CN204996123U - Multi -axis aircraft - Google Patents
Multi -axis aircraft Download PDFInfo
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- CN204996123U CN204996123U CN201520669035.4U CN201520669035U CN204996123U CN 204996123 U CN204996123 U CN 204996123U CN 201520669035 U CN201520669035 U CN 201520669035U CN 204996123 U CN204996123 U CN 204996123U
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- axis aircraft
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Abstract
The utility model provides a multi -axis aircraft, includes organism, a plurality of motor and rotor, the organism has the foot rest, be equipped with a plurality of wing framves on the organism, the end of wing frame all is equipped with the motor, motor connection rotor, the output shaft of motor set up down, the rotor connect on the output shaft of motor below. The organism on be equipped with four wing framves, the outer end of four wing framves all is equipped with the frame that protects that the strip body constitutes. Protect the frame for fan -shaped, the fan -shaped periphery of protecting an encirclement at the motor. The utility model discloses a multi -axis aircraft adopts a plurality of CD -ROM drive motors and all disposes the structure of putting the rotor down for an in -process is sent out going up to the air to the aircraft, and the rotor need not to overcome the forward resistance that the motor cross section brought, has advantage rational in infrastructure moreover.
Description
Technical field:
The utility model belongs to the remote control Multi-axis aircraft in remotely-piloted vehicle field, and what be specifically related to is a kind of Multi-axis aircraft.
Background technology:
Existing remote-controlled aircraft can arbitrarily remote control distributor with it, the feature that playability is high and deeply welcomed by the people, and camera can be attached carry out video capture, be used in some particular surroundings, the particularly aircraft of some multiaxis, drive with its multiaxis and there is good stability and well received, if the patent No. is 201420808807.3, name is called three axle aerobat toy Chinese utility model patents, it discloses a kind of three axle aerobat toys, comprise fuselage and three rotor unit, the rotorshaft of first rotor unit is positioned at the dead ahead of fuselage, the rotorshaft of second rotor unit is positioned at the left back of fuselage, the rotorshaft of the 3rd rotor unit is positioned at the right back of fuselage, second rotor unit and the 3rd rotor unit are symmetrically arranged, the rotor quantity of described second rotor unit is one group, the rotor quantity of the 3rd rotor unit is also one group, the rotor quantity of described first rotor unit is two groups, and these two groups of rotors are arranged up and down and rotation direction is contrary, and the rotating shaft of two groups of rotors forms coaxial relation.But the output of the motor of the Multi-axis aircraft of this kind of structure is all arrange upward, screw is all mounted in the upper end of motor, the process risen, utilize propeller rotational, downward blow out air, utilize downward air stream to order about aircraft and rise, but due to underlying motor, certain direct inhibition can be produced to air-flow, the process need making aircraft increase air stream more fast than theoretical value, cause the lift-off decline of efficiency and the waste of the energy.
Summary of the invention:
For the defect that prior art exists, the purpose of this utility model is to provide a kind of Multi-axis aircraft that can overcome above-mentioned defect.
The technical scheme in the invention for solving the technical problem is: a kind of Multi-axis aircraft, key is that described Multi-axis aircraft comprises body, multiple motor and rotor, described body has foot rest, described body is provided with multiple wing frame, the end of wing frame is equipped with motor, motor connects rotor, and the output shaft of described motor is arranged down, and described rotor is connected on the output shaft below motor.
Described body is provided with four wing framves, and the outer end of four wing framves is equipped with the retaining frame of strip shape body formation.
Described retaining frame is fan-shaped, and described fan-shaped retaining frame is enclosed in the periphery of motor.
Multi-axis aircraft of the present utility model adopts multiple CD-ROM drive motor and all configures the structure of underlying rotor, aircraft is sent out in process, the forward resistance that rotor brings without the need to overcoming motor cross section in lift-off, and has advantage rational in infrastructure.
Accompanying drawing illustrates:
Fig. 1 is the utility model structural representation.
Fig. 2 is the utility model structure schematic side view.
Detailed description of the invention:
As shown in Figure 1 to Figure 2, a kind of Multi-axis aircraft, described Multi-axis aircraft comprises body 1, multiple motor 2 and rotor 3, described body has foot rest 4, described body is provided with multiple wing frame, and the end of wing frame is equipped with motor, and motor connects rotor, the output shaft of described motor is arranged down, and described rotor is connected on the output shaft below motor.Described body, remote control and control section circuit and motor are product of the prior art.After the height of foot rest is arranged on motor 2 with rotor, put on the ground, rotor can not touch ground and be as the criterion.Body 1 comprises main part and wing frame part, is provided with the component such as mainboard and battery in main part, and the wing erects the effect of the arm of force supporting and extend motor, is vertically installed with motor and adopts to be wired to mainboard in wing frame end.
Described body is provided with four wing framves, and the outer end of four wing framves is equipped with the retaining frame 5 of strip shape body formation.Time described retaining frame is for preventing aircraft from landing, rotor touches ground or other hard object.As embodiment, motor rotor can adopt three groups, i.e. three-axis structure.Also four axle construction or five axle construction can be adopted.
Described retaining frame 5 is fan-shaped, and described fan-shaped retaining frame is enclosed in the periphery of motor.Retaining frame is that the fan-shaped retaining frame that makes also has good protective effect while having simple structure.
Claims (3)
1. a Multi-axis aircraft, it is characterized in that described Multi-axis aircraft comprises body, multiple motor and rotor, described body has foot rest, described body is provided with multiple wing frame, the end of wing frame is equipped with motor, motor connects rotor, and the output shaft of described motor is arranged down, and described rotor is connected on the output shaft below motor.
2. Multi-axis aircraft according to claim 1, is characterized in that described body is provided with four wing framves, and the outer end of four wing framves is equipped with the retaining frame of strip shape body formation.
3. Multi-axis aircraft according to claim 2, is characterized in that described retaining frame is fan-shaped, and described fan-shaped retaining frame is enclosed in the periphery of motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520669035.4U CN204996123U (en) | 2015-08-29 | 2015-08-29 | Multi -axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520669035.4U CN204996123U (en) | 2015-08-29 | 2015-08-29 | Multi -axis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204996123U true CN204996123U (en) | 2016-01-27 |
Family
ID=55153030
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520669035.4U Active CN204996123U (en) | 2015-08-29 | 2015-08-29 | Multi -axis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204996123U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| JP2021181309A (en) * | 2020-08-04 | 2021-11-25 | 株式会社A.L.I.Technologies | Flying body |
-
2015
- 2015-08-29 CN CN201520669035.4U patent/CN204996123U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| JP2021181309A (en) * | 2020-08-04 | 2021-11-25 | 株式会社A.L.I.Technologies | Flying body |
| JP7002801B2 (en) | 2020-08-04 | 2022-01-20 | 株式会社A.L.I.Technologies | Flying object |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20200304 Granted publication date: 20160127 |
|
| PP01 | Preservation of patent right | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20230304 Granted publication date: 20160127 |
|
| PD01 | Discharge of preservation of patent | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20230304 Granted publication date: 20160127 |
|
| PP01 | Preservation of patent right |