CN209535439U - A kind of easy-to-mount composite material unmanned plane - Google Patents
A kind of easy-to-mount composite material unmanned plane Download PDFInfo
- Publication number
- CN209535439U CN209535439U CN201822126097.7U CN201822126097U CN209535439U CN 209535439 U CN209535439 U CN 209535439U CN 201822126097 U CN201822126097 U CN 201822126097U CN 209535439 U CN209535439 U CN 209535439U
- Authority
- CN
- China
- Prior art keywords
- buckle
- wing
- mounting plate
- connector
- fuselage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of easy-to-mount composite material unmanned plane, including head, fuselage body, wing and empennage positioned at fuselage body end；It is rearwardly shunk by head in the section of fuselage body, fuselage body includes main machine body and endpiece fuselage, head is removably connect with main machine body using the first connector, main machine body is removably connect with endpiece fuselage using the second connector, wing and main machine body junction are provided with transition edge strip, wing is respectively port wing and starboard wing, port wing and starboard wing are located at the two sides of main machine body, port wing is removably connect with transition edge strip using third connector respectively with starboard wing, and empennage is removably connect with endpiece fuselage using the 4th connector.The unmanned plane uses split-type design, directly can more renew component after some parts damages, is not necessarily to integral replacing, and interchangeability is preferable；It is easy for assemble or unload, it is easy to carry.
Description
Technical field
The utility model relates to fixed-wing air vehicle technique fields, and in particular to a kind of easy-to-mount composite material nobody
Machine.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target
Machine.Civilian aspect, unmanned plane are taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, are observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself.
The development of unmanned air vehicle technique is an important directions of World Airways industrial development, in addition to aircraft flight performance and
Except the horizontal swift and violent promotion of load information post-processing technology, Flight Vehicle Structure installation reliability, stability, functional module structure
Convenience and reliability between electrical communications connection also become and determine the important of assessment UAV system aircraft performance superiority and inferiority
Functional performance index.The increasingly broader, application environment using field of UAV system becomes increasingly complex, and mentions to aircraft handling
Requirements at the higher level are gone out.
In existing fixed-wing unmanned plane, the length of wing and empennage has key effect to the pitching stability of aircraft,
Wing and the longer stability of empennage are better, but since the too long transport that can make fixed-wing unmanned plane of fuselage becomes difficult, fuselage
Too long unmanned plane needs bigger space to be transported.So on the market mainly with short fuselage, short wing fixed-wing based on.
And each functional module installation of small drone on the market relies on the screw standard component or locking device of different size model
It is fixed, assembles and dismantle that time-consuming, maintenance procedures are complicated, need to be equipped with specific purpose tool, and maintenance and use cost are high.
Utility model content
To be solved in the utility model is that wing and empennage are long in the prior art, causes fuselage is integrally too long can make to fix
The technical issues of transport of wing unmanned plane becomes difficult, and the too long unmanned plane of fuselage needs bigger space to be transported, purpose
It is to provide a kind of easy-to-mount composite material unmanned plane.
The utility model is achieved through the following technical solutions:
A kind of easy-to-mount composite material unmanned plane, including head, fuselage body, wing and be located at fuselage body end
Empennage；
The section of the fuselage body is rearwardly shunk by head, and the fuselage body includes main machine body and endpiece fuselage,
The head and the main machine body are removably connect using the first connector, and the main machine body and the endpiece fuselage are using the
Two connectors removably connect, and the wing and the main machine body junction are provided with transition edge strip, the transition edge strip by
The junction of the wing and the main machine body extends to the head of the main machine body and tail portion respectively and incorporates the main machine body
Curved surface, the wing is respectively port wing and starboard wing, and the port wing and the starboard wing are located at the main machine body
Two sides, the port wing and the starboard wing removably connect with the transition edge strip using third connector respectively, institute
It states empennage and is removably connect with the endpiece fuselage using the 4th connector.
Preferred embodiment, first connector include quick-joint male head and quick-joint mother head, and the quick-joint male head includes and host
The buckle fixed frame that body front end is fixedly connected, being rotatably connected on the buckle fixed frame has the card connecting with the quick-joint mother head
Button, the quick-joint mother head include the card slot fixed frame being fixedly connected with head, and the card slot fixed frame is equipped with and is clasped
The card slot of connection.
Preferred embodiment, the buckle fixed frame includes the first annular mounting plate being fixedly connected with main machine body front end,
The outer rim of one annular mounting plate is equipped with the first convex block extended along first annular mounting plate axial direction, in the outer of the first convex block
Portion opens up fluted, is snapped with buckle hinged block in groove, one end of the buckle hinged block and buckle passes through pin rotation
Connection, the other end of the buckle are T-shaped structure, and the card slot fixed frame includes the second annular being fixedly connected with back-end of machine head
Mounting plate is equipped with the second convex block extended along the second annular mounting plate axial direction in the outer rim of the second annular mounting plate,
The outside of second convex block opens up the card slot, and the other end of the buckle snaps onto card slot.
Preferred embodiment, there are two first convex block is set, center line pair of two the first convex blocks along first annular mounting plate
Claim setting, there are two second convex block is set, center line symmetrical setting of two the second convex blocks along the second annular mounting plate.
Preferred embodiment, second connector is identical as the first connector, the quick-joint mother head and tail of second connector
The front end of section fuselage is fixedly connected, and the quick-joint male head of the second connector is fixedly connected with the rear end of main machine body.
Preferred embodiment, the third connector include Quick Release male connector and Quick Release female, and the Quick Release male connector includes and transition
The first elongated mounting plate that edge strip is fixedly connected, is respectively equipped with third convex block at the top and bottom of the first elongated mounting plate,
The outside of third convex block opens up fluted, is snapped with buckle hinged block in groove, one end of the buckle hinged block and buckle
It is connected by pin rotation, the other end of the buckle is T-shaped structure, and the Quick Release female includes and port wing and/or right machine
The second elongated mounting plate that the wing is fixedly connected, is respectively equipped with the 4th convex block at the top and bottom of the second elongated mounting plate,
The outside of four convex blocks offers card slot, and the other end of the buckle snaps onto card slot.
Preferred embodiment, the mother that the 4th connector includes the sub-buckle connecting with endpiece back body and connect with empennage
Button, the sub-buckle include straight pin and snap-gauge, the rear end pivot connection of the straight pin and endpiece fuselage, one end of the snap-gauge
Equipped with the circular hole with cylinder pin connection, the other end of snap-gauge is equipped with card slot, and the female thread includes the buckle being fixedly connected with empennage,
Two trunnions that one end of the buckle is provided symmetrically are equipped with the arc groove with cylinder pin connection, institute in the end of trunnion
The clamping groove for offering on buckle and connecting with snap-gauge is stated, the clamping groove is located between two trunnions, the other end of the buckle
Equipped with buttonhole, it is snapped with buckle hinged block in buttonhole, hook is hinged on the buckle hinged block, the hook includes
Two extensions of articulated section and the other end and two trunnion snappings on buckle that one end is connect with buckle hinged block by pin rotation
Plate offers the arc groove with cylinder pin connection on the hanging plate.
Preferred embodiment, it is described buckle hinged block side wall on and groove inner wall be equipped with mutual snapping bump, institute
The junction for stating bump is arc-shaped curved surface.
Preferred embodiment, removal hole is offered at the top of the buckle hinged block, and the removal hole is used for buckle hinged block
It is pulled out out of groove.
Preferred embodiment offers the pin hole hinged with buckle hinged block, the pin difference on the side wall of the groove
It is connect with buckle, buckle hinged block and groove.
The utility model compared with prior art, has the following advantages and benefits: 1) one kind of the utility model
Easy-to-mount composite material unmanned plane, head, fuselage body, wing and the empennage positioned at fuselage body end of the unmanned plane
The connection type opened and unloaded is respectively adopted and carries out assembly and disassembly, this unmanned plane is disassembled into fission in packaging and transportational process
State reduces occupied space, is convenient for packaging and transport, reduction production cost is user-friendly simultaneously and stores.2) this nobody
Machine uses split-type design, directly can more renew component after some parts damages, is not necessarily to integral replacing, and interchangeability is preferable；Installation
Convenient disassembly, it is easy to carry.3) junction of each component of the unmanned plane is connected using dismountable connector, and connector uses
It is assembled convenient for the mode that snaps connection of manual operation, it is easy to operate, object is locked without other tools or screw etc.,
Mutually matched buckle and card slot are provided on connector, by being buckled in indentation card slot and can be locked by handle when assembling.
Detailed description of the invention
Attached drawing described herein is used to provide to further understand the utility model embodiment, constitutes the one of the application
Part does not constitute the restriction to the utility model embodiment.In the accompanying drawings:
Fig. 1 is the structural exploded view of the utility model；
Fig. 2 is partial enlarged view at I in Fig. 1；
Fig. 3 is partial enlarged view at II in Fig. 1；
Fig. 4 is partial enlarged view at III in Fig. 1；
Fig. 5 is the first connecting-piece structure exploded view of the utility model；
Fig. 6 is the 4th connecting-piece structure exploded view of the utility model.
Label and corresponding parts title in attached drawing:
1- head, 2- main machine body, 3- endpiece fuselage, 4- transition edge strip, 5- wing, 6- empennage, the first connector of 7-, 8-
Two connectors, 9- third connector, the 4th connector of 10-, the first annular mounting plate of 701-, the first convex block of 702-, 703- buckle
Hinged block, 704- buckle, the second annular mounting plate of 705-, the second convex block of 706-, 707- card slot, 708- groove, 901- first are long
Shape mounting plate, 902- third convex block, the elongated mounting plate of 903- second, the 4th convex block of 904-, 1001- straight pin, 1002- snap-gauge,
1003- buckle, 1004- hook, 10021- circular hole, 10022- card slot, 10031- trunnion, 10032- clamping groove, 10033- snapping
Hole, the articulated section 10041-, 10042- hanging plate.
Specific embodiment
For the purpose of this utility model, technical solution and advantage is more clearly understood, below with reference to embodiment and attached drawing,
The utility model is described in further detail, and the exemplary embodiment and its explanation of the utility model are only used for explaining this
Utility model is not intended to limit the scope of the present invention.
Embodiment
As shown in Figure 1, a kind of easy-to-mount composite material unmanned plane of the utility model, including head 1, fuselage body,
Wing 5 and empennage 6 positioned at fuselage body end；
The section of fuselage body is rearwardly shunk by head, and fuselage body includes main machine body 2 and endpiece fuselage 3, head 1 with
For main machine body 2 using the first removably connection of connector 7, main machine body 2 and endpiece fuselage 3 are dismountable using the second connector 8
Connection.Wing 5 and 2 junction of main machine body are provided with transition edge strip 4, and transition edge strip 4 is punished by the connection of wing 5 and main machine body 2
The curved surface for not extending and incorporating main machine body 2 to the head of main machine body 2 and tail portion reduces the resistance of unmanned plane during flying.Wing 5 is distinguished
For port wing and starboard wing, port wing is located at the two sides of main machine body 2 with starboard wing, and port wing and starboard wing are in main machine body 2
It is upper to be symmetrical arranged.Port wing is removably connect with transition edge strip 4 using third connector 9 respectively with starboard wing, empennage 6 and tail
Section fuselage 3 is using the 4th removably connection of connector 10.
The unmanned plane of the present embodiment, head 1, fuselage body, wing 5 and the tail positioned at fuselage body end of the unmanned plane
The wing 6, which is respectively adopted, to be opened the connection type unloaded and carries out assembly and disassembly, in packaging and transportational process the dismantling of this unmanned plane at
Seperated state reduces occupied space, is convenient for packaging and transport, reduction production cost is user-friendly simultaneously and stores.Simultaneously
This unmanned plane use split-type design, directly can more renew component after some parts damages, be not necessarily to integral replacing, interchangeability compared with
It is good；It is easy for assemble or unload, it is easy to carry.
Referring to figure 2. and shown in Fig. 5, wherein the first connector 7 includes quick-joint male head and quick-joint mother head, quick-joint male head includes
The buckle fixed frame being fixedly connected with 2 front end of main machine body, buckling to be rotatably connected on fixed frame has the card connecting with quick-joint mother head
Button 704.Buckling fixed frame includes the first annular mounting plate 701 being fixedly connected with 2 front end of main machine body, first annular mounting plate
701 appearance profile is identical as the cross section profile of 2 front end of main machine body, and in order to mitigate the weight of unmanned plane complete machine, this is first annular
Mounting plate 701 reduces materials, lightweight production using annular hollow structure, and certain first annular mounting plate 701 can also be adopted
It is made of solid construction.It is equipped in the outer rim of first annular mounting plate 701 and prolongs along first annular 701 axial direction of mounting plate
The first convex block 702 stretched, there are two the first convex block 702 is set in first annular mounting plate 701, two the first convex blocks 702 are along first
The center line symmetrical setting of annular mounting plate 701, certain first convex block 702 can also be equipped with multiple.
Fluted 708 are opened up in the outside of the first convex block 702, buckle hinged block 703, groove are snapped in groove 708
708 are connect with buckle hinged block 703 using snap fit, buckle on the side wall of hinged block 703 and the inner wall of groove 708 is equipped with
The bump of mutual snapping, the junction between the bump is arc-shaped curved surface；Hinged block 703 is buckled when by pressed by external force
Buckle hinged block 703 is snapped onto groove 708, buckles hinged block 703 at this time on groove 708 with the bump of mutual snapping
Mutual snapping realizes positioning.Buckle hinged block 703 with buckle 704 one end connect by pin rotation, buckle 704 one end with
Pin is that shaft is freely rotated on buckle hinged block 703.
Quick-joint mother head includes the card slot fixed frame being fixedly connected with head 1, and card slot fixed frame is equipped with to be cooperated with buckle 704
The card slot 707 of connection.The other end of buckle 704 is T-shaped structure, the card slot matched with the T-shaped structure of 704 other ends of buckle
707 be T connected in star.Card slot fixed frame includes the second annular mounting plate 705 being fixedly connected with 1 rear end of head, the second annular peace
The appearance profile of loading board 705 is identical as the cross section profile of 1 rear end of head, in order to mitigate the weight of unmanned plane complete machine, this second ring
Shape mounting plate 705 reduces materials using annular hollow structure, lightweight production, and certain second annular mounting plate 705 can also be with
It is made of solid construction.It is equipped in the outer rim of the second annular mounting plate 705 along 705 axial direction of the second annular mounting plate
The second convex block 706 extended, there are two the second convex block 706 is set in the second annular mounting plate 705, two the second convex blocks 706 are symmetrical
It is arranged on the second annular mounting plate 705, certain second convex block 706 can also be equipped with multiple.It is opened in the outside of the second convex block 706
Equipped with card slot 707, buckles 704 other end and snap onto card slot 707.
Second connector 8 is identical as 7 structure of the first connector, before the quick-joint mother head and endpiece fuselage 3 of the second connector 8
End is fixedly connected, and the quick-joint male head of the second connector 8 is fixedly connected herein no longer to the second connector 8 with the rear end of main machine body 2
Specific structure do repetition and repeat.
Shown in referring to figure 3., third connector 9 includes Quick Release male connector and Quick Release female, and Quick Release male connector includes and transition side
The first elongated mounting plate 901 that item 4 is fixedly connected, the appearance profile of the first elongated mounting plate 901 and the section of transition edge strip 4 are taken turns
It is wide identical.In order to mitigate the weight of unmanned plane complete machine, multiple preformed holes are offered to reduce use on the first elongated mounting plate 901
Material, lightweight production, certain first elongated mounting plate 901 can also be made of solid construction.In the first elongated mounting plate
901 top and bottom are respectively equipped with third convex block 902, there are four third convex block 902 is set, four third convex blocks 902 two-by-two one
To the top and bottom that the first elongated mounting plate 901 is arranged in, there are four certain third convex block 902 is not limited to set.
Fluted, the structure phase of the groove and the groove 708 on the first connector 7 is opened up in the outside of third convex block 902
Together.Buckle hinged block 703 is snapped in groove 708, the structure buckle hinged block 703 of groove 708 is connected using snap fit,
It buckles on the side wall of hinged block 703 and the inner wall of groove 708 is equipped with the bump of mutual snapping, the company between the bump
Meeting place is arc-shaped curved surface；Buckle hinged block 703 snaps onto buckle hinged block 703 in groove 708 when by pressed by external force, at this time
The mutual snapping of bump for buckling mutually snapping on hinged block 703 and groove 708, which is realized, to be positioned.Buckle hinged block 703 and buckle
704 one end is connected by pin rotation, and buckling 704 one end using pin is that shaft is freely rotated on buckling hinged block 703.
Quick Release female includes the second elongated mounting plate 903 being fixedly connected with port wing and starboard wing, the second elongated installation
The appearance profile of plate 903 is identical as the cross section profile of port wing and starboard wing.In order to mitigate the weight of unmanned plane complete machine, second is long
Multiple preformed holes are offered on shape mounting plate 903 to reduce materials, lightweight production, certain second elongated mounting plate 903
It can be made of solid construction.It is respectively equipped with the 4th convex block 904 in the top and bottom of the second elongated mounting plate 903, the
There are four four convex blocks 904 are set, four the 4th convex blocks 904 a pair of top and bottom that second elongated mounting plate 903 is set two-by-two,
There are four certain 4th convex block 904 is not limited to set.Card slot is offered in the outside of the 4th convex block 904, which connect with first
707 structure of card slot on part 7 is identical, buckles 704 other end and snaps onto card slot 707.
Referring to figure 4. and shown in Fig. 6, the 4th connector 10 include the sub-buckle being connect with 3 rear end of endpiece fuselage and with empennage 6
The female thread of connection, sub-buckle include straight pin 1001 and snap-gauge 1002, and straight pin 1001 and the rear end of endpiece fuselage 3 are pivotally connected,
One end of snap-gauge 1002 is equipped with the circular hole 10021 connecting with straight pin 1001, and the other end of snap-gauge 1002 is equipped with card slot 10022.
Corresponding female thread includes the buckle 1003 being fixedly connected with empennage 6, two trunnions that one end of buckle 1003 is provided symmetrically
10031, it is equipped with the arc groove that connect with straight pin 1001 in the end of trunnion 10031, is also provided on buckle 1003 and snap-gauge
The clamping groove 10032 of 1002 connections, clamping groove 10032 are located between two trunnions 10031.It is equipped in the other end of buckle 1003
Buttonhole 10033 is snapped with buckle hinged block 703 in buttonhole 10033, is hinged with hook on buckle hinged block 703
1004, the articulated section 10041 and the other end and button that hook 1004, which includes one end, to be connect by pin rotation with buckle hinged block 703
Two hanging plates 10042 of two 10031 snappings of trunnion on plate 1003 are offered on hanging plate 10042 and to be connect with straight pin 1001
Arc groove.
When four connectors 10 is installed: the card slot 10022 of snap-gauge 1002 being connected to manually first the clamping of buckle 1003
In slot 10032, then the both ends of straight pin 1001 is separately mounted to manually in the arc groove of the end of trunnion 10031, is connect down
Manually to connect the arc groove of two hanging plates 10042 with the both ends of straight pin 1001 respectively.In the end of two trunnions 10031
Arc groove and two hanging plates 10042 arc groove clamp the both ends of straight pin 1001 after, with 1004 hinged cards of hook
Button hinged block 703 presses the installation that the 4th connector 10 can be completed in the buttonhole 10033 for entering snap-gauge 1002, opposite way
Disassemble the 4th connector 10, dismantling step is not described in detail herein.
Preferred embodiment scheme, the top of buckle hinged block 703 offer removal hole, and removal hole is used for buckle hinged block
It is pulled out out of groove.Dismantling when using dedicated head buckle hard wire insertion removal hole in, buckle hinged block 703 from
It is pulled out in groove 708.
Preferred embodiment scheme offers the pin hole hinged with buckle hinged block 703 on the side wall of groove 708, in pin
Nail hole has penetrated pin, and pin is connect with buckle 704, buckle hinged block 703 and groove 708 respectively, prevents buckle 704 and buckle
Hinged block 703 is fallen from groove 708 after pulling out in groove 708, in buckle 704 and buckles hinged block 703 from groove
It can also be connected to by pin on groove 708 after being pulled out in 708, prevent buckle 704 and buckle hinged block 703 from losing.
Above-described specific embodiment, to the purpose of this utility model, technical scheme and beneficial effects carried out into
One step is described in detail, it should be understood that being not used to limit the foregoing is merely specific embodiment of the present utility model
Determine the protection scope of the utility model, within the spirit and principle of the utility model, any modification for being made equally is replaced
It changes, improve, should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of easy-to-mount composite material unmanned plane, which is characterized in that including head, fuselage body, wing and be located at machine
The empennage of body body tip；
The section of the fuselage body is rearwardly shunk by head, and the fuselage body includes main machine body and endpiece fuselage, described
Head is removably connect with main machine body using the first connector, and the main machine body and the endpiece fuselage use the second connector
Dismountable connection, the wing and main machine body junction are provided with transition edge strip, and the transition edge strip is by the wing and institute
The junction for stating main machine body extends to the head of the main machine body and tail portion respectively and incorporates the curved surface of the main machine body, the machine
The wing is respectively port wing and starboard wing, and the port wing and the starboard wing are located at the two sides of the main machine body, the left side
Wing is removably connect with the transition edge strip using third connector respectively with the starboard wing, the empennage and the tail
Section fuselage is removably connected using the 4th connector.
2. a kind of easy-to-mount composite material unmanned plane according to claim 1, which is characterized in that first connection
Part includes quick-joint male head and quick-joint mother head, and the quick-joint male head includes the buckle fixed frame being fixedly connected with main machine body front end, institute
It states to be rotatably connected on buckle fixed frame and has the buckle connecting with the quick-joint mother head, the quick-joint mother head includes fixing with head
The card slot fixed frame of connection, the card slot fixed frame are equipped with and the card slot that snaps fit attachment.
3. a kind of easy-to-mount composite material unmanned plane according to claim 2, which is characterized in that the buckle is fixed
Frame includes the first annular mounting plate being fixedly connected with main machine body front end, is equipped in the outer rim of first annular mounting plate along first
The first convex block that annular mounting plate axial direction extends, opens up fluted in the outside of the first convex block, and card is snapped in groove
Hinged block is detained, by pin rotation connection, the other end of the buckle is T shape knot for described one end for buckling hinged block and buckle
Structure, the card slot fixed frame include the second annular mounting plate being fixedly connected with back-end of machine head, in the outer of the second annular mounting plate
Edge is equipped with the second convex block extended along the second annular mounting plate axial direction, opens up the card slot in the outside of the second convex block,
The other end of the buckle snaps onto card slot.
4. a kind of easy-to-mount composite material unmanned plane according to claim 3, which is characterized in that first convex block
If there are two, two the first convex blocks are along the center line symmetrical setting of first annular mounting plate, there are two second convex block is set, two
Center line symmetrical setting of a second convex block along the second annular mounting plate.
5. a kind of easy-to-mount composite material unmanned plane according to claim 2 or 3, which is characterized in that described second
Connector is identical as the first connector, and the quick-joint mother head of second connector is fixedly connected with the front end of endpiece fuselage, and second
The quick-joint male head of connector is fixedly connected with the rear end of main machine body.
6. a kind of easy-to-mount composite material unmanned plane according to claim 1, which is characterized in that the third connection
Part includes Quick Release male connector and Quick Release female, and the Quick Release male connector includes the first elongated mounting plate being fixedly connected with transition edge strip,
Be respectively equipped with third convex block at the top and bottom of the first elongated mounting plate, opened up in the outside of third convex block it is fluted, recessed
Be snapped with buckle hinged block in slot, one end of the buckle hinged block and buckle by pin rotation connection, the buckle it is another
One end is T-shaped structure, and the Quick Release female includes the second elongated mounting plate being fixedly connected with port wing and/or starboard wing,
It is respectively equipped with the 4th convex block at the top and bottom of second elongated mounting plate, offers card slot, the card in the outside of the 4th convex block
The other end of button snaps onto card slot.
7. a kind of easy-to-mount composite material unmanned plane according to claim 1, which is characterized in that the 4th connection
Part includes the sub-buckle connecting with endpiece back body and the female thread that connect with empennage, and the sub-buckle includes straight pin and snap-gauge, institute
The rear end for stating straight pin and endpiece fuselage is pivotally connected, and one end of the snap-gauge is equipped with the circular hole with cylinder pin connection, snap-gauge
The other end is equipped with card slot, and the female thread includes the buckle being fixedly connected with empennage, what one end of the buckle was provided symmetrically
Two trunnions are equipped with the arc groove with cylinder pin connection in the end of trunnion, offer the card connecting with snap-gauge on the buckle
Access slot, the clamping groove are located between two trunnions, and the other end of the buckle is equipped with buttonhole, and card is snapped in buttonhole
Hinged block is detained, hook is hinged on the buckle hinged block, the hook includes that one end and buckle hinged block pass through pin rotation
Two hanging plates of two trunnion snappings on the articulated section of connection and the other end and buckle offer on the hanging plate and straight pin connect
The arc groove connect.
8. a kind of easy-to-mount composite material unmanned plane according to claim 3 or 6, which is characterized in that the buckle
On the side wall of hinged block and the inner wall of groove is equipped with the bump of mutual snapping, and the junction of the bump is that arc is bent
Face.
9. a kind of easy-to-mount composite material unmanned plane according to claim 3 or 6, which is characterized in that the buckle
Removal hole is offered at the top of hinged block, the removal hole is for pulling out buckle hinged block out of groove.
10. a kind of easy-to-mount composite material unmanned plane according to claim 3 or 6, which is characterized in that the groove
Side wall on offer and connect respectively with buckle, buckle hinged block and groove with the hinged pin hole of buckle hinged block, the pin
It connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822126097.7U CN209535439U (en) | 2018-12-18 | 2018-12-18 | A kind of easy-to-mount composite material unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822126097.7U CN209535439U (en) | 2018-12-18 | 2018-12-18 | A kind of easy-to-mount composite material unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209535439U true CN209535439U (en) | 2019-10-25 |
Family
ID=68264566
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822126097.7U Expired - Fee Related CN209535439U (en) | 2018-12-18 | 2018-12-18 | A kind of easy-to-mount composite material unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209535439U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113665782A (en) * | 2021-09-24 | 2021-11-19 | 肇庆市海特复合材料技术研究院 | Composite material unmanned aerial vehicle bonding structure and bonding method thereof |
| CN114013625A (en) * | 2021-11-17 | 2022-02-08 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
-
2018
- 2018-12-18 CN CN201822126097.7U patent/CN209535439U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113665782A (en) * | 2021-09-24 | 2021-11-19 | 肇庆市海特复合材料技术研究院 | Composite material unmanned aerial vehicle bonding structure and bonding method thereof |
| CN114013625A (en) * | 2021-11-17 | 2022-02-08 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
| CN114013625B (en) * | 2021-11-17 | 2024-05-31 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209535439U (en) | A kind of easy-to-mount composite material unmanned plane | |
| WO2016141742A1 (en) | Fixed-wing unmanned aircraft capable of being quickly disassembled and installed | |
| CN207106851U (en) | Wing quick-disassembly structure and unmanned plane | |
| CN204895844U (en) | Many rotor unmanned aerial vehicle | |
| WO2019033768A1 (en) | Propeller, power system and unmanned aerial vehicle | |
| CN212556826U (en) | Unmanned aerial vehicle load module quick detach connection structure | |
| CN201849660U (en) | Supporting arm structure of multi-rotary aerofoil | |
| CN107010244B (en) | A kind of split type unmanned plane | |
| CN108910013A (en) | A kind of fast disassembly type fuselage wing attachment structure | |
| CN212243787U (en) | Unmanned aerial vehicle pole quick detach subassembly that hangs down | |
| CN208915424U (en) | A kind of detachable empennage bindiny mechanism | |
| CN208731246U (en) | The fast shackle of unmanned plane tailplane composite material | |
| CN209535438U (en) | A kind of easy-to-mount composite material unmanned plane connection component | |
| WO2023143199A1 (en) | Gimbal connecting assembly, and unmanned aerial vehicle | |
| CN204368408U (en) | For being fixedly connected with the mounting structure of model plane fuselage and wing | |
| CN215205401U (en) | Unmanned plane | |
| CN211196589U (en) | Wing disassembly assembly and aircraft | |
| CN210000564U (en) | wings capable of being assembled and separated quickly | |
| CN211336402U (en) | But quick assembly disassembly wing coupling mechanism | |
| CN203932297U (en) | A kind of antenna structure of quick dismounting | |
| CN211592904U (en) | Unmanned aerial vehicle | |
| CN210258808U (en) | Quick detach horn of unmanned aerial vehicle | |
| CN209521851U (en) | A kind of unmanned vehicle and its wing components | |
| CN212267827U (en) | Many rotors plug-in horn rapid disassembly structure | |
| CN208715460U (en) | Unmanned plane overloads composite material self-unloading connector |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191025 Termination date: 20211218 |