CN204776014U - Low -latitude flying device - Google Patents
Low -latitude flying device Download PDFInfo
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- CN204776014U CN204776014U CN201520476280.3U CN201520476280U CN204776014U CN 204776014 U CN204776014 U CN 204776014U CN 201520476280 U CN201520476280 U CN 201520476280U CN 204776014 U CN204776014 U CN 204776014U
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- rosette
- armed
- low
- galianconism
- long
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Abstract
The utility model provides a low -latitude flying device, including base, storage battery, 16 rotors and four cross supports, the top and the top of base are fixed with first rosette and second rosette respectively, the cross support includes cross cruciate fixation's long arm and galianconism, every all install two on long arm and the galianconism the rotor, the one end of long arm with first rosette fixed connection, the middle part of long arm pass through the stiffener with second rosette fixed connection, the long arm with first rosette is in same horizontal plane, and this kind of low -latitude flying device has simple mechanical structure, utilizes storage battery as flight power, very big reduction the cost, accord with very much ordinary consumer's receipt degree, the flight operation is fairly simple in addition, need not pass through the strict training can be from the line operate, can satisfy the needs of people's low -latitude flying.
Description
Technical field
The utility model relates to vehicle technology field, particularly relates to a kind of low-latitude flying device.
Background technology
The mankind have the dream of flying aloft, especially oneself beam riding device leaves bottom surface, breaks away from gravitational comfortable, but in order to realize this dream, not only need the aircraft handling training accepting specialty, and the price of present Private Flight device common people neither can be born; Present aircraft is generally provide power by combustion engine, and physical construction is very complicated, cause cost to remain high, be difficult to realize popular, and manipulation gets up to have certain complexity.
Utility model content
The technical problems to be solved in the utility model is: in order to solve current individual lift device complex structure, price is high and operation easier is large problem, the utility model provides a kind of low-latitude flying device and solves the problems referred to above.
The utility model solves the technical scheme that its technical matters adopts: a kind of low-latitude flying device, comprise pedestal, battery pack, 16 rotors and four cross frames, the top of described pedestal and top are fixed with the first rosette and the second rosette respectively, described cross frame comprises the fixing long-armed and galianconism of right-angled crossing, each described long-armed and galianconism is all provided with two described rotors, described long-armed one end is fixedly connected with described first rosette, described long-armed middle part is fixedly connected with described second rosette by stirrup, described long-armed and described first rosette is in same level, described first rosette is also fixed with seat, the point of crossing place of described cross frame is fixed with the support that rises and falls, the described support that rises and falls extends obliquely, each described rotor is connected with a motor, described motor is connected with described battery pack.
As preferably, the point of crossing of cross frame is the middle part of described long-armed middle part and galianconism, two described rotors are arranged on the two ends of described galianconism, and two described rotors are arranged on the described long-armed midway location in point of crossing both sides, and described long-armed length is the twice of galianconism.
As preferably, described in the rise and fall bottom of support be provided with cushion rubber.
As preferably, the bottom of described second salver is provided with elastic ball, and described elastic ball is fixed by the base plate of bottom and elastic threads and described four stirrups.
As preferably, also comprise for control system, described control system comprises controller and control circuit, and described control circuit is connected with 16 described motors, battery pack and controllers, and described controller is fixed on the right side of described seat.
The beneficial effects of the utility model are, this low-latitude flying device has simple physical construction, utilize battery pack as flying power, greatly reduce cost, meet very much the reception degree of ordinary consumer, and flight operation is fairly simple, does not need to get final product Self-operating through strict training, the needs of the low-latitude flying of people can be met.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is the structural representation of the optimum embodiment of low-latitude flying device of the present utility model.
In figure 1, rotor, the 2, first rosette, 3, long-armed, 4, galianconism, 5, rise and fall support, 6, cushion rubber, 7, elastic ball.
Detailed description of the invention
Be described below in detail embodiment of the present utility model, the example of described embodiment is shown in the drawings, and wherein same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Being exemplary below by the embodiment be described with reference to the drawings, only for explaining the utility model, and can not being interpreted as restriction of the present utility model.On the contrary, embodiment of the present utility model comprise fall into attached claims spirit and intension within the scope of all changes, amendment and equivalent.
In description of the present utility model, it will be appreciated that, term " " center ", " longitudinal direction ", " transverse direction ", " length ", " width ", " thickness ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end " " interior ", " outward ", " axis ", " radial direction ", orientation or the position relationship of the instruction such as " circumference " are based on orientation shown in the drawings or position relationship, only the present invention for convenience of description and simplified characterization, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore limitation of the present invention can not be interpreted as.
In addition, term " first ", " second " etc. only for describing object, and can not be interpreted as instruction or hint relative importance.In description of the present utility model, it should be noted that, unless otherwise clearly defined and limited, term " is connected ", " connection " should be interpreted broadly, such as, can be fixedly connected with, also can be removably connect, or connect integratedly; Can be mechanical connection, also can be electrical connection; Can be directly be connected, also indirectly can be connected by intermediary.For the ordinary skill in the art, particular case the concrete meaning of above-mentioned term in the utility model can be understood.In addition, in description of the present utility model, except as otherwise noted, the implication of " multiple " is two or more.
As shown in Figure 1, the utility model provides a kind of low-latitude flying device, comprise pedestal, battery pack, 16 rotors 1 and four cross frames, the top of pedestal and top are fixed with the first rosette 2 and the second rosette respectively, cross frame comprises right-angled crossing fixing long-armed 3 and galianconism 4, each long-armed 3 and galianconism 4 on two rotors 1 are all installed, one end of long-armed 3 is fixedly connected with the first rosette 2, the middle part of long-armed 3 is fixedly connected with the second rosette by stirrup, long-armed 3 and first rosette 2 in same level, first rosette 2 is also fixed with seat (not shown), the point of crossing place of cross frame is fixed with the support 5 that rises and falls, the support 5 that rises and falls extends obliquely, each rotor 1 is connected with a motor, motor is connected with battery pack, the point of crossing of cross frame is the middle part of long-armed 3 and the middle part of galianconism 4, two rotors 1 are arranged on the two ends of galianconism 4, two rotors 1 are arranged on long-armed 3 midways location in point of crossing both sides, the length of long-armed 3 is the twice of galianconism 4, the rise and fall bottom of support 5 is provided with cushion rubber 6, the bottom of the second salver is provided with elastic ball 7, elastic ball 7 is fixed by the base plate of bottom and elastic threads and four stirrups, also comprise for control system, control system comprises controller and control circuit, control circuit and 16 motors, battery pack is connected with controller, controller is fixed on the right side of seat.
In the description of this specification sheets, specific features, structure, material or feature that the description of reference term " embodiment ", " some embodiments ", " example ", " concrete example " or " some examples " etc. means to describe in conjunction with this embodiment or example are contained at least one embodiment of the present utility model or example.In this manual, identical embodiment or example are not necessarily referred to the schematic representation of described term.And the specific features of description, structure, material or feature can combine in an appropriate manner in any one or more embodiment or example.
With above-mentioned according to desirable embodiment of the present utility model for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this utility model technological thought, can carry out various change and amendment completely.The technical scope of this utility model is not limited to the content on specification sheets, must determine its technical scope according to right.
Claims (5)
1. a low-latitude flying device, it is characterized in that: comprise pedestal, battery pack, 16 rotors and four cross frames, the top of described pedestal and top are fixed with the first rosette and the second rosette respectively, described cross frame comprises the fixing long-armed and galianconism of right-angled crossing, each described long-armed and galianconism is all provided with two described rotors, described long-armed one end is fixedly connected with described first rosette, described long-armed middle part is fixedly connected with described second rosette by stirrup, described long-armed and described first rosette is in same level, described first rosette is also fixed with seat, the point of crossing place of described cross frame is fixed with the support that rises and falls, the described support that rises and falls extends obliquely, each described rotor is connected with a motor, described motor is connected with described battery pack.
2. low-latitude flying device as claimed in claim 1, it is characterized in that: the point of crossing of cross frame is the middle part of described long-armed middle part and galianconism, two described rotors are arranged on the two ends of described galianconism, two described rotors are arranged on the described long-armed midway location in point of crossing both sides, and described long-armed length is the twice of galianconism.
3. low-latitude flying device as claimed in claim 2, is characterized in that: described in the rise and fall bottom of support be provided with cushion rubber.
4. low-latitude flying device as claimed in claim 3, is characterized in that: the bottom of described second salver is provided with elastic ball, and described elastic ball is fixed by the base plate of bottom and elastic threads and described four stirrups.
5. low-latitude flying device as claimed in claim 4, it is characterized in that: also comprise for control system, described control system comprises controller and control circuit, described control circuit is connected with 16 described motors, battery pack and controllers, and described controller is fixed on the right side of described seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520476280.3U CN204776014U (en) | 2015-07-04 | 2015-07-04 | Low -latitude flying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520476280.3U CN204776014U (en) | 2015-07-04 | 2015-07-04 | Low -latitude flying device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204776014U true CN204776014U (en) | 2015-11-18 |
Family
ID=54516116
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520476280.3U Expired - Fee Related CN204776014U (en) | 2015-07-04 | 2015-07-04 | Low -latitude flying device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204776014U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104925251A (en) * | 2015-07-04 | 2015-09-23 | 苏州科锐恒机械科技有限公司 | Low-altitude flight device |
-
2015
- 2015-07-04 CN CN201520476280.3U patent/CN204776014U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104925251A (en) * | 2015-07-04 | 2015-09-23 | 苏州科锐恒机械科技有限公司 | Low-altitude flight device |
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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: 20151118 Termination date: 20160704 |