CN201139948Y - Model aerial vehicle - Google Patents
Model aerial vehicle Download PDFInfo
- Publication number
- CN201139948Y CN201139948Y CNU2007200601901U CN200720060190U CN201139948Y CN 201139948 Y CN201139948 Y CN 201139948Y CN U2007200601901 U CNU2007200601901 U CN U2007200601901U CN 200720060190 U CN200720060190 U CN 200720060190U CN 201139948 Y CN201139948 Y CN 201139948Y
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- China
- Prior art keywords
- model aircraft
- main frame
- model
- fixed
- power component
- 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 - Lifetime
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- 230000005540 biological transmission Effects 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000003796 beauty Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
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- Toys (AREA)
Abstract
The utility model discloses a model aerial craft, which comprises a main body frame, a head casing, a leg support, a controller and four shafts, wherein the head casing is connected with the top portion of the main body frame, the leg support connected with the lower portion of the main body frame is used to support the main body frame, the controller can receive controlling signals of outside, and the four shafts arranged on four corners of the main body frame are respectively fixed in cross shape, and each shaft fixes a dynamic component which comprises a motor, a screw propeller and a gear connecting device. The model aerial craft can control take-off and landing of the model aerial craft better through a quarternary control system of the four dynamic components, thereby being capable of flying in a narrow space, and maintaining balance for a long time during the flying process.
Description
Technical field
The utility model relates to a kind of electronic toy, and more particularly, the utility model relates to a kind of model aircraft.
Background technology
The model aircraft of prior art is generally all only controlled two screws and is made its balance flight, such model aircraft is not easy to keep for a long time balance in flight course, the easy disequilibrium in case be interfered, and it takes off and lands and all requires the flying field that broader space is arranged, therefore, often can only carry out the flight of model aircraft in open open-air place.Along with the variation of society, broad place is fewer and feweri in the city, and a lot of people wish and can also can play the model aircraft in the narrow space relatively.
Therefore, provide a kind of above-mentioned deficiency of model aircraft that can overcome prior art, can also can play the model aircraft in relative narrow space becomes the industry urgent problem.
Summary of the invention
Technical problem to be solved in the utility model is that the balance that can keep for a long time that provides at above-mentioned existing in prior technology defective is flown, and can be at the model aircraft of narrow space flight.
Solving the technical scheme that the utility model technical problem adopted is: a kind of model aircraft comprises main frame, the head-shield that is connected with the main frame top, is connected the foot rest that is used to support this main frame, the controller that is arranged at the Power Component on the described main frame and can receives external control signal with the main frame bottom, the angle of four correspondences of described main frame is fixed into criss-cross four axles respectively, and every axle is fixed a Power Component.
The beneficial effects of the utility model are: be fixed into criss-cross four axles respectively by the angle in four correspondences of described model aircraft body frame, every axle is fixed four of a Power Component and is closed control system and can control model aircraft takeoff and landing better, thereby can fly at narrow space, and in flight course, can keep balance for a long time.
Preferred implementation as the utility model model aircraft, described Power Component comprises motor and screw, described motor is connected by transmission device with screw, described transmission device comprises that the gear that is installed on the power output shaft on this motor and is fixed in this end is connected the main shaft that the other end is fixedlyed connected with screw with an end with described gears engaged.
As another preferred implementation of the utility model model aircraft, also comprise the battery carrier that is arranged at the foot rest lower end, fixing promising consuming parts provides the battery of electric energy in the described battery carrier.
As another preferred implementation of the utility model model aircraft, at least one camera and the steering wheel that is connected with camera by Swing Arm are also fixed in the lower end of described battery carrier, steering wheel is in order to the orientation of control camera, make the operator can clearly see the scape shape that model aircraft flight scope is interior, thereby have more recreational and interesting.
As another preferred implementation of the utility model model aircraft, described controller has built-in gyroscope, can change the heading of model aircraft at any time according to operator's instruction.
Below in conjunction with drawings and Examples, the technical solution of the utility model is described in further detail.
Description of drawings
Fig. 1 is the schematic diagram of the model aircraft of a preferred embodiment of the utility model.
Fig. 2 is the explosive view of Fig. 1.
Fig. 3 is the enlarged drawing at Figure 1A place.
The specific embodiment
With reference now to accompanying drawing, preferred embodiment of the present utility model is described.
With reference to figure 1, Fig. 2, the utility model model aircraft comprises main frame 10, the head-shield 20 that is connected with the main frame top, be connected the foot rest 30 that is used to support this main frame with the main frame bottom, be arranged at the Power Component 40 on the described main frame and can receive external control signal controller 50.
Referring to figs. 2 and 3, the angle of 10 4 correspondences of described main frame is fixed into criss-cross four axles 11 respectively, article four, axle 11 is hollow pipes, every axle 11 other ends are fixed a Power Component 40, Power Component 40 is used for the model aircraft and produces buoyancy, so that make the lift-off of model aircraft, described Power Component 40 comprises motor 46, screw 41, be installed on the power output shaft on this motor and be fixed in the gear 44 of this end, one end is connected with described gears engaged, main shaft 43 that the other end is fixedlyed connected with screw 41 and fixture 42 thereof, Power Component 40 is fixed on an end of axle 11 by fixture 42 usefulness screws or other detachable apparatus, the LED lamp 45 that is arranged on the motor 46 sends the colour lamplight of flicker when the model aircraft flight, to increase the visual effect of model aircraft.
With reference to figure 2, fixing promising motor 46, controller 50, steering wheel 61, camera 63 and LED lamp 45 provide the battery 64 of electric energy in the described battery carrier 60, also be fixed with a steering wheel 61 and a camera 63 on the battery carrier 60, steering wheel 61 is connected with camera 63 by only swing arm 62, steering wheel 61 is controlled the angle of camera 63 shootings by only swing arm 62, make the operator can clearly see the scape shape that model aircraft flight scope is interior, thereby have more recreational and interesting.
With reference to figure 2; described main body rack 10 tops are provided with the antenna 21 that receives external control signal; antenna 21 passes the head-shield 20 that is connected with the main frame top; described head-shield 20 1 is to protect the controller of fixing on it 50; another purpose is exactly a decorative effect, strengthens the visual sense of beauty of model aircraft.
With reference to figure 2, described controller 50 passes hollow shaft 11 with the connecting line (not shown) and is connected to Power Component 40, controller 50 has built-in gyroscope 51, heading in order to control model aircraft, the signal that controller 50 can the wireless receiving operator sends, control motor 46, steering wheel 61 according to the signal that the operator sends, so that the model aircraft is carried out remote control.
With reference to figure 2, described foot rest 30 is connected in the bottom of main body rack 10, bolster model aircraft when being used for model aircraft takeoff and landing, and the lighter aluminum pipe 31 of foot rest bottom two parallel weight of Corner Strapped is beneficial to model aircraft grease it in.
Last institute should be noted that; above embodiment is only in order to the explanation the technical solution of the utility model but not to the restriction of the utility model protection domain; although the utility model has been done detailed description with reference to preferred embodiment; but those of ordinary skill in the art is to be understood that; can make amendment or be equal to replacement the technical solution of the utility model, and not break away from the essence and the scope of technical solutions of the utility model.
Claims (10)
1. model aircraft, comprise main frame, the head-shield that is connected with the main frame top, be connected the foot rest that is used to support this main frame, the controller that is arranged at the Power Component on the described main frame and can receives external control signal with the main frame bottom, it is characterized in that: the angle of four correspondences of described main frame is fixed into criss-cross four axles respectively, and every axle is fixed a Power Component.
2. model aircraft as claimed in claim 1 is characterized in that: described Power Component comprises motor and screw, and described motor is connected by transmission device with screw.
3. model aircraft as claimed in claim 2, it is characterized in that: described transmission device comprises that the gear that is installed on the power output shaft on this motor and is fixed in this end is connected the main shaft that the other end is fixedlyed connected with screw with an end with described gears engaged.
4. model aircraft as claimed in claim 1 is characterized in that: also comprise the battery carrier that is arranged at the foot rest lower end, fixing promising consuming parts provides the battery of electric energy in the described battery carrier.
5. model aircraft as claimed in claim 4 is characterized in that: at least one camera is also fixed in the lower end of described battery carrier.
6. model aircraft as claimed in claim 4 is characterized in that: at least one steering wheel is also fixed in the lower end of described battery carrier, and described steering wheel is connected with camera by waving fraud.
7. model aircraft as claimed in claim 1 is characterized in that: described controller has built-in gyroscope.
8. model aircraft as claimed in claim 1 is characterized in that: it is hollow pipes that the angle of four correspondences of described main frame is fixed into criss-cross four axles respectively, and described controller passes this axle with connecting line and is connected to Power Component.
9. model aircraft as claimed in claim 1 is characterized in that: described main frame top is provided with the antenna that receives external control signal.
10. model aircraft as claimed in claim 1 is characterized in that: described foot rest bottom is provided with two parallel pipes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200601901U CN201139948Y (en) | 2007-11-27 | 2007-11-27 | Model aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200601901U CN201139948Y (en) | 2007-11-27 | 2007-11-27 | Model aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201139948Y true CN201139948Y (en) | 2008-10-29 |
Family
ID=40067665
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200601901U Expired - Lifetime CN201139948Y (en) | 2007-11-27 | 2007-11-27 | Model aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201139948Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102743880A (en) * | 2012-07-05 | 2012-10-24 | 罗之洪 | Disc-shaped aircraft toy |
| US9016617B2 (en) | 2012-11-15 | 2015-04-28 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| CN106081108A (en) * | 2016-08-10 | 2016-11-09 | 成都蜀尚星科技有限公司 | A kind of Combined unmanned machine |
| CN106628173A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Four power-driven aircraft |
-
2007
- 2007-11-27 CN CNU2007200601901U patent/CN201139948Y/en not_active Expired - Lifetime
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102743880A (en) * | 2012-07-05 | 2012-10-24 | 罗之洪 | Disc-shaped aircraft toy |
| CN102743880B (en) * | 2012-07-05 | 2014-12-10 | 罗之洪 | Disc-shaped aircraft toy |
| US9394048B2 (en) | 2012-11-15 | 2016-07-19 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US10189562B2 (en) | 2012-11-15 | 2019-01-29 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US9221536B2 (en) | 2012-11-15 | 2015-12-29 | Sz Dji Technology, Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US9233754B1 (en) | 2012-11-15 | 2016-01-12 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US9284049B1 (en) | 2012-11-15 | 2016-03-15 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US9321530B2 (en) | 2012-11-15 | 2016-04-26 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US9016617B2 (en) | 2012-11-15 | 2015-04-28 | SZ DJI Technology Co., Ltd | Unmanned aerial vehicle and operations thereof |
| US11338912B2 (en) | 2012-11-15 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10472056B2 (en) | 2012-11-15 | 2019-11-12 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10155584B2 (en) | 2012-11-15 | 2018-12-18 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US9221537B2 (en) | 2012-11-15 | 2015-12-29 | Sz Dji Technology, Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10196137B2 (en) | 2012-11-15 | 2019-02-05 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| US10272994B2 (en) | 2012-11-15 | 2019-04-30 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| CN106628173A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Four power-driven aircraft |
| CN106081108A (en) * | 2016-08-10 | 2016-11-09 | 成都蜀尚星科技有限公司 | A kind of Combined unmanned machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170328 Address after: 511475 Nansha District, Guangdong, Tung Chung Town, Tai Po Industrial Zone Patentee after: Guangzhou city huakeer Polytron Technologies Inc Address before: 511430 Guangdong city of Guangzhou province Panyu District yuwotou town Taishi Industrial Zone huakeer Technology Co. Ltd Patentee before: Luo Zhihong |