG passes through nut
Seat LMZ is connected as a single entity with the installing plate of screw lift SGSJ, and the rotary motion of longitudinal ball screw ZXSG passes through sliding panel band
Dynamic screw lift SGSJ is moved horizontally along longitudinal direction line slideway ZXDG.
As shown in figure 8, the 3rd pose_adjuster 5 also includes a servomotor SFDJ, it passes through diaphragm type servo shaft coupling
LZJ is connected with horizontal ball wire HXSG rods and is open into driving means, and the nut LM on transverse ball lead screw HXSG passes through nut
Seat LMZ is connected as a single entity with the mounting seat of screw lift SGSJ, the rotational movement screw mandrel lifting of transverse ball lead screw HXSG
Transversely line slideway HXDG is moved horizontally machine SGSJ.
As shown in figure 9, the 4th pose_adjuster 6 does not connect vertical and horizontal driving means.
As shown in Figures 6 to 9, each servomotor is respectively by diaphragm type servo shaft coupling LZJ and corresponding driving member
The transmission of motion is realized in connection.The screw lift driven by servomotor has that installing space is little, stroke length advantage, together
When can carry out accurate position and speed controlling.Servomotor drives the elevating movement of each screw mandrel to carry out angle tune to bracket
It is whole because bracket can wire winding rod upper end bulb rotate.
The outside of the horizontal line slideway of correspondence on the sliding panel of each pose_adjuster is can be seen that with reference to Fig. 3 and Fig. 6 to Fig. 9
It is connected with protective plate and surrounds rectangle with the end plate of fixed lateral line slideway.
As shown in Figure 10, carriage assembly 7 is main plays a part of to hold up, fix and position to rear gate, including rectangle
Bracket 71, connecting seat 72, adpting flange 73, ball cup 74 and locating piece 75.Bracket 71 is the rectangle support body surrounded by square tube, even
Joint chair 72 is arranged at the downside of bracket 71, and adpting flange 73 and ball cup 74 are sequentially connected to the downside of connecting seat 72, locating piece
75 are connected in the slotted hole on bracket 71 by connecting screw rod 76 and locking nut 77.There is divider longitudinal one end of bracket 71
78, the inner side of divider 78 and the horizontal skeleton upper surface of bracket 71 post rubber strip 79.Connecting screw rod 76 and locking nut 77 are used
Stability of the gate in switching process after the gate after being connected, rubber strip and divider guarantee.
As Fig. 1 is combined shown in Fig. 6 to Figure 10, the bulb QT of screw lift SGSJ screw mandrels upper end is connected with ball cup 74,
Ball cup 74 can be rotated around bulb QT, carriage assembly is arbitrarily rotated around the upper end of each screw lift.
Operation principle of the present utility model is as follows：The height change of AGV dolly lifting assemblies makes the support of platform base upper end
Frame group valency height respective change, makes whole work platformses reach suitable working depth.Four pose_adjusters have can be longitudinally and horizontal
To moving horizontally and oscilaltion, there is only vertical equity movement and lifting of reaching the standard grade, have only transverse horizontal movement and on
Lower lifting, also can only oscilaltion.Carriage assembly can lift arbitrarily angled turn of the bulb of upper screw rod upper end around each screw mandrel
It is dynamic, so the cooperation of horizontal movement and the elevating movement for passing through pose_adjuster, can make bracket angle and direction deflection on demand,
So as to the rolling flip at rear gate and pitching upset thereon.
It is as follows the step of gate after this work platforms dismounting aircraft：
（1）Remote control AGV dollies control the angle of pose_adjuster motion adjustment bracket to appointed place, turn over bracket pitching
Specified angle is gone to, the original state of the linkage of AGV dolly lifting assemblies is folded state, make lifting assembly in minimum
State；
（2）Control lifting assembly rises, gate after making bracket rise and hold up；
（3）Operator extract ladder out, climb up work platformses by the dovetail on gate after the connecting screw rod insertion on bracket
Lock in groove and with locking nut, make rear gate be linked to be an entirety with bracket；If on the dovetail groove and bracket on rear gate
Oval hole site it is inconsistent, can be moved horizontally being finely adjusted by controlling pose_adjuster；
（4）Connection member after operator's dismounting between gate and aircraft body；
（5）Control lifting assembly support the height that rear gate continuously rises to specify, and control pose_adjuster motion is big after making
15 ° of rolling flip of door；
（6）Control lifting assembly declines makes rear gate depart from aircraft body；
（7）The angle of control pose_adjuster motion adjustment bracket, makes the rear gate on bracket with step（5）Middle lowest point is in
Horizontality；
（8）Control AGV dollies are moved to the specified location in Factory Building.
The step of this work platforms installs gate after aircraft is as follows：
（1）Rear gate is positioned on bracket and is fixed at rear gate by the connecting screw rod and locking nut on bracket
It is good, then control AGV dollies and be moved to specific bit, the original state of the linkage of AGV dolly lifting assemblies is folded state,
Lifting assembly is set to be in minimum state；
（2）The angle of control pose_adjuster motion adjustment bracket, 15 ° of rolling flip again after making rear gate pitching overturn 23 °；
（3）Control lifting assembly rises, and makes rear gate rise to aircraft the inside；
（4）The angle of control pose_adjuster motion adjustment bracket, makes rear gate and step（2）Backscrolling overturns same angular
Degree again reverse pitching flip an angle make rear gate be in setting angle；
（5）Control lifting assembly drops to specified altitude assignment, the connection after operator's assembling between gate and aircraft body
Part, if being afterwards that single ears are docked between gate and aircraft body, can be moved horizontally come micro- by controlling pose_adjuster
Adjust, it is ensured that what single ears were docked completes；
（6）Control lifting assembly is folded and pose_adjuster drops to original state；
（7）Control AGV dollies are moved to Factory Building specified location.
The screw mandrel for controlling the first and second pose_adjuster screw lifts rises simultaneously, controls the third and fourth pose_adjuster
The screw mandrel of screw lift declines simultaneously, and the longitudinal driving device for controlling the first and second pose_adjusters drives accordingly screw mandrel liter
Simultaneously toward the movement of the third and fourth pose_adjuster direction, the pitching at gate after realization overturns drop machine.Will be rear big in this utility model
Door is defined as " pitching upset " along the upset of its own axis of pitch.
The screw mandrel of the pose_adjuster screw lift of control first and the 3rd rises simultaneously, the pose_adjuster of control first and the 3rd
Lateral driver device drive corresponding screw lift toward second and the 4th pose_adjuster movement, while control first and second
The longitudinal driving device of pose_adjuster drives corresponding screw lift to vertically move simultaneously, the pose_adjuster of control first and the 3rd
Lateral driver device drive corresponding screw lift transverse shifting simultaneously, the rolling flip at gate after realization.This practicality is new
Horizontal upset in type by rear gate along axes of aircraft is defined as " rolling flip ".
Claims (8)
1. loading, unloading work platformses in gate after a kind of aircraft, it is characterised in that：The platform mainly includes posture adjustment platform and bracket group
Part, posture adjustment platform includes AGV dollies, platform base and some pose_adjusters for assembling successively, and the height adjustable of AGV dollies is adjusted
Appearance mechanism liftable and move horizontally, carriage assembly is connected to the upper end of pose_adjuster to be used to place gate after aircraft, bracket group
Part can be rotated around the upper end of each pose_adjuster.
2. loading, unloading work platformses in gate after aircraft as claimed in claim 1, it is characterised in that：The AGV dollies, main bag
Rectangle frame, four groups of road wheels and its driving means, deployable and folding lifting assembly, the power set of lifting assembly are included,
Four groups of road wheels and its driving means are installed on respectively four corners outside of rectangle frame by support, and lifting assembly includes connecting
The rectangular slab of linkage and its upper end, power set are arranged between rectangle frame and rectangular slab, and power set promote rectangular slab
Linkage launches during rising, and when power set drive non-rectangle plate to decline, linkage is folded and drawn in；Power set adopt two
Individual heavily loaded Electrohydraulic push rod, two heavily loaded Electrohydraulic push rods are arranged on the length direction median plane of rectangle frame and rectangular slab；
The surrounding of AGV dollies is disposed with the soft emergency stop device of noncontact obstacle detection and software self diagnosis.
3. loading, unloading work platformses in gate after aircraft as claimed in claim 2, it is characterised in that：The platform base include by
The frame body of the cuboid that square tube is surrounded and be connected to frame body corner cuboid link；Frame body is connected to institute
The upside of rectangular slab is stated, its upper frame upper surface laying walkway board, its surrounding is connected with guard rail and coaming plate；Stretch the upper end of link
Outside for walkway board, section of stretching out surrounding closures；Link has two kinds of higher link and relatively low link, and they distinguish
Two vertex angle parts of longitudinal direction of frame body are arranged in, the upper end of each link is connected to rectangular mounting plate, on rectangular mounting plate
There are two pieces of bar blocks being longitudinally arranged along frame body, have rectangular opening between two bar blocks；Being connected with the underframe of frame body to stretch
The ladder of contracting.
4. loading, unloading work platformses in gate after aircraft as claimed in claim 3, it is characterised in that：The pose_adjuster has first
Pose_adjuster to four sets of the 4th pose_adjuster, often cover pose_adjuster include two groups of longitudinal line slideways being arranged in parallel, two groups
The horizontal line slideway being arranged in parallel and a screw lift；Longitudinal line slideway is fixed in the bar blocks, and two ends connect
End plate is connected to, is fixed on rectangular mounting plate on the downside of end plate；Slide block on longitudinal line slideway is connected with sliding panel, laterally straight
Line guide rail parallel is connected on sliding panel, has rectangular opening between two horizontal line slideways of correspondence on sliding panel；Screw lift leads to
Cross installing plate to be connected as a single entity with the slide block on horizontal line slideway, the shaft lower end of screw lift is installed from sliding panel and rectangle
Pass through in the rectangular opening of plate, the upper end of the screw mandrel of shaft upper end connection is connected with bulb, and its power set adopts servomotor.
5. loading, unloading work platformses in gate after aircraft as claimed in claim 4, it is characterised in that：First pose_adjuster connects
It is connected on one of them higher link, also including two servomotors, they are connected respectively by diaphragm type servo shaft coupling
There is vertical and horizontal ball screw to form vertical and horizontal driving means respectively, the nut on longitudinal ball screw passes through nut seat
It is connected as a single entity with the sliding panel, the nut on transverse ball lead screw is connected by nut seat with the installing plate of the screw lift
It is integrated, the rotary motion of longitudinal ball screw drives screw lift to move horizontally along longitudinal line slideway by sliding panel,
Transversely line slideway is moved horizontally the rotational movement screw lift of transverse ball lead screw.
6. loading, unloading work platformses in gate after aircraft as claimed in claim 4, it is characterised in that：Second pose_adjuster connects
It is connected on another higher link, also including a servomotor, it is connected with longitudinal rolling by diaphragm type servo shaft coupling
Ballscrew forms longitudinal driving device, and the nut on longitudinal ball screw is connected as a single entity by nut seat with the sliding panel, indulges
Screw lift is driven to move horizontally along longitudinal line slideway by sliding panel to the rotary motion of ball screw.
7. loading, unloading work platformses in gate after aircraft as claimed in claim 4, it is characterised in that：3rd pose_adjuster connects
Be connected on one of them relatively low link, with first pose_adjuster be located at platform base frame body longitudinal two ends, the 3rd
Pose_adjuster also includes a servomotor, and it is connected with transverse ball lead screw and forms laterally drive by diaphragm type servo shaft coupling
Dynamic device, the nut on transverse ball lead screw is connected as a single entity by nut seat with the installing plate of the screw lift, laterally rolling
Transversely line slideway is moved horizontally the rotational movement screw lift of ballscrew.
8. loading, unloading work platformses in gate after aircraft as claimed in claim 4, it is characterised in that：The carriage assembly includes square
The bracket of shape, connecting seat, adpting flange, ball cup and locating piece, bracket is the rectangle support body surrounded by square tube, and connecting seat is arranged
In the downside of rectangle support body, adpting flange and ball cup are sequentially connected to the downside of connecting seat, locating piece by connecting screw rod and
Locking nut is connected in the slotted hole on bracket；The bulb of screw lift screw mandrel connects in the ball cup, and ball cup can
Rotate around bulb；There is divider longitudinal one end of bracket, and the inner side of divider and the horizontal skeleton upper surface of bracket post rubber strip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620933101.9U CN206125461U (en) | 2016-08-25 | 2016-08-25 | Gate is adorned behind aircraft, unload work platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620933101.9U CN206125461U (en) | 2016-08-25 | 2016-08-25 | Gate is adorned behind aircraft, unload work platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206125461U true CN206125461U (en) | 2017-04-26 |
Family
ID=58565125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620933101.9U Withdrawn - After Issue CN206125461U (en) | 2016-08-25 | 2016-08-25 | Gate is adorned behind aircraft, unload work platform |
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| Country | Link |
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| CN (1) | CN206125461U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184815A (en) * | 2016-08-25 | 2016-12-07 | 长沙市天映机械制造有限公司 | Gate loading, unloading work platforms and application process thereof after aircraft |
| CN107253084A (en) * | 2017-07-03 | 2017-10-17 | 上海昂恒航空自动化装备有限公司 | Efficient high-precision robot milling automatic system in aircraft digital assembling |
| CN108238281A (en) * | 2017-10-17 | 2018-07-03 | 西安飞机工业（集团）有限责任公司 | A kind of aircraft hold moves assembly work platform |
| WO2019134635A1 (en) * | 2018-01-05 | 2019-07-11 | 菜鸟智能物流控股有限公司 | Equipment control method and device |
| CN111132902A (en) * | 2017-07-24 | 2020-05-08 | 布勒特耶自动控制设备有限责任公司 | Machining device for aircraft structural components |
| CN112694033A (en) * | 2020-12-24 | 2021-04-23 | 天津迦自机器人科技有限公司 | Heavy load AGV transfer car (buggy) |
| CN113548194A (en) * | 2021-08-12 | 2021-10-26 | 中航西安飞机工业集团股份有限公司 | Turnover transportation device and method based on modular design |
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2016
- 2016-08-25 CN CN201620933101.9U patent/CN206125461U/en not_active Withdrawn - After Issue
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184815A (en) * | 2016-08-25 | 2016-12-07 | 长沙市天映机械制造有限公司 | Gate loading, unloading work platforms and application process thereof after aircraft |
| CN106184815B (en) * | 2016-08-25 | 2018-11-02 | 长沙市天映机械制造有限公司 | Gate loading, unloading workbench and its application process after aircraft |
| CN107253084A (en) * | 2017-07-03 | 2017-10-17 | 上海昂恒航空自动化装备有限公司 | Efficient high-precision robot milling automatic system in aircraft digital assembling |
| CN111132902A (en) * | 2017-07-24 | 2020-05-08 | 布勒特耶自动控制设备有限责任公司 | Machining device for aircraft structural components |
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| CN108238281A (en) * | 2017-10-17 | 2018-07-03 | 西安飞机工业（集团）有限责任公司 | A kind of aircraft hold moves assembly work platform |
| WO2019134635A1 (en) * | 2018-01-05 | 2019-07-11 | 菜鸟智能物流控股有限公司 | Equipment control method and device |
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| CN112694033A (en) * | 2020-12-24 | 2021-04-23 | 天津迦自机器人科技有限公司 | Heavy load AGV transfer car (buggy) |
| CN113548194A (en) * | 2021-08-12 | 2021-10-26 | 中航西安飞机工业集团股份有限公司 | Turnover transportation device and method based on modular design |
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