CN106585970A - Foldable aerial camera - Google Patents
Foldable aerial camera Download PDFInfo
- Publication number
- CN106585970A CN106585970A CN201611218158.1A CN201611218158A CN106585970A CN 106585970 A CN106585970 A CN 106585970A CN 201611218158 A CN201611218158 A CN 201611218158A CN 106585970 A CN106585970 A CN 106585970A
- Authority
- CN
- China
- Prior art keywords
- foldable
- aerial photography
- photography device
- propeller
- fuselage body
- 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.)
- Withdrawn
Links
- 238000013461 design Methods 0.000 claims abstract description 8
- 241000251730 Chondrichthyes Species 0.000 claims description 3
- 230000000007 visual effect Effects 0.000 abstract description 3
- 238000005516 engineering process Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000003592 biomimetic effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 235000001968 nicotinic acid Nutrition 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011664 nicotinic acid Substances 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Classifications
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- 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
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C27/50—Blades foldable to facilitate stowage of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention discloses a foldable aerial camera. The foldable aerial camera comprises a camera body. Four shaft rods arranged in two-to-two symmetry with the longitudinal center axis of the camera body as the center are connected to the camera body. A rotary foldable shaft arm is connected to each shaft rod, wherein a propeller is connected to one end of the rotary foldable shaft arm, and a driving motor is connected to the propeller. A tripod head is connected to the camera body along the longitudinal center axis of the camera body through a connection rod. A high-speed camera is connected to the lower portion of the tripod head. Compared with the prior art, the foldable aerial camera completes folding through the multiple symmetrically arranged rotary foldable shaft arms and propeller structures in a rotary shaft rotation mode, the space size of the aerial camera is reduced, carrying is more convenient, style design is ingenious and beautiful, visual experience is good, and market prospects are broad.
Description
Technical field
The present invention relates to unmanned aerial photography equipment technical field, more particularly to a kind of foldable aerial photography device.
Background technology
At present, unmanned plane mainly has five key technologies such as housing construction designing technique, organism material technology, flight control
Technology, radio communication telecontrol engineering and wireless image passback technology, becomes and modernizes the development of intelligent unmanned machine and improve
Focal point.However, in terms of the housing construction of unmanned aerial photography device, armshaft mostly is fixed form, the form that extends out of multiaxis makes
Many unmanned aerial photography devices are not convenient enough when carrying, moulding is not attractive in appearance enough, to using bringing inconvenience.
The content of the invention
It is an object of the present invention to be directed to the above-mentioned deficiency of prior art, there is provided a kind of foldable aerial photography device, utilize
Accommodation space is saved after rotating shaft rotary type folding, shape-designing is unique, and easy to carry, market prospect is good.
The technical scheme that adopted to reach above-mentioned purpose of the present invention is：
A kind of foldable aerial photography device, including fuselage body, the fuselage body is connected with vertical with the fuselage body
To centered on central axis in symmetrically arranged four axostylus axostyles two-by-two, rotatable folding armshaft, institute are connected with each axostylus axostyle
The one end for stating rotatable folding armshaft is connected with propeller, and the propeller is connected with motor, the fuselage body edge
Fuselage body longitudinal center axis is connected with head by a connecting rod, and below the head high-speed camera is connected with.
Preferably, described rotatable folding armshaft may be folded in the underface of the fuselage body, described propeller
May be folded in the outside of the rotatable folding armshaft.
Preferably, one end of described rotatable folding armshaft is by the described axostylus axostyle of spacing wheel shaft connection.
Preferably, the axle center bottom of described spacing wheel shaft is connected with fin type leg.
Preferably, described propeller is connected with hub by two blades and is formed, and described two blades are in 180 ° during expansion
Arrange, described two blades are in 30 ° or 45 ° settings during folding.
Preferably, described fuselage body is using the shark profile of biomimetic features principle design.
Preferably, described high-speed camera connects the head by a frame.
Preferably, described frame is to coordinate to form after three L-type support head and the tail connect；The section of described head is in just
Square setting.
Preferably, the upper surface of described fuselage body is provided with function button.
Compared with prior art, the foldable aerial photography device that the present invention is provided, by symmetrically arranged multiple rotatable
Armshaft and propeller arrangement are folded, completes to fold using rotating shaft rotation mode, reduce the space size of aerial photography device, be beneficial to receive
Receive, carry convenient, and design ingenious in moulding, using the moulding of bionics and aerodynamic principle to aerial photography device
Bionic Design and airflow design have been done, it is more attractive in appearance, give user a kind of brand-new visual experience, wide market.
Above-mentioned is the general introduction of inventive technique scheme, below in conjunction with accompanying drawing and specific embodiment, the present invention is done further
Explanation.
Description of the drawings
Fig. 1 is the overall structure diagram after the folding of the present invention；
Fig. 2 is another overall structure diagram after the folding of the present invention；
Fig. 3 is the overall structure diagram after the expansion of the present invention；
Fig. 4 is another overall structure diagram after the expansion of the present invention.
Specific embodiment：
In order that the purpose of the present invention and technical scheme and advantage become more apparent, make with reference to embodiments specifically
It is bright.It should be appreciated that specific embodiment described herein is not intended to limit the present invention only to explain the present invention.
The foldable aerial photography device that the present embodiment is provided, with reference to Fig. 1-4, including fuselage body 1, fuselage body is connected with
In symmetrically arranged four axostylus axostyles 2 two-by-two centered on fuselage body longitudinal center axis, being connected with each axostylus axostyle to revolve
The folded armshaft 3 of turnover, the one end of rotatable folding armshaft is connected with propeller 4, and propeller is connected with motor, motor
In a cylindrical shell 13, fuselage body 1 is connected with head 6, head along fuselage body longitudinal center axis by a connecting rod 5
Lower section be connected with high-speed camera 7.Head is used to fixing and stablizing high-speed camera, and high-speed camera is located at fuselage body
The middle part of lower section, shoots convenient, and coverage is wide.
Further, rotatable folding armshaft 3 may be folded in the underface of the fuselage body, and propeller 4 may be folded in can
The outside of rotary folding armshaft, four rotatable folding armshafts are divided into the two lower section sides for being mounted on fuselage body, and the two of per group
In stacked on top of one another, rotatable folding armshaft and propeller are folded to fuselage to individual rotatable folding armshaft by rotating shaft rotation mode
The lower section of body, and the blade of propeller is also folded to fuselage body lower section, saves space, has reached more preferable storage effect
Really, solve user and carry inconvenient puzzlement.One end of rotatable folding armshaft 3 connects described axle by spacing wheel shaft 8
Bar, the axle center bottom of spacing wheel shaft is connected with fin type leg 9, can play support fuselage, stable and anti-skidding effect, spiral shell
Rotation oar is connected with hub 11 by two blades 10 and is formed, and described two blades are described two during folding in 180 ° of settings during expansion
Blade can also be other rational angles certainly in 30 ° or 45 ° settings.
Further, fuselage body 1 is, using the shark profile of biomimetic features principle design, to be set using bionics principle
Meter, it is handsome in appearance, and aerodynamic is combined, and airflow design has been done to appearance and modeling, cleanliness is good, can be a kind of complete to user
New visual experience.High-speed camera 7 connects the head by a frame 12, and frame 12 is that three L-type support head and the tail connect
Coordinate afterwards and form, the square setting in section of head, being equipped with for frame and head is beneficial to the steady of camera structure
Fixed, the upper surface of fuselage body is provided with function button 14, such as switch key, remote control direction key.
The announcement and teaching of book according to the above description, those skilled in the art in the invention can also be to above-mentioned embodiment party
Formula is changed and changed.Therefore, specific embodiment disclosed and described above is the invention is not limited in, to invention
A little modifications and changes should also be as falling in the scope of the claims of the present invention.
Claims (9)
1. a kind of foldable aerial photography device, it is characterised in that including fuselage body, the fuselage body is connected with the machine
In symmetrically arranged four axostylus axostyles two-by-two centered on body body longitudinal center axis, on each axostylus axostyle rotatable folding is connected with
Armshaft, the one end of the rotatable folding armshaft is connected with propeller, and the propeller is connected with motor, the fuselage
Body is connected with head along fuselage body longitudinal center axis by a connecting rod, and below the head high-speed camera is connected with
Machine.
2. foldable aerial photography device as claimed in claim 1, it is characterised in that described rotatable folding armshaft is foldable
In the underface of the fuselage body, described propeller may be folded in the outside of the rotatable folding armshaft.
3. foldable aerial photography device as claimed in claim 1, it is characterised in that one end of described rotatable folding armshaft
By the described axostylus axostyle of spacing wheel shaft connection.
4. foldable aerial photography device as claimed in claim 3, it is characterised in that the axle center bottom of described spacing wheel shaft connects
It is connected to fin type leg.
5. foldable aerial photography device as claimed in claim 1, it is characterised in that described propeller is by two blades and hub
It is connected and forms, in 180 ° of settings, described two blades is in 30 ° or 45 ° settings during folding for described two blades during expansion.
6. foldable aerial photography device as claimed in claim 1, it is characterised in that described fuselage body is using bionical knot
The shark profile of structure principle design.
7. foldable aerial photography device as claimed in claim 1, it is characterised in that described high-speed camera passes through a frame
Connect the head.
8. foldable aerial photography device as claimed in claim 7, it is characterised in that described frame is three L-type supports head
WEILIAN coordinates after connecing and forms；The square setting in section of described head.
9. foldable aerial photography device as claimed in claim 1, it is characterised in that the upper surface of described fuselage body is arranged
Functional button.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611218158.1A CN106585970A (en) | 2016-12-26 | 2016-12-26 | Foldable aerial camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611218158.1A CN106585970A (en) | 2016-12-26 | 2016-12-26 | Foldable aerial camera |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106585970A true CN106585970A (en) | 2017-04-26 |
Family
ID=58604258
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611218158.1A Withdrawn CN106585970A (en) | 2016-12-26 | 2016-12-26 | Foldable aerial camera |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106585970A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110118A (en) * | 2017-06-23 | 2019-01-01 | 昊翔电能运动科技(昆山)有限公司 | Unmanned plane and its frame assembly |
| WO2019041876A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市道通智能航空技术有限公司 | Foldable frame and unmanned aerial vehicle |
| CN110877726A (en) * | 2019-11-12 | 2020-03-13 | 徐州迪沃通讯工程有限公司 | Foldable unmanned aerial vehicle |
| CN112793771A (en) * | 2021-02-03 | 2021-05-14 | 南京安元科技有限公司 | Collapsible unmanned aerial vehicle of fuselage |
-
2016
- 2016-12-26 CN CN201611218158.1A patent/CN106585970A/en not_active Withdrawn
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110118A (en) * | 2017-06-23 | 2019-01-01 | 昊翔电能运动科技(昆山)有限公司 | Unmanned plane and its frame assembly |
| WO2019041876A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市道通智能航空技术有限公司 | Foldable frame and unmanned aerial vehicle |
| CN110877726A (en) * | 2019-11-12 | 2020-03-13 | 徐州迪沃通讯工程有限公司 | Foldable unmanned aerial vehicle |
| CN112793771A (en) * | 2021-02-03 | 2021-05-14 | 南京安元科技有限公司 | Collapsible unmanned aerial vehicle of fuselage |
| CN112793771B (en) * | 2021-02-03 | 2022-05-13 | 南京安元科技有限公司 | Collapsible unmanned aerial vehicle of fuselage |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170426 |
|
| WW01 | Invention patent application withdrawn after publication |