CN206984312U - Empennage quick-disassembly structure - Google Patents
Empennage quick-disassembly structure Download PDFInfo
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- CN206984312U CN206984312U CN201720512133.6U CN201720512133U CN206984312U CN 206984312 U CN206984312 U CN 206984312U CN 201720512133 U CN201720512133 U CN 201720512133U CN 206984312 U CN206984312 U CN 206984312U
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- empennage
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- stage casing
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Abstract
The utility model proposes a kind of empennage quick-disassembly structure, including：Empennage stage casing, port tailplane point, starboard tailplane point and bayonet connection；The port tailplane point and starboard tailplane point are detachably connected on the left and right sides in the empennage stage casing by the bayonet connection respectively.Empennage quick-disassembly structure of the present utility model, dismounting is very convenient, is advantageous to packaging miniaturization.
Description
Technical field
It the utility model is related to unmanned vehicle empennage technical field, more particularly to a kind of empennage quick-disassembly structure.
Background technology
Typically there is empennage on fixed-wing unmanned vehicle.The stable and manipulation that rises that empennage is mounted in aircraft aft is made
Device.Empennage is generally divided into vertical tail and tailplane.
Vertical tail abbreviation vertical fin or vertical tail, by fixed fixed fin with movable rudder unit into it is flying
Main direction of plaing a part of is stabilized and directional control on device.Vertical tail is positioned only at the top of aircraft axis, because
During takeoff and anding, Vehicle nose faces upward, and it is close that afterbody is liftoff, can not arrange vertical fin aerofoil.It is identical with horizontal tail, vertical fin aerofoil
What first half was usually fixed, claim fixed fin, latter half is hinged on stabilization rear portion, can manipulate deflection, claims direction
Rudder.
At present, the empennage of unmanned vehicle is connected with fuselage, once it is made just non-dismountable or needs specific purpose tool
Dismantled and placed, it is necessary to configure larger space in packing box, cause the Package size larger, not readily transportable storage etc..
Utility model content
Technical problem to be solved in the utility model is to provide a kind of empennage quick-disassembly structure, and dismounting is very convenient, favorably
Minimized in packaging.
To solve the above problems, the utility model proposes a kind of empennage quick-disassembly structure, including：Empennage stage casing, port tailplane point,
Starboard tailplane point and bayonet connection；The port tailplane point and starboard tailplane point are detachably connected on by the bayonet connection respectively
The left and right sides in the empennage stage casing.
According to one embodiment of the present utility model, the port tailplane point, the stable facial and empennage of starboard tailplane point
The stable facial docking location in stage casing is provided with the bayonet connection；In the rudder face portion and the empennage of the port tailplane point
The right standard rudder face in the rudder face portion and the empennage stage casing of the facial docking location of the left rudder of section and starboard tailplane point docks position
Put the male-female engagement part for being provided with mutually contraposition grafting.
According to one embodiment of the present utility model, it is provided with the left rudder in empennage stage casing face, right standard rudder face
Projection or groove, the rudder face portion of the port tailplane point, the starboard tailplane are provided with groove or projection in sharp rudder face portion, described
The facial rudder face portion with the rudder face portion of port tailplane point, starboard tailplane point of left rudder face, right standard rudder in empennage stage casing passes through convex
Achieved a butt joint in block insertion groove, so that left rudder face, the right standard rudder face in the empennage stage casing can drive the port tailplane point
Rudder face portion, the starboard tailplane point rudder face action.
According to one embodiment of the present utility model, in addition to rudder face drive device and transmission mechanism；The rudder face driving
Device is arranged on the stable face in the empennage stage casing, to drive the transmission mechanism to act；The transmission mechanism connection
Left rudder face, the right standard rudder face in the empennage stage casing, drive the left rudder face, the right side under the driving of the rudder face drive device
Rudder face action.
According to one embodiment of the present utility model, it is additionally provided with the sharp stable face of the port tailplane point, starboard tailplane
Locating piece or locating slot, the stable facial correspondence position in the empennage stage casing also set up locating slot or locating piece, the left tail
Wing tip, stable facial realized with the stable face in the empennage stage casing by locating piece insertion locating slot of starboard tailplane point position.
According to one embodiment of the present utility model, the port tailplane point, starboard tailplane point, the bayonet connection in empennage stage casing
The both sides of position are provided with locating piece or locating slot.
According to one embodiment of the present utility model, the port tailplane is sharp with also having connect the in the empennage stage casing
One strengthens passage, and the first bracing piece is inserted with the first reinforcement passage, is also had in the starboard tailplane point and empennage stage casing
The second of connection strengthens passage, and the second bracing piece is inserted with the second reinforcement passage.
According to one embodiment of the present utility model, the stable face in the empennage stage casing is also fixed with for connecting fuselage
Foot piece.
According to one embodiment of the present utility model, the bayonet connection includes pin thread structure and box structure；It is described
Empennage stage casing sets the pin thread structure or box structure, and the port tailplane point and starboard tailplane point set the box structure or public affairs
Buckle structure；
The pin thread structure includes the body portion and head of connection, and the both sides on the head are outstanding；The box structure
Including gateway and positioned at gateway with respect to both sides left card, right card, and the left card and right card relatively it is described go out
The distal end of entrance is close to each other；The opening degree of the gateway is enough to make the head to pass in and out, the left card and right card
The distal end elastic deformation can step down under the extruding of the protrusion both sides on head and pass in and out head, the left card and right card
Piece can hold the head of entrance tightly.
According to one embodiment of the present utility model, the left card and right card from the near-end of relatively described gateway to
Distal end is gradually close to each other, and the relative distance of the left card and right card is proximally to distally gradually from more than the head
The outermost end spacing of prominent both sides fades to the outermost end spacing of the protrusion both sides less than the head.
After adopting the above technical scheme, the utility model has the advantages that compared with prior art：
Empennage is divided into three sections, thus in packaging, port tailplane point and starboard tailplane point can be torn open from empennage stage casing
Unload down, reasonable disposition space is placed, and is advantageous to reduce Package size, is readily transported storage；Port tailplane point, starboard tailplane point with
Empennage is connected between stage casing by bayonet connection, need to only align clamping during connection, need to only extract separation during dismounting, can be tool-free
Dismounting, it is very convenient；
By rudder face drive device be arranged on empennage stage casing rather than port tailplane point, on starboard tailplane point, by transmission mechanism come
Drive rudder face rather than rudder face drive device directly to drive, the thicker wall in empennage stage casing can be made full use of to be driven to house rudder face
Device, it is ensured that empennage point structure is not strong easily broken, it also avoid electrical between fuselage control circuit and rudder face drive device
Circuit is long, connects the problem of unstable etc. in detachable part.
Brief description of the drawings
Fig. 1 is the structural representation of the empennage quick-disassembly structure of the embodiment of the utility model one；
Fig. 2 is the X partial enlargement structural representations of Fig. 1 empennage quick-disassembly structure；
Fig. 3 is the structural representation of the bayonet connection of the embodiment of the utility model one.
Description of symbols in figure：
1- empennages stage casing, the stable face in 11- empennages stage casing, the right standard rudder face in 12- empennages stage casing, 2- port tailplanes point, 3-
Starboard tailplane point, the stable face of 31- starboard tailplanes point, the rudder face portion of 32- starboard tailplanes point, the bracing pieces of 4- first, the bracing pieces of 5- second,
6- foot pieces, 71- pin thread structures, 72- box structures, 121- projections, 321- grooves, 711- bodies portion, 712- heads, the left cards of 721-
Piece, the right cards of 722-, 81- locating slots, 82- locating pieces, 9- transmission mechanisms.
Embodiment
To enable above-mentioned purpose of the present utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings to this
The embodiment of utility model is described in detail.
Many details are elaborated in the following description in order to fully understand the utility model.But this practicality is new
Type can be to be much different from other manner described here to implement, and those skilled in the art can be new without prejudice to this practicality
Similar popularization is done in the case of type intension, therefore the utility model is not limited by following public specific implementation.
Referring to Fig. 1, in one embodiment, empennage quick-disassembly structure includes：Empennage stage casing 1, port tailplane point 2, starboard tailplane point 3
And bayonet connection (71 and 72).Port tailplane point 2 and starboard tailplane point 3 are detachably connected in empennage by bayonet connection respectively
The left and right sides of section 1.
Empennage is divided into three sections, and respectively empennage stage casing 1, port tailplane point 2 and starboard tailplane point 3, port tailplane point 2 is connected by buckle
Fitting is detachably connected on the left side in empennage stage casing 1, and starboard tailplane point 3 is detachably connected empennage stage casing 1 by bayonet connection
Right side.
In the present embodiment, thus it is shown that vertical tail is divided into three sections and is connected with each other by bayonet connection, but
It is appreciated that or tailplane be divided into three sections and be connected with each other by bayonet connection, difference is empennage
It is horizontal.
Empennage is divided into three sections, thus in packaging, can be from empennage stage casing 1 by port tailplane point 2 and starboard tailplane point 3
Disassemble, reasonable disposition space is placed, and is advantageous to reduce Package size, is readily transported storage；Port tailplane point 2, starboard tailplane
Connected between point 3 and empennage stage casing 1 by bayonet connection, need to only align clamping during connection, need to only extract separation during dismounting, can
Tool-free dismounting, it is very convenient.
In one embodiment, the stable face and stable facial pair in empennage stage casing 1 of port tailplane point 2, starboard tailplane point 3
Connect position and be provided with bayonet connection.Referring to Fig. 1 and Fig. 2, optionally, bayonet connection includes pin thread structure 71 and box structure
72, port tailplane point 2 it is stable face, starboard tailplane point 3 stable facial 31 docking location on be provided with box structure 72, tail
Pin thread structure 71 is provided with stable facial 11 docking location in wing stage casing 1, certainly also can be conversely, port tailplane point 2, right tail
The box structure 72 of wing tip 3 gets up to complete the assembling of empennage with the snapping of pin thread structure 71 in empennage stage casing 1.
The docking location of left rudder face and the rudder face portion of starboard tailplane point 3 of the rudder face portion of port tailplane point 2 with empennage stage casing 1
32 are provided with the male-female engagement part of mutually contraposition grafting with the docking location of the right standard rudder face 12 in empennage stage casing 1.Due to empennage
Stabilization and rudder face be hinged, thus also need to when clamping is relatively fixed between each section of stabilization to ensure each section of rudder face it
Between be also relatively fixed, the rudder face portion of port tailplane point 2 is inserted with the left rudder face in empennage stage casing 1 by the contraposition of male-female engagement part
Connect and realize both be relatively fixed, the rudder face portion 32 of starboard tailplane point 3 passes through male-female engagement part with the right standard rudder face 12 in empennage stage casing 1
Contraposition grafting realize that both are relatively fixed.
In one embodiment, male-female engagement part is groove and projection.Referring to Fig. 2, the left rudder face in empennage stage casing 1, the right side
Projection 121 is provided with rudder face portion 12, groove is provided with the rudder face portion of port tailplane point 2, the rudder face portion 32 of starboard tailplane point 3
321.Certainly also can be conversely, the left rudder face in empennage stage casing 1, being provided with groove, the rudder face of port tailplane point 2 on right standard rudder face
Portion, starboard tailplane point 3 rudder face portion on be provided with projection.Empennage stage casing 1 left rudder face, right standard rudder face 12 respectively with port tailplane
Sharp 2 rudder face portion, the rudder face portion 32 of starboard tailplane point 3 are inserted in groove 321 by projection 121 and achieved a butt joint, so that empennage stage casing 1
Left rudder face, right standard rudder face 12 the rudder face portion 32 of the rudder face portion of port tailplane point 2, starboard tailplane point 3 can be driven to act.
Because the stable face of empennage stage casing 1, port tailplane point 2, starboard tailplane point 3 has been snapped connection and is fixed up, thus
Only need to limit the relative movement of other side between rudder face portion by male-female engagement part, without being carried out again between rudder face portion
Clamping, when empennage is connected, groove and the projection in rudder face portion only need contraposition to insert, and dismounting is more convenient.
In one embodiment, empennage quick-disassembly structure can also include rudder face drive device (not shown) and driver
Structure 9.Rudder face drive device is, for example, steering wheel etc., is arranged on stable facial the 11 of empennage stage casing 1, to drive transmission device 9
Action.Transmission mechanism 9 can include two groups, on the one hand one group of transmission mechanism connects output end, the opposing party of rudder face drive device
On the one hand the left rudder face in face connection empennage stage casing 1, another group of transmission mechanism connect output end, the opposing party of rudder face drive device
The right standard rudder face 12 in face connection empennage stage casing 1, drive left rudder face, right standard rudder face 12 dynamic under the driving of rudder face drive device
Make.Two groups of transmission mechanisms 9 can under the driving of rudder face drive device synchronization action, realize the synchronization action of left and right rudder face.Pass
Motivation structure 9 can be existing transmission mechanism, can be formed by several rod hinge connections, under the driving of rudder face drive device,
The rudder face action that linkage drives the other end occurs between connecting rod.
By rudder face drive device be arranged on empennage stage casing 1 rather than port tailplane point 2, starboard tailplane point 3 on, pass through transmission mechanism
9 drive the rudder face rather than rudder face drive device directly to drive, and can make full use of the thicker wall in empennage stage casing 1 to house rudder face
Drive device, it is ensured that empennage point structure is not strong easily broken, it also avoid between fuselage control circuit and rudder face drive device
Electrical interconnection is long, connects the problem of unstable etc. in detachable part.
In one embodiment, referring to Fig. 2, locating slot, starboard tailplane point 3 are additionally provided with the stable face of port tailplane point 2
Stable facial 31 on be additionally provided with locating slot 81, stable facial 11 correspondence position in empennage stage casing 1 also sets up locating piece 82,
Can certainly be conversely, being provided with locating piece, the stable facial corresponding position in empennage stage casing on the stable face of left and right empennage point
Install locating slot.The stable face of port tailplane point 2 inserts locating slot reality with stable facial the 11 of empennage stage casing 1 by locating piece
Now position, stable facial the 31 of starboard tailplane point 3 insert locating slot 81 in fact with stable facial the 11 of empennage stage casing 1 by locating piece 82
Now position.
Preferably, port tailplane point 2, starboard tailplane point 3, empennage stage casing 1 bayonet connection position both sides be provided with it is fixed
Position block or locating slot.Locating slot on the stable face of port tailplane point 2 is arranged on the both sides of box structure, on starboard tailplane point 3
It is in this way, stable facial 11 locating piece 82 in empennage stage casing 1 is arranged on the both sides of pin thread structure 71, locating piece 82 and locating slot
81 are collinearly set with bayonet connection, fast positioning can be achieved, after connection, locating piece 82 and locating slot 81 can limit the two of connection
Individual part rotates or moved up and down so that structure is more stable.
More excellent, the locating piece 82 of both sides or the shape of cross section of locating slot 81 are in half frame-type, and frame opening is towards each
Self-corresponding bayonet connection structure.The mutual cooperation of left and right location structure, locating piece 82 are not easy to be broken off, and structure is more firm,
Connection is also more stable.
In one embodiment, with also having connect first to strengthen passage in empennage stage casing 1, first adds port tailplane point 2
Be inserted with the first bracing piece 4 in strong passage, starboard tailplane point 3 with also there is the second reinforcement passage for connect in empennage stage casing 1, second
Strengthen being inserted with the second bracing piece 5 in passage.First bracing piece 4 and the second bracing piece 5 are preferably carbon fiber bar, light weight and
Sound construction, can be hollow.
In other words, the part of the first bracing piece 4 is through in port tailplane point 2, another part is through in empennage stage casing 1, and second
The part of bracing piece 5 is through in starboard tailplane point 3, another part is through in empennage stage casing 1, the first bracing piece 4 and the second bracing piece 5
The bonding strength for being detachably connected position can be strengthened, it is not readily separated or is disconnected, ensure the stability and fastness of structure.
In one embodiment, stable facial the 11 of empennage stage casing 1 are also fixed with the foot piece 6 for connecting fuselage.Fuselage
Electrical interconnection between control circuit and rudder face drive device can be from the interior cabling of foot piece 6, and foot piece 6 is connected with empennage stage casing 1 can
Ensure the connective stability of electrical interconnection or reduce the electrical connection complexity of connecting portion.
In one embodiment, bayonet connection includes pin thread structure and box structure；Empennage stage casing sets pin thread structure
Or box structure, port tailplane point and starboard tailplane point set box structure or pin thread structure, box structure or pin thread structure with it is corresponding
Connector can be formed in one structure.Referring to Fig. 2 and Fig. 3, empennage stage casing 1 sets pin thread structure 71, port tailplane point 2 and the right side
Empennage point 3 sets box structure 72.
Pin thread structure 71 includes the body portion 711 and head 712 of connection, and the both sides on head 712 are outstanding.Preferably, head
It is integrally formed structure between portion 712 and body portion 711, structure is more firm.More preferably, can be among head 712 and body portion 711
It is hollow out, is merely presented as frame-type, overall weight can be mitigated.
Box structure 72 includes gateway and positioned at left card 721, right card 722 of the gateway with respect to both sides.Gateway
It can open up to be formed on port tailplane point 2 and starboard tailplane point 3.Left card 721 and right card 722 are respectively positioned at the relative of gateway
Both sides, and left card 721 and right card 722 are close to each other with respect to the distal end of gateway, in other words, left card 721 and right card
The distance between 722 both ends of remote gateway are than the distance between near-end closer to the distance between specific distal end root
The outermost spacing protruded according to the both sides on head determines.Left card 721, right card 722 can be the hard with certain elasticity
Plates.
The opening degree of gateway is enough to pass in and out head 712, so as to which pin thread structure 71 can not set left card from gateway
The side of piece 721 and right card 722 enters, and is plugged between left card 721 and right card 722, can also be exited from gateway.It is left
The distal end of card 721 and right card 722 elastic deformation can step down under the extruding of the protrusion both sides on head and enter head 712
Go out.In other words, when needing clamping, head 712 enters from gateway, when reaching far-end, is acted on by pressed by external force, head
712 protrusion both sides extrude left card 721 and right card 722, left card 721 and the elastic deformation of right card 721 and opened to both sides,
When the protrusion both sides on head 712 reach the outside of left card 721 and right card 722, left card 721 and right card 722
Reset and collapse again, head is just held tightly by left card 721 and right card 722, realizes empennage stage casing 1 and port tailplane point 2, starboard tailplane point
3 connect and fix.When detachment is desired, acted on by external force drawing, the protrusion both sides on head 712 extrude left card 721 and the right side again
Card 722 makes its elastic deformation open and step down to both sides, so as to which head 712 can depart from left card 721 and right card 722,
Come out from gateway, realize that empennage stage casing 1 and the dismounting of port tailplane point 2, starboard tailplane point 3 separate.
Pin thread structure 71 and box structure 72 pass through between the protrusion both sides on head 712 and left card 721, right card 722
Cooperation realize clamping, depart from, head 712 protrude both sides can by strut left card 721 and right card 722 and enter or move back
Go out, only needing during use to apply relative pressing force or pulling capacity in pin thread structure 71 and box structure 72 can realize soon
Speed dismounting, it is very convenient；Meanwhile left card 721 and right card 722 can hold the head 712 entered therebetween tightly, and due to head
The protrusion both sides limitation in portion 712 is, it is necessary to left card 721 and right card 722 could be opened by applying certain pulling capacity, thus head
Spacing effect, thus the He of pin thread structure 71 after connection are played to left card 721 and right card 722 in the protrusion both sides in portion 712
It is not easy to loosen between box structure 72, empennage stage casing 1 and the connection of port tailplane point 2, starboard tailplane point 3 are more stable.
In one embodiment, with continued reference to Fig. 3, left card 721 and right card 722 are from the near-end of relative gateway to remote
End is gradually close to each other, that is to say, that the relative distance of left card 721 and right card 722 proximally to being distally gradually reduced, and
And the relative distance of left card 721 and right card 722 is proximally to distally gradually from the outermost of the protrusion both sides more than head 712
End spacing fades to the outermost end spacing of the protrusion both sides less than head 712.The outermost end spacing of the protrusion both sides on head 712 refers to
Head 712 protrudes the distance between outermost end of both sides.
It is gradually reduced left card 721 and right card 722 are arranged at the gateway to distant place spacing, and from big
Outermost end spacing in the protrusion both sides on head 712 becomes less than the outermost end spacing of the protrusion both sides on head 712, thus head
712 protrusion both sides can start gradually to strut the left He of card 721 at the midway position for entering left card 721 and right card 722
Right card 722, connects very comfortable, is not easy to damage left card 721 and right card 722.
Although the utility model is disclosed as above with preferred embodiment, it is not for limiting claim, Ren Heben
Art personnel are not being departed from spirit and scope of the present utility model, can make possible variation and modification, therefore
The scope of protection of the utility model should be defined by the scope that the utility model claims are defined.
Claims (9)
- A kind of 1. empennage quick-disassembly structure, it is characterised in that including：Empennage stage casing, port tailplane point, starboard tailplane is sharp and snaps connection Part；The port tailplane point and starboard tailplane point are detachably connected on the left and right in the empennage stage casing by the bayonet connection respectively Both sides；The bayonet connection includes pin thread structure and box structure；The empennage stage casing sets the pin thread structure or box knot Structure, the port tailplane point and starboard tailplane point set the box structure or pin thread structure；The pin thread structure includes the body portion and head of connection, and the both sides on the head are outstanding；The box structure includes Gateway and left card, the right card positioned at the relative both sides in gateway, and the left card and the relatively described gateway of right card Distal end it is close to each other；The opening degree of the gateway is enough to make the head to pass in and out, the left card and right card it is described Distal end elastic deformation can step down under the extruding of the protrusion both sides on head and pass in and out head, the left card and right card energy Hold tightly on enough heads by entrance.
- 2. empennage quick-disassembly structure as claimed in claim 1, it is characterised in that the port tailplane point, the stabilization of starboard tailplane point The stable facial docking location in portion and the empennage stage casing is provided with the bayonet connection；The rudder face portion of the port tailplane point With the docking location of the left rudder face in the empennage stage casing and the rudder face portion of starboard tailplane point and the right standard rudder in the empennage stage casing The docking location of face is provided with the male-female engagement part of mutually contraposition grafting.
- 3. empennage quick-disassembly structure as claimed in claim 2, it is characterised in that the left rudder face in the empennage stage casing, right standard rudder face Projection or groove are provided with portion, is provided with the rudder face portion of the port tailplane point, the rudder face portion of starboard tailplane point recessed Groove or projection, left rudder face, the right standard rudder in the empennage stage casing are facial sharp with the rudder face portion of port tailplane point, the starboard tailplane Rudder face portion by projection insert groove in achieve a butt joint so that the empennage stage casing left rudder face, right standard rudder face being capable of band The rudder face portion of the dynamic port tailplane point, the rudder face action of starboard tailplane point.
- 4. empennage quick-disassembly structure as claimed in claim 2 or claim 3, it is characterised in that also including rudder face drive device and driver Structure；The rudder face drive device is arranged on the stable face in the empennage stage casing, to drive the transmission mechanism to act；Institute State transmission mechanism and connect the left rudder face in the empennage stage casing, right standard rudder face, driven under the driving of the rudder face drive device The left rudder face, right standard rudder face action.
- 5. empennage quick-disassembly structure as claimed in claim 2, it is characterised in that the port tailplane point, the stabilization of starboard tailplane point Locating piece or locating slot are additionally provided with portion, the stable facial correspondence position in the empennage stage casing also sets up locating slot or positioning Block, the port tailplane point, the stable facial stable face with the empennage stage casing of starboard tailplane point are inserted by locating piece and positioned Groove realizes positioning.
- 6. empennage quick-disassembly structure as claimed in claim 5, it is characterised in that the port tailplane point, starboard tailplane point, empennage stage casing The both sides of bayonet connection position be provided with locating piece or locating slot.
- 7. empennage quick-disassembly structure as claimed in claim 2, it is characterised in that the port tailplane is sharp with being gone back in the empennage stage casing First with connection strengthens passage, and the first bracing piece, the starboard tailplane point and empennage are inserted with the first reinforcement passage Also have the second of connection to strengthen passage in stage casing, the second bracing piece is inserted with the second reinforcement passage.
- 8. empennage quick-disassembly structure as claimed in claim 2, it is characterised in that the stable face in the empennage stage casing is also fixed with For connecting the foot piece of fuselage.
- 9. empennage quick-disassembly structure as claimed in claim 1, it is characterised in that the left card and right card from relatively it is described go out The near-end of entrance is gradually close to each other to distal end, and the relative distance of the left card and right card is proximally to distally gradually from big Outermost end spacing in the protrusion both sides on the head fades to the outermost end spacing of the protrusion both sides less than the head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512133.6U CN206984312U (en) | 2017-05-09 | 2017-05-09 | Empennage quick-disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512133.6U CN206984312U (en) | 2017-05-09 | 2017-05-09 | Empennage quick-disassembly structure |
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| Publication Number | Publication Date |
|---|---|
| CN206984312U true CN206984312U (en) | 2018-02-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201720512133.6U Active CN206984312U (en) | 2017-05-09 | 2017-05-09 | Empennage quick-disassembly structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
-
2017
- 2017-05-09 CN CN201720512133.6U patent/CN206984312U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
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