CN202289467U - Empennage device of wireless remotely-controlled flying vehicle - Google Patents
Empennage device of wireless remotely-controlled flying vehicle Download PDFInfo
- Publication number
- CN202289467U CN202289467U CN2011203912129U CN201120391212U CN202289467U CN 202289467 U CN202289467 U CN 202289467U CN 2011203912129 U CN2011203912129 U CN 2011203912129U CN 201120391212 U CN201120391212 U CN 201120391212U CN 202289467 U CN202289467 U CN 202289467U
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- China
- Prior art keywords
- empennage
- buckle
- vertical
- vertical tail
- groove
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- 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
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Abstract
The utility model discloses an empennage device of a wireless remotely-controlled flying vehicle. The empennage device comprises a vertical empennage and a horizontal empennage, wherein the vertical empennage is connected with a rudder capable of swinging leftwards and rightwards through a rotating device; a signal wire leading to a driving power supply at the front end of the flying vehicle is connected to the rotating device; the bottom end face of the vertical empennage is provided with a buckle; the upper surface of the horizontal empennage is provided with a clamping groove which corresponds to the buckle; and the vertical empennage is clamped on the horizontal empennage through the buckle. In the empennage device, the vertical empennage is directly clamped on the horizontal empennage through the buckle which is vertical to the bottom end face of the vertical empennage and the clamping groove in the upper surface of the horizontal empennage, so that the empennage device has a simple structure and is convenient to operate, and the installation accuracy and stability of the vertical empennage can be ensured effectively; and meanwhile, a groove for accommodating a signal wire of the rudder rotating device of the vertical empennage is formed at a contact position between the upper surface of the horizontal empennage and the vertical empennage, so that the rudder signal wire is prevented from being exposed out of the outer surface of the horizontal empennage, an entire product is neat and attractive, and the rudder signal wire is prevented from loosening and falling off.
Description
Technical field
The utility model relates to a kind of tail gear, particularly a kind of tail gear of wireless remote control aircraft.
Background technology
At present, in the general wireless remote control aircraft (specifically can be toy fly-bird), vertical tail generally directly sticks on the tailplane; This has weakened the stability of vertical tail, and the required precision when installing is higher, is not easy to make vertical tail to install along captain's direction; In addition, in the prior art, the general direct surface that the holding wire that leads to aircraft front-end driven power supply on the tumbler on the vertical tail is adhered to tailplane; Make holding wire exposed outside; This has not only influenced the attractive in appearance of single unit system, and comes off easily, influences the stability of aircraft flight.
The utility model content
In order to overcome above-mentioned technical problem, the purpose of the utility model is to provide a kind of vertical tail that the tail gear that simple and reliable, as to connect vertical tail pendulous device and aircraft front-end driven power supply holding wire is placed wireless remote control aircraft firmly attractive in appearance is installed.
The utility model solves the technical scheme that its technical problem adopted:
A kind of tail gear of wireless remote control aircraft; It comprises vertical tail and tailplane; Vertical tail is connected with the rudder that can swing through tumbler, is connected with on the tumbler towards the holding wire of aircraft front-end driven power supply, and the bottom face of said vertical tail is provided with buckle; The upper surface of tailplane is provided with and the corresponding draw-in groove of buckle, and vertical tail is connected on the tailplane through buckle.
Further, the number of said buckle and draw-in groove is greater than or equal to 1, and buckle is arranged along aircraft captain direction.
Further, holding wire sets up along the sidepiece and the bottom margin of vertical tail.
Further, the bottom face of said vertical tail is provided with the screens that is used to place holding wire, screens by about the dislocation buckle form.
Further, said tailplane is provided with the groove that is used to place holding wire, and draw-in groove is opened on the groove, and buckle is provided with groove or the screens that is used for through holding wire, and the right side of vertical tail is provided with the Tibetan wire casing that is used to place holding wire.
The beneficial effect of the utility model is: this product is through the buckle of vertical tail bottom face and the draw-in groove of tailplane upper surface; Directly be connected in vertical tail on the tailplane; Simple in structure, easy to operate, can effectively guarantee precision and steadiness that vertical tail is installed; Simultaneously offer the groove that is used to place vertical tail rudder tumbler holding wire at tailplane upper surface and vertical tail contact position; Avoided the rudder holding wire to expose, made product integral body become neat and artistic, made that also the rudder holding wire is difficult for becoming flexible and coming off at the tailplane outer surface.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the utility model is further specified.
Fig. 1 is the overall structure scheme of installation of the utility model;
Fig. 2 is the side view of the utility model;
Fig. 3 is the utility model decomposing schematic representation;
Fig. 4 is the partial enlarged drawing of A among Fig. 3;
Fig. 5 is the partial enlarged drawing of B among Fig. 3;
Fig. 6 is the opposite side view of the utility model;
Fig. 7 is the cutaway view in C among Fig. 6-C cross section;
Fig. 8 is the projection view that the D parts are looked up by the vertical tail bottom surface among Fig. 3.
The specific embodiment
Referring to figs. 1 through Fig. 8; The tail gear of a kind of wireless remote control aircraft of the utility model; It comprises vertical tail 1 and tailplane 2, and vertical tail 1 is connected with the rudder 3 that can swing through tumbler 11, is connected with on the tumbler 11 towards the holding wire 4 of aircraft front-end driven power supply; The bottom face of said vertical tail 1 is provided with buckle 12; Buckle 12 and vertical tail 1 direct injection mo(u)lding, the upper surface of tailplane 2 is provided with and buckle 12 corresponding draw-in grooves 21, and vertical tail 1 is connected on the tailplane 2 through buckle 12.Because vertical tail 1 all is plastic products with tailplane 2, all have certain compressed capability, therefore directly vertical tail 1 is fixedly mounted on the tailplane 2 through the elasticity extruding force between buckle 12 and the draw-in groove 21.
In order to increase the steadiness of vertical tail 1, the number of said buckle 12 and draw-in groove 21 is greater than or equal to 1, and buckle 12 is arranged along aircraft captain direction.
In the utility model; Holding wire 4 sets up along the sidepiece and the bottom margin of vertical tail 1; The bottom face of said vertical tail 1 is provided with the screens that is used to place holding wire 4, and screens is formed by the alternate buckle 12 of dislocation, during installation; Press holding wire 4 between the alternate buckle of dislocation 12, block holding wire 4 through the slit of left and right sides buckle 12.
In the utility model, said tailplane is provided with the groove 22 that is used to place holding wire, and draw-in groove 21 is opened on the groove 22; Groove 22 is slightly long than the length of vertical tail 1, is positioned in the wire casing 13 of Tibetan with convenient holding wire 4 is drawn, and buckle 12 is provided with groove or the screens that is used for through holding wire; The right side of vertical tail is provided with the Tibetan wire casing that is used to place holding wire, during installation, holding wire 4 is placed on groove 22 and hides in the wire casing; Then vertical tail 1 is connected on the tailplane 2; At this moment, holding wire 4 is by vertical tail 1 and tailplane 2 chuckings, and holding wire 4 is not easy to get loose.
Claims (5)
1. the tail gear of a wireless remote control aircraft; Comprise vertical tail (1) and tailplane (2); Vertical tail (1) is connected with the rudder (3) that can swing through tumbler (11); Be connected with holding wire (4) on the tumbler (11) towards aircraft front-end driven power supply; It is characterized in that: the bottom face of said vertical tail (1) is provided with buckle (12), and the upper surface of tailplane (2) is provided with and the corresponding draw-in groove of buckle (12) (21), and vertical tail (1) is connected on the tailplane (2) through buckle (12).
2. the tail gear of a kind of wireless remote control aircraft according to claim 1 is characterized in that: the number of said buckle (12) and draw-in groove (21) is greater than or equal to 1, and buckle (12) is arranged along aircraft captain direction.
3. the tail gear of a kind of wireless remote control aircraft according to claim 1 is characterized in that: holding wire (4) sets up along the sidepiece and the bottom margin of vertical tail (1).
4. the tail gear of a kind of wireless remote control aircraft according to claim 3 is characterized in that: the bottom face of said vertical tail (1) is provided with the screens that is used to place holding wire (4), screens by about the dislocation buckle (12) form.
5. according to the tail gear of claim 3 or 4 described a kind of wireless remote control aircraft; It is characterized in that: said tailplane (2) is provided with the groove (22) that is used to place holding wire (4); Draw-in groove (21) is opened on the groove (22); Buckle (12) is provided with groove or the screens that is used for through holding wire, and the right side of vertical tail (1) is provided with the Tibetan wire casing that is used to place holding wire.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011203912129U CN202289467U (en) | 2011-10-14 | 2011-10-14 | Empennage device of wireless remotely-controlled flying vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011203912129U CN202289467U (en) | 2011-10-14 | 2011-10-14 | Empennage device of wireless remotely-controlled flying vehicle |
Publications (1)
Publication Number | Publication Date |
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CN202289467U true CN202289467U (en) | 2012-07-04 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011203912129U Expired - Fee Related CN202289467U (en) | 2011-10-14 | 2011-10-14 | Empennage device of wireless remotely-controlled flying vehicle |
Country Status (1)
Country | Link |
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CN (1) | CN202289467U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106362415A (en) * | 2015-07-20 | 2017-02-01 | 赖清坤 | Toy airplane combined component |
-
2011
- 2011-10-14 CN CN2011203912129U patent/CN202289467U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106362415A (en) * | 2015-07-20 | 2017-02-01 | 赖清坤 | Toy airplane combined component |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120704 Termination date: 20141014 |
|
CF01 | Termination of patent right due to non-payment of annual fee |