CN109159897A - A kind of unmanned plane throwing device - Google Patents
A kind of unmanned plane throwing device Download PDFInfo
- Publication number
- CN109159897A CN109159897A CN201811052808.9A CN201811052808A CN109159897A CN 109159897 A CN109159897 A CN 109159897A CN 201811052808 A CN201811052808 A CN 201811052808A CN 109159897 A CN109159897 A CN 109159897A
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- Prior art keywords
- connecting portion
- outer ring
- swingle
- unmanned plane
- fixed outer
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 35
- 230000005611 electricity Effects 0.000 claims description 5
- 230000009471 action Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 18
- 238000010304 firing Methods 0.000 description 18
- 238000010586 diagram Methods 0.000 description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 230000017525 heat dissipation Effects 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000000926 separation method Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 230000036632 reaction speed Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000032696 parturition Effects 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
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- 230000009466 transformation Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of unmanned plane throwing devices, including Fast detachable unit and pendant of jettisoninging；Fast detachable unit includes the first connection component and the second connection component；First connection component includes first connecting portion and fixed outer ring, and first connecting portion is rotatably set in fixed outer ring, and the upper surface of fixed outer ring is fixedly connected with the bottom of unmanned plane；It is fixedly connected at the top of the lower surface of the second connecting portion of second connection component and the ontology for pendant of jettisoninging；Pendant of jettisoninging includes ontology and support component；Driving assembly and fixed part are provided in support component, torque output is provided on driving assembly, driving assembly is connected by torque output with a rotating part, and rotating part is rotated with the rotation of torque output, and driving assembly drives rotating part to contact or separate with fixed part.The mechanical connection and circuit connection that the present invention can be achieved at the same time unmanned plane between pendant of jettisoninging, and can guarantee to jettisoning and homing action is gone on smoothly, have many advantages, such as easy to operate and structurally reasonable.
Description
Technical field
The present invention relates to unmanned plane equipment technical field more particularly to a kind of unmanned plane throwing devices.
Background technique
Unmanned plane be using the not manned aircraft of radio robot manipulation, it is increasingly mature with unmanned air vehicle technique,
Its reliability is higher and higher, therefore unmanned plane is widely used in various fields.
When unmanned plane, which needs to be implemented, jettisonings task, it is necessary first to load onto pendant of jettisoninging on unmanned plane.It is existing to jettisoning
Pendant is usually horizontally disposed hanging rod, and the article that needs are jettisoninged before unmanned plane takes off is hung on hanging rod, then controls
Unmanned plane takes off and after its flight to locality, is moved horizontally to the left or to the right by controlling hanging rod, and to hang
Article on hanging rod is fallen.
It jettisonings on pendant other than being provided with the component for hanging article, is additionally provided with circuit structure.Therefore, at nobody
It is loaded on machine during jettisoninging pendant, not only to realize mechanical connection, but also to realize circuit connection.
Unmanned plane throwing device in the prior art has the following problems:
1. not can be implemented simultaneously the mechanical connection and circuit connection of unmanned plane with pendant of jettisoninging, it is necessary to be first mechanically connected, be led to
It crosses after mechanical connection secures the two together and carries out circuit connection again, the problems such as there are complicated for operation and unreasonable structures；
2. the existing hook rail structure moved horizontally is easy to cause hanging rod or article that can not move horizontally due to past by card, leads
Cause can not be successfully progress article and jettisoning；
It is resetted 3. hanging rod needs are moved horizontally towards other direction after the completion of jettisoninging, and hanging rod once goes out during jettisoninging
Show deformation, will can not carry out normal reset.
Therefore, the existing technology needs to be improved and developed.
Summary of the invention
The technical problem to be solved in the present invention is that in view of the above drawbacks of the prior art, a kind of unmanned plane is provided and is jettisoninged
Device, the mechanical connection and circuit connection that can be achieved at the same time unmanned plane between pendant of jettisoninging, and can guarantee to jettisoning and answer
Going on smoothly for position movement, has many advantages, such as easy to operate and structurally reasonable.
The technical proposal for solving the technical problem of the invention is as follows:
A kind of unmanned plane throwing device, including Fast detachable unit and pendant of jettisoninging；
The Fast detachable unit includes the first connection component and the second connection component；
First connection component includes first connecting portion and fixed outer ring, and the first connecting portion is rotatably set in described
In fixed outer ring, the upper surface of the fixed outer ring is fixedly connected with the bottom of unmanned plane；
Second connection component includes second connecting portion, the top of the lower surface of the second connecting portion and the ontology for pendant of jettisoninging
Portion is fixedly connected；
First interface slot is offered in the first connecting portion, is offered in the second connecting portion and the first interface slot pair
The second interface slot answered；It is provided with the first locking piece in the first connecting portion, the second lock is provided in the second connecting portion
Determine part, after first locking piece and the second locking piece mutually locking, the second connecting portion is revolved with the first connecting portion
Then rotation；
It is provided with the first shackle member on the fixed outer ring, is provided with the second shackle member in the second connecting portion, described second
Interconnecting piece is connected in the first shackle member by the second shackle member and is fixedly connected with the fixed outer ring；
The pendant of jettisoninging includes the multiple support components of ontology and setting on the body；
It is provided with driving assembly and fixed part in the support component, torque output is provided in the driving component, it is described
Driving assembly is connected by torque output with a rotating part, and the rotating part is revolved with the rotation of the torque output
Turn, the hook for hanging article is provided on the rotating part, the driving component drives the rotation by torque output
Transfer part contacts or separates with the fixed part.
Now compare with the prior art, the beneficial effect of the technical program is: machinery can be achieved at the same time by above-mentioned Fast detachable unit
Connection and circuit connection, on the one hand, the circuit interface for being electrically connected is provided on first interface slot and second interface slot,
After first connecting portion and second connecting portion pass through the first locking piece and the second locking piece mutually locking, first interface slot and second is connect
It can keep opposing stationary between mouth slot, realize circuit connection；On the other hand, fixed outer ring and second connecting portion pass through the first card
Fitting and the second shackle member are fixedly connected, and realize mechanical connection.Therefore, this Fast detachable unit can be achieved at the same time unmanned plane and jettisoning
Mechanical connection and circuit connection between pendant have many advantages, such as easy to operate and structurally reasonable.And pass through above-mentioned pendant of jettisoninging
It can guarantee to jettisoning and homing action is gone on smoothly, on the one hand, rotating part need to only be can be realized by rotation and be connect with fixed part
Perhaps separation avoids can not be successfully and jettisoninging because article or rotating part are past by card during jettisoninging for touching；Another party
Face, rotating part are moved by way of rotation, even if rotating part is deformed because article is too heavy, also can guarantee after the completion of jettisoninging
Rotating part being capable of normal reset.
Further, first connection component further includes the first pedestal, and the upper surface of the fixed outer ring passes through described
First pedestal is fixedly connected with the bottom of unmanned plane, and the upper surface of the lower surface of first pedestal and the fixed outer ring connects
It connects, the first connecting portion is arranged between first pedestal and the fixed outer ring；
Second connection component further includes the second pedestal, and the second connecting portion is fixed at the upper table of second pedestal
Face, the second connecting portion at the top of second pedestal and the ontology for pendant of jettisoninging by being fixedly connected.
Beneficial effect using the above scheme is: on the one hand, the first pedestal and the second pedestal primarily serve connection function, Gu
Determine outer ring and is fixedly connected by the first pedestal with the bottom of unmanned plane, the sheet that second connecting portion passes through the second pedestal and pendant of jettisoninging
It is fixedly connected at the top of body；On the other hand, first connecting portion setting is between the first pedestal and fixed outer ring, and the first pedestal is the
One interconnecting piece, which is limited in the space of fixed outer ring, to be rotated, so that the connection between first connecting portion and second connecting portion is more firm
Gu reliable.
Further, the inner wall of the fixed outer ring is circumferentially arranged support annulus, and the first connecting portion is set in
In the fixed outer ring, and the bottom of the first connecting portion is connected on the support annulus.
Beneficial effect using the above scheme is: by being provided with support annulus in the inner wall of fixed outer ring, and first connects
The bottom of socket part is connected on support annulus, so that it may realize that first connecting portion rotates in fixed outer ring, to realize quick releasing function
Basis is provided.
Further, first shackle member is the blind slot being circumferentially disposed on the inner wall of the fixed outer ring, described
The lower section of the support annulus is arranged in blind slot；
The bottom of the inner wall of the fixed outer ring is provided with several mounting grooves, and the lower section of the blind slot is arranged in the mounting groove
And it is connected with the blind slot；
Second shackle member is several protruding blocks being arranged on the outer wall of the second connecting portion, the protruding block and institute
It states mounting groove to be mutually matched, for the protruding block after the mounting groove is inserted in the blind slot, the second connecting portion passes through institute
Protruding block is stated to be connected in the blind slot and be fixedly connected with the fixed outer ring.
Beneficial effect using the above scheme is: protruding block is inserted in blind slot by mounting groove, then enables second connecting portion
The relative rotation between fixed outer ring can be realized unmanned plane and jettisoning so that protruding block is installed in a staggered manner slot and is stuck in blind slot
The mechanical connection of pendant has many advantages, such as the simple good connecting effect of structure.
Further, there are three the mounting groove and the protruding block are respectively provided with, the size of one of mounting groove and another
The size of outer two mounting grooves is not identical, and the size of one of protruding block and the size of other two protruding block be not identical.
Beneficial effect using the above scheme is: relative position of first locking piece in first connecting portion is fixed, equally
Ground, relative position of second locking piece in second connecting portion is also fixed, and only the first locking piece and the second locking piece are mutual
After locking, the second connection component can be rotated with the rotation of the first connection component, therefore, the size of a mounting groove with
The size of other two mounting groove is not identical, accordingly, the size of the size of a protruding block and other two protruding block not phase
Together, it can play mark action, operator is helped to determine the position of the first locking piece and the second locking piece, locking the of being more convenient for
One locking piece and the second locking piece.
Further, first locking piece is positioning protrusion, and the first connecting portion is arranged in the positioning protrusion
Lower surface, second locking piece are positioning groove corresponding with the positioning protrusion, and positioning groove setting is described the
The upper surface of two interconnecting pieces.
Beneficial effect using the above scheme is: after positioning protrusion is embedded in positioning groove, can mutually locking, at this time second
Connection component will be rotated with the rotation of the first connection component, and the lock of two components can be realized by simple structure
It is fixed.
Further, limiting groove, the outer wall of the first connecting portion are offered at the top of the inner wall of the fixed outer ring
It is provided with spacing block set corresponding with the limiting groove, the first connecting portion drives the spacing block set recessed in the limit
It is rotated in the range of slot.
Beneficial effect using the above scheme is: second connecting portion rotates in a certain range can be realized and fixed outer ring
Connection or be not connected to, therefore, offer limiting groove at the top of fixed outer ring inner wall, then cooperate spacing block set that can lead to
First connecting portion is crossed to limit the rotation angle of second connecting portion, more convenient to install and disassembly.
Further, locking through-hole is offered on the side wall of the fixed outer ring, is movably set in the locking through-hole
It is equipped with dead bolt, the outer wall of the first connecting portion is provided with locking blind hole, is provided with spring firing pin in the locking blind hole；
When the locking through-hole and the locking blind hole are on same straight line, the spring firing pin presses the locking outward
Bolt is simultaneously inserted into the locking through-hole, at this time the first connecting portion and the fixed outer ring mutually locking；
When the dead bolt moves inward, the dead bolt presses the spring firing pin, and spring firing pin is exited
The locking through-hole, the first connecting portion can rotate in the fixed outer ring at this time.
Beneficial effect using the above scheme is: after realizing mechanical connection between unmanned plane and pendant of jettisoninging, passing through
It is achieved that first connecting portion is fixedly connected with fixation outer ring in spring firing pin insertion locking through-hole, and cannot continue to rotate,
It can effectively avoid falling off because of caused by maloperation.
Further, the support component includes top panel, bottom panel, the first side plate and the second side plate；
The top panel, first side plate, the bottom panel and second side plate join end to end and form frame structure, described
One end of frame structure is connected with the ontology, and the other end of the frame structure forms installing port, and the driving component passes through
Installing port is arranged in support component.
Beneficial effect using the above scheme is: each support component is by top panel, bottom panel, the first side plate and
The frame structure that two side plates are surrounded, frame structure are extended outwardly centered on ontology, and driving assembly is mounted in far from ontology
One end, on the one hand, provide bigger space be used to hang up more articles；On the other hand, each supporting point is uniformly distributed
Around center of gravity, so that the center of gravity of unmanned plane is more stable, so that unmanned plane is more steady in flight course.
Further, the bottom panel is further fixedly arranged on an extension plate, the driving in one end far from the ontology
Component is arranged on the bottom panel and the extension plate；
The side of the extension plate lower surface is arranged in the fixed part, and the rotating part is movably disposed in the extension plate
The other side of lower surface.
Beneficial effect using the above scheme is: extension plate enables to the article hung up farther away from the center of ontology,
Further expansion hangs up the space of article, and the side of lower surface of extension plate is arranged in fixed part, rotating part activity is arranged
In the other side of extension plate lower surface, then article is enabled to, always in bottom, to be convenient for article during flight
It jettisonings.
Further, the lower surface of the extension plate side opposite with the fixed part is additionally provided with a limiting slot, institute
Rotating part is stated to be movably disposed in the limiting slot.
Beneficial effect using the above scheme is: rotating part is movably disposed in limiting slot, so that rotating part is revolving
It is maintained at movement in limiting slot during turning, rotating part is avoided to occur deforming and leading to not rotate, guarantees that rotating part can
Realization is normally jettisoninged and is resetted.
Further, first side plate and second side plate are engraved structure.
Beneficial effect using the above scheme is: being conducive to mitigate the weight of equipment, improves the cruising ability of unmanned plane.
Further, the rotating part includes connector, the first swingle, the second swingle, third swingle and the 4th
Swingle, the connector are fixedly connected with the torque output, and one end of first swingle and the connector are solid
Fixed connection, first swingle, second swingle, the third swingle and the 4th swingle are sequentially connected；
Second swingle is vertically arranged, and the angle between first swingle and second swingle is 120 °, institute
Stating the angle between the second swingle and the third swingle is 120 °, the third swingle and the 4th swingle it
Between angle be 120 °.
Beneficial effect using the above scheme is: on the one hand, the angle between third swingle and the 4th swingle is
120 °, hook is formed between third swingle and the 4th swingle, guarantees that rotating part will not be weighed as traditional hanging rod
Object is bent；On the other hand, rotating part is mobile to side-lower during jettisoninging, rather than moving horizontally merely, avoids out
Existing article, which is stuck in hook, above to be led to not jettisoning.
Further, the bottom center of the ontology is additionally provided with electromagnet, and it is U-shaped that the bottom surface of the electromagnet is provided with one
Metalwork, when the electromagnet is powered, the U-shaped metalwork is adsorbed on the bottom surface of the electromagnet, when the electromagnet powers off
The U-shaped metalwork of Shi Suoshu is fallen from the bottom surface of the electromagnet.
Beneficial effect using the above scheme is: electromagnet has the advantages that reaction speed is fast, is suitable for emergency relief etc.
Scene, while also improving the delivered payload capability for pendant of originally jettisoninging.
Further, the first switch for controlling the magnet switching electricity, the branch are additionally provided on the ontology
The second switch for controlling the driving component movement is additionally provided on support component.
Beneficial effect using the above scheme is: when loading article, passing through the i.e. controllable U of first switch and the second switch
The state of type metalwork and driving assembly, it is convenient that article is loaded before unmanned plane takes off.
Further, the ontology includes first side plate, second side plate, third side panel, fourth side panel, the 5th
Side panel and sixth side panel, the first side plate, the second side plate, the third side panel, the 4th side
Plate, the fifth side panel and the sixth side panel surround the tubular structure of a regular hexagon, the centre of the tubular structure
Offer the circular cavity for placing electromagnet, the first side plate, the third side panel and the fifth side panel
Outer surface on be provided with heat dissipation vertical bar.
Beneficial effect using the above scheme is: on the one hand, heat dissipation vertical bar can be improved radiating efficiency, export electromagnetism in time
Iron heat caused by the course of work；On the other hand, electromagnet is arranged in circular cavity, can be improved its electromagnetism interference
Ability.
Further, there are three the support components, three support components to be arranged same for setting on the ontology
On horizontal plane, three support components are separately positioned on the second side plate, the fourth side panel and the 6th side
On the outer surface of panel.
Beneficial effect using the above scheme is: three support components are uniformly distributed on the body, guarantee that unmanned plane is flying
The stability of row in the process.
Detailed description of the invention
Fig. 1 is a kind of overall schematic of unmanned plane throwing device of the present invention.
Fig. 2 is the schematic diagram of Fast detachable unit in a kind of unmanned plane throwing device of the present invention.
Fig. 3 is the bottom view of the first connection component in a kind of unmanned plane throwing device of the present invention.
Fig. 4 is the top view of the second connection component in a kind of unmanned plane throwing device of the present invention.
Fig. 5 is the top view fixed after outer ring and the assembly of the first connection component in a kind of unmanned plane throwing device of the present invention.
Fig. 6 is the schematic diagram that outer ring is fixed in a kind of unmanned plane throwing device of the present invention.
Fig. 7 is the schematic diagram of pendant of jettisoninging in a kind of unmanned plane throwing device of the present invention.
Fig. 8 is the schematic diagram of support component in a kind of unmanned plane throwing device of the present invention.
Fig. 9 is the schematic diagram of rotating part in a kind of unmanned plane throwing device of the present invention.
Figure 10 is the assembling schematic diagram of support component and driving assembly in a kind of unmanned plane throwing device of the present invention.
Figure 11 is the bottom view of pendant of jettisoninging in a kind of unmanned plane throwing device of the present invention.
Figure 12 is the side view of electromagnet in a kind of unmanned plane throwing device of the present invention.
Specific embodiment
To make the objectives, technical solutions, and advantages of the present invention clearer and more explicit, right as follows in conjunction with drawings and embodiments
The present invention is further described.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and do not have to
It is of the invention in limiting.
Referring to Fig. 1-Figure 12, wherein Fig. 1 is a kind of overall schematic of unmanned plane throwing device of the present invention；Fig. 2 is this hair
The schematic diagram of Fast detachable unit in a kind of bright unmanned plane throwing device；Fig. 3 is the first connection in a kind of unmanned plane throwing device of the present invention
The bottom view of component 1；Fig. 4 is the top view of the second connection component 2 in a kind of unmanned plane throwing device of the present invention；Fig. 5 is this hair
Top view after fixing outer ring 12 and the assembly of the first connection component 1 in a kind of bright unmanned plane throwing device；Fig. 6 is of the invention a kind of
The schematic diagram of outer ring 12 is fixed in unmanned plane throwing device；Fig. 7 is pendant of jettisoninging in a kind of unmanned plane throwing device of the present invention
Schematic diagram；Fig. 8 is the schematic diagram of support component 4 in a kind of unmanned plane throwing device of the present invention；Fig. 9 is a kind of unmanned plane of the present invention
The schematic diagram of rotating part 7 in throwing device；Figure 10 is support component 4 and driving assembly in a kind of unmanned plane throwing device of the present invention
5 assembling schematic diagram；Figure 11 is the bottom view of pendant of jettisoninging in a kind of unmanned plane throwing device of the present invention；Figure 12 is the present invention one
The side view of electromagnet 8 in kind unmanned plane throwing device.
As shown in Figure 1, a kind of unmanned plane throwing device, mainly includes Fast detachable unit and two parts of pendant of jettisoninging.Below according to
It is secondary that Fast detachable unit and pendant of jettisoninging are described in detail.
As shown in Fig. 2, Fast detachable unit includes the first connection component 1 and the second connection component 2.Wherein, the first connection group
Part 1 is fixedly connected with the bottom of unmanned plane, and second connection component 2 is fixedly connected with the top of the ontology 3 for pendant of jettisoninging.
As shown in figure 3, first connection component 1 includes first connecting portion 11 and fixed outer ring 12；As shown in figure 4, institute
Stating the second connection component 2 includes second connecting portion 21.Specifically, the first connecting portion 11 and the second connecting portion 21 are circle
Shape structure, the fixed outer ring 12 are cirque structure.
For the circuit connection for realizing unmanned plane between pendant of jettisoninging, first is offered in the first connecting portion 11 and is connect
Mouthful slot 112, offers second interface slot 211 corresponding with the first interface slot 112 in the second connecting portion 21, and described the
The circuit interface for being electrically connected is provided on one interface slot 112 and the second interface slot 211.
It is provided with the first locking piece 113 in the first connecting portion 11, is provided with the second lock in the second connecting portion 21
Determine part 212, after 212 mutually locking of first locking piece 113 and the second locking piece, the second connecting portion 21 is with described
One interconnecting piece 11 is rotated and is rotated.Therefore, it opposite can be protected between the first interface slot 112 and the second interface slot 211
Hold it is static so that the circuit interface being arranged on the first interface slot 112 and the second interface slot 211 being capable of the moment
Keep connection.
It is provided with the first shackle member 122 on the fixed outer ring 12, is provided with the second clamping in the second connecting portion 21
Part 213, the second connecting portion 21 are connected in the first shackle member 122 and the fixed outer ring by the second shackle member 213
12 are fixedly connected.By the mutual cooperation between first shackle member 122 and second shackle member 213, so that first connects
It is fixedly connected between connected components 1 and the second connection component 2, realizes the mechanical connection of unmanned plane and pendant of jettisoninging.
When specific works, pass through the first locking piece 113 and the second locking between first connecting portion 11 and second connecting portion 21
After 212 mutually locking of part, the second connection component 2 can rotate, first interface slot 112 as the first connection component 1 rotates
It is opposite between second interface slot 211 to remain stationary, so that being arranged on first interface slot 112 and second interface slot 211
Circuit interface can keep connecting constantly, and then realize circuit connection.Further, second connecting portion 21 passes through the second clamping
Part 213 is connected in the first shackle member 122 and is fixedly connected with fixed outer ring 12, to realize mechanical connection.In this way,
It just can be achieved at the same time the mechanical connection and circuit connection between unmanned plane and pendant of jettisoninging by this Fast detachable unit, there is operation letter
The advantages that single and structurally reasonable.
Preferably, first connection component 1 further includes the first pedestal 13, and the upper surface of the fixed outer ring 12 passes through institute
It states the first pedestal 13 to be fixedly connected with the bottom of unmanned plane, the lower surface of first pedestal 13 is upper with the fixed outer ring 12
Surface connection, the first connecting portion 11 are arranged between first pedestal 13 and the fixed outer ring 12.Second connection group
Part 2 includes second connecting portion 21 and the second pedestal 22, and the second connecting portion 21 is fixed at the upper of second pedestal 22
Surface, the second connecting portion 21 are fixedly connected by second pedestal 22 with the top of the ontology 3 for pendant of jettisoninging.
First connection component, 1 specific structure are as follows: the first connection component 1 includes first connecting portion 11, fixed outer ring 12 and the
One pedestal 13, for the setting of first connecting portion 11 between the first pedestal 13 and fixed outer ring 12, first connecting portion 11 can be in fixation
Rotation in outer ring 12.
First pedestal 13 and the second pedestal 22 primarily serve connection function, and fixed outer ring 12 passes through the first pedestal 13 and nobody
The bottom of machine is fixedly connected, and second connecting portion 21 is fixedly connected by the second pedestal 22 with the top of the ontology 3 for pendant of jettisoninging；Separately
Outside, for the setting of first connecting portion 11 between the first pedestal 13 and fixed outer ring 12, the first pedestal 13 limits first connecting portion 11
It is rotated in the space of fixed outer ring 12, it can so that the connection between first connecting portion 11 and second connecting portion 21 is stronger
It leans on.
In order to enable first connecting portion 11 can preferably rotate in fixed outer ring 12, to realize unmanned plane and extension of jettisoninging
Mechanical connection between part, as shown in fig. 6, the inner wall of the fixed outer ring 12 is circumferentially arranged a support annulus 123, described the
One interconnecting piece 11 is set in the fixed outer ring 12, and the bottom of the first connecting portion 11 is connected to the support annulus
On 123.Support annulus 123 is actually the circle protrusion being arranged on the inner wall of fixed outer ring 12, plays support first and connects
The effect of socket part 11.
As shown in figure 5, offering limiting groove 121, the first connecting portion at the top of the inner wall of the fixed outer ring 12
11 outer wall is provided with spacing block set 111 corresponding with the limiting groove 121, and the first connecting portion 11 drives the limit
Convex block 111 rotates in the range of limiting groove 121.
When second connecting portion 21 drives first connecting portion 11 with rotation, because being provided with limit convex in first connecting portion 11
Block 111, therefore first connecting portion 11 can only rotate in a certain range, when spacing block set 111 is connected to the two of limiting groove 121
Bian Shi cannot be further rotated, is easy for installation and removal.
The step that first connecting portion 11 is mounted on fixed outer ring 12 is specifically included: alignment spacing block set 111 and limit
First connecting portion 11 is inserted in from the top of fixed outer ring 12, and the bottom of first connecting portion 11 is supported in the position of groove 121
It is connected on support annulus 123.At this point, first connecting portion 11 can rotate in fixed outer ring 12.
In order to enable second connecting portion 21 can be preferably mounted on fixed outer ring 12, first shackle member 122 is
The lower section of the support annulus 123 is arranged in the blind slot being circumferentially disposed on the inner wall of the fixed outer ring 12, the blind slot；
The bottom of the inner wall of the fixed outer ring 12 is provided with several mounting grooves 124, and the blind slot is arranged in the mounting groove 124
Lower section is simultaneously connected with the blind slot.
Accordingly, second shackle member 213 is several protrusions being arranged on the outer wall of the second connecting portion 21
Block, the protruding block are mutually matched with the mounting groove 124, and the protruding block is inserted in the blind slot through the mounting groove 124
Afterwards, the second connecting portion 21 is connected in the blind slot by the protruding block and is fixedly connected with the fixed outer ring 12.
The step that second connecting portion 21 is mounted on fixed outer ring 12 is specifically included: alignment mounting groove 124 and protruding block
Position, protruding block is inserted in from mounting groove 124, so that protruding block enters blind slot, then rotates second connecting portion 21, the
Two interconnecting pieces 21 will drive protruding block to rotate when rotating, so that protruding block is installed in a staggered manner slot 124 and is clamped with blind slot.
In said structure, the quantity of protruding block is identical as the quantity of mounting groove 124, the shape of each protruding block and and its
The shape of corresponding mounting groove 124 is identical, and the size of protruding block is less than the size of mounting groove 124 identical with its shape, with
It is easily installed.Protruding block is mutually matched with mounting groove 124, is that each protruding block has corresponding mounting groove 124, so that
Each protruding block can be inserted in blind slot.When specific installation, a direction is first selected, each protruding block is just passed through
Corresponding mounting groove 124 and enter in blind slot, after protruding block is completely into blind slot, the first locking piece 113 and the second locking piece
212 mutually lockings immediately, the second connection component 2 can be rotated as the first connection component 1 rotates at this time.Further, it rotates
Second connecting portion 21 makes itself and fixed 12 relative rotation of outer ring, when so that protruding block being installed in a staggered manner slot 124 and is stuck in blind slot, just
Second connecting portion 21 may make to be fixedly connected with fixed outer ring 12.
Specifically, there are three the mounting groove 124 and the protruding block be respectively provided with, the size of one of mounting groove 124
Not identical as the size of other two mounting groove 124, the size of the size of one of protruding block and other two protruding block is not
It is identical.That is two sizes in three mounting grooves 124 are the same, and the size of another mounting groove 124 and the two mounting grooves 124
Difference, accordingly, two sizes in three protruding blocks are the same, and the size of another protruding block and the two protruding blocks is not
Together.
Relative position of first locking piece 113 in first connecting portion 11 is fixed, and similarly, the second locking piece 212 is
Relative position on two interconnecting pieces 21 is also fixed, and only after 212 mutually locking of the first locking piece 113 and the second locking piece, the
One interconnecting piece 11 can be rotated with the rotation of second connecting portion 21.If each mounting groove 124 all is the same size,
First need to confirm the position of the first locking piece 113 and the second locking piece 212 before installation.Therefore, by the way that various sizes of peace is arranged
Tankage 124 and protruding block, it will be able to mark action is played, as long as making each mounting groove 124 corresponding with each protruding block,
It can enable 212 mutually locking of the first locking piece 113 and the second locking piece.Setting in this way, operator can
The position for determining the first locking piece 113 and the second locking piece 212 more conveniently, the first locking piece 113 of locking of being more convenient for
With the second locking piece 212.
Specifically, first locking piece 113 is positioning protrusion, and the positioning protrusion is arranged in the first connecting portion 11
Lower surface, second locking piece 212 is positioning groove corresponding with the positioning protrusion, and the positioning groove is arranged in institute
State the upper surface of second connecting portion 21.It is each after second connecting portion 21 is packed into fixed outer ring 12 from the lower section of fixed outer ring 12
Positioning protrusion is embedded in corresponding positioning groove, at this point, when second connecting portion 21 rotates, between positioning protrusion and positioning groove
Active force is generated, drives first connecting portion 11 with rotation.
In order to enable being installed rear unmanned plane and pendant of jettisoninging can be securely attached together, the fixed outer ring 12
Side wall on offer locking through-hole, dead bolt, the first connecting portion 11 are movably provided in the locking through-hole
Outer wall be provided with locking blind hole, be provided with spring firing pin in the locking blind hole.
When locking through-hole and locking blind hole is on same straight line, spring firing pin presses dead bolt, also, this outward
When spring firing pin insertion locking through-hole in, first connecting portion 11 and fixed 12 mutually locking of outer ring at this time.Specifically, when need
When wanting first connecting portion 11 and fixed 12 mutually locking of outer ring, second connecting portion 21 is rotated, so that locking through-hole and locking blind hole
On same straight line, spring firing pin is pressed lock by the center of circle along the radius of fixed outer ring 12 by its own elastic force outward at this time
Determine bolt, locked in through-hole so that spring firing pin is inserted into, at this moment first connecting portion 11 and fixed 12 mutually locking of outer ring, Jin Ershi
Existing 2 mutually locking of first connection component 1 and the second connection component.
When driving dead bolt inwardly movable, dead bolt compressed spring striker, and spring firing pin is made to exit locking
Through-hole, first connecting portion 11 can fix rotation in outer ring at this time.Specifically, when needs connect the second connection component 2 from first
When disassembling on connected components 1, driving dead bolt is moved along the half radial center of circle of fixed outer ring 12, at this time dead bolt pressure
Contracting spring firing pin simultaneously forces spring firing pin to exit locking through-hole, because spring firing pin has exited locking through-hole, as long as at this moment rotation the
Two interconnecting pieces 21 just may make spring firing pin to withstand on the side wall of fixed outer ring 12, and the first connection component 1 and second connects at this time
Connected components 2 can mutually activity.
Further, dead bolt can be driven to move inward by a spanner.One end of spanner is provided with smoothly excessive support
It is consecutive, when user moves the other end of spanner, abuts platform and gradually push dead bolt mobile to the center of circle in locking through-hole, thus
Spring firing pin is forced to exit locking through-hole.It should be noted that it is multiple that spanner is unable to drive dead bolt in this technical solution
Position.During dead bolt resets, needs to rotate second connecting portion 21 and to lock through-hole and lock blind hole to be in always
On line, dead bolt is pushed out by the elastic force of spring firing pin, then moves spanner and abutting platform is made to leave dead bolt, so that
Spring firing pin enters locking through-hole, that is, completes the reset of dead bolt.
In conclusion Fast detachable unit provided by the invention includes the first connection component 1 and the second connection component 2；Described first
Connection component 1 includes first connecting portion 11 and fixed outer ring 12, and the first connecting portion 11 is rotatably set in the fixation
In outer ring 12, the upper surface of the fixed outer ring 12 is fixedly connected with the bottom of unmanned plane；Second connection component 2 includes the
The top of two interconnecting pieces 21, the ontology 3 of the lower surface and pendant of jettisoninging of the second connecting portion 21 is fixedly connected；Described first connects
First interface slot 112 is offered in socket part 11, is offered in the second connecting portion 21 corresponding with the first interface slot 112
Second interface slot 211；It is provided with the first locking piece 113 in the first connecting portion 11, is provided in the second connecting portion 21
Second locking piece 212, after 212 mutually locking of first locking piece 113 and the second locking piece, the second connecting portion 21 with
The first connecting portion 11 is rotated and is rotated；The first shackle member 122, the second connecting portion are provided on the fixed outer ring 12
The second shackle member 213 is provided on 21, the second connecting portion 21 is connected to the first shackle member 122 by the second shackle member 213
Above it is fixedly connected with the fixed outer ring 12.
Now compare with the prior art, the beneficial effect of the Fast detachable unit in the technical program is: on the one hand, first interface slot 112
Be provided with the circuit interface for being electrically connected on second interface slot 211, first connecting portion 11 and second connecting portion 21 are logical
After crossing 212 mutually locking of the first locking piece 113 and the second locking piece, then protected between first interface slot 112 and second interface slot 211
Hold opposing stationary, realization circuit connection；On the other hand, fixed outer ring 12 and second connecting portion 21 pass through 122 He of the first shackle member
Second shackle member 213 is fixedly connected, and realizes mechanical connection.Therefore, this Fast detachable unit can be achieved at the same time unmanned plane and extension of jettisoninging
Mechanical connection and circuit connection between part have many advantages, such as easy to operate and structurally reasonable.
As shown in fig. 7, pendant of jettisoninging includes ontology 3 and multiple support components 4 for being arranged on the ontology 3.Specifically,
There are three the support components 4, three support components 4 to be arranged in same level for setting on the ontology 3, three institutes
Support component 4 is stated to be uniformly arranged on around the ontology 3.
5, fixed parts 6 of a driving assembly and a rotating part 7 are provided in one support component 4.Wherein,
Torque output 51 is provided in the driving component 5, the driving component 5 is connected by torque output 51 with rotating part 7,
The rotating part 7 is rotated with the rotation of the torque output 51, is provided on the rotating part 7 for hanging article
Hook, the driving component 5 drive the rotating part 7 to contact or separate with the fixed part 6 by torque output 51.?
During progress article is jettisoninged, the fixed part 6 is motionless, and the rotating part 7 then passes through institute by the driving component 5
The drive of torque output 51 is stated, contacts or separates with the fixed part 6.
After being provided with the hook for hanging article on rotating part 7,7 need of rotating part can be realized and be consolidated by rotation
The contact or separation for determining portion 6, when driving assembly 5 drives rotating part 7 and fixed part 6 to contact, rotating part 7 and fixed part 6 it
Between be mutually closed, article can be then hung on hook；And when driving assembly 5 drives rotating part 7 to separate with fixed part 6, it hangs
Article on hook is then fallen therewith.Rotating part 7 by way of rotation rather than the mode that moves horizontally and fixed part 6
Perhaps separation can be avoided article or rotating part 7 is past by card and can not jettisoning for contact, while also can guarantee to jettisoning and completing back spin
It transfer part 7 being capable of normal reset.In the technical scheme, driving assembly 5 is steering engine, using steering engine as driving assembly 5, Neng Gougeng
It is suitable on unmanned plane well, accurately makes corresponding movement preferably to control rotating part 7.
After hanging article, the very big pressure born on rotating part 7, and three support components 4 are uniformly arranged on ontology 3
Around, can dispensed weight well, greatly improve the stability of unmanned plane in the process in flight.
As shown in figure 8, each support component 4 includes top panel 41, bottom panel 42, the first side plate 43 and the second side plate
44；The top panel 41, first side plate 43, the bottom panel 42 and second side plate 44 join end to end and form frame knot
Structure, one end of the frame structure are connected with the ontology 3, and the other end of the frame structure forms installing port, the driving
Component 5 is arranged in support component 4 by installing port.In order to mitigate equipment quality, so that the cruising ability of unmanned plane is improved, institute
It states the first side plate 43 and second side plate 44 is engraved structure.
Each support component 4 is the frame surrounded by top panel 41, bottom panel 42, the first side plate 43 and the second side plate 44
Frame structure, frame structure are extended outwardly centered on ontology 3, and driving assembly 5 is mounted in one end far from ontology 3, on the one hand,
Bigger space is provided to be used to hang up more articles；On the other hand, each supporting point is evenly distributed on around center of gravity, is made
It is more stable to obtain center of gravity, is conducive to stability of the unmanned plane in flight course.
Preferably, the bottom panel 42 is further fixedly arranged on an extension plate 45, the drive in one end far from the ontology 3
Dynamic component 5 is arranged on the bottom panel 42 and the extension plate 45；The fixed part 6 is arranged in 45 lower surface of extension plate
Side, the rotating part 7 is movably disposed in the other side of 45 lower surface of extension plate.The setting of extension plate 45, makes
Driving assembly 5 can extend further out, further expansion article hangs up space, and further improves unmanned plane and exist
Stability in flight course.
As shown in Figure 10, during installing driving assembly 5 in support component 4, a part of driving assembly 5 is extend into
Inside support component 4, and the top of extension plate 45 is then arranged in another part.Bottom panel 42 and extension plate 45 support drive jointly
Dynamic component 5.
The torque output 51 of driving assembly 5 is arranged in front of it, and one end of rotating part 7 is arranged in torque output 51
On, the other end of rotating part 7 extends to the side of 45 lower surface of extension plate.In this way, which fixed part 6 and rotating part 7 are just arranged
In the correspondence two sides of 45 lower surface of extension plate, driving assembly 5 drives rotating part 7 to rotate, and rotating part 7 and fixed part 6 can be realized
Contact or separation.
Preferably, the lower surface of the extension plate 45 side opposite with the fixed part 6 is additionally provided with a limiting slot 46,
The rotating part 7 is movably disposed in the limiting slot 46.Rotating part 7 is movably disposed in limiting slot 46, so that
Rotating part 7 moves in the range of being maintained at limiting slot 46 during rotation, and rotating part 7 is avoided to occur deforming and leading to not
Rotation guarantees that rotating part 7 can be realized and normally jettisonings and reset.
As shown in figure 9, the rotating part 7 includes connector 71, the first swingle 72, the second swingle 73, third rotation
Bar 74 and the 4th swingle 75.The effect of connector 71 is so that rotating part 7 is fixedly connected with torque output 51.The company
Fitting 71 is fixedly connected with the torque output 51, one end of first swingle 72 and the fixed company of the connector 71
It connects, first swingle 72, second swingle 73, the third swingle 74 and the 4th swingle 75 successively phase
Even；Second swingle 73 is vertically arranged, and the angle between first swingle 72 and second swingle 73 is
120 °, the angle between second swingle 73 and the third swingle 74 is 120 °, the third swingle 74 and institute
Stating the angle between the 4th swingle 75 is 120 °.
Different from traditional hanging rod, in the technical scheme, rotating part 7 is the structure of a similar regular hexagon.Driving
Component 5 drives rotating part 7 to rotate, and during rotating part 7 is separated with fixed part 6, driving assembly 5 drives rotating part 7 to rotate,
First swingle 72, the second swingle 73, third swingle 74 and the 4th swingle 75 are transported in the range of limiting slot 46 together
Dynamic, the 4th swingle 75 is separated with fixed part 6 at leisure, and the opening between the 4th swingle 75 and fixed part 6 is increasing, most
Article is fallen between being open afterwards.And during loading article, after first hanging article on rotating part 7, driving assembly 5
Rotating part 7 is driven to rotate, the first swingle 72, the second swingle 73, third swingle 74 and the 4th swingle 75 are limiting together
Moved in the range of the slot 46 of position, the 4th swingle 75 is contacted with fixed part 6 at leisure, the 4th swingle 75 and fixed part 6 it
Between opening it is smaller and smaller and be finally closed, article can be locked in fixed part 6 and rotating part 7.
Rotating part 7 is set to the structure of similar regular hexagon, the shape between third swingle 74 and the 4th swingle 75
At the hook for hanging article, using 120 ° of angles between third swingle 74 and the 4th swingle 75, when driving assembly 5
When rotating part 7 being driven to separate with fixed part 6, the article being hung on hook can smoothly streak the 4th swingle 75, thus
Opening between 4th swingle 75 and fixed part 6 is fallen, and can effectively avoid jettisoninging unsuccessful.
On the one hand, the angle between third swingle 74 and the 4th swingle 75 is 120 °, in third swingle 74 and
Hook is formed between four swingles 75, guarantees that rotating part 7 will not be bent as traditional hanging rod by weight；On the other hand, exist
Rotating part 7 is mobile to side-lower during jettisoninging, rather than moving horizontally merely, avoids the occurrence of article and is stuck on hook
And lead to not jettisoning.
As is illustrated by figs. 11 and 12, the bottom center of the ontology 3 is additionally provided with electromagnet 8, the bottom surface of the electromagnet 8
It is provided with a U-shaped metalwork 9, when the electromagnet 8 is powered, the U-shaped metalwork 9 is adsorbed on the bottom surface of the electromagnet 8,
When the electromagnet 8 power-off, the U-shaped metalwork 9 is fallen from the bottom surface of the electromagnet 8.
Other than passing through rotating part 7 around ontology 3 and hanging with article, article can also be hung up in the lower section of ontology 3.?
When loading article on U-shaped metalwork 9, first controls electromagnet 8 and power off, article is hung on U-shaped metalwork 9, then U-shaped metal
Part 9 is placed on the bottom surface of electromagnet 8, then controls electromagnet 8 and be powered so that U-shaped metalwork 9 is adsorbed on the bottom surface of electromagnet 8, so that it may
Completion loads article on U-shaped metalwork 9.After unmanned plane during flying is to locality, it is only necessary to control the power-off of electromagnet 8, electricity
Article will be fallen with U-shaped metalwork 9 after magnet 8 loses magnetism, and complete to jettisoning.
It is jettisoninged by electromagnet 8 and U-shaped metalwork 9, electromagnet 8 has the advantages that reaction speed is fast, is suitable for tight
First aid such as helps at the scenes.Meanwhile article hangs over the lower section of ontology 3 by U-shaped metalwork 9, improves the loading energy for pendant of originally jettisoninging
Power.
The material of the U-shaped metalwork 9 is iron.Iron is a kind of excellent hard magnetic material, using iron as U-shaped metalwork 9
Material, electromagnet 8 be powered after enable to U-shaped metalwork 9 to be preferably adsorbed on electromagnet 8.In addition, giving birth in order to prevent
Rust is provided with a nickel protection layer on the surface of U-shaped metalwork 9, and U-shaped metal is arranged in by the way of plating in the nickel protection layer
The surface of part 9.
Preferably, the first switch 31 for controlling 8 power on/off of electromagnet is additionally provided on the ontology 3, it is described
The second switch 32 for controlling the movement of the driving component 5 is additionally provided in support component 4.
It under normal conditions, is all that 8 power on/off of electromagnet and the control movement ability of driving assembly 5 are controlled by remotely operating
Realization is jettisoninged, and during loading article, if controlling 8 power on/off of electromagnet and control driving group yet by remote operation
Part 5 acts, and great inconvenience will be brought to loading process, it is disconnected that operator must control electromagnet 8 by remotely operating
Electricity and control driving assembly 5 drive rotating part 7 far from fixed part 6, after loading onto article, then by remotely operating control electromagnet
8, which are powered and control driving assembly 5, drives rotating part 7 to contact with fixed part 6.Therefore, it is additionally provided on the body 3 for controlling electricity
The first switch 31 of 8 power on/off of magnet is additionally provided with the second switch 32 for controlling the movement of driving assembly 5 in support component 4.
It during loading article, presses first switch 31 and controls the power-off of electromagnet 8, press the control of first switch 31 again after loading onto article
Electromagnet 8 processed is powered, and article can be locked on U-shaped metalwork 9；Likewise, pressing the just controllable driving of second switch 32
Component 5 drives rotating part 7 to separate with fixed part 6, presses second switch 32 again after loading onto article, control driving assembly 5 drives rotation
Transfer part 7 is contacted with fixed part 6, article can be locked on rotating part 7.Therefore, pass through first switch 31 and second switch 32
Article loading can easily be carried out.
Preferably, the ontology 3 includes first side plate, second side plate, third side panel, fourth side panel, the 5th
Side panel and sixth side panel, the first side plate, the second side plate, the third side panel, the 4th side
Plate, the fifth side panel and the sixth side panel surround the tubular structure of a regular hexagon, the centre of the tubular structure
Offer the circular cavity for placing electromagnet 8, the first side plate, the third side panel and the fifth side panel
Outer surface on be provided with heat dissipation vertical bar.
On the one hand, heat dissipation vertical bar can be improved radiating efficiency, export the heat caused by the course of work of electromagnet 8 in time
Amount；On the other hand, electromagnet 8 is arranged in circular cavity, can be improved its anti-electromagnetic interference capability, so that control unmanned plane
Interference will not be generated between electromagnetic signal and the electromagnetic signal for controlling electromagnet 8.
Preferably, ontology 3 is the tubular structure of a regular hexagon, and three support components 4 are separately positioned on described the
On the outer surface of two side faces plate, the fourth side panel and the sixth side panel, enable to three support components 4 uniform
Distribution on the body 3, guarantees the stability of unmanned plane in the process in flight.
It jettisonings in conclusion being different from hanging rod in the prior art and carrying out article by way of moving horizontally, is originally jettisoninging
In pendant, rotating part 7 is contacted or is separated with fixed part 6 by way of rotation.On the one hand, 7 need of rotating part pass through rotation
Can be realized contacted with fixed part 6 perhaps separate avoid during jettisoninging because article or rotating part 7 are past by card can not
Smoothly jettisoning；On the other hand, rotating part 7 is moved by way of rotation, even if rotating part 7 is deformed because article is too heavy,
Also it can guarantee that rotating part 7 being capable of normal reset after the completion of jettisoninging.
It should be understood that the application of the present invention is not limited to the above for those of ordinary skills can
With improvement or transformation based on the above description, all these modifications and variations all should belong to the guarantor of appended claims of the present invention
Protect range.
Claims (10)
1. a kind of unmanned plane throwing device, it is characterised in that: including Fast detachable unit and pendant of jettisoninging；
The Fast detachable unit includes the first connection component and the second connection component；
First connection component includes first connecting portion and fixed outer ring, and the first connecting portion is rotatably set in described
In fixed outer ring, the upper surface of the fixed outer ring is fixedly connected with the bottom of unmanned plane；
Second connection component includes second connecting portion, the top of the lower surface of the second connecting portion and the ontology for pendant of jettisoninging
Portion is fixedly connected；
First interface slot is offered in the first connecting portion, is offered in the second connecting portion and the first interface slot pair
The second interface slot answered；It is provided with the first locking piece in the first connecting portion, the second lock is provided in the second connecting portion
Determine part, after first locking piece and the second locking piece mutually locking, the second connecting portion is revolved with the first connecting portion
Then rotation；
It is provided with the first shackle member on the fixed outer ring, is provided with the second shackle member in the second connecting portion, described second
Interconnecting piece is connected in the first shackle member by the second shackle member and is fixedly connected with the fixed outer ring；
The pendant of jettisoninging includes the multiple support components of ontology and setting on the body；
It is provided with driving assembly and fixed part in the support component, torque output is provided in the driving component, it is described
Driving assembly is connected by torque output with a rotating part, and the rotating part is revolved with the rotation of the torque output
Turn, the hook for hanging article is provided on the rotating part, the driving component drives the rotation by torque output
Transfer part contacts or separates with the fixed part.
2. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: first connection component further includes
The upper surface of first pedestal, the fixed outer ring is fixedly connected by first pedestal with the bottom of unmanned plane, and described first
The lower surface of pedestal is connect with the upper surface of the fixed outer ring, and first connecting portion setting is in first pedestal and described
Between fixed outer ring；
Second connection component further includes the second pedestal, and the second connecting portion is fixed at the upper table of second pedestal
Face, the second connecting portion at the top of second pedestal and the ontology for pendant of jettisoninging by being fixedly connected.
3. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: the inner wall of the fixed outer ring is along week
To support annulus is provided with, the first connecting portion is set in the fixed outer ring, and the bottom of the first connecting portion
It is connected on the support annulus；
First shackle member is the blind slot being circumferentially disposed on the inner wall of the fixed outer ring, and the blind slot is arranged described
Support the lower section of annulus；
The bottom of the inner wall of the fixed outer ring is provided with several mounting grooves, and the lower section of the blind slot is arranged in the mounting groove
And it is connected with the blind slot；
Second shackle member is several protruding blocks being arranged on the outer wall of the second connecting portion, the protruding block and institute
It states mounting groove to be mutually matched, for the protruding block after the mounting groove is inserted in the blind slot, the second connecting portion passes through institute
Protruding block is stated to be connected in the blind slot and be fixedly connected with the fixed outer ring.
4. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: first locking piece is convex
It rises, the lower surface of the first connecting portion is arranged in the positioning protrusion, and second locking piece is and the positioning protrusion pair
The upper surface of the second connecting portion is arranged in the positioning groove answered, the positioning groove.
5. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: the top of the inner wall of the fixed outer ring
Portion offers limiting groove, and the outer wall of the first connecting portion is provided with spacing block set corresponding with the limiting groove, described
First connecting portion drives the spacing block set to rotate in the range of the limiting groove.
6. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: the support component includes top surface
Plate, bottom panel, the first side plate and the second side plate；
The top panel, first side plate, the bottom panel and second side plate join end to end and form frame structure, described
One end of frame structure is connected with the ontology, and the other end of the frame structure forms installing port, and the driving component passes through
Installing port is arranged in support component；
The bottom panel is further fixedly arranged on an extension plate in one end far from the ontology, and the driving component is arranged described
On bottom panel and the extension plate；
The side of the extension plate lower surface is arranged in the fixed part, and the rotating part is movably disposed in the extension plate
The other side of lower surface.
7. a kind of unmanned plane throwing device according to claim 6, it is characterised in that: the lower surface of the extension plate and institute
It states the opposite side of fixed part and is additionally provided with a limiting slot, the rotating part is movably disposed in the limiting slot.
8. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: the rotating part include connector,
First swingle, the second swingle, third swingle and the 4th swingle, the connector and the torque output are fixed to be connected
It connects, one end of first swingle is fixedly connected with the connector, first swingle, second swingle, institute
It states third swingle and the 4th swingle is sequentially connected；
Second swingle is vertically arranged, and the angle between first swingle and second swingle is 120 °, institute
Stating the angle between the second swingle and the third swingle is 120 °, the third swingle and the 4th swingle it
Between angle be 120 °.
9. a kind of unmanned plane throwing device according to claim 1, it is characterised in that: the bottom center of the ontology is also set
It is equipped with electromagnet, the bottom surface of the electromagnet is provided with a U-shaped metalwork, the U-shaped metalwork when the electromagnet is powered
It is adsorbed on the bottom surface of the electromagnet, the U-shaped metalwork is fallen from the bottom surface of the electromagnet when electromagnet power-off.
10. a kind of unmanned plane throwing device according to claim 9, it is characterised in that: be additionally provided with use on the ontology
It is dynamic for controlling the driving component in being additionally provided in the first switch for controlling the magnet switching electricity, the support component
The second switch of work.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811052808.9A CN109159897B (en) | 2018-09-10 | 2018-09-10 | Unmanned aerial vehicle jettison device |
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| CN201811052808.9A CN109159897B (en) | 2018-09-10 | 2018-09-10 | Unmanned aerial vehicle jettison device |
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| CN109159897B CN109159897B (en) | 2022-04-05 |
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| CN106956776A (en) * | 2017-05-11 | 2017-07-18 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane throwing device and unmanned plane |
| CN108001695A (en) * | 2017-11-15 | 2018-05-08 | 深圳市科比特航空科技有限公司 | The device for quickly disassembling of unmanned plane |
| CN207565852U (en) * | 2017-11-23 | 2018-07-03 | 深圳市科比特航空科技有限公司 | Fast disassembly type throwing device and Quick-dismantle component |
| CN207826556U (en) * | 2017-12-12 | 2018-09-07 | 常州市庆中风机制造有限公司 | Unmanned plane dropping gear |
| CN108128461A (en) * | 2017-12-28 | 2018-06-08 | 深圳城际快机科技有限公司 | A kind of throwing device based on unmanned aerial vehicle platform |
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