CN205092910U - Photographic lens control structure of remote control flight ware - Google Patents
Photographic lens control structure of remote control flight ware Download PDFInfo
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- CN205092910U CN205092910U CN201520814923.0U CN201520814923U CN205092910U CN 205092910 U CN205092910 U CN 205092910U CN 201520814923 U CN201520814923 U CN 201520814923U CN 205092910 U CN205092910 U CN 205092910U
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- lens
- angle
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Abstract
The utility model discloses a photographic lens control structure of remote control flight ware, angle about the more convenient control of its photographic lens who makes the aircraft, mainly lie in: assemble a turned angle's lens mount but the organism is equipped with the axle bed, the lens mount supplies the equipment camera lens, and in addition, the organism is equipped with the motor, and the pivot of motor is even established and is cranked arm, universal joint, interlock arm, interlock arm reconnection in lens mount. Through foretell structure, can by the control motor just, reversal and the rotatory number of turns, and can control that the camera lens is faced upward, the nutation angle, need not control the flight angle of aircraft to reach and operate efficiency simple and easy, convenient to use.
Description
Technical field
The utility model relates to a kind of remotely-piloted vehicle equipment, particularly relates to a kind of phtographic lens control structure of remotely-piloted vehicle, its make the upper and lower angle of the phtographic lens of aircraft be able to simple and easy, control easily.
Background technology
During the aerophotography of remotely-piloted vehicle, must have that shooting is faced upward, the angle of nutation, level.But the upper and lower camera angle of existing control is all the flight angle that must control aircraft, thin speech it, general camera lens is all installed on body front end, when the angle of wish shooting nutation, must operate the angle of body flight in nutation, shooting face upward, level angle time, also all need to make body be face upward, level angle, but, lower angle flight in operate aircraft, comparatively difficulty, and more easily make shooting effect rock, unstable; In addition, have and be installed on bottom aircraft by phtographic lens, it can only take the angle of overlooking, more difficult shooting level, the angle of facing upward.
Utility model content
The utility model is for improving above-mentioned existing shortcoming, main technical schemes, object are: be provided with the lens mount of angle rotatable in body for assembling camera lens, body is also provided with motor, the rotating shaft of motor be provided with crank arm, coupled arm, universal joint be connected to lens mount, therefore, motor forward and backward and rotating cycle can be controlled, the various angles such as camera lens is faced upward, nutation, level can be controlled, do not need the flight angle controlling aircraft, reach and use simple and easy, convenient, stable effect of photographing.
For achieving the above object, the utility model provides a kind of phtographic lens control structure of remotely-piloted vehicle, and a body is provided with axle bed, and this axle bed has axle center and group establishes a lens mount, this lens mount is for assembling camera lens, in addition, body is provided with motor, and the rotating shaft of motor is provided with cranks arm, and be provided with coupled arm be connected to crank arm, lens mount, by controlling the forward and backward of motor shaft and the anglec of rotation, thus interlock is cranked arm, coupled arm, and then make to control the upper and lower angle of lens mount.
Preferably, this lens mount is provided with universal joint and connects coupled arm one end, and this is cranked arm and is provided with the universal joint connection coupled arm other end.
Accompanying drawing explanation
Fig. 1 is the utility model unitary construction frontal perspective outside drawing;
Fig. 2 is that the utility model separates lens stereo outside drawing;
Fig. 3 is the utility model structure side-looking tilt angle cutaway view;
Fig. 4 is the utility model camera lens is level angle schematic diagram.
Description of reference numerals:
10 bodies
15,23 universal joints
11 axle beds
20 motors
12 lens mounts
21 rotating shafts
13 camera lenses
22 crank arm
14 axle center
24 coupled arms.
Embodiment
Refer to Fig. 1, Fig. 2, Fig. 3, Fig. 4, one body 10 is provided with axle bed 11, this axle bed 11 has axle center 14 and group establishes a lens mount 12, this lens mount 12 is for assembling camera lens 13 and have universal joint 15, in addition, body 10 is provided with motor 20, the rotating shaft 21 of motor 20 is provided with cranks arm 22, this is cranked arm and 22 has another universal joint 23, crank arm 22 universal joint 23 and lens mount 12 universal joint 15 between, be provided with coupled arm 24 and be integrally connected, in addition, this motor 20 servo motor, can control the number of turns that rotating shaft 21 rotates.
By above-mentioned structure, effect of the present utility model, effect, be described in detail as follows at this: referring again to Fig. 3, the rotating shaft 21 controlling motor 20 rotates forward an angle, it is cranked arm 22 can be driven forward coupled arm 24, and makes lens mount 12 in tilt angle, is namely to make camera lens 13 take tilt angle.When for shooting level angle, as shown in Figure 4, control motor 20 rotating shaft 21 and to reverse an angle, it is cranked arm and 22 can in pulling back, and make lens mount 12 in level angle.In like manner, during angle for shooting nutation, motor 20 rotating shaft 21, crank arm 22, coupled arm 24 also can make lens mount 12 in nutation angle; In addition, the utility model also can install the gyroscope of an induction body level angle in body 10, and automatically can respond to the angle of body, automatically makes body keep level angle.
As shown in the above description, the utility model only need control motor 20 rotating shaft 21 forward and backward and rotating cycle, control the upper and lower angle of camera lens 13, do not need the flight angle controlling aircraft body, reach the smoothness of easy to use, simple and easy, easy maintenance lens shooting image, there is splendid practicality and promote effect.
Claims (2)
1. the phtographic lens control structure of a remotely-piloted vehicle, it is characterized in that, a body is provided with axle bed, and this axle bed has axle center and group establishes a lens mount, this lens mount is for assembling camera lens, in addition, body is provided with motor, and the rotating shaft of motor is provided with cranks arm, and be provided with coupled arm be connected to crank arm, lens mount, by controlling the forward and backward of motor shaft and the anglec of rotation, to crank arm with interlock, coupled arm, and then control the upper and lower angle of lens mount.
2. the phtographic lens control structure of remotely-piloted vehicle as claimed in claim 1, is characterized in that, this lens mount is provided with universal joint and connects coupled arm one end, and this is cranked arm and is provided with the universal joint connection coupled arm other end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520814923.0U CN205092910U (en) | 2015-10-20 | 2015-10-20 | Photographic lens control structure of remote control flight ware |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520814923.0U CN205092910U (en) | 2015-10-20 | 2015-10-20 | Photographic lens control structure of remote control flight ware |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205092910U true CN205092910U (en) | 2016-03-16 |
Family
ID=55483559
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520814923.0U Active CN205092910U (en) | 2015-10-20 | 2015-10-20 | Photographic lens control structure of remote control flight ware |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205092910U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113586887A (en) * | 2021-06-23 | 2021-11-02 | 北京航空航天大学 | Device and method for acquiring surface image of inner cavity of solid rocket engine |
-
2015
- 2015-10-20 CN CN201520814923.0U patent/CN205092910U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113586887A (en) * | 2021-06-23 | 2021-11-02 | 北京航空航天大学 | Device and method for acquiring surface image of inner cavity of solid rocket engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |