CN109552618A - A kind of unmanned plane emergency back-up flight device - Google Patents
A kind of unmanned plane emergency back-up flight device Download PDFInfo
- Publication number
- CN109552618A CN109552618A CN201811460994.XA CN201811460994A CN109552618A CN 109552618 A CN109552618 A CN 109552618A CN 201811460994 A CN201811460994 A CN 201811460994A CN 109552618 A CN109552618 A CN 109552618A
- Authority
- CN
- China
- Prior art keywords
- wing
- unmanned plane
- motor
- flabellum
- hydraulic device
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Abstract
The present invention discloses a kind of unmanned plane emergency back-up flight device, including fuselage main body, the fuselage main body is equipped with wing, the inner end portion of the wing is equipped with motor one, the transmission shaft of the motor one is equipped with flabellum one, middle is equipped with groove above the wing, and hydraulic device is equipped with inside the bottom surface of the groove, and the other end of the hydraulic device is equipped with aircraft.Advantages of the present invention: when existing flabellum can not move, it is only necessary to motor two be stretched out outside wing by hydraulic device, flabellum two can be carried out using will increase the service life of unmanned plane, reduce use cost, provided convenience to people.
Description
Technical field
The present invention relates to a kind of unmanned plane, specifically a kind of unmanned plane emergency back-up flight device.
Background technique
Unmanned plane can encounter various problem in flight, and all be the retard motion of flabellum in many cases,
In such cases, it will air crash causes entire unmanned plane to damage, and can not reuse, it will increase the use of unmanned plane at
This, and keep user extremely inconvenient.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides a kind of unmanned plane emergency back-up flight devices, existing
When flabellum can not move, it is only necessary to stretch out outside wing motor two by hydraulic device, can be carried out to flabellum two using will increase
The service life for adding unmanned plane, reduces use cost, provides convenience to people.
To achieve the goals above, a kind of unmanned plane emergency back-up flight device that the present invention uses, including fuselage main body, institute
The fuselage main body stated is equipped with wing, and the inner end portion of the wing is equipped with motor one, on the transmission shaft of the motor one
Equipped with flabellum one, middle is equipped with groove above the wing, and hydraulic device is equipped with inside the bottom surface of the groove, described
Hydraulic device the other end be equipped with aircraft.
The aircraft includes the motor two being connected with the hydraulic device other end, is set on the transmission shaft of the motor two
There is flabellum two.
The quantity of the wing is at least 3.
When existing flabellum can not move, it is only necessary to motor two is stretched out outside wing by hydraulic device, it can be to flabellum
Two carry out using will increase the service life of unmanned plane, reduce use cost, provide convenience to people.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
In figure: 1, fuselage main body, 2, wing, 3, motor one, 4, flabellum one, 5, groove, 6, hydraulic device, 7, aircraft, 8, electricity
Machine two, 9, flabellum two.
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, a kind of unmanned plane emergency back-up flight device that the present invention uses, including fuselage main body 1, the machine
Body main body 1 is equipped with wing 2, and the inner end portion of the wing 2 is equipped with motor 1, sets on the transmission shaft of the motor 1
There is flabellum 1, middle is equipped with groove 5 to the wing 2 above, it is equipped with hydraulic device 6 inside the bottom surface of the groove 5,
The other end of the hydraulic device 6 is equipped with aircraft 7.
The aircraft 7 includes the motor 28 being connected with 6 other end of hydraulic device, the transmission shaft of the motor 28
It is equipped with flabellum 29.
The quantity of the wing 2 is at least 3.
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. a kind of unmanned plane emergency back-up flight device, including fuselage main body (1), the fuselage main body (1) is equipped with wing
(2), it is characterised in that: the inner end portion of the wing (2) is equipped with motor one (3), on the transmission shaft of the motor one (3)
Equipped with flabellum one (4), middle is equipped with groove (5) to the wing (2) above, is equipped with inside the bottom surface of the groove (5)
The other end of hydraulic device (6), the hydraulic device (6) is equipped with aircraft (7).
2. a kind of unmanned plane emergency back-up flight device according to claim 1, which is characterized in that the aircraft (7)
Including the motor two (8) being connected with hydraulic device (6) other end, the transmission shaft of the motor two (8) is equipped with flabellum two
(9).
3. a kind of unmanned plane emergency back-up flight device according to claim 1, which is characterized in that the wing (2)
Quantity is at least 3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811460994.XA CN109552618A (en) | 2018-12-01 | 2018-12-01 | A kind of unmanned plane emergency back-up flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811460994.XA CN109552618A (en) | 2018-12-01 | 2018-12-01 | A kind of unmanned plane emergency back-up flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109552618A true CN109552618A (en) | 2019-04-02 |
Family
ID=65868443
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811460994.XA Pending CN109552618A (en) | 2018-12-01 | 2018-12-01 | A kind of unmanned plane emergency back-up flight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109552618A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101535123A (en) * | 2005-11-01 | 2009-09-16 | 城市航空公司 | Roof and floor flows |
| CN101602403A (en) * | 2008-06-12 | 2009-12-16 | 张庆柳 | Vertical take-off and landing aircraft (VTOL aircraft) |
| CN205044949U (en) * | 2015-09-21 | 2016-02-24 | 温州乐享科技信息有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN205499356U (en) * | 2016-01-21 | 2016-08-24 | 何智杰 | Variable flying method unmanned aerial vehicle aircraft |
| CN205707320U (en) * | 2016-03-21 | 2016-11-23 | 柳应泽 | Manned vehicle |
| CN106542085A (en) * | 2015-09-23 | 2017-03-29 | 陈康 | The Electric aircraft of many shrouded propeller retractable wings and fuselage |
| CN206107569U (en) * | 2016-09-26 | 2017-04-19 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle |
| US20180141652A1 (en) * | 2015-05-11 | 2018-05-24 | Christian Roger Rene Deslypper | Convertible airplane with exposable rotors |
| CN108466691A (en) * | 2018-05-31 | 2018-08-31 | 江苏常探机器人有限公司 | The compound rotor aircraft of rear single ducted fan formula of double compound auxiliary wings of ducted fan |
-
2018
- 2018-12-01 CN CN201811460994.XA patent/CN109552618A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101535123A (en) * | 2005-11-01 | 2009-09-16 | 城市航空公司 | Roof and floor flows |
| CN101602403A (en) * | 2008-06-12 | 2009-12-16 | 张庆柳 | Vertical take-off and landing aircraft (VTOL aircraft) |
| US20180141652A1 (en) * | 2015-05-11 | 2018-05-24 | Christian Roger Rene Deslypper | Convertible airplane with exposable rotors |
| CN205044949U (en) * | 2015-09-21 | 2016-02-24 | 温州乐享科技信息有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN106542085A (en) * | 2015-09-23 | 2017-03-29 | 陈康 | The Electric aircraft of many shrouded propeller retractable wings and fuselage |
| CN205499356U (en) * | 2016-01-21 | 2016-08-24 | 何智杰 | Variable flying method unmanned aerial vehicle aircraft |
| CN205707320U (en) * | 2016-03-21 | 2016-11-23 | 柳应泽 | Manned vehicle |
| CN206107569U (en) * | 2016-09-26 | 2017-04-19 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle |
| CN108466691A (en) * | 2018-05-31 | 2018-08-31 | 江苏常探机器人有限公司 | The compound rotor aircraft of rear single ducted fan formula of double compound auxiliary wings of ducted fan |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190402 |