CN206813338U - Disk coal instrument is installed on the fixing device on unmanned plane - Google Patents
Disk coal instrument is installed on the fixing device on unmanned plane Download PDFInfo
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- CN206813338U CN206813338U CN201720497999.4U CN201720497999U CN206813338U CN 206813338 U CN206813338 U CN 206813338U CN 201720497999 U CN201720497999 U CN 201720497999U CN 206813338 U CN206813338 U CN 206813338U
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- fix bar
- unmanned plane
- suspension rod
- fixed
- fixing device
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Abstract
It the utility model is related to the fixing device that a discharge plate coal instrument is installed on unmanned plane, the fix bar being slidably connected including the guide rod with being arranged on head, the suspension rod with fix bar grafting on disk coal instrument is fixed on, and with fix bar to a pair of clamp assemblies close to either accordingly linked away from unmanned plane clamping or release suspension rod；When fix bar is slid into close to unmanned plane minimum range, clamp assemblies bottom sets the temporary fixing piece of fixed derrick and clamp assemblies.
Description
Technical field
It the utility model is related to the fixing device that a discharge plate coal instrument is installed on unmanned plane.
Background technology
Disk coal instrument is generally used for coal yard exploration, for measuring volume, the weight of material heap.Because the dump in coal yard compares
When height, Pan Meiyi are positioned over ground and surveyed, different angles is generally chosen, collects substantial amounts of data.With unmanned plane
Occur, disk coal instrument is arranged on unmanned plane, it is more convenient that coal yard is surveyed in the overhead of coal yard.
Unmanned plane generally includes fuselage, the wing on fuselage, head is set below fuselage, and support fuselage
Support.Neck, buckle structure are generally set below head, for the filming instrument being fixedly installed on below head.Using neck,
During buckle structure establishing shot instrument, it usually needs further reinforce the company of filming instrument and head using fixing band outside it
Connect., it is necessary to first pull down fixing band after shooting is completed, then neck, buckle structure are removed, it is more inconvenient.
Utility model content
The purpose of this utility model is to provide the fixing device that a discharge plate coal instrument is installed on unmanned plane, in disk coal instrument and
Quick grafting, the fastener of fast quick-detach are set between the head of unmanned plane, simplify the installation step between disk coal instrument and unmanned plane
Suddenly.
Above-mentioned purpose of the present utility model technical scheme is that：One discharge plate coal instrument is installed on nobody
Fixing device on machine, including the fix bar that the guide rod with being arranged on head is slidably connected, it is fixed on disk coal instrument and solid
The suspension rod of fixed pole grafting, and a pair with fix bar to close either accordingly linked away from head clamping or release suspension rod
Clamp assemblies；When fix bar is slid into close to head minimum range, clamp assemblies bottom sets fixed derrick and clamp assemblies
Temporary fixing piece.
Using above technical scheme, when Pan Meiyi is fixed on unmanned plane, when suspension rod is with fix bar grafting, fix bar is driven
Slided along guide rod to close to head direction.Fix bar drives two clamp assemblies to suspension rod side along guide rod sliding process
To close, and clamp suspension rod.Clamp assemblies are moved to when clamping suspension rod, and temporary fixing piece, which is taken advantage of a situation, consolidates suspension rod and clamp assemblies
It is fixed, and then realize the interim fixation of disk coal instrument and unmanned plane.
During dismounting, temporary fixing piece is unclamped, disk coal instrument drives suspension rod and fix bar to be slided away from head under weight effect.
Now, two clamp assemblies accordingly separate away from suspension rod, release the clamping action to suspension rod.Afterwards by suspension rod and fix bar point
From disk coal instrument is pulled down from unmanned plane.
Further, it is arranged damping spring on the outside of guide rod.
Using above technical scheme, damping spring one end abuts with head, and the other end abuts with fix bar upper end.Suspension rod
During with fix bar plugged and fixed, the rigidity between fix bar and guide rod is slidably connected and is changed into elastic connection, plays damping
Effect.After temporary fixing piece releases, damping spring aids in fix bar to be slided away from head, and auxiliary rod separates with fix bar.
Further, clamp assemblies include supporting rod, and the hinge bar being hinged between supporting rod and fix bar, two
Supporting rod and fix bar apart from it is farthest when, hinge bar is arranged in horizontal direction.
Using above technical scheme, hinge bar is as link gear, when fix bar is along guide rod to close to or away from cloud
When platform direction is slided, hinge bar accordingly drives two supporting rods close or remote, realizes fix bar and the connection of two supporting rods
Action.
Further, the bottom of the supporting rod side fixed clamp block relative with fix bar, grip block is close to suspension rod
Side sets the depression matched with suspension rod.
Using above technical scheme, fix bar slide into close to head it is nearest when, two grip blocks accordingly clamp suspension rod,
And the recessed position of grip block further increases the stable connection of grip block and suspension rod with being matched outside suspension rod.
Further, temporary fixing piece includes the bearing plate being slidably connected with supporting rod, and suspension rod is set through bearing plate；Hang
Bolt component is set when bar extruding fix bar is to head spacing minimum, between suspension rod and bearing plate.
Using above technical scheme, holder is slidably connected with bearing plate, and the spacing between bearing plate and head keeps one
It is fixed.Suspension rod uses bolt group through bearing plate and fix bar grafting, and when promoting the fix bar to slide into head spacing minimum
Part fixes suspension rod and bearing plate, and then realizes the interim fixation of disk coal instrument and unmanned plane.
Further, the fixed plate that component includes being fixed on suspension rod is bolted, is hinged with bearing plate, fixed plate is pressed in and held
Tightening latch on weight plate, and it is fixed on the bolt groove on bearing plate with tightening latch bolt.
Using above technical scheme, when fix bar is slid into head spacing minimum, fixed plate is bonded with bearing plate.This
When, fixed plate can be as the keeper of the state.In addition, rotating tightening latch and bolt groove bolt, fixed plate is accordingly crushed on and held
On weight plate, the interim fixation of disk coal instrument and unmanned plane is realized.
Further, the fix bar grafting that relative set matches with claw on one end of suspension rod setting claw, suspension rod
Ball.
Using above technical scheme, the position of suspension rod and claw grafting is arranged to grafting ball, and disk coal instrument turns by axle of suspension rod
Dynamic different angle and claw grafting, can corresponding adjustment plate coal instrument angle.
In summary, the utility model has the advantages that：
1st, disk coal instrument and unmanned plane are fixed using inserting mode, and it drives supporting rod to clamp suspension rod during grafting,
Realize the interim fixation of disk coal instrument and unmanned plane.
2nd, the boom end of disk coal instrument is arranged to grafting ball, when it is with claw grafting, can turn to difference by axle of suspension rod
Angle, accommodation can be carried out to the angle of disk coal instrument in a small range.
Brief description of the drawings
Fig. 1 is the unmanned plane structural representation for being provided with disk coal instrument；
Fig. 2 is the exploded perspective view that unmanned plane hides support；
Fig. 3 is the partial sectional view of fixed mechanism, clamp assemblies and bearing plate；
Fig. 4 is the upward view of bearing plate, to show tightening latch, bolt groove.
In figure, 1, unmanned plane；11st, fuselage；12nd, wing；13rd, head；131st, the first slippage slot；132nd, fixing groove；14th, prop up
Frame；2nd, fixed mechanism；21st, fix bar；211st, fixed block；212nd, guide rod；213rd, damping spring；214th, claw；3rd, clamping group
Part；31st, supporting rod；32nd, hinge bar；33rd, grip block；4th, support mechanism；41st, bearing plate；411st, the second slippage slot；412nd, grafting
Hole；413rd, neck；414th, tightening latch；415th, groove is bolted；5th, Pan Meiyi；51st, suspension rod；511st, grafting ball；52nd, fixed plate.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
One discharge plate coal instrument is installed on the fixing device on unmanned plane, as shown in figure 1, being arranged under the head 13 of unmanned plane 1
End.Unmanned plane 1 includes fuselage 11, and a wing 12 is fixed in the top of fuselage 11 respectively along the four direction of its drift angle, under fuselage 11
End face connects head 13, the support 14 of the also fixed support fuselage 11 in the lower section of fuselage 11, the concrete structure and md4-1000 of unmanned plane 1
Four rotor wing unmanned aerial vehicle systems are identical.Power source is set in fuselage 11（Not shown in figure）, power source drive wing 12 rotates, and drives
Fuselage 11 takes off.
When support 14 supports whole fuselage 11, head 13 has a certain distance apart from ground.The connection of the lower section of head 13 is solid
Determine mechanism 2, the one end of fixed mechanism 2 away from head 13 connects the support mechanism 4 parallel with head 13, in head 13 and load-bearing machine
A pair of clamp assemblies 3 are set between structure 4.Disk coal instrument 5 is connected through support mechanism 4 with fixed mechanism 2, disk coal instrument 5 and fixed machine
Clamp assemblies 3 are driven further to be clamped close to fixed mechanism 2, and by disk coal instrument 5 in the connection procedure of structure 2.
With reference to Fig. 2 and Fig. 3, the bottom of head 13 opens up fixing groove 132, and is symmetrically opened up in the both sides of fixing groove 132
One group of first slippage slot 131.Fixed mechanism 2 includes the fix bar 21 being connected with fixing groove 132, and concrete structure is fixing groove 132
Bottom land center be adhesively fixed block 211, the center of fixed block 211 extends guide rod 212 away from head 13, outside guide rod 212
Damping spring 213 is socketed, fix bar 21 is socketed on guide rod 212, is coaxially disposed with guide rod 212, and along guide rod 212
Slide axially.One end of damping spring 213 abuts with fixed block 211, and the other end abuts with fix bar 21.Fix bar 21 is away from cloud
One end stationary jaw 214 of platform 13, claw 214 itself has certain elastic deformation, for terminal pad coal instrument 5.
Clamp assemblies 3 include the supporting rod 31 being slidably connected with the first slippage slot 131, and two supporting rods 31 are right with it respectively
The first slippage slot 131 answered is slidably connected, and is slid to the direction close to or away from fix bar 21.Supporting rod 31 is with fixing
Hinge bar 32 is rotatablely connected between bar 21, when fix bar 21 is to close to the movement of the direction of fixed block 211, hinge bar 32 and fix bar 21
One end of connection is moved with fix bar 21, and hinge bar 32 drives two supporting rods 31 to fix bar during movement
21 directions are close.
The one end of supporting rod 31 away from head 13 is fixed respectively to contract, and in the relative side of two supporting rods 31
One grip block 33.This one end of supporting rod 31 is connected with support mechanism 4, and support mechanism 4 includes bearing plate 41, on bearing plate 41
One group of second slippage slot 411 being slidably connected respectively with supporting rod 31 is opened up, the centre of two the second slippage slots 411 is opened up with consolidating
Spliced eye 412 corresponding to fixed pole 21, so that disk coal instrument 5 is connected with claw 214.
With reference to Fig. 3 and Fig. 4, bearing plate 41 opens up neck 413 away from the side of the second slippage slot 411, and bearing plate 41 is close
The side of neck 413 is respectively articulated with a tightening latch 414, and tightening latch 414 is turned to across neck 413, and with being fixed on bearing plate
The plugged and fixed of bolt groove 415 on 41, the secondary fixation for disk coal instrument 5.Wherein the first slippage slot 131 and the second slippage slot
411 be T-slot, one end that supporting rod 31 is slidably connected with the first slippage slot 131 and the second slippage slot 411 respectively be with it is T-shaped
T-shaped piece of groove matching, in case supporting rod 31 departs from the first slippage slot 131 and the second slippage slot 411.
With reference to Fig. 2 and Fig. 3, disk coal instrument 5 includes suspension rod 51 fixed thereto, and end of the suspension rod 51 away from disk coal instrument 5 is fixed
Grafting ball 511, grafting ball 511 pass through spliced eye 412, and with the clamping of claw 214.When grafting ball 511 and the grafting of claw 214, and
And damping spring 213 is promoted when being compressed to largest deformation, hinge bar 32 drives two supporting rods 31 close, drives two grip blocks
33 by the clamping of suspension rod 51.Normal thereto on suspension rod 51 to fix one piece of fixed plate 52, in the state, fixed plate 52 is embedded just below card
In groove 413, tightening latch 414 is realized the interim fixation of fixed plate 52 and neck 413, entered across fixed plate 52 and the bolt grafting of groove 415
And realize the fixation of disk coal instrument 5 and unmanned plane 1.
In use, grafting ball 511 passes through spliced eye 412, when it inserts claw 214, elastic deformation, which occurs, for claw 214 blocks
Grafting ball 511.Suspension rod 51 promotes fix bar 21 further up, it is slided along guide rod 212 and further compression shock absorption bullet
Spring 213, during the upward sliding of fix bar 21, the hinge bar 32 being attached thereto accordingly drives two supporting rods 31 to fix bar 21
Direction is close.For the upward sliding of fix bar 21 to when damping spring 213 is compressed into largest deformation, grip block 33 clamps suspension rod 51.
Meanwhile fixed plate 52 is embedded in neck 413, the insertion bolt groove 415 of tightening latch 414 is rotated, realizes consolidating for disk coal instrument 5 and unmanned plane 1
Fixed connection.
During dismounting, tightening latch 414 departs from from bolt groove 415, and damping spring 213 recovers deformation, promotes fix bar 21 along leading
Slided to bar 212 to the direction of bearing plate 41, for fix bar 21 in sliding process, hinge bar 32 promotes two supporting rods 31 away from solid
The direction of fixed pole 21 is slided, and two grip blocks 33 release the clamping to suspension rod 51 therewith.Suspension rod 51 is pulled, makes grafting ball 511 and card
Pawl 214 departs from, and realizes the dismounting of disk coal instrument 5 and unmanned plane 1.
This specific embodiment is only that it is not to limitation of the present utility model, ability to explanation of the present utility model
Field technique personnel can make the modification of no creative contribution to the present embodiment as needed after this specification is read, but
As long as all protected in right of the present utility model by Patent Law.
Claims (7)
1. a discharge plate coal instrument is installed on the fixing device on unmanned plane, it is characterised in that：Including with being arranged at head（13）On
Guide rod（212）The fix bar being slidably connected（21）, it is fixed on Pan Meiyi（5）Upper and fix bar（21）The suspension rod of grafting（51）,
And with fix bar（21）To close or remote head（13）And accordingly link clamping or release suspension rod（51）A pair of folder
Hold component（3）；Fix bar（21）Slide into close to head（13）During minimum range, clamp assemblies（3）Bottom sets fixation to hang
Bar（51）With clamp assemblies（3）Temporary fixing piece.
2. disk coal instrument according to claim 1 is installed on the fixing device on unmanned plane, it is characterised in that：Guide rod
（212）Outside is arranged damping spring（213）.
3. disk coal instrument according to claim 2 is installed on the fixing device on unmanned plane, it is characterised in that：Clamp assemblies
（3）Including supporting rod（31）, and in supporting rod（31）And fix bar（21）Between be hinged hinge bar（32）, two supporting rods
（31）With fix bar（21）Apart from it is farthest when, hinge bar（32）Arrange in horizontal direction.
4. disk coal instrument according to claim 3 is installed on the fixing device on unmanned plane, it is characterised in that：Supporting rod（31）
Bottom and fix bar（21）Relative side fixed clamp block（33）, grip block（33）Close to suspension rod（51）Side set
With suspension rod（51）The depression of matching.
5. disk coal instrument according to claim 3 is installed on the fixing device on unmanned plane, it is characterised in that：Temporary fixing piece
Including with supporting rod（31）The bearing plate being slidably connected（41）, suspension rod（51）Through bearing plate（41）Set；Suspension rod（51）Extruding
Fix bar（21）To and head（13）During spacing minimum, suspension rod（51）With bearing plate（41）Between set bolt component.
6. disk coal instrument according to claim 5 is installed on the fixing device on unmanned plane, it is characterised in that：Bolt component bag
Include and be fixed on suspension rod（51）On fixed plate（52）, with bearing plate（41）It is be hinged, by fixed plate（52）It is pressed in bearing plate（41）On
Tightening latch（414）, and it is fixed on bearing plate（41）Upper and tightening latch（414）The bolt groove of bolt（415）.
7. disk coal instrument according to claim 1 is installed on the fixing device on unmanned plane, it is characterised in that：Fix bar（21）
Close to suspension rod（51）One end set claw（214）, suspension rod（51）Upper relative set and claw（214）The grafting ball of matching
（511）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720497999.4U CN206813338U (en) | 2017-05-06 | 2017-05-06 | Disk coal instrument is installed on the fixing device on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720497999.4U CN206813338U (en) | 2017-05-06 | 2017-05-06 | Disk coal instrument is installed on the fixing device on unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206813338U true CN206813338U (en) | 2017-12-29 |
Family
ID=60755163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720497999.4U Expired - Fee Related CN206813338U (en) | 2017-05-06 | 2017-05-06 | Disk coal instrument is installed on the fixing device on unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206813338U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974379A (en) * | 2018-05-28 | 2018-12-11 | 芜湖华诚农业技术有限公司 | A kind of general aviation low-altitude monitor operation aircraft |
| CN109292101A (en) * | 2018-11-07 | 2019-02-01 | 南通理工学院 | A kind of unmanned plane during flying stabilizing control system and method |
-
2017
- 2017-05-06 CN CN201720497999.4U patent/CN206813338U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974379A (en) * | 2018-05-28 | 2018-12-11 | 芜湖华诚农业技术有限公司 | A kind of general aviation low-altitude monitor operation aircraft |
| CN109292101A (en) * | 2018-11-07 | 2019-02-01 | 南通理工学院 | A kind of unmanned plane during flying stabilizing control system and method |
| CN109292101B (en) * | 2018-11-07 | 2021-08-27 | 南通理工学院 | Unmanned aerial vehicle flight stability control system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171229 Termination date: 20200506 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |