CN208193677U - A kind of telecontrolled aircraft shell - Google Patents
A kind of telecontrolled aircraft shell Download PDFInfo
- Publication number
- CN208193677U CN208193677U CN201820765036.2U CN201820765036U CN208193677U CN 208193677 U CN208193677 U CN 208193677U CN 201820765036 U CN201820765036 U CN 201820765036U CN 208193677 U CN208193677 U CN 208193677U
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- fixedly connected
- wing
- fixed frame
- frame
- fixed
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Abstract
The utility model discloses a kind of telecontrolled aircraft shells, including body, it is characterized by: two middle side part of body is fixedly connected with wing fixed frame, installation sliding rail is fixedly connected on the outside of the wing fixed frame, the wing fixed frame is fixedly connected with assembling wing by installation sliding rail, the assembling wing is fixedly connected by fixed device with installation sliding rail close to the side of wing fixed frame, powered support is fixedly connected on the outside of the wing fixed frame, position inside the powered support close to wing fixed frame is provided with motor mounting groove, the powered support is rotatably connected to flabellum far from one end of wing fixed frame, the utility model relates to remote-control toy technical fields.The telecontrolled aircraft shell has achieved the purpose that be freely disassembled assembling wing, the receipts of telecontrolled aircraft is facilitated to fill, reduced telecontrolled aircraft the space occupied, easy to carry, and different components can be used and reequip to telecontrolled aircraft, improve the profit of enterprise.
Description
Technical field
The utility model relates to remote-control toy technical field, specially a kind of telecontrolled aircraft shell.
Background technique
Telecontrolled aircraft refers to the aircraft that can be flown with far distance control, and appearing in China's Mainland place earliest is with single machine pin
Sell (i.e. aircraft and remote controler is separately sold), in this way can be very high to consumer cost, and at that time science and technology be not it is very flourishing, can not
The idea according to oneself achieved one's goal completely goes to fly, and needs pretty troublesome debugging aircraft and remote controler, causes the office of the consumer group
It is sex-limited.With the prosperity of science and technology, the most of all all-in-one machines of telecontrolled aircraft are sold, and producer is good after debugging, for some first
It learns type and has reached winged state in one's hands, and price is relatively low, telecontrolled aircraft has come into average family,
In to play as dominant direction；Also there is part enthusiast to reequip it, (such as take photo by plane, carry to reach more entertainment way
Again etc.).Existing telecontrolled aircraft receives dress inconvenience, and occupied space is big, and repacking space is small.
Utility model content
(1) the technical issues of solving: in view of the deficiencies of the prior art, the utility model provides outside a kind of telecontrolled aircraft
Shell solves receipts dress inconvenience, and occupied space is big, the small problem of repacking space.
(2) technical solution: in order to achieve the above object, the utility model is achieved by the following technical programs: Yi Zhongyao
Control airplane skin, including body, it is characterised in that: two middle side part of body is fixedly connected with wing fixed frame, the wing
Installation sliding rail is fixedly connected on the outside of fixed frame, the wing fixed frame is fixedly connected with kludge by installation sliding rail
The wing, the assembling wing are fixedly connected by fixed device with installation sliding rail close to the side of wing fixed frame, the wing
It is fixedly connected with powered support on the outside of fixed frame, the position of wing fixed frame is provided with motor inside the powered support and pacifies
Tankage, the powered support are rotatably connected to flabellum far from one end of wing fixed frame, and the one end of the body far from flabellum is solid
Surely it is connected with empennage frame, the middle position of the empennage top of the trellis is fixedly connected with the shunting wing, and the empennage frame is far from body
One end is fixedly connected with empennage, and empennage top of the trellis two sides are fixedly connected with rotating device, rotation at the top of the rotating device
It is connected with deflector.
Preferably, the fixed device includes fixed frame, and the middle position inside the fixed frame is provided with sliding groove, institute
It states both ends on the outside of sliding groove and is fixedly connected to fixed frame, bracket, the mid-stent are fixedly connected with inside the fixed frame
Fixed link is slidably connected, the fixed link runs through and extends to outside fixed frame, slides rail with installation on the inside of the sliding groove
It is slidably connected.
Preferably, it is fixedly connected with pulling unit at the top of the fixed link, the fixed link outer wall is located at fixed frame inner wall
Spring is arranged between bracket.
Preferably, the rotating device includes mounting seat, and the mounting seat bottom passes through fixing screws and empennage frame
It is fixedly connected, rotation axis is fixedly connected with inside the mounting seat, is arranged with rotating block, the rotation in the middle part of the rotation axis
Connecting rod is fixedly connected at the top of block, the mounting seat top is rotatably connected to deflector mounting base, institute by bolt axis
Deflector mounting base inside bottom is stated to be fixedly connected with the connecting rod.
Preferably, the body surface two sides are equipped with streamer lamp.
Preferably, the middle position inside the body is provided with controller mounting groove.
(3) the utility model has the advantages that the utility model provides a kind of telecontrolled aircraft shell.Have it is following the utility model has the advantages that
(1), the telecontrolled aircraft shell will assemble wing by the sliding groove on assembling wing and wing fixed frame slided
Dynamic installation, installation sliding track surface offer fixed groove, and when sliding into specific position, fixed link can be injected into fixation by spring
In groove, assembling wing is fixed, it can be by fixed link from fixed groove by the pulling unit at the top of fixed device
It pulls out, assembling wing is removed along installation sliding rail, has achieved the purpose that be freely disassembled assembling wing, has facilitated telecontrolled aircraft
Dress is received, telecontrolled aircraft the space occupied is reduced, it is easy to carry；
(2), the telecontrolled aircraft shell, wing fixed frame inside, which is provided with motor mounting groove, can install motor, band motivation
The controller mounting groove of flabellum rotation at the top of wing fixed frame, the inside setting of body can install controller, realize remote controler
Aircraft is operated, body surface is equipped with streamer lamp, and the rotating device of empennage frame two sides installation will be pacified by fixing screws
Dress pedestal is fixed on empennage frame, and user can rotate deflector mounting base by rotating block and bolt axis, to change
The angle of deflector has achieved the purpose that the more playabilities of realization, and different components can be used and change to telecontrolled aircraft
Dress can produce the accessory for adapting to different consumer groups, improve the profit of enterprise.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the structural schematic diagram of the fixed device of the utility model；
Fig. 3 is the structural schematic diagram of the utility model rotating device；
Fig. 4 is the structural schematic diagram of the utility model fixed frame.
In figure: 1 body, 2 wing fixed frames, 3 installation sliding rails, 4 assembling wings, 5 fixed devices, 501 fixed frames, 502
Sliding groove, 503 fixed frames, 504 brackets, 505 fixed links, 506 springs, 507 pull units, 6 powered supports, 7 motor mounting grooves,
8 flabellums, 9 rotating devices, 901 mounting seats, 902 fixing screws, 903 rotation axis, 904 rotating blocks, 905 connecting rods, 906 bolts
Shaft, 10 shunt the wing, 11 empennage framves, 12 deflectors, 13 empennages, 14 controller mounting grooves, 15 streamer lamps, the installation of 16 deflectors
Seat.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-4 is please referred to, the utility model provides a kind of technical solution: a kind of telecontrolled aircraft shell, including body 1, body
1 liang of middle side part of body is fixedly connected with wing fixed frame 2, installation sliding rail 3 is fixedly connected on the outside of wing fixed frame 2, wing is solid
Determine frame 2 and assembling wing 4 is fixedly connected with by installation sliding rail 3, assembling wing 4 passes through solid close to the side of wing fixed frame 2
Determine device 5 to be fixedly connected with installation sliding rail 3, powered support 6 is fixedly connected on the outside of wing fixed frame 2, inside powered support 6
The position of wing fixed frame 2 is provided with motor mounting groove 7, powered support 6 is rotatablely connected far from one end of wing fixed frame 2
There is flabellum 8, body 1 is fixedly connected with empennage frame 11 far from one end of flabellum 8, and the middle position at 11 top of empennage frame is fixedly connected
Have and shunt the wing 10, empennage frame 11 is fixedly connected with empennage 13 far from one end of body 1, and 11 top two sides of empennage frame are fixedly connected with
Rotating device 9 is rotatably connected to deflector 12 at the top of rotating device 9.
Fixed device 5 includes fixed frame 501, and the middle position inside fixed frame 501 is provided with sliding groove 502, sliding groove
502 outsides both ends are fixedly connected to fixed frame 503, and bracket 504 is fixedly connected with inside fixed frame 503, is slided in the middle part of bracket 504
Dynamic to be connected with fixed link 505, fixed link 505 runs through and extends to outside fixed frame 503, and 502 inside of sliding groove is slided with installation
Rail 3 is slidably connected.
It is fixedly connected at the top of fixed link 505 and pulls unit 507,505 outer wall of fixed link is located at 503 inner wall of fixed frame and branch
Spring 506 is arranged between frame 504.
Rotating device 9 includes mounting seat 901, and 901 bottom of mounting seat is fixed by fixing screws 902 and empennage frame 11
It connects, is fixedly connected with rotation axis 903 inside mounting seat 901, rotating block 904, rotating block are arranged in the middle part of rotation axis 903
904 tops are fixedly connected with connecting rod 905, are rotatably connected to deflector by bolt axis 906 at the top of mounting seat 901 and install
Seat 16,16 inside bottom of deflector mounting base is fixedly connected with connecting rod 905.
1 surface two sides of body are equipped with streamer lamp 15.
Middle position inside body 1 is provided with controller mounting groove 14.
In use, user can will be assembled by the sliding groove 502 on assembling wing 4 wing 4 and wing fixed frame 2 into
Row is slidably installed, and installation sliding 3 surface of rail offers fixed groove, and when sliding into specific position, spring 506 can be by fixed link
505 are injected into fixed groove, and assembling wing 4 is fixed, and can be incited somebody to action by the pulling unit 507 at 5 top of fixation device
Fixed link 505 is pulled out from fixed groove, and assembling wing 4 is removed along installation sliding rail 3, is arranged inside wing fixed frame 2
Motor mounting groove 7 can install motor, and the flabellum 8 at 2 top of wing fixed frame is driven to rotate, the control of the inside setting of body 1
Device mounting groove 14 processed can install controller, realize that remote controler operates aircraft, and 1 surface of body is equipped with streamer lamp 15,
Mounting seat 901 is fixed on empennage frame 11 by the rotating device 9 of 11 two sides of empennage frame installation by fixing screws 902, is used
Person can rotate deflector mounting base 16 by rotating block 904 and bolt axis 906, to change the angle of deflector 12.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions.By sentence " element limited including one ..., it is not excluded that
There is also other identical elements in the process, method, article or apparatus that includes the element ".
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of telecontrolled aircraft shell, including body (1), it is characterised in that: (1) two middle side part of body is fixedly connected with machine
Wing fixed frame (2), wing fixed frame (2) outside are fixedly connected with installation sliding rail (3), and the wing fixed frame (2) is logical
It crosses installation sliding rail (3) and is fixedly connected with assembling wing (4), assembling wing (4) is logical close to the side of wing fixed frame (2)
It crosses fixed device (5) to be fixedly connected with installation sliding rail (3), is fixedly connected with powered support on the outside of the wing fixed frame (2)
(6), the internal position close to wing fixed frame (2) of the powered support (6) is provided with motor mounting groove (7), the power branch
Frame (6) is rotatably connected to flabellum (8) far from the one end of wing fixed frame (2), and the one end of the body (1) far from flabellum (8) is solid
Surely it is connected with empennage frame (11), the middle position at the top of the empennage frame (11), which is fixedly connected with, shunts the wing (10), the empennage
Frame (11) is fixedly connected with empennage (13) far from the one end of body (1), and two sides, which are fixedly connected with, at the top of the empennage frame (11) turns
Dynamic device (9), rotating device (9) top are rotatably connected to deflector (12).
2. a kind of telecontrolled aircraft shell according to claim 1, it is characterised in that: the fixed device (5) includes fixing
Frame (501), the internal middle position of the fixed frame (501) is provided with sliding groove (502), two on the outside of the sliding groove (502)
End is fixedly connected to fixed frame (503), is fixedly connected with bracket (504), the bracket inside the fixed frame (503)
(504) middle part slidably connects fixed link (505), and the fixed link (505) runs through and extends to fixed frame (503) outside, institute
It states and is slidably connected on the inside of sliding groove (502) with installation sliding rail (3).
3. a kind of telecontrolled aircraft shell according to claim 2, it is characterised in that: fixed at the top of the fixed link (505)
It is connected with and pulls unit (507), fixed link (505) outer wall, which is located between fixed frame (503) inner wall and bracket (504), to be arranged
There are spring (506).
4. a kind of telecontrolled aircraft shell according to claim 1, it is characterised in that: the rotating device (9) includes installation
Pedestal (901), mounting seat (901) bottom are fixedly connected by fixing screws (902) with empennage frame (11), the installation
It is fixedly connected with rotation axis (903) inside pedestal (901), is arranged with rotating block (904) in the middle part of the rotation axis (903), it is described
It is fixedly connected with connecting rod (905) at the top of rotating block (904), is turned at the top of the mounting seat (901) by bolt axis (906)
Dynamic to be connected with deflector mounting base (16), deflector mounting base (16) inside bottom is fixedly connected with connecting rod (905).
5. a kind of telecontrolled aircraft shell according to claim 1, it is characterised in that: body (1) the surface two sides installation
There are streamer lamp (15).
6. a kind of telecontrolled aircraft shell according to claim 1, it is characterised in that: the internal interposition of the body (1)
It installs and is equipped with controller mounting groove (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820765036.2U CN208193677U (en) | 2018-05-22 | 2018-05-22 | A kind of telecontrolled aircraft shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820765036.2U CN208193677U (en) | 2018-05-22 | 2018-05-22 | A kind of telecontrolled aircraft shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208193677U true CN208193677U (en) | 2018-12-07 |
Family
ID=64518144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820765036.2U Expired - Fee Related CN208193677U (en) | 2018-05-22 | 2018-05-22 | A kind of telecontrolled aircraft shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208193677U (en) |
-
2018
- 2018-05-22 CN CN201820765036.2U patent/CN208193677U/en not_active Expired - Fee Related
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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: 20181207 |