CN105857570B - Lockable mechanism and unmanned plane - Google Patents
Lockable mechanism and unmanned plane Download PDFInfo
- Publication number
- CN105857570B CN105857570B CN201610183415.6A CN201610183415A CN105857570B CN 105857570 B CN105857570 B CN 105857570B CN 201610183415 A CN201610183415 A CN 201610183415A CN 105857570 B CN105857570 B CN 105857570B
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- China
- Prior art keywords
- inserted link
- matching seat
- fuselage
- card hole
- hole
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
Abstract
The present invention relates to the technical fields of pieces of equipment used in unmanned plane and its, provide a kind of lockable mechanism and unmanned plane, wherein lockable mechanism includes: matching seat, inserted link and locking part, the inserted link can be plugged in the matching seat, and the locking part is plugged in the locking realized on the matching seat to the inserted link.Using the above structure, without being cut off to intubation, it can linking together fuselage and wing or fuselage and fin stabilization, specially, the intubation not cut off is plugged in sleeve, at this point, synchronous inserted link can be plugged in matching seat, then again by the cooperation of locking part and matching seat, so as to ensure to be locked in inserted link is safe and reliable in matching seat.
Description
Technical field
The present invention relates to the technical fields of pieces of equipment used in unmanned plane and its, more particularly, to lockable mechanism and nobody
Machine.
Background technique
With the continuous development of science and technology, more and more unmanned planes are and large-scale towards the trend development of enlargement
The development trend of change just will increase the volume of unmanned plane, so that the whole Transporting to unmanned plane brings many inconvenience；However, being
It solving the above problems, it is ensured that lesser transport space can also complete the hauling operation of the unmanned plane to enlargement, so, people
Devise the unmanned plane that can be dismounted, that is, when transport, will be disassembled with wing and empennage slave, when it is desired to be used,
Then unmanned plane is re-assemblied again.
However, have higher requirement with respect to the stability of fuselage to wing and empennage since unmanned plane is in flight course,
Therefore, how by wing and fin stabilization, be simply locked on fuselage just and become extremely important.
Meanwhile in the prior art, wing and empennage are also fixed on fuselage through the mode frequently with grafting by people, and
This mode then needs to carry out semicircular excision to the intubation of connection fuselage and wing, so that it is guaranteed that wing and empennage can be steady
Fixed is connected on fuselage；Aforesaid way, due to that can cut off to intubation, this will reduce the stiffness and strength of intubation, from
And the service life of unmanned plane is reduced, but also safety can be reduced.
Summary of the invention
The purpose of the present invention is to provide lockable mechanisms and unmanned plane, existing in the prior art by wing and tail to solve
The connection type security reliability that the wing is locked on fuselage is poor but also the technical issues of reducing the service life of unmanned plane.
A kind of lockable mechanism provided by the invention, comprising: matching seat, inserted link and locking part, the inserted link can be plugged in
In the matching seat, the locking part is plugged in the locking realized on the matching seat to the inserted link.
Further, butt hole, the first card hole and the second card hole are provided on the matching seat, first card hole and described
Second card hole is symmetrically distributed in the two sides of the docking axially bored line, and runs through the butt hole；
Flange is provided on the inserted link, the flange is inserted into the butt hole；The locking part passes through described
The plane contact of first card hole and second card hole and the flange, to realize the locking to the inserted link.
Further, the flange is located on one end end face of the inserted link.
Further, the middle part of the inserted link is arranged in the flange, and third card hole and are additionally provided on the matching seat
Four card holes；
The third card hole and the 4th card hole are symmetrically distributed in the two sides of the docking axially bored line, and through described
Butt hole；
And the third card hole and the 4th card hole are respectively using the flange as axis and first card hole and described the
Two card holes are symmetrical arranged.
Further, the locking part is U-shaped fastener, and the fastener has the pretightning force inwardly engaged.
Further, the both ends of the fastener are in the curved portion being bent outwardly.
Further, fastener hole is provided on the matching seat, the fastener hole is used to for the matching seat being connected to described
On wing or fuselage.
The present invention also provides a kind of unmanned planes, comprising: lockable mechanism described in fuselage, wing and claim as above；
The matching seat and the inserted link are separately positioned on the interface of the fuselage and the wing；
Alternatively,
The matching seat and the inserted link are separately positioned on the interface of the wing and the fuselage.Further, institute
State inserted link and the matching seat quantity be it is multiple,
And multiple inserted links and multiple matching seats are evenly distributed on the interface of the fuselage and the wing
On；
Alternatively,
Multiple inserted links and multiple matching seats are evenly distributed on the interface of the wing and the fuselage.
The present invention also provides a kind of unmanned planes, comprising: lockable mechanism described in fuselage, empennage and claim as above；
The matching seat and the inserted link are separately positioned on the interface of the fuselage and the empennage；
Alternatively,
The matching seat and the inserted link are separately positioned on the interface of the empennage and the fuselage.
Compared with prior art, the invention has the benefit that
Lockable mechanism provided by the invention, comprising: matching seat, inserted link and locking part, inserted link can be plugged in matching seat,
Inserted link can be locked in matching seat by locking part and matching seat collective effect.Using the above structure, without being cut to intubation
Remove, can linking together fuselage and wing or fuselage and fin stabilization, specifically, the intubation not cut off is plugged
In sleeve, at this point, synchronous inserted link can be plugged in matching seat, then pass through the cooperation of locking part and matching seat again, thus
It can ensure to be locked in inserted link is safe and reliable in matching seat.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the cross-sectional view one of lockable mechanism provided in an embodiment of the present invention after mounting；
Fig. 2 is the structural schematic diagram of the matching seat of lockable mechanism shown in FIG. 1；
Fig. 3 is the cross-sectional view two of lockable mechanism provided in an embodiment of the present invention after mounting；
Fig. 4 is the structural schematic diagram of the matching seat of lockable mechanism shown in Fig. 3；
Fig. 5 be another embodiment of the present invention provides lockable mechanism cross-sectional view after mounting；
Fig. 6 is the structural schematic diagram of the matching seat of lockable mechanism shown in fig. 5.
Appended drawing reference:
1- matching seat；2- butt hole；The first card hole of 3-；The second card hole of 4-；5- inserted link；6- fastener；7- third card hole；8-
4th card hole；
51- flange；61- curved portion.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for description the present invention and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
Fig. 1 is the cross-sectional view one of lockable mechanism provided in an embodiment of the present invention after mounting；Fig. 2 is locking shown in FIG. 1
The structural schematic diagram of the matching seat of mechanism；Fig. 3 is the cross-sectional view two of lockable mechanism provided in an embodiment of the present invention after mounting；Figure
4 be the structural schematic diagram of the matching seat of lockable mechanism shown in Fig. 3；Fig. 5 be another embodiment of the present invention provides lockable mechanism
Cross-sectional view after mounting；Fig. 6 is the structural schematic diagram of the matching seat of lockable mechanism shown in fig. 5.Illustrate: Fig. 1's and Fig. 3 cuts open
Upper thread is mutually perpendicular to.
As shown in figures 1 to 6, a kind of lockable mechanism provided in this embodiment, comprising: matching seat 1, inserted link 5 and locking part are inserted
Bar 5 can be plugged in matching seat 1, and locking part is plugged in the locking realized on matching seat 1 to inserted link 5.
When wing or empennage and fuselage are by being intubated and after sleeve is attached, if not to its fortune in the axial direction
Dynamic to be defined, then, in the flight course of unmanned plane, intubation is just likely to backing out out of sleeve, therefore, is
The appearance for avoiding above situation, installs locking machine provided in this embodiment on the interface of wing or empennage and fuselage
Structure, to limit the movement of intubation and sleeve in the axial direction.
It is illustrated with the connection of the wing and fuselage, empennage and fuselage of unmanned plane, it is first when carrying out the assembling of unmanned plane
It first needs the sleeve grafting in the intubation and fuselage on wing perhaps empennage so that it is guaranteed that the phase of wing or empennage and fuselage
To position；Since inserted link 5 is arranged on wing or empennage, matching seat 1 is arranged on fuselage, so during plugging herein,
Inserted link 5 can be also plugged in therewith in matching seat 1, after inserted link 5 is plugged in completely in matching seat 1, then by locking part and matching seat 1
Connection, to realize the restriction to inserted link 5.It should be noted that inserted link 5 also can be set on fuselage, and corresponding match
Seat 1 is closed to be arranged on wing or empennage.
The shape of matching seat 1 can there are many selections, such as: cuboid, cylindrical body or other shape phases with fuselage
The shape of cooperation, so that matching seat 1 be enable to be fitted on fuselage completely.
Locking part and matching seat 1 plug that connection type can there are many selections, such as: locking part is screw rod, matching seat 1
Be respectively provided with through-hole on inserted link 5, and after inserted link 5 is inserted into matching seat 1, the axis of the through-hole of the two point-blank, then
Two through-holes are passed through with screw rod, the position of screw rod are finally secured with nuts, to complete the locking of inserted link 5.
Certainly it should be noted that multiple through-holes can also be arranged on the different location of matching seat 1 and inserted link 5, thus
Using multiple screw rods, inserted link 5 is limited in different positions, to ensure that inserted link 5 can be more stable is locked in cooperation
In seat 1, so that wing or empennage are more steady, it will not shake.
Lockable mechanism provided in this embodiment, comprising: matching seat 1, inserted link 5 and locking part, inserted link 5 can be plugged in cooperation
In seat 1, inserted link 5 can be locked in matching seat 1 by locking part and 1 collective effect of matching seat.Using the above structure, without to slotting
Pipe is cut off, can linking together fuselage and wing or fuselage and fin stabilization, specifically, will not cut off
It is plugged in sleeve, at this point, synchronous inserted link 5 can be plugged in matching seat 1, then passes through locking part and matching seat 1 again
Cooperation, so as to ensure to be locked in inserted link 5 is safe and reliable in matching seat 1.
On the basis of the above embodiments, specifically, butt hole 2, the first card hole 3 and the second card are provided on matching seat 1
Hole 4, the first card hole 3 and the second card hole 4 are symmetrically distributed in the two sides of 2 axis of butt hole, and run through butt hole 2；It is set on inserted link 5
It is equipped with flange 51, flange 51 is inserted into butt hole 2；Locking part passes through the flat of the first card hole 3 and the second card hole 4 and flange 51
Face contact, to realize the locking to inserted link 5.
Flange 51 is set on inserted link 5, and the position of the flange 51 on inserted link 5 can there are many selections, such as: end face
Upper or other any positions；Specifically, as shown in figure 3, flange 51 is arranged on one end end face of inserted link 5, when using this
When set-up mode, inserted link 5 can directly select the screw with socket cap or the screw rod with end.
It should be noted that the diameter of the flange 51 should be greater than the diameter of 5 other parts of inserted link；Docking on matching seat 1
2 diameter of hole should be equal to or more than the diameter of flange 51, to ensure that flange 51 can be inserted in butt hole 2.As a kind of preferred
Scheme, flange 51 is inserted into just in butt hole 2, that is, the outer surface of flange 51 is contacted with the inner sidewall of butt hole 2, this
Sample can shake in butt hole 2 to avoid inserted link 5, so that wing or empennage be driven to generate unnecessary shaking.
Locking part includes two fixed links, and two fixed links are plugged in the first card hole 3 and the second card hole 4 respectively, need
Illustrate be the first card hole 3 and the second card hole 4 is through-hole, fixed link is fed through matching seat 1, fixed link the other end use
Fixed link is fixed on matching seat 1 by fixing sleeve；At this time since fixed link is when passing through the first card hole 3 and the second card hole 4, support
It is located on the surface of flange 51, it is thereby achieved that inserted link 5 is locked in the purpose in matching seat 1.
On the basis of the above embodiments, specifically, as shown in Figure 5 and Figure 6, the middle part of inserted link 5 is arranged in flange 51, matches
It closes and is additionally provided with third card hole 7 and the 4th card hole 8 on seat 1；Third card hole 7 and the 4th card hole 8 are symmetrically distributed in 2 axis of butt hole
Two sides, and run through butt hole 2；And third card hole 7 and the 4th card hole 8 are respectively axis and the first card hole 3 and the with flange 51
Two card holes 4 are symmetrical arranged.
The middle part of inserted link 5 is arranged in flange 51, that is, the shape of inserted link 5 is cross, and a part of inserted link 5 is located at flange
51 side, another part of inserted link 5 are located at the other side of flange 51；First card hole 3 and third card hole 7, the second card hole 4 and
Four card holes 8 are axial symmetry distribution with flange 51.
When the first card hole 3, the second card hole 4, third card hole 7 and four card holes 8 is arranged, the quantity of locking part is two,
One of locking part passes through the first card hole 3 and the second card hole 4 is abutted with a side of flange 51, another locking part is worn
It crosses third card hole 7 and the 4th card hole 8 is abutted with another side of flange 51；It using the above structure, can be more firm by inserted link 5
Gu, it is stable be locked in matching seat 1, prevent it from being moved forward and backward.
On the basis of the above embodiments, specifically, locking part is U-shaped fastener 6, and fastener 6 has inwardly card
The pretightning force of conjunction.
Using above-described embodiment, certain preload can be generated after fastener 6 is inserted in the first card hole 3 and the second card hole 4
Power so that fastener 6 itself can be locked in the first card hole 3 and the second card hole 4 using the pretightning force, and then locks inserted link
5.Specifically, fastener 6 can choose circlip.
On the basis of the above embodiments, specifically, the both ends of fastener 6 are in the curved portion 61 being bent outwardly.
After fastener 6 is plugged in the first card hole 3 and the second card hole 4, which can be stuck on matching seat 1, from
And avoid when not by external force, fastener 6 is backing out out of the first card hole 3 and the second card hole 4.
On the basis of the above embodiments, specifically, fastener hole is provided on matching seat 1, fastener hole is used for matching seat 1
It is connected on wing or fuselage.
For the ease of being arranged matching seat 1 on wing or fuselage, therefore, fastener hole being set on matching seat 1, is passed through
Matching seat 1 is firmly arranged on fuselage or wing or empennage for the cooperation of fastener and fastener hole.
The quantity of fastener hole can have it is multiple, such as: two or four, when for four, four fastener holes can be set
It sets on four angles of matching seat 1.
The present embodiment additionally provides a kind of unmanned plane, comprising: the lockable mechanism of fuselage, wing and claim as above；Match
It closes seat 1 and inserted link 5 is separately positioned on the interface of fuselage and wing；Alternatively, matching seat 1 and inserted link 5 are separately positioned on wing
On the interface of fuselage.
It should be noted that the interface of fuselage and wing refers to, the two is separately positioned on the side wall of the two in connection
On two be oppositely arranged surface.
When carrying out the assembling of unmanned plane, it is necessary first to insert the sleeve in the intubation and fuselage on wing or empennage
It connects, so that it is guaranteed that the relative position of wing or empennage and fuselage；It is arranged on wing with inserted link 5, matching seat 1 is arranged in fuselage
It is illustrated for upper:
During the grafting of intubation and casing, inserted link 5 can be also plugged in therewith in matching seat 1, when inserted link 5 plugs completely
After in matching seat 1, then locking part connect with matching seat 1, to realize the restriction to inserted link 5.It should be noted that inserted link
5 also can be set on fuselage, and corresponding matching seat 1 is arranged on wing.
On the basis of the above embodiments, specifically, the quantity of inserted link 5 and matching seat 1 is multiple, and multiple inserted links 5
It is evenly distributed on the interface of fuselage and wing with multiple matching seats 1；Alternatively, multiple inserted links 5 and multiple matching seats 1 are equal
On the even interface for being distributed in wing and fuselage.
The stress on interface in order to make wing and fuselage is more balanced, therefore, on the interface of wing and fuselage
It is symmetrically arranged multiple matching seats 1 and multiple inserted links 5, certainly, the quantity and position of matching seat 1 and inserted link 5, which should all correspond to, to be set
It sets, can be plugged in a matching seat 1 with ensuring each inserted link 5.
The present embodiment additionally provides a kind of unmanned plane, comprising: the lockable mechanism of fuselage, empennage and claim as above；Match
It closes seat 1 and inserted link 5 is separately positioned on the interface of fuselage and empennage；Alternatively, matching seat 1 and inserted link 5 are separately positioned on empennage
On the interface of fuselage.
When carrying out the assembling of unmanned plane, it is necessary first to by the sleeve grafting in the intubation and fuselage on empennage, thus really
Protect the relative position of empennage and fuselage；It is arranged on empennage with inserted link 5, matching seat 1 is illustrated for being arranged on fuselage:
During the grafting of intubation and casing, inserted link 5 can be also plugged in therewith in matching seat 1, when inserted link 5 plugs completely
After in matching seat 1, then locking part connect with matching seat 1, to realize the restriction to inserted link 5.It should be noted that inserted link
5 also can be set on fuselage, and corresponding matching seat 1 is arranged on empennage.
On the basis of the above embodiments, specifically, the quantity of inserted link 5 and matching seat 1 is multiple, and multiple inserted links 5
It is evenly distributed on the interface of fuselage and empennage with multiple matching seats 1；Alternatively, multiple inserted links 5 and multiple matching seats 1 are equal
On the even interface for being distributed in empennage and fuselage.
The stress on interface in order to make empennage and fuselage is more balanced, therefore, on the interface of empennage and fuselage
It is symmetrically arranged multiple matching seats 1 and multiple inserted links 5, certainly, the quantity and position of matching seat 1 and inserted link 5, which should all correspond to, to be set
It sets, can be plugged in a matching seat 1 with ensuring each inserted link 5.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (8)
1. a kind of lockable mechanism characterized by comprising matching seat, inserted link and locking part, the inserted link can be plugged in described
In matching seat, the locking part is plugged in the locking realized on the matching seat to the inserted link；
Butt hole, the first card hole and the second card hole, first card hole and second card hole pair are provided on the matching seat
Claim the two sides for being distributed in the docking axially bored line, and runs through the butt hole；Flange, the flange are provided on the inserted link
It is inserted into the butt hole；The locking part passes through the plane of first card hole and second card hole and the flange
Contact, to realize the locking to the inserted link；
The middle part of the inserted link is arranged in the flange, and third card hole and the 4th card hole are additionally provided on the matching seat；It is described
Third card hole and the 4th card hole are symmetrically distributed in the two sides of the docking axially bored line, and run through the butt hole；And institute
It states third card hole and the 4th card hole is symmetrically set by axis and first card hole and second card hole of the flange respectively
It sets.
2. lockable mechanism according to claim 1, which is characterized in that the flange is located at one end end face of the inserted link
On.
3. lockable mechanism according to claim 1 or 2, which is characterized in that the locking part is U-shaped fastener, institute
Stating fastener has the pretightning force inwardly engaged.
4. lockable mechanism according to claim 3, which is characterized in that the both ends of the fastener are in the arc being bent outwardly
Portion.
5. lockable mechanism according to claim 1 or 2, which is characterized in that fastener hole is provided on the matching seat, it is described
Fastener hole is used to the matching seat being connected to wing or fuselage.
6. a kind of unmanned plane characterized by comprising fuselage, wing and locking machine as described in any one in claim 1-5
Structure；The matching seat and the inserted link are separately positioned on the interface of the fuselage and the wing；Alternatively, the matching seat
It is separately positioned on the inserted link on the interface of the wing and the fuselage.
7. unmanned plane according to claim 6, which is characterized in that the quantity of the inserted link and the matching seat is more
It is a, and multiple inserted links and multiple matching seats are evenly distributed on the interface of the fuselage and the wing；Or
Person, multiple inserted links and multiple matching seats are evenly distributed on the interface of the wing and the fuselage.
8. a kind of unmanned plane characterized by comprising fuselage, empennage and locking machine as described in any one in claim 1-5
Structure；The matching seat and the inserted link are separately positioned on the interface of the fuselage and the empennage；Alternatively, the matching seat
It is separately positioned on the inserted link on the interface of the empennage and the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610183415.6A CN105857570B (en) | 2016-03-28 | 2016-03-28 | Lockable mechanism and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610183415.6A CN105857570B (en) | 2016-03-28 | 2016-03-28 | Lockable mechanism and unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105857570A CN105857570A (en) | 2016-08-17 |
| CN105857570B true CN105857570B (en) | 2019-01-11 |
Family
ID=56624999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610183415.6A Active CN105857570B (en) | 2016-03-28 | 2016-03-28 | Lockable mechanism and unmanned plane |
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| Country | Link |
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| CN (1) | CN105857570B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101214852A (en) * | 2007-12-28 | 2008-07-09 | 北京航空航天大学 | Connecting structure for unmanned aerial vehicle body and wing |
| CN202953170U (en) * | 2012-09-26 | 2013-05-29 | 北京观典航空设备公司 | Unmanned aerial vehicle (UAV) empennage connecting rod |
| CN202997190U (en) * | 2012-12-05 | 2013-06-12 | 昆山思瑞奕电子有限公司 | Line terminal locking mechanism |
| EP2716543A1 (en) * | 2012-10-03 | 2014-04-09 | Sensefly S.A. | Connection set for aircraft with detachable wings |
| CN204716711U (en) * | 2015-05-27 | 2015-10-21 | 中国航天空气动力技术研究院 | One can repeat the locking wing attachment structure of dismounting |
| CN204802065U (en) * | 2015-04-30 | 2015-11-25 | 深圳一电科技有限公司 | Collapsible oar arm component and unmanned aerial vehicle |
| CN205076039U (en) * | 2015-09-08 | 2016-03-09 | 零度智控（北京）智能科技有限公司 | Horn installation component and aircraft |
| CN205615706U (en) * | 2016-03-28 | 2016-10-05 | 北京迈凯飞工程技术有限公司 | Locking mechanism and unmanned aerial vehicle |
-
2016
- 2016-03-28 CN CN201610183415.6A patent/CN105857570B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101214852A (en) * | 2007-12-28 | 2008-07-09 | 北京航空航天大学 | Connecting structure for unmanned aerial vehicle body and wing |
| CN202953170U (en) * | 2012-09-26 | 2013-05-29 | 北京观典航空设备公司 | Unmanned aerial vehicle (UAV) empennage connecting rod |
| EP2716543A1 (en) * | 2012-10-03 | 2014-04-09 | Sensefly S.A. | Connection set for aircraft with detachable wings |
| CN202997190U (en) * | 2012-12-05 | 2013-06-12 | 昆山思瑞奕电子有限公司 | Line terminal locking mechanism |
| CN204802065U (en) * | 2015-04-30 | 2015-11-25 | 深圳一电科技有限公司 | Collapsible oar arm component and unmanned aerial vehicle |
| CN204716711U (en) * | 2015-05-27 | 2015-10-21 | 中国航天空气动力技术研究院 | One can repeat the locking wing attachment structure of dismounting |
| CN205076039U (en) * | 2015-09-08 | 2016-03-09 | 零度智控（北京）智能科技有限公司 | Horn installation component and aircraft |
| CN205615706U (en) * | 2016-03-28 | 2016-10-05 | 北京迈凯飞工程技术有限公司 | Locking mechanism and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105857570A (en) | 2016-08-17 |
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