CN109552596A - It is a kind of can be with the unmanned plane of stabilized flight - Google Patents
It is a kind of can be with the unmanned plane of stabilized flight Download PDFInfo
- Publication number
- CN109552596A CN109552596A CN201811447064.0A CN201811447064A CN109552596A CN 109552596 A CN109552596 A CN 109552596A CN 201811447064 A CN201811447064 A CN 201811447064A CN 109552596 A CN109552596 A CN 109552596A
- Authority
- CN
- China
- Prior art keywords
- hydraulic device
- groove
- motor
- unmanned plane
- wing
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hydraulic Motors (AREA)
Abstract
The present invention discloses one kind can be with the unmanned plane of stabilized flight, including fuselage main body, the upper surface of described fuselage main body is equipped with groove, hydraulic device one is equipped with inside the bottom surface of the groove, the hydraulic device one protrudes into one end in groove equipped with motor, it is uniformly hingedly equipped with several flabellums on the transmission shaft of the motor, hydraulic device two is equipped with inside the transmission shaft of the motor, one end that the hydraulic device two stretches out transmission shaft is equipped with pressing plate.Advantages of the present invention: it only needs that wing can be controlled in the folding and unfolding of groove by the flexible of hydraulic device one, it will not be again when not in use by wing exposure, also wing would not occur and break phenomenon, and wing can be fixed by hydraulic device two and pressing plate, to make its flight stability.
Description
Technical field
The present invention relates to a kind of unmanned plane, it is specifically a kind of can be with the unmanned plane of stabilized flight.
Background technique
Existing unmanned plane known to us, is substantially wing and fuselage is fixed together, and places not side
Just, and its wing be easy encountered and damaged, thus make entire unmanned plane will be unable to using；Have again be exactly existing unmanned plane machine
The stability of the wing is inadequate, easily shakes, and can not adjust.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides one kind can be with the unmanned plane of stabilized flight, it is only necessary to
It, will not be again when not in use by wing exposure, also just not by the flexible wing that can control of hydraulic device one in the folding and unfolding of groove
It will appear wing and break phenomenon, and wing can be fixed by hydraulic device two and pressing plate, to make its flight stability.
To achieve the goals above, one kind that the present invention uses can be with the unmanned plane of stabilized flight, including fuselage main body, institute
The upper surface of fuselage main body stated is equipped with groove, is equipped with hydraulic device one, the hydraulic device inside the bottom surface of the groove
One, which protrudes into one end in groove, is equipped with motor, several flabellums are uniformly hingedly equipped on the transmission shaft of the motor, described
Hydraulic device two is equipped with inside the transmission shaft of motor, one end that the hydraulic device two stretches out transmission shaft is equipped with pressing plate.
The groove is cylinder shape groove.
The diameter of the motor is less than the diameter of groove.
It only needs that wing can be controlled in the folding and unfolding of groove by the flexible of hydraulic device one, it will not be again when not in use by machine
Wing exposure, wing would not also occurs and break phenomenon, and wing can be fixed by hydraulic device two and pressing plate, to make
Its flight stability.
Detailed description of the invention
Fig. 1 is that one kind of the present invention can be with the structural schematic diagram of the unmanned plane of stabilized flight；
In figure: 1, fuselage main body, 2, groove, 3, hydraulic device one, 4, motor, 5, flabellum, 6, hydraulic device two, 7, pressing plate.
Specific embodiment
It is right below by attached drawing and embodiment to keep purpose of the present invention technical solution and advantage more clear
The present invention is further elaborated.However, it should be understood that specific embodiment described herein is only used to explain this hair
Range that is bright, being not intended to restrict the invention.
As shown in Figure 1, one kind that the present invention uses can be with the unmanned plane of stabilized flight, including fuselage main body 1, the machine
The upper surface of body main body 1 is equipped with groove 2, is equipped with hydraulic device 1, the hydraulic device 1 inside the bottom surface of the groove 2
It protrudes into one end in groove 2 and is equipped with motor 4, several flabellums 5 are uniformly hingedly equipped on the transmission shaft of the motor 4, it is described
Motor 4 transmission shaft inside be equipped with hydraulic device 26, one end that the hydraulic device 26 stretches out transmission shaft is equipped with pressing plate
7。
The groove 2 is cylinder shape groove.
The diameter of the motor 4 is less than the diameter of groove 2.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modification, equivalent replacement or improvement etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (3)
1. one kind can be with the unmanned plane of stabilized flight, including fuselage main body (1), it is characterised in that: the fuselage main body (1)
Groove (2) are equipped with above, hydraulic device one (3), the hydraulic device one (3) are equipped with inside the bottom surface of the groove (2)
It protrudes into one end in groove (2) and is equipped with motor (4), several flabellums are uniformly hingedly equipped on the transmission shaft of the motor (4)
(5), hydraulic device two (6) is equipped with inside the transmission shaft of the motor (4), the hydraulic device two (6) stretches out transmission shaft
One end be equipped with pressing plate (7).
2. one kind according to claim 1 can be with the unmanned plane of stabilized flight, which is characterized in that the groove (2) is
Cylinder shape groove.
3. one kind according to claim 1 can be with the unmanned plane of stabilized flight, which is characterized in that the motor (4)
Diameter is less than the diameter of groove (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447064.0A CN109552596A (en) | 2018-11-29 | 2018-11-29 | It is a kind of can be with the unmanned plane of stabilized flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447064.0A CN109552596A (en) | 2018-11-29 | 2018-11-29 | It is a kind of can be with the unmanned plane of stabilized flight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109552596A true CN109552596A (en) | 2019-04-02 |
Family
ID=65868102
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811447064.0A Pending CN109552596A (en) | 2018-11-29 | 2018-11-29 | It is a kind of can be with the unmanned plane of stabilized flight |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109552596A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2653383A1 (en) * | 2012-04-18 | 2013-10-23 | EUROCOPTER DEUTSCHLAND GmbH | An airfoil blade of a bearingless rotor of a helicopter |
| CN207129146U (en) * | 2017-06-27 | 2018-03-23 | 汕头市大业塑胶玩具有限公司 | Unmanned plane folding rotor |
| CN207417150U (en) * | 2017-09-19 | 2018-05-29 | 成都云鼎智控科技有限公司 | A kind of foldable propeller of longitudinal register expansion |
| CN108528708A (en) * | 2018-04-12 | 2018-09-14 | 华南智能机器人创新研究院 | A kind of blade and unmanned plane |
| CN207935118U (en) * | 2017-12-29 | 2018-10-02 | 台山市美金电机有限公司 | A kind of intake type Lamp with ceiling fan |
| CN108750085A (en) * | 2018-08-02 | 2018-11-06 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
-
2018
- 2018-11-29 CN CN201811447064.0A patent/CN109552596A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2653383A1 (en) * | 2012-04-18 | 2013-10-23 | EUROCOPTER DEUTSCHLAND GmbH | An airfoil blade of a bearingless rotor of a helicopter |
| CN207129146U (en) * | 2017-06-27 | 2018-03-23 | 汕头市大业塑胶玩具有限公司 | Unmanned plane folding rotor |
| CN207417150U (en) * | 2017-09-19 | 2018-05-29 | 成都云鼎智控科技有限公司 | A kind of foldable propeller of longitudinal register expansion |
| CN207935118U (en) * | 2017-12-29 | 2018-10-02 | 台山市美金电机有限公司 | A kind of intake type Lamp with ceiling fan |
| CN108528708A (en) * | 2018-04-12 | 2018-09-14 | 华南智能机器人创新研究院 | A kind of blade and unmanned plane |
| CN108750085A (en) * | 2018-08-02 | 2018-11-06 | 西安君晖航空科技有限公司 | A kind of attack unmanned plane using Terminal Sensitive Projectile medicine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190402 |
|
| WD01 | Invention patent application deemed withdrawn after publication |