CN206645037U - Head Quick-disassembling mechanism and unmanned plane - Google Patents

Head Quick-disassembling mechanism and unmanned plane Download PDF

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Publication number
CN206645037U
CN206645037U CN201720109044.7U CN201720109044U CN206645037U CN 206645037 U CN206645037 U CN 206645037U CN 201720109044 U CN201720109044 U CN 201720109044U CN 206645037 U CN206645037 U CN 206645037U
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head
quick
elastomer
accommodating cavity
tight lock
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CN201720109044.7U
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Chinese (zh)
Inventor
张显志
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Sichuan Yidian Aviation Technology Co., Ltd
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Shenzhen AEE Technology Co Ltd
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Priority to CN201720109044.7U priority Critical patent/CN206645037U/en
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Abstract

The utility model discloses a kind of head Quick-disassembling mechanism and unmanned plane, the head Quick-disassembling mechanism includes fixture and quick-disassembly structure, the fixture is provided with fixed shell, the quick-disassembly structure includes base, drawing article and elastomer, jack is provided with the side wall vertical with the elastomer of the fixed shell, the base covers the fixed shell and forms accommodating cavity, the elastomer is arranged in the accommodating cavity, one end of the elastomer connects the drawing article and the other end connects the base, the drawing article includes draw ring and tight lock part, it is outer to apply external force that the tab part stretches out the accommodating cavity, the tight lock part can pass through the jack and part is stretched out outside accommodating cavity and the tight lock part can be collapsible into accommodating cavity under the drive of external force through the jack.By way of draw ring is using the installation and dismounting of rear pull type, tight lock part is set to be slided in disassembly process more smooth, so that head Quick-disassembling mechanism is more laborsaving in disassembly process.

Description

Head Quick-disassembling mechanism and unmanned plane
Technical field
It the utility model is related to unmanned air vehicle technique field, more particularly to a kind of head Quick-disassembling mechanism and unmanned plane.
Background technology
Increasingly mature with unmanned air vehicle technique, unmanned plane has been widely used in take photo by plane photography, electric inspection process, environment prison The fields such as survey, forest fire protection, disaster inspection, anti-terrorism lifesaving, military surveillance, battle assessment.In such applications, it usually needs Various airborne equipments are carried on unmanned plane, to obtain certain types of environmental information, wherein using preferably at most picture pick-up device.Generally In the case of, picture pick-up device is arranged on unmanned plane by head, and head is directly fixedly connected with unmanned plane, is adopted mostly between the two It is locked with screw, so that convenient transportation, head and picture pick-up device are all that unmanned plane is arranged on before execution task On, existing head rapid dismounting apparatus is relatively elaborate when using hand push push rod in disassembly process, can exist during drawing Obvious interim card sense.
In view of the defects of above-mentioned, it is necessary to which a kind of new head Quick-disassembling mechanism is provided.
Utility model content
Main purpose of the present utility model is to provide a kind of head Quick-disassembling mechanism, it is intended to solves existing head assembling structure peace Dress is with dismantling the problem of harder.
To achieve the above object, the utility model proposes head Quick-disassembling mechanism include fixture and quick-disassembly structure, institute State fixture and be provided with fixed shell, the quick-disassembly structure includes base, drawing article and elastomer, the fixed shell with institute State and jack is provided with the vertical side wall of elastomer, the base covers the fixed shell and forms accommodating cavity, the elastomer It is arranged in the accommodating cavity, one end of the elastomer connects the drawing article and the other end connects the base, the drawing Moving part includes draw ring and tight lock part, and the tab part is stretched out outside the accommodating cavity to apply external force, and the tight lock part can Through the jack, part is stretched out outside accommodating cavity and the tight lock part can shrink under the drive of external force through the jack Enter in accommodating cavity.
Preferably, the tight lock part includes being formed as wedge, and the wedge reaches the appearance through the jack Put outside chamber.
Preferably, guide groove is provided with the fixed shell, being provided with the draw ring can be in the guide groove The projection of slip.
Preferably, the base includes bottom plate, on bottom plate in two supporting parts that are oppositely arranged and is connected to described two The baffle plate set between support part and close to one end of the supporting part, one end of the elastomer is connected with the draw ring, another End is connected with the baffle plate.
Preferably, the draw ring is provided with stopper slot on the side inwall of tight lock part, is provided with the baffle plate blind Hole, one end of the elastomer are connected by stopper slot with the draw ring, the other end of the elastomer by blind hole with it is described Baffle plate is connected.
Preferably, the base is also included in outside the blind hole and worn in two pieces of limiting plates being oppositely arranged, the elastomer The accommodation space that two pieces of limiting plates are formed is crossed with the bottom hole of the blind hole to be connected.
In addition, the utility model also provides a kind of unmanned plane, it includes fuselage, head and connected between fuselage and head Head erecting device, wherein, the head erecting device includes head damping device and head Quick Release machine as described above Structure, the fuselage are fixed on the fixture, and the base is fixed on the head damping device.
Preferably, the head damping device is provided with some inserted blocks, if the fixture corresponds to the inserted block and is provided with Dry socket, the inserted block are inserted into the socket with the fixation fixture and the head damping device.
Preferably, the limited block in the accommodating cavity is provided with the head damping device, on the limited block It is provided with the spacing hole passed through for the tight lock part.
Preferably, two inserted blocks, two inserted blocks and the limited block are provided with the head damping device On three angles of triangle.
In technical solutions of the utility model, quick-disassembly structure includes tight lock part and the draw ring being connected with tight lock part etc., and base is put In in draw ring, elastomer is resilient compressively being arranged between the inwall and base of close tight lock part one end of draw ring.This practicality The Detachable connection structure that new head Quick-disassembling mechanism is made up of quick-disassembly structure can realize the quick of head and unmanned plane Dismounting, while by way of draw ring is using the installation and dismounting of rear pull type, tight lock part is slided in disassembly process more smooth, from And make head Quick-disassembling mechanism more laborsaving in disassembly process.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 is the structure chart of the fixture of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 2 is the structure chart of the head damping device of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 3 is the structure decomposition figure of the quick-disassembly structure of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 4 is the enlarged drawing of the inserted block of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 5 is the enlarged drawing of the base of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 6 is the enlarged drawing of the drawing article of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 7 is the enlarged drawing of the limited block of the head Quick-disassembling mechanism of the utility model embodiment;
Fig. 8 is the quick-disassembly structure of head Quick-disassembling mechanism and the assembling figure of fixture of the utility model embodiment;
The sectional view that Fig. 9 is cut by the head Quick-disassembling mechanism in Fig. 8 along line A-A.
Drawing reference numeral explanation:
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only part of the embodiment of the present utility model, rather than all Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise Lower obtained every other embodiment, belong to the scope of the utility model protection.
It is to be appreciated that the directional instruction (such as up, down, left, right, before and after ...) of institute in the utility model embodiment It is only used for explaining relative position relation under a certain particular pose (as shown in drawings) between each part, motion conditions etc., such as When the fruit particular pose changes, then directionality instruction also correspondingly changes therewith.
In addition, and it can not be managed in the utility model such as relating to the description of " first ", " second " etc. is only used for describing purpose Solve to indicate or implying its relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, define " the One ", at least one this feature can be expressed or be implicitly included to the feature of " second ".It is " more in description of the present utility model It is individual " it is meant that at least two, such as two, three etc., unless otherwise specifically defined.
In the utility model, unless otherwise clearly defined and limited, term " connection ", " fixation " etc. should do broad sense reason Solution, for example, " fixation " can be fixedly connected or be detachably connected, or integrally;Can mechanically connect, also may be used Be electrical connection;Can be joined directly together, can also be indirectly connected by intermediary, can be the connection of two element internals Or the interaction relationship of two elements, limited unless otherwise clear and definite.For the ordinary skill in the art, can be with Concrete meaning of the above-mentioned term in the utility model is understood as the case may be.
In addition, the technical scheme between each embodiment of the utility model can be combined with each other, but must be with ability Domain those of ordinary skill can be implemented as basis, will be understood that when the combination appearance of technical scheme is conflicting or can not realize The combination of this technical scheme is not present, also not within the protection domain of the requires of the utility model.
The utility model proposes a kind of head Quick-disassembling mechanism, it is intended to solves existing head assembling structure installation with dismounting compared with expense The problem of power.
It refer to Fig. 1, Fig. 2, Fig. 3 and Fig. 4, in a kind of embodiment of the present utility model, head Quick-disassembling mechanism includes fixing Part 200 and quick-disassembly structure 300, fixture 200 are provided with fixed shell (not indicating), quick-disassembly structure 300 include base 310, Drawing article 330 and elastomer (not indicating), jack 230, base 310 are provided with the side wall vertical with elastomer of fixed shell Cover fixed shell and form accommodating cavity (not indicating), elastomer is arranged in accommodating cavity, one end connection drawing article 330 of elastomer And other end connect base 310, drawing article 330 include draw ring 332 and tight lock part 331, the part of draw ring 332 stretch out accommodating cavity it is outer with Just external force is applied, tight lock part 331 can pass through jack 230 and part stretches out outside accommodating cavity and tight lock part 331 can be in external force It is collapsible under drive through jack 230 in accommodating cavity.
The utility model also provides a kind of unmanned plane, it include fuselage, head and connection fuselage and head between cloud Platform erecting device, head erecting device includes head damping device 100 and head Quick-disassembling mechanism as described above, wherein fixed Part 200 is arranged on the fuselage of unmanned plane, can be fixed between the two by screw, base 310 is fixed on head damping device 100 On, and head is arranged on head damping device 100, and capture apparatus, such as video camera are carried by head.Thus, in nothing During man-machine execution task, being rapidly assembled and disassembled for capture apparatus can be realized by the head Quick-disassembling mechanism, and it is time saving and energy saving.
Specifically, head erecting device includes the fixture 200 that can be fixed on unmanned plane in the above-described embodiment With the head damping device 100 that can be fixed on head, be provided between fixture 200 and head damping device 100 for The quick-disassembly structure 300 and at least one inserted block 400 fixture 200 being removably mounted on head damping device 100.This reality Apply example to illustrate so that quick-disassembly structure and inserted block 400 are arranged on head damping device 100 as an example, quick-disassembly structure 300 includes Base 310, drawing article 330, elastomer and limited block 340, base 310 are fixed on head damping dress with the compartment of terrain of limited block 340 Put on 100, limited block 340 is located in accommodating cavity, and drawing article 330 (being specially tight lock part 331 hereinafter) slides with base 310 Coordinate.As shown in fig. 6, drawing article 330 includes tight lock part 331 and the draw ring 332 being connected with tight lock part, elastomer are resilient compressing Ground is arranged on base 310 and draw ring 332 between the inwall of the one end of tight lock part 331, as shown in fig. 7, limited block 340 is in face of lock Tight portion 331 and it is provided with the spacing hole 341 for being available for tight lock part 331 to insert.
The Detachable connection structure that head Quick-disassembling mechanism of the present utility model is made up of quick-disassembly structure 300 and inserted block 400 The fast assembling-disassembling of head and unmanned plane, while the dismounting mode by draw ring 332 using rear pull type can be realized, makes drawing article 330 in disassembly process, and slip is more smooth, so that head Quick-disassembling mechanism is more laborsaving in disassembly process.
In addition, in order to ensure that draw ring 332 can move in the predetermined direction, i.e. in order that tight lock part 331 can be suitable Its part is stretched out accommodating cavity outer and be collapsible into accommodating cavity, be provided with guide groove 240 in fixed shell, on draw ring 332 The projection (not indicating) that can be slided in guide groove 240 is provided with, stopper slot 333 of the projection in Fig. 6 is set, projection Slide in guide groove 240, be oriented to so as to the movement to draw ring 332.Also, drawing article 330 is parallel to fixture 200 are set, and drawing article 330 are oriented to by fixture 200, to cause Quick Release process more smooth.
Wherein, spacing hole 341 can be the be open blind hole or through hole of face tight lock part 331, the limit of the present embodiment Position hole 341 uses through-hole structure, thus provides more preferable firm effect to tight lock part.Draw ring 332 extend out to user and can held The position of operation, in assembly and disassembly head damping device 100, the lock for making drawing article 330 is pulled back by the hand-held draw ring Spacing hole 341 is left in tight portion 331, simple to operate.
In addition, as shown in figure 3, elastomer is preferably arranged to spring 320, it is easily compressed, and elasticity is big, is easy to head The dismounting of mounting structure.Or elastomer can also be rubber column (not shown), realize that head is installed using the elasticity of rubber column The dismounting of structure.
In the present embodiment, as shown in Fig. 2 head damping device 100 includes the first fixed plate 110, the second fixed plate 120 And be connected to multiple shock absorber parts 130 between the first fixed plate 110 and the second fixed plate 120, wherein quick-disassembly structure 300 and insert Block 400 is arranged in the first fixed plate 110, and respectively close to the opposite end of the first fixed plate 110.Shock absorber part 130 is in circle Tubular, naturally it is also possible in other any suitable shapes, there is the through hole through its both ends, consolidate for locking first will be used for The fastener 140 of the fixed plate 120 of fixed board 110 and second passes through, it is to be understood that in order that shock absorber part 130 effectively acts as Cushioning effect, at least one in the first fixed plate 110 and the second fixed plate 120 are slidably connected with fastener 140, and first is solid It can be movable relatively between the fixed plate 120 of fixed board 110 and second.In better embodiment, shock absorber part 130 is along the first fixed plate 110 and second fixed plate 120 circumferential distribution, such as in structure shown in Fig. 2, the first fixed plate 110 and the second fixed plate 120 Opposite sides be respectively arranged with three shock absorber parts 130.Thus, head rapid dismounting apparatus of the present utility model also has damping Function, when unmanned plane performs task (for example taking photo by plane), the vibrations of unmanned plane can be prevented to be transferred to by the head erecting device On picture pick-up device, the quality of data acquisition is improved.It should be noted that in other embodiments, above-mentioned head damping device 100 structure type can also be substituted by other structures, such as, head damping device 100 is only made up of a platy structure, structure It is simple and practical.
In addition, inserted block 400 is arranged on head damping device 100, and inserted block 400 and quick-disassembly structure 300 are respectively close to cloud The opposite end of platform damping device, as shown in figure 1, fixture 200 is provided with and the position correspondence of each inserted block 400 and supplies inserted block The socket 210 of 400 insertions, inserted block 400 are inserted into socket 210 to fix head damping device 100 and fixture 200, Gu Determine the jack 230 that part 200 is additionally provided with the position correspondence of tight lock part 331 and inserted for tight lock part 331.
During specific assembling, inserted block 400 is inserted into socket 210 first, now head damping device 100 is relative to solid Determine the angled angle of part 200 to set, i.e., one end of inserted block 400 is provided with head damping device 100 close to fixture 200, and one end of quick-disassembly structure 300 is provided with head damping device 100 away from fixture 200, then using external force backward Draw ring 332 is drawn, the tight lock part 331 of quick-disassembly structure 300 is slid into and releases the position that tight lock part 331 is interfered with jack 230, then make Head damping device 100 is positioned at the installation site relative to fixture 200, i.e., head damping device 100 is away from fixture 200 one end is moved towards fixture 200, finally cancels external force, and as shown in Figure 8 and Figure 9, tight lock part 331 is in restoring force It is extend under effect through jack 230 in spacing hole 3471, and completes the locking of fixture 200 and head damping device 100;Point When tearing open, apply external force first and pull back draw ring, the tight lock part of quick-disassembly structure 300 is housed completely into 230 space, then make Head damping device 100 leaves the installation site relative to fixture 200 and cancels external force, finally by inserted block 400 from socket 210 Middle extraction, and complete the dismounting to head damping device 100.So, head damping device 100 and fixture 200 are just realized Assembly and disassembly.
As can be seen here, the Detachable connection structure being made up of quick-disassembly structure 300 and inserted block 400 realizes head and nobody The fast assembling-disassembling of machine, structure design is simple, simple operation, switching performance are reliable, meanwhile, the tight lock part 331 of quick-disassembly structure 300 is logical Later pull-type slip, its slip is more smooth, so that disassembly process is more laborsaving.
Further, as shown in fig. 6, tight lock part 331 is arranged to lozenges (not indicating) in face of the end face of limited block 340, Lozenges is used to insert on fixture 200 and lozenges is close to the side of head damping device 100.So set and dismantling During head damping device 100, the hole wall of jack 230 is connected on lozenges, is acted on head damping device 100 so that head Damping device 100, which leaves itself and the external force of the installation site of fixture 200, can drive the opposing receptacle 230 of drawing article 330 to make a concession, So as to realize the fast quick-detach of head damping device 100.
Specifically, refer to Fig. 5, base 310 includes bottom plate 311, on bottom plate in two supporting parts 312 being oppositely arranged and The baffle plate 313 for being connected between two supporting parts and being set close to one end of supporting part, one end and the drawing article 330 of spring 320 (being specially draw ring 332) is connected, and the other end is connected with baffle plate 313.It is convex that the outside of supporting part 312 is provided with the installation to stretch out Portion (does not indicate), the lug-shaped of the installation convex portion semicircular in shape, and installation convex portion is provided with through hole, and the first fixed plate 110 is provided with Corresponding first screwed hole 111 of through hole with installing convex portion, base 310 is by the through hole through installation convex portion and screws in corresponding the The screw of one screwed hole 111 and be fixed in the first fixed plate 110.Limited block 340 is in square, itself and the first fixed plate 110 Two screwed holes (not shown) are provided with the end face to connect, the first fixed plate 110 is provided with each screw thread with limited block 340 One-to-one 3rd screwed hole 113 in hole, by screwing in screw back to the side of limited block 340 in the first fixed plate 110 Limited block 340 is securely locked.
Further, as shown in fig. 6, draw ring 332 is provided with stopper slot 333 on the side inwall of tight lock part 331, such as Shown in Fig. 5, blind hole 314 is provided with baffle plate 313, one end of spring 320 (is specially drawn by stopper slot 333 and drawing article 330 Ring 332) it is connected, the other end is connected by blind hole 314 with baffle plate 313, under the cooperation of stopper slot 333 and blind hole 314 so that bullet Spring 320 is limited in elastic telescopic in fixed position, can preferably consolidate spring 320, it is ensured that spring 320 is along drawing article The glide direction elongation and compression of 330 settings.
Specifically, as shown in figure 5, base 310 is also included in outside blind hole 314 in two pieces of limiting plates 315 being oppositely arranged, bullet The accommodation space that spring 320 is formed through limiting plate 315 is connected with the bottom hole of blind hole 314, so as to further limit the position of spring 320 Put.
Further, two inserted blocks 400 are provided with head damping device 100, it will be appreciated that the number of inserted block 400 is only For citing, in practical application, the number can be selected flexibly.Quick-disassembly structure 300 (being specially limited block 340) and two inserted blocks 400 On three angles of triangle, so that the attachment structure being collectively forming by quick-disassembly structure 300 and two inserted blocks 400 has Higher stability.Fixture 200 extends formed with avris plate with 400 corresponding edge of inserted block towards head damping device 100 (not indicating), avris plate include the first avris plate 211 and the second avris plate 212, avris plate, the first avris plate 211 and Two avris plates 212 are collectively forming fixed shell, and the through hole set on avris plate forms socket 210, wherein, the first avris plate 211 And second avris plate 212 be preferably set perpendicularly to the main part of fixture 200, and relative to pair of fixture 200 Plane is claimed to be symmetric.Fixture 200 and 300 corresponding side of quick-disassembly structure towards head damping device extend formed with In two piece of first plate 221 being oppositely arranged, and the second plate 222 being connected between two piece of first plate 221, two piece of first plate 221 And second plate 222 enclose the adapted space to be formed and be adapted to the face shaping of quick-disassembly structure 300 jointly, set on the second plate 222 Through hole form jack 230.It is noted that in order to simplify structure design, production cost is reduced, can also be not provided with two pieces the One plate 221, only retaining the second plate 222, this structure type equally meets the cooperation requirement of quick-disassembly structure 300 and fixture 200, But the above-mentioned structure with adapted space can prevent from coordinating head damping device 100 in place with more preferable fixed effect Swing is produced with fixture 200, reliability is higher.
Specifically, as shown in figure 4, inserted block 400 includes installation portion 410 and the shape being fixedly connected with head damping device 100 Into the plug division 420 on installation portion 410, plug division 420 has the clamping tongue 421 of the one end for protruding from installation portion 410, Clamping tongue 421 coordinates with the inserting of socket 210.In the present embodiment, inserted block 400 is fastened in the first fixed plate 110 by screw, For example installation portion 410 is provided with two screwed holes (not shown) in face of the first fixed plate, the first fixed plate 110 be provided with Second screwed hole 112 corresponding to each screwed hole of installation portion 410.When the first fixed plate 110 and inserted block 400 are working of plastics When, inserted block 400 can be shaped in the first fixed plate 110 by Shooting Technique, thus not only have higher bonding strength, and And save assembly process.For the ease of installation, while the scratch during socket 210 is inserted into of inserted block 400 is avoided to fix Chamfering or fillet processing are made in part 200, the end of clamping tongue 421.
Further, during head damping device 100 is installed, in order to reduce between plug division 420 and socket 210 Positioning requirements, plug division 420 is provided with the convex portion 422 away from clamping tongue 421 in face of the end face of fixture 200, such as Fig. 4 institutes Show, clamping tongue 421 and convex portion 422 are respectively positioned at the opposite end of plug division 420, and the convex portion 422 is used for and the shape of fixture 200 , must be bigger than clamping tongue 421 so as to which socket 210 is set into the cooperation being close to.
Finally, it should be noted that, in other embodiments, above-mentioned quick-disassembly structure 300 and inserted block 400 also may be provided at On fixture 200;Or quick-disassembly structure 300 is arranged on fixture 200, and inserted block 400 is arranged on head damping device 100 On;Or quick-disassembly structure 300 is arranged on head damping device 100, and inserted block 400 is arranged on fixture 200.At this Under a little embodiments, the assembling mode between fixture 200 and head damping device 100 can refer to described above, and remaining is not described Part will not be repeated here referring to above-described embodiment.
Preferred embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, Every equivalent structure under utility model of the present utility model design, made using the utility model specification and accompanying drawing content Conversion, or directly/be used in other related technical areas indirectly and be included in scope of patent protection of the present utility model.

Claims (10)

1. a kind of head Quick-disassembling mechanism, it is characterised in that the head Quick-disassembling mechanism includes fixture and quick-disassembly structure, described Fixture is provided with fixed shell, and the quick-disassembly structure includes base, drawing article and elastomer, the fixed shell with it is described Jack is provided with the vertical side wall of elastomer, the base covers the fixed shell and forms accommodating cavity, and the elastomer is set It is placed in the accommodating cavity, one end of the elastomer connects the drawing article and the other end connects the base, the pulling Part includes draw ring and tight lock part, and the tab part is stretched out outside the accommodating cavity to apply external force, and the tight lock part can be worn Cross the jack and part stretches out that accommodating cavity is outer and the tight lock part can be collapsible under the drive of external force through the jack In accommodating cavity.
2. head Quick-disassembling mechanism according to claim 1, it is characterised in that the tight lock part includes being formed as wedge, The wedge is reached outside the accommodating cavity through the jack.
3. head Quick-disassembling mechanism according to claim 1, it is characterised in that guide groove is provided with the fixed shell, The projection that can be slided in the guide groove is provided with the draw ring.
4. the head Quick-disassembling mechanism according to any one of claim 1-3, it is characterised in that the base include bottom plate, In two supporting parts that are oppositely arranged and it is connected between two supporting part and is set close to one end of the supporting part on bottom plate The baffle plate put, one end of the elastomer are connected with the draw ring, and the other end is connected with the baffle plate.
5. head Quick-disassembling mechanism according to claim 4, it is characterised in that side inwall of the draw ring close to tight lock part On be provided with stopper slot, blind hole is provided with the baffle plate, one end of the elastomer is connected by stopper slot with the draw ring, The other end of the elastomer is connected by blind hole with the baffle plate.
6. head Quick-disassembling mechanism according to claim 5, it is characterised in that the base, which is also included in outside the blind hole, is in Two pieces of limiting plates being oppositely arranged, the accommodation space and the hole of the blind hole that the elastomer is formed through two pieces of limiting plates Bottom is connected.
7. a kind of unmanned plane, it includes the head erecting device between fuselage, head and connection fuselage and head, and its feature exists In the head erecting device includes head damping device and the head Quick Release machine as any one of claim 1-6 Structure, the fuselage are fixed on the fixture, and the base is fixed on the head damping device.
8. unmanned plane as claimed in claim 7, it is characterised in that the head damping device is provided with some inserted blocks, described solid Determine part and correspond to the inserted block to be provided with some sockets, the inserted block is inserted into the socket with the fixation fixture and institute State head damping device.
9. unmanned plane as claimed in claim 8, it is characterised in that be provided with the head damping device positioned at the accommodating cavity Interior limited block, the spacing hole passed through for the tight lock part is provided with the limited block.
10. unmanned plane as claimed in claim 9, it is characterised in that two inserted blocks are provided with the head damping device, Two inserted blocks are located on three angles of triangle with the limited block.
CN201720109044.7U 2017-02-05 2017-02-05 Head Quick-disassembling mechanism and unmanned plane Active CN206645037U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720109044.7U CN206645037U (en) 2017-02-05 2017-02-05 Head Quick-disassembling mechanism and unmanned plane

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Application Number Priority Date Filing Date Title
CN201720109044.7U CN206645037U (en) 2017-02-05 2017-02-05 Head Quick-disassembling mechanism and unmanned plane

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CN206645037U true CN206645037U (en) 2017-11-17

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113911362A (en) * 2021-11-19 2022-01-11 广州成至智能机器科技有限公司 Unmanned aerial vehicle system ammunition throwing device
CN113911363A (en) * 2021-11-19 2022-01-11 广州成至智能机器科技有限公司 Unmanned aerial vehicle system ammunition dispenser

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113911362A (en) * 2021-11-19 2022-01-11 广州成至智能机器科技有限公司 Unmanned aerial vehicle system ammunition throwing device
CN113911363A (en) * 2021-11-19 2022-01-11 广州成至智能机器科技有限公司 Unmanned aerial vehicle system ammunition dispenser
CN113911362B (en) * 2021-11-19 2022-07-12 广州成至智能机器科技有限公司 Unmanned aerial vehicle system ammunition throwing device

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