CN104691750B - A kind of can be used for photographic aviation device waterborne and aerial photographing - Google Patents
A kind of can be used for photographic aviation device waterborne and aerial photographing Download PDFInfo
- Publication number
- CN104691750B CN104691750B CN201510100296.9A CN201510100296A CN104691750B CN 104691750 B CN104691750 B CN 104691750B CN 201510100296 A CN201510100296 A CN 201510100296A CN 104691750 B CN104691750 B CN 104691750B
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- Prior art keywords
- aircraft
- motor
- lower floor
- controller
- upper strata
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- 229910000831 Steel Inorganic materials 0.000 claims description 19
- 239000010959 steel Substances 0.000 claims description 19
- 238000009434 installation Methods 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 23
- 230000002159 abnormal effect Effects 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 3
- 238000003306 harvesting Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 208000033999 Device damage Diseases 0.000 description 1
- 206010044565 Tremor Diseases 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
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- Accessories Of Cameras (AREA)
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Abstract
A kind of can be used for photographic aviation device waterborne and aerial photographing，Including charging hole、Axle sleeve、First camera、First motor、Support、Screw、Anti-collision ring、Oar rudder、Controller、Battery、Parking leg、Aircraft lower floor and aircraft upper strata，First camera is on axle sleeve，Axle sleeve lower end is hinged on aircraft upper strata，Axle sleeve right-hand member is on the output shaft of the first motor，First motor is on support，Support is on aircraft upper strata，Charging hole is arranged on aircraft upper strata，Screw is respectively installed at aircraft upper strata or so two ends，Screw is externally provided with anti-collision ring，Aircraft upper strata is in aircraft lower floor，Oar rudder is arranged on aircraft lower floor，Aircraft lower interior part installs battery and controller，Battery is connected with controller by wire，Controller is connected with the first motor and screw respectively by wire，Aircraft lower floor is on parking leg.
Description
Technical field
The present invention relates to a kind of can be used for photographic aviation device waterborne and aerial photographing, belong to vehicle technology field.
Background technology
Now, with the continuous development of society, the continuous lifting of people's quality of life, people will be by right to the pursuit that lives
The pursuit of aspect of material has been increasingly turned to the pursuit to spirit level, and it is essential in people's life to photograph, and photographic equipment exists
Also must not or lack in people's life, and easy loss device when the aircraft used on water surface top of prior art shoots, or
Cause device damage.In order to solve above-mentioned difficulties, need to develop a photographic aviation with surface propeller and anti-settling facility
Device.
Content of the invention
It is an object of the invention to provide a kind of can be used for photographic aviation device waterborne and aerial photographing.
The problem to be solved in the present invention is easy loss device when being shot using the aircraft of prior art, or causes equipment
The problem of damage.
For realizing the purpose of the present invention, the technical solution used in the present invention is：
A kind of can be used for photographic aviation device waterborne and aerial photographing, including charging hole, axle sleeve, the first camera, first
Motor, support, screw, anti-collision ring, oar rudder, controller, battery, parking leg, aircraft lower floor and aircraft upper strata, institute
The first camera is stated on axle sleeve, axle sleeve lower end is hinged on aircraft upper strata, axle sleeve right-hand member is defeated installed in the first motor
On shaft, on support, on aircraft upper strata, charging hole is arranged on aircraft upper strata to support to the first motor, flies
Screw is respectively installed at row device upper strata or so two ends, and screw is externally provided with anti-collision ring, and aircraft upper strata is arranged in aircraft lower floor,
Oar rudder is arranged on aircraft lower floor, and aircraft lower interior part installs battery and controller, and battery is by wire and controller
It is connected, controller is connected with the first motor and screw respectively by wire, aircraft lower floor is on parking leg.
The aircraft lower floor is separable on parking leg.
The remote control includes antenna, control stick and control button, and antenna is arranged on remote control front end, antenna and controller
Signal is connected, and remote control face is provided with more than one control stick and control button.
The charging hole is configured with watertight rubber stopper, stoppers charging hole after being available in charging complete, makes charging hole reach water
Close state.
The aircraft lower floor is in Ship Structure.
The aircraft lower level floor installs the second motor, and six contiguous blocks are connected by two springs each other, position
Aircraft lower level floor is hinged in first contiguous block top on the left side, through hole in contiguous block, is offered, steel wire left end winds
On the output shaft of the second motor, steel wire right-hand member is arranged on the right-hand member of steel wire through the through hole of five contiguous blocks, the 3rd motor, the
On the output shaft of the 3rd motor, controller is connected with the second motor and the 3rd motor respectively two cameras by wire.
It is an advantage of the invention that：The navigation of the aircraft can be controlled using the aircraft when being shot by remote control
And operation；Controller is adjusted by remote control to control the forward or reverse of the first motor, axle sleeve forward or reverse is made, drive
First camera leans forward or swings back, prevent the aircraft from when navigating by water in water, causing the first camera elevation angle excessive because of turning or
Too small and cause shooting abnormal；By the startup of remote control adjustable screw oar, screw provides power for the aircraft, flies this
Row device can be navigated by water on the water surface；Anti-collision ring, prevents aircraft from encountering barrier in flight course and damages screw；Oar rudder
Offer power is navigated by water in water for the aircraft and provide steering moment when turning in water；Charging hole is configured with watertight rubber
Plug, stoppers charging hole, makes charging hole reach watertight state after being available in charging complete；Parking leg has been used in the aircraft
The support of aircraft is put in harvesting afterwards, prevents the aircraft using making which be damaged because placing unstable after complete；Controller
Control the second motor forward or reverse, loosen steel wire, so that steel wire right-hand member is moved down with the contiguous block for being located at right, make the
Two cameras are moved down with steel wire；Controller controls the 3rd motor forward or reverse, adjusts the shooting of second camera
Angle.
Description of the drawings
Fig. 1 is that the present invention is a kind of can be used for photographic aviation device overall structure figure waterborne and aerial photographing；
Fig. 2 is the structural representation of remote control；
Fig. 3 is a portion structure enlarged diagram；
In figure：1st, charging hole 2, axle sleeve 3, the first camera 4, the first motor 5, support 6, screw 7,
Anti-collision ring 8, oar rudder 9, controller 10, battery 11, parking leg 12, in aircraft lower floor 13, aircraft
Layer 14, remote control 15, antenna 16, control stick 17, control button 18, the second motor 19, contiguous block 20, logical
Hole 21, spring 22, the 3rd motor 23, second camera 24, steel wire.
Specific embodiment
Below in conjunction with the accompanying drawings and embodiment the present invention is further illustrated.
The present invention is a kind of to can be used for photographic aviation device waterborne and aerial photographing, images including charging hole 1, axle sleeve 2, first
The 3, first motor 4, support 5, screw 6, anti-collision ring 7, oar rudder 8, controller 9, battery 10, parking leg 11, aircraft
Lower floor 12 and aircraft upper strata 13, on axle sleeve 2,2 lower end of axle sleeve is hinged on aircraft upper strata to first camera 3
13, on the output shaft of the first motor 4, on support 5, support 5 is installed in flight for the first motor 4 for 2 right-hand member of axle sleeve
On device upper strata 13, controller 9 is adjusted controlling the forward or reverse of the first motor 4 by remote control 14, rotate forward axle sleeve 2 or
Reversion, drives the first camera 3 to lean forward or swing back, prevents the aircraft from causing the first camera because of turning when navigating by water in water
3 elevations angle are excessive or too small and cause shooting abnormal；Charging hole 1 is arranged on aircraft upper strata 13, and charging hole 1 is configured with watertight rubber
Plug, stoppers charging hole 1, makes charging hole 1 reach watertight state after being available in charging complete；13 or so two ends of aircraft upper strata are respectively pacified
Dress screw 6, screw 6 are externally provided with anti-collision ring 7, and by the startup of 14 adjustable screw oar 6 of remote control, screw 6 is the flight
Device provides power, so that the aircraft is navigated by water on the water surface, and anti-collision ring 7 prevents aircraft from encountering barrier in flight course
And damage screw 6；In aircraft lower floor 12, aircraft lower floor 12 is in Ship Structure on aircraft upper strata 13；Oar rudder 8 is pacified
Aircraft lower floor 12 is mounted in, and oar rudder 8 navigates by water offer power in water for the aircraft and steering moment provided when turning in water；
Aircraft lower floor 12 is internal to install battery 10 and controller 9, and controller 9 is to change main circuit or control electricity according to predefined procedure
The wiring on road and change resistance value in circuit to control the startup of motor, speed governing, braking and reverse main make device, battery
10 are connected with controller 9 by wire, and controller 9 is connected with the first motor 4 and screw 6 respectively by wire, under aircraft
On the parking leg 11, aircraft lower floor 12 is separable on parking leg 11 for layer 12, parking leg 11 be
The aircraft puts the support of aircraft using harvesting after complete, prevents the aircraft using receiving which because placing unstable after complete
To damage；Remote control 14 includes antenna 15, control stick 16 and control button 17, and antenna 15 is arranged on 14 front end of remote control, antenna
15 are connected with 9 signal of controller, and 14 surface of remote control is provided with more than one control stick 16 and control button 17, using the aircraft
Navigation and the operation of the aircraft can be controlled when being shot by remote control 14；The second electricity is installed in 12 bottom of aircraft lower floor
Machine 18, six contiguous blocks 19 are connected by two springs 21 each other, and first 19 top of contiguous block positioned at the left side is hinged
Through hole 20 is offered in 12 bottom of aircraft lower floor, contiguous block 19,24 left end of steel wire is wrapped in the output shaft of the second motor 18
On, 24 right-hand member of steel wire controls 18 forward or reverse of the second motor, makes steel wire 24 through the through hole 20 of five contiguous blocks 19, controller
Loosen, so that 24 right-hand member of steel wire is moved down with the contiguous block 19 for being located at right, make second camera 23 downward with steel wire 24
Mobile；3rd motor 22 controls on the output shaft of the 3rd motor 22 installed in the right-hand member of steel wire 24, second camera 23
Device is connected with the second motor 18 and the 3rd motor 22 respectively by wire, and controller controls 22 forward or reverse of the 3rd motor, is come
Adjust the shooting angle of second camera 23.
Using method of the present invention：The boat of the aircraft can be controlled using the aircraft when being shot by remote control 14
Row and operation；Controller 9 is adjusted controlling the forward or reverse of the first motor 4 by remote control 14, rotates forward axle sleeve 2 or instead
Turn, drive the first camera 3 to lean forward or swing back, prevent the aircraft from when navigating by water in water, causing the first camera 3 because of turning
The elevation angle is excessive or too small and cause shooting abnormal；By the startup of 14 adjustable screw oar 6 of remote control, screw 6 is the aircraft
Power is provided, so that the aircraft is navigated by water on the water surface；Anti-collision ring 7 prevent aircraft from encountering barrier in flight course and
Damage screw 6；Oar rudder 8 navigates by water offer power in water for the aircraft and provides steering moment when turning in water；Charge
Hole 1 is configured with watertight rubber stopper, stoppers charging hole 1 after being available in charging complete, makes charging hole 1 reach watertight state；Park and prop up
Frame 11 is the support for putting aircraft in the aircraft using harvesting after complete, prevents the aircraft because placing shakiness after use
And so which is damaged；Controller controls 18 forward or reverse of the second motor, loosens steel wire 24, makes 24 right-hand member of steel wire with position
Move down in the contiguous block 19 of right, so that second camera 23 is moved down with steel wire 24；Controller controls the 3rd motor
22 forward or reverse, adjust the shooting angle of second camera 23.
Claims (4)
1. a kind of can be used for photographic aviation device waterborne and aerial photographing, including charging hole（1）, axle sleeve（2）, the first camera
（3）, the first motor（4）, support（5）, screw（6）, anti-collision ring（7）, oar rudder（8）, controller（9）, battery（10）, park
Support（11）, aircraft lower floor（12）With aircraft upper strata（13）, it is characterized in that：First camera（3）Installed in axle sleeve
（2）On, axle sleeve（2）Lower end is hinged on aircraft upper strata（13）, axle sleeve（2）Right-hand member is arranged on the first motor（4）Output shaft on,
First motor（4）Installed in support（5）On, support（5）Installed in aircraft upper strata（13）On, charging hole（1）Installed in flight
Device upper strata（13）, aircraft upper strata（13）Screw is respectively installed at left and right two ends（6）, screw（6）It is externally provided with anti-collision ring（7）, fly
Row device upper strata（13）Installed in aircraft lower floor（12）On, oar rudder（8）Installed in aircraft lower floor（12）, aircraft lower floor（12）
Internal installation battery（10）And controller（9）, battery（10）By wire and controller（9）It is connected, controller（9）Pass through
Wire respectively with the first motor（4）And screw（6）It is connected, aircraft lower floor（12）Installed in parking leg（11）On, charge
Hole（1）Watertight rubber stopper is configured with, after being available in charging complete, stoppers charging hole（1）, make charging hole（1）Reach watertight state,
Aircraft lower floor（12）In Ship Structure.
2. according to claim 1 a kind of can be used for photographic aviation device waterborne and aerial photographing, it is characterized in that：Described winged
Hang Qi lower floor（12）Separable installed in parking leg（11）On.
3. according to claim 2 a kind of can be used for photographic aviation device waterborne and aerial photographing, it is characterized in that：The control
Device processed（9）With remote control（14）Signal is connected, remote control（14）Including antenna（15）, control stick（16）And control button（17）,
Antenna（15）Installed in remote control（14）Front end, antenna（15）With controller（9）Signal is connected, remote control（14）Surface is provided with not
An only control stick（16）And control button（17）.
4. according to claim 1 a kind of can be used for photographic aviation device waterborne and aerial photographing, it is characterized in that：Described winged
Hang Qi lower floor（12）The second motor is installed in bottom（18）, six contiguous blocks（19）Pass through two springs each other（21）It is connected,
First contiguous block positioned at the left side（19）Top is hinged on aircraft lower floor（12）Bottom, contiguous block（19）Through hole is inside offered
（20）, steel wire（24）Left end is wrapped in the second motor（18）Output shaft on, steel wire（24）Right-hand member passes through six contiguous blocks（19）
Through hole（20）, the 3rd motor（22）Installed in steel wire（24）Right-hand member, second camera（23）Installed in the 3rd motor（22）
Output shaft on, controller by wire respectively with the second motor（18）With the 3rd motor（22）It is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510100296.9A CN104691750B (en) | 2015-03-09 | 2015-03-09 | A kind of can be used for photographic aviation device waterborne and aerial photographing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510100296.9A CN104691750B (en) | 2015-03-09 | 2015-03-09 | A kind of can be used for photographic aviation device waterborne and aerial photographing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104691750A CN104691750A (en) | 2015-06-10 |
| CN104691750B true CN104691750B (en) | 2017-03-08 |
Family
ID=53339389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510100296.9A Expired - Fee Related CN104691750B (en) | 2015-03-09 | 2015-03-09 | A kind of can be used for photographic aviation device waterborne and aerial photographing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104691750B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428534A (en) * | 2016-09-19 | 2017-02-22 | 浙江鸣远科技发展有限公司 | Landing gear device of unmanned aerial vehicle and unmanned aerial vehicle using same |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101495365A (en) * | 2005-11-09 | 2009-07-29 | 贝尔直升机泰克斯特龙公司 | Crash attenuation system for aircraft |
| CN103837322A (en) * | 2013-11-18 | 2014-06-04 | 中国特种飞行器研究所 | Hydrodynamic performance testing method of water surface aircraft |
| CN104097767A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Four-rotor aircraft |
| CN204822067U (en) * | 2015-03-09 | 2015-12-02 | 浙江海洋学院 | Photographic aviation ware that can be used to on water and aerial shooting |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8646720B2 (en) * | 2010-05-10 | 2014-02-11 | Donald Orval Shaw | Modular flight vehicle with wings |
| WO2014080386A2 (en) * | 2014-03-25 | 2014-05-30 | Alshdaifat, Wasfi | Drone service aero-carrier |
-
2015
- 2015-03-09 CN CN201510100296.9A patent/CN104691750B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101495365A (en) * | 2005-11-09 | 2009-07-29 | 贝尔直升机泰克斯特龙公司 | Crash attenuation system for aircraft |
| CN103837322A (en) * | 2013-11-18 | 2014-06-04 | 中国特种飞行器研究所 | Hydrodynamic performance testing method of water surface aircraft |
| CN104097767A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Four-rotor aircraft |
| CN204822067U (en) * | 2015-03-09 | 2015-12-02 | 浙江海洋学院 | Photographic aviation ware that can be used to on water and aerial shooting |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104691750A (en) | 2015-06-10 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| 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: 20170308 Termination date: 20180309 |