CN205738059U - A kind of adjustable wing aeromodelling aerocraft - Google Patents
A kind of adjustable wing aeromodelling aerocraft Download PDFInfo
- Publication number
- CN205738059U CN205738059U CN201620414033.5U CN201620414033U CN205738059U CN 205738059 U CN205738059 U CN 205738059U CN 201620414033 U CN201620414033 U CN 201620414033U CN 205738059 U CN205738059 U CN 205738059U
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- wing
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- outfan
- microprocessor
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Abstract
The utility model discloses a kind of adjustable wing aeromodelling aerocraft, including wing, fuselage, head, signal emission module, supply module and microprocessor, the described fuselage left and right sides is provided with wing mount plate, described wing is arranged on wing mount plate, described wing is mounted below wing frame, described wing is flexibly connected with wing frame by wing bearing rod, described wing frame is mounted below expansion link, on described head, propeller is installed, described afterbody is provided with vertical tail and tailplane, the outfan of described signal emission module is electrically connected with the input of signal receiving module, the outfan of described microprocessor is electrically connected with the input of power take-off module, being electrically connected with microprocessor of described supply module.This utility model uses the toothed disc break-in technology to wing, devises a kind of adjustable wing aircraft, improves the flight stability of aircraft and enrich the multiformity of aircraft flight track.
Description
Technical field
This utility model relates to aeromodelling aerocraft technical field, is specially a kind of adjustable wing aeromodelling aerocraft.
Background technology
At present, along with the scientific and technological innovation with technology and development, the most capable replacement of aeromodelling aerocraft, aeromodelling aerocraft, as its name suggests, it it is a kind of mould imitating actual aircraft, aeromodelling aerocraft not only outward appearance imitates actual aircraft, internal structure and principle are also such, aeromodelling aerocraft is not only a simple mould or toy, aeromodelling aerocraft embodies the technological achievement of actual aircraft to a certain extent, on the market, although common aeromodelling aerocraft energy normal flight, but flight stability is not fine, controlled flight path is the most single, not fully up to expectations, the biggest reason is that in the design of wing and there is certain defect.
Summary of the invention
The purpose of this utility model is to provide a kind of adjustable wing aeromodelling aerocraft, to solve the problem proposed in above-mentioned background technology, is had an advantageous effect in that；The wing of this equipment design is connected with fuselage by movable part, and it is mounted with toothed disc, expansion link and the servomotor being attached thereto, user can be by the sweep angle of the control break wing of remote control and dihedral, there is such design, in the flight course of this equipment more stable, flight path the most more multiformity.
nullFor achieving the above object，This utility model following technical scheme of offer: a kind of adjustable wing aeromodelling aerocraft，Including wing、Fuselage、Head、Signal emission module、Supply module and microprocessor，The described fuselage left and right sides is provided with wing mount plate，Described wing is arranged on wing mount plate，And wing is flexibly connected with wing mount plate，Described wing is mounted below wing frame，And wing frame is flexibly connected with wing mount plate，Described wing is flexibly connected with wing frame by wing bearing rod，Described wing bearing rod is connected with toothed disc，And toothed disc is connected with sweep angle servomotor，Described wing frame is mounted below expansion link，And expansion link and wing mount plate are fixing is connected，On described head, propeller is installed，Described afterbody is provided with vertical tail and tailplane，And on vertical tail, it is provided with direction top，Lifting top it is provided with on tailplane，The outfan of described signal emission module is electrically connected with the input of signal receiving module，And the input of the outfan of signal receiving module and microprocessor is electrically connected with，The outfan of described microprocessor is electrically connected with the input of power take-off module，And the input of the outfan of power take-off module and actuator is electrically connected with，Being electrically connected with microprocessor of described supply module，And supply module is electrically connected with power take-off module.
Preferably, described wing is internally installed wing extending transversely, and wing extending transversely is connected with wing inwall gap.
Preferably, described head, wing and afterbody lower end are fitted with on undercarriage, and undercarriage being provided with road wheel.
Preferably, described fuselage lower end is provided with horizontal turbine and vertical turbine.
Preferably, the outfan of described microprocessor is electrically connected with the input of radiating module, and the input of the outfan of power take-off module and radiating module is electrically connected with.
Compared with prior art, the beneficial effects of the utility model are: this equipment has had more perfect design to wing, the wing of existing aeromodelling aerocraft is all fixing, the stability that aeromodelling aerocraft is flown by fixing wing can not well ensure, by contrast, the wing of existing aeromodelling aerocraft is optimized by this equipment, the wing of this equipment design is connected with fuselage by movable part, and it is mounted with the toothed disc being attached thereto, expansion link and servomotor, user can be by the sweep angle of the control break wing of remote control and dihedral, there is such design, in the flight course of this equipment more stable, flight path the most more multiformity.
Accompanying drawing explanation
Fig. 1 is surface structure schematic diagram of the present utility model；
Fig. 2 is wing structure schematic diagram of the present utility model；
Fig. 3 is system structure schematic diagram of the present utility model.
In figure: 1-propeller；2-wing；3-fuselage；4-tailplane；5-lifts top；6-vertical tail；7-direction top；8-head；9-undercarriage；10-road wheel；11-vertical turbine；12-horizontal turbine；13-wing extending transversely；14-sweep angle servomotor；15-toothed disc；16-wing mount plate；17-wing bearing rod；18-wing frame；19-expansion link；20-signal emission module；21-signal receiving module；22-supply module；23-microprocessor；24-radiating module；25-power take-off module；26-actuator.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1-3，A kind of embodiment that this utility model provides: a kind of adjustable wing aeromodelling aerocraft，Including wing 2、Fuselage 3、Head 8、Signal emission module 20、Supply module 22 and microprocessor 23，Fuselage 3 left and right sides is provided with wing mount plate 16，Wing 2 is arranged on wing mount plate 16，And wing 2 is flexibly connected with wing mount plate 16，Wing 2 is mounted below wing frame 18，And wing frame 18 is flexibly connected with wing mount plate 16，Wing 2 is flexibly connected with wing frame 18 by wing bearing rod 17，Wing bearing rod 17 is connected with toothed disc 15，And toothed disc 15 is connected with sweep angle servomotor 14，Wing frame 18 is mounted below expansion link 19，And expansion link 19 and wing mount plate 16 is fixing is connected，Propeller 1 is installed on head 8，Fuselage 3 afterbody is provided with vertical tail 6 and tailplane 4，And on vertical tail 6, it is provided with direction top 7，Lifting top 5 it is provided with on tailplane 4，The outfan of signal emission module 20 is electrically connected with the input of signal receiving module 21，And the input of the outfan of signal receiving module 21 and microprocessor 23 is electrically connected with，The outfan of microprocessor 23 is electrically connected with the input of power take-off module 25，And the input of the outfan of power take-off module 25 and actuator 26 is electrically connected with，Being electrically connected with microprocessor 23 of supply module 22，And supply module 22 is electrically connected with power take-off module 25，Wing 2 is internally installed wing 13 extending transversely，And wing 13 extending transversely is connected with wing 2 inwall gap，Head 8、Wing 2 and fuselage 3 afterbody lower end are fitted with undercarriage 9，And road wheel 10 is installed on undercarriage 9，Fuselage 3 lower end is provided with horizontal turbine 12 and vertical turbine 11，The outfan of microprocessor 23 is electrically connected with the input of radiating module 24，And the input of the outfan of power take-off module 25 and radiating module 24 is electrically connected with.
Operation principle: during use, signal emission module 20 launches signal, signal receiving module 21 transmits a signal to microprocessor 23 after receiving signal, microprocessor 23 controls corresponding motor after receiving appointment order, the power take-off modules such as servomotor 25 run, under the operation power of horizontal turbine 12 and vertical turbine 11, aeromodelling aerocraft takes off, the controllers rotation by remote pilot wing 2, start sweep angle servomotor 14, sweep angle servomotor 14 changes wing 2 sweep angle by toothed disc 15, manipulation expansion link 19, wing 2 dihedral can be changed, change of flight track is carried out by the sweep angle and dihedral controlling wing 2, vertical tail 6 and extension wing 13 can improve the stability of flight, tailplane 4 rises for aircraft provides a determined power.
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to realize this utility model in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes fallen in the implication of equivalency and scope of claim included in this utility model.Should not be considered as limiting involved claim by any reference in claim.
Claims (5)
- null1. an adjustable wing aeromodelling aerocraft，Including wing (2)、Fuselage (3)、Head (8)、Signal emission module (20)、Supply module (22) and microprocessor (23)，It is characterized in that: described fuselage (3) left and right sides is provided with wing mount plate (16)，Described wing (2) is arranged on wing mount plate (16)，And wing (2) is flexibly connected with wing mount plate (16)，Described wing (2) is mounted below wing frame (18)，And wing frame (18) is flexibly connected with wing mount plate (16)，Described wing (2) is flexibly connected with wing frame (18) by wing bearing rod (17)，Described wing bearing rod (17) is connected with toothed disc (15)，And toothed disc (15) is connected with sweep angle servomotor (14)，Described wing frame (18) is mounted below expansion link (19)，And expansion link (19) and wing mount plate (16) are fixing is connected，Propeller (1) is installed on described head (8)，Described fuselage (3) afterbody is provided with vertical tail (6) and tailplane (4)，And on vertical tail (6), it is provided with direction top (7)，Lifting top (5) it is provided with on tailplane (4)，The outfan of described signal emission module (20) is electrically connected with the input of signal receiving module (21)，And the input of the outfan of signal receiving module (21) and microprocessor (23) is electrically connected with，The outfan of described microprocessor (23) is electrically connected with the input of power take-off module (25)，And the input of the outfan of power take-off module (25) and actuator (26) is electrically connected with，Being electrically connected with microprocessor (23) of described supply module (22)，And supply module (22) is electrically connected with power take-off module (25).
- A kind of adjustable wing aeromodelling aerocraft the most according to claim 1, it is characterised in that: described wing (2) is internally installed wing extending transversely (13), and wing extending transversely (13) is connected with wing (2) inwall gap.
- A kind of adjustable wing aeromodelling aerocraft the most according to claim 1, it is characterised in that: described head (8), wing (2) and fuselage (3) afterbody lower end are fitted with on undercarriage (9), and undercarriage (9) being provided with road wheel (10).
- A kind of adjustable wing aeromodelling aerocraft the most according to claim 1, it is characterised in that: described fuselage (3) lower end is provided with horizontal turbine (12) and vertical turbine (11).
- A kind of adjustable wing aeromodelling aerocraft the most according to claim 1, it is characterized in that: the outfan of described microprocessor (23) is electrically connected with the input of radiating module (24), and the input of the outfan of power take-off module (25) and radiating module (24) is electrically connected with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414033.5U CN205738059U (en) | 2016-05-10 | 2016-05-10 | A kind of adjustable wing aeromodelling aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414033.5U CN205738059U (en) | 2016-05-10 | 2016-05-10 | A kind of adjustable wing aeromodelling aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205738059U true CN205738059U (en) | 2016-11-30 |
Family
ID=57370583
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620414033.5U Expired - Fee Related CN205738059U (en) | 2016-05-10 | 2016-05-10 | A kind of adjustable wing aeromodelling aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205738059U (en) |
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2016
- 2016-05-10 CN CN201620414033.5U patent/CN205738059U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161130 Termination date: 20170510 |