CN210852968U

CN210852968U - Rotary single-lens oblique photographing mechanism for aircraft

Info

Publication number: CN210852968U
Application number: CN201921763870.9U
Authority: CN
Inventors: 田志; 田凯; 王翊赫; 李智宝; 孔令凱
Original assignee: Tianjin Hanyu Haode Technology Development Co ltd
Current assignee: Tianjin Hanyu Haode Technology Development Co ltd
Priority date: 2019-10-18
Filing date: 2019-10-18
Publication date: 2020-06-26
Anticipated expiration: 2029-10-18

Abstract

The utility model discloses a rotation type single-lens oblique photography mechanism for airborne vehicle, including the mounting disc, through the first frame of bolt fixedly connected with between the left front and back both sides of mounting disc bottom, and the inside fixedly connected with camera of first frame, the equal fixedly connected with second frame in both sides around the mounting disc bottom right side, the equal fixedly connected with X type frame in bottom of two second frames, the utility model relates to a photographic mechanism technical field. This a rotation type single lens tilt photography mechanism for airborne vehicle, through setting up a mirror, and adjust it to different angles, can realize the regulation to camera shooting angle, only need use a picture frame of a camera cooperation and mirror can satisfy the preceding below, under and the shooting demand of the three angle in rear below, holistic weight has not only been reduced, and the space has been reduced, can guarantee picture frame and mirror pivoted steady simultaneously, the shake problem has been reduced, it is more clear to make the picture of shooing.

Description

Rotary single-lens oblique photographing mechanism for aircraft

Technical Field

The utility model relates to a photographic mechanism technical field specifically is a rotation type single-lens oblique photography mechanism for airborne vehicle.

Background

An aircraft refers to an aircraft capable of controlled flight in the atmosphere. Any aircraft must generate lift greater than its own weight in order to be able to ascend into the air. Aircraft can be divided into two main categories according to the principle of generating lift: lighter-than-air aircraft and heavier-than-air aircraft. The former is lifted off by air static buoyancy; the latter is lifted off against its own weight by aerodynamic force. Aircraft is a large category of aircraft, and refers to any machine that achieves aerodynamic lift-off flight through the relative movement of the fuselage and air (not the reaction of the air against the ground). Including balloons, airships, airplanes, gliders, gyroplanes, helicopters, ornithopters, tiltrotors, etc.

The oblique photography automatic modeling technology is a high and new technology which is rapidly developed in the field of international remote sensing and surveying and mapping in recent years. At present, a plurality of surveying and mapping units and related enterprises at home and abroad widely adopt the technology to produce three-dimensional model data, and gradually replace the traditional manual modeling, so that the technology becomes an important mode for producing a new three-dimensional model. The large-scene live-action three-dimensional model based on the oblique images can provide richer geographic information for users, is more friendly to user experience, and is widely popular at home and abroad. However, this technique is slow in development and difficult to popularize, and is mainly limited by an imaging device for acquiring an oblique image.

In the prior art, as the rotary single-lens oblique photographing device for the aircraft disclosed in CN 107367886 a, a rotary turntable is arranged to drive three reflectors thereon to sequentially rotate to the front side of a camera, and different reflection angles are used to shoot different angles, but a rack is used to connect the three reflectors to the rotary turntable, so that the occupied space is large, the problem of unstable gravity center is easy to occur, and a lot of weight can be increased.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a not enough to prior art, the utility model provides a rotation type single-lens tilt photography mechanism for airborne vehicle has solved and has used the frame to be connected to the rotatory carousel with three reflector, and the space that occupies is great, appears the unstable problem of focus easily, and also can increase the problem of not few weight.

(II) technical scheme

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a rotary single-lens oblique photographing mechanism for an aircraft comprises a mounting disc, wherein a first frame is fixedly connected between the front side and the rear side of the left side of the bottom of the mounting disc through bolts, a camera is fixedly connected in the first frame, second frames are fixedly connected on the front side and the rear side of the right side of the bottom of the mounting disc, X-shaped frames are fixedly connected at the bottoms of the two second frames, a picture frame is rotatably connected between the two X-shaped frames, and the left side inside the mirror frame is fixedly connected with a reflective mirror, the two second machine frames are rotatably connected with a push type screw motor positioned at the upper right corner of the mirror frame, the outer surface of the left end of the output shaft of the propulsion screw motor is sleeved with a fixed sleeve, the outer part of the fixed sleeve is sleeved with a rotating sleeve, and the front side and the rear side of the rotating sleeve are fixedly connected with connecting sleeves, and the right side of the mirror frame is fixedly connected with hinge seats in a rotating way with the connecting sleeves.

Preferably, the centers of the front side and the rear side of the mirror frame are fixedly connected with a central rotating shaft, and the surfaces of the two central rotating shafts are rotatably connected with the inner side of the X-shaped frame through bearings.

Preferably, the middle of the front side and the middle of the rear side of the propulsion screw motor are fixedly connected with long shafts, and one ends, far away from the propulsion screw motor, of the long shafts are rotatably connected with the inner side of the second rack through bearings.

Preferably, the upper side and the lower side of one side, opposite to the X-shaped frame, of each X-shaped frame are fixedly connected with arc-shaped limiting frames, and arc-shaped sliding grooves are formed in the opposite side of each arc-shaped limiting frame.

Preferably, the front side and the rear side of the spectacle frame are fixedly connected with short shafts inside the arc-shaped sliding grooves, and the surfaces of the short shafts are in sliding connection with the inner surfaces of the arc-shaped sliding grooves.

Preferably, the center of the mounting disc is fixedly connected with a rotating column, and the top end of the rotating column is fixedly connected with a coupler.

Preferably, the outer circumference of the mounting disc is provided with six U-shaped frames, the six U-shaped frames are arranged at equal intervals, and the upper half part of each U-shaped frame is fixedly connected with the aircraft frame.

Preferably, the bottom of the inner surface of the U-shaped frame is rotatably connected with steel balls, and the periphery of the bottom of the mounting disc is provided with an annular groove matched with the steel balls.

Preferably, the process of the propulsion screw motor is provided with three gear positions corresponding to three rotation positions of the lens frame, and the included angles between the three rotation positions of the lens frame and the horizontal plane are 67.5 degrees, 45 degrees and 22.5 degrees respectively.

(III) advantageous effects

The utility model provides a rotation type single-lens oblique photography mechanism for airborne vehicle. Compared with the prior art, the method has the following beneficial effects:

(1) the rotary single-lens oblique photography mechanism for the aircraft is characterized in that a first frame is fixedly connected between the front side and the rear side of the left side of the bottom of an installation disc through bolts, a camera is fixedly connected inside the first frame, second frames are fixedly connected to the front side and the rear side of the right side of the bottom of the installation disc, X-shaped frames are fixedly connected to the bottoms of the two second frames, a picture frame is rotatably connected between the two X-shaped frames, a reflective mirror is fixedly connected to the left side inside the picture frame, a push-type screw motor is rotatably connected to the two second frames and positioned at the upper right corner of the picture frame, a fixing sleeve is sleeved on the outer surface of the left end of an output shaft of the push-type screw motor, a rotating sleeve is sleeved on the outer portion of the fixing sleeve, connecting sleeves are fixedly connected to the front side and the rear, and adjust it to different angles, can realize the regulation to camera shooting angle, only need use a camera cooperation picture frame and reflector can satisfy the shooting demand of three angle in front below, under and back below, not only reduced holistic weight, and reduced the space, can guarantee picture frame and reflector pivoted steady simultaneously, reduced the shake problem, make the picture of shooing more clear.

(2) The rotary single-lens oblique photographing mechanism for the aircraft is characterized in that a rotating column is fixedly connected to the center of a mounting disc, a coupler is fixedly connected to the top end of the rotating column, a U-shaped frame is arranged on the outer circumference of the mounting disc, six U-shaped frames are equidistantly arranged, the upper half part of each U-shaped frame is fixedly connected with a rack of the aircraft, steel balls are rotatably connected to the bottom of the inner surface of each U-shaped frame, annular grooves matched with the steel balls are formed in the periphery of the bottom of the mounting disc, the rotating columns are connected with an upper stepping motor shaft through couplers and used for controlling the mounting disc and a lower structure of the mounting disc to rotate for 90 degrees, shooting on the lower left and the lower right is realized, the mounting disc is supported by the six U-shaped frames, the mounting disc can be more stable during rotation and shooting, the burden of the motor shaft can be reduced, and, and set up the steel ball between U type frame and mounting disc, can make the mounting disc pivoted more smooth and easy, and reduced wearing and tearing.

(3) This a rotation type single lens tilt photography mechanism for airborne vehicle is equipped with the three rotation position that three gear corresponds the picture frame through the process with impulse type screw motor, and the three rotation position of picture frame is 67.5 °, 45 and 22.5 respectively with the contained angle of horizontal plane, utilizes impulse type screw motor as the driving force, cooperates the control of corresponding procedure, but the turned angle of accurate control reflector, makes the operation simpler, and the shooting angle is more accurate.

Drawings

FIG. 1 is a front view of the overall structure of the present invention;

FIG. 2 is a schematic structural view of the frame and the arc-shaped spacing frame of the present invention;

FIG. 3 is an enlarged view of a portion of the substrate of FIG. 2;

FIG. 4 is a schematic view of the structure of the mirror frame and the reflective mirror of the present invention;

fig. 5 is a bottom view of the mounting plate structure of the present invention;

FIG. 6 is a sectional view of a partial structure of the present invention;

fig. 7 is a schematic view of the reflective mirror reflecting light at three angles.

In the figure, 1-a mounting disc, 2-a first frame, 3-a camera, 4-a second frame, 5-an X-shaped frame, 6-a picture frame, 7-a reflector, 8-a push-type screw motor, 9-a fixed sleeve, 10-a rotating sleeve, 11-a connecting sleeve, 12-a hinge base, 13-a central rotating shaft, 14-a long shaft, 15-an arc-shaped limiting frame, 16-an arc-shaped chute, 17-a short shaft, 18-a rotating column, 19-a coupler, 20-a U-shaped frame, 21-a steel ball and 22-an annular groove.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-7, an embodiment of the present invention provides a technical solution: a rotary single-lens oblique photography mechanism for an aircraft comprises a mounting disc 1, wherein a rotary column 18 is fixedly connected to the center of the mounting disc 1, a coupler 19 is fixedly connected to the top end of the rotary column 18, U-shaped frames 20 are arranged on the outer circumference of the mounting disc 1, six U-shaped frames 20 are arranged at equal intervals, the upper half portion of each U-shaped frame 20 is fixedly connected with a rack of the aircraft, steel balls 21 are rotatably connected to the bottom of the inner surface of each U-shaped frame 20, annular grooves 22 matched with the steel balls 21 are formed in the periphery of the bottom of the mounting disc 1, the rotary columns 18 are connected with an upper stepping motor shaft through the couplers 19 and used for controlling the mounting disc 1 and a lower structure of the mounting disc 1 to rotate 90 degrees to shoot a left lower portion and a right lower portion, the six U-shaped frames 20 are arranged to support the mounting disc 1, so that the mounting disc 1 can be more stable, the influence on the shooting effect caused by large shaking is avoided, the steel balls 21 are arranged between the U-shaped frame 20 and the mounting disc 1, the mounting disc 1 can rotate more smoothly, the abrasion is reduced, the first frame 2 is fixedly connected between the front side and the rear side of the left side of the bottom of the mounting disc 1 through bolts, the camera 3 is fixedly connected inside the first frame 2, the camera 3 is horizontally installed, the second frame 4 is fixedly connected to the front side and the rear side of the right side of the bottom of the mounting disc 1, the X-shaped frames 5 are fixedly connected to the bottoms of the two second frames 4, the arc-shaped limiting frames 15 are fixedly connected to the upper side and the lower side of the opposite sides of the two X-shaped frames 5, the arc-shaped chutes 16 are respectively arranged on the opposite sides of the two arc-shaped limiting frames 15, the arc-shaped limiting frames 15 are matched with the arc-shaped chutes 16, the picture frames 6 can rotate more stably, the shaking is reduced, and the left side of the inside of the picture frame 6 is fixedly connected with a reflector 7, the front side and the back side of the picture frame 6 and the inside of the arc-shaped chute 16 are fixedly connected with short shafts 17, the surface of each short shaft 17 is connected with the inner surface of the arc-shaped chute 16 in a sliding manner, the middle of the front side and the back side of the picture frame 6 is fixedly connected with a central rotating shaft 13, the surfaces of the two central rotating shafts 13 are rotatably connected with the inner side of the X-shaped frame 5 through bearings, the two second frames 4 and the right upper corners of the picture frame 6 are rotatably connected with a push-type screw motor 8, the middle of the front side and the back side of the push-type screw motor 8 are fixedly connected with long shafts 14, one ends of the long shafts 14, far away from the push-type screw motor 8, are rotatably connected with the inner side of the second frames 4 through bearings, the process of the push-type screw motor 8 is provided, 45 degrees and 22.5 degrees, the rotation of the push type screw motor 8 in the rotation process needs to be considered, the space of each push of the push type screw motor 8 is determined after the calculation of an internal program of the aircraft, the push type screw motor 8 is used as a driving force, the rotation angle of the reflector 7 can be accurately controlled by matching the control of a corresponding program, the operation is simpler, the shooting angle is more accurate, the outer surface of the left end of the output shaft of the push type screw motor 8 is sleeved with a fixed sleeve 9, the fixed sleeve 9 is arranged to be matched with a rotation sleeve 10, the rotation sleeve 10 can not rotate when the screw of the push type screw motor 8 rotates and pushes, the outer sleeve of the fixed sleeve 9 is sleeved with the rotation sleeve 10, the front side and the rear side of the rotation sleeve 10 are fixedly connected with connecting sleeves 11, the right side of the mirror frame 6 is fixedly connected with a hinge base 12 which is rotatably connected with the connecting sleeve 11, can realize the regulation to 3 shooting angles of camera, only need to use 3 camera of a picture frame 6 of cooperation and reflector 7 can satisfy the shooting demand of three angles in front below, under and the back below, not only reduced holistic weight, and reduced the space, can guarantee picture frame 6 and reflector 7 pivoted steady simultaneously, reduced the shake problem, make the shooting picture more clear.

And those not described in detail in this specification are well within the skill of those in the art.

When the aircraft is used, the aircraft is started to fly in the air according to a specified route, the camera 3 is started to shoot, the included angle between the reflector 7 and the horizontal plane is 67.5 degrees at the initial position, then the picture shot by the camera 3 is the picture facing to the rear lower angle by utilizing the reflection of light, then the push type screw motor 8 is controlled to work by a control element in the aircraft, the screw of the push type screw motor 8 is pushed out leftwards, the hinge base 12 is pushed by the connecting sleeve 11 to enable the mirror frame 6 to drive the reflector 7 to rotate for 22.5 degrees and stop, the included angle between the reflector 7 and the horizontal plane is 45 degrees, the picture shot by the camera is the picture right below at the moment, after shooting at the shooting angle is finished, the push type screw motor 8 is controlled to continuously push the mirror frame 6 to rotate to the position where the included angle between the mirror frame and the horizontal plane is 22.5 degrees, the picture shot by the camera at the moment is the picture, then the step motor above the rotating column 18 is controlled to work to drive the structure below the mounting disc 1 to integrally rotate for 90 degrees, then the aircraft flies according to the original route again, and then the first operation is repeated to finish the shooting of the pictures at the left lower part, the right lower part and the right lower part.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a rotation type single lens tilt photography mechanism for airborne vehicle, includes mounting disc (1), there is first frame (2) through bolt fixedly connected with between the left front and back both sides in mounting disc (1) bottom, and the inside fixedly connected with camera (3) of first frame (2), its characterized in that: the front side and the rear side of the right side of the bottom of the mounting disc (1) are fixedly connected with second racks (4), the bottoms of the two second racks (4) are fixedly connected with X-shaped racks (5), a picture frame (6) is rotatably connected between the two X-shaped racks (5), a reflective mirror (7) is fixedly connected on the left side inside the mirror frame (6), two second machine frames (4) are rotatably connected with a push type screw motor (8) positioned at the upper right corner of the mirror frame (6), the outer surface of the left end of the output shaft of the propulsion screw motor (8) is sleeved with a fixed sleeve (9), the outer part of the fixed sleeve (9) is sleeved with a rotating sleeve (10), and the front side and the rear side of the rotating sleeve (10) are both fixedly connected with connecting sleeves (11), the right side of the spectacle frame (6) is fixedly connected with a hinge seat (12) which is rotatably connected with the connecting sleeve (11).

2. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the middle of the front side and the back side of the mirror frame (6) is fixedly connected with a central rotating shaft (13), and the surfaces of the two central rotating shafts (13) are rotatably connected with the inner side of the X-shaped frame (5) through bearings.

3. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the middle of the front side and the rear side of the propulsion type screw motor (8) are fixedly connected with a long shaft (14), and one end, far away from the propulsion type screw motor (8), of the long shaft (14) is rotatably connected with the inner side of the second rack (4) through a bearing.

4. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: two equal fixedly connected with arc spacing frame (15) in upper and lower both sides of the relative one side of X type frame (5), two arc spout (16) have all been seted up to the relative one side of arc spacing frame (15).

5. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the front side and the rear side of the spectacle frame (6) are respectively fixedly connected with a short shaft (17) in the arc-shaped sliding groove (16), and the surface of the short shaft (17) is connected with the inner surface of the arc-shaped sliding groove (16) in a sliding manner.

6. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the center of the mounting disc (1) is fixedly connected with a rotating column (18), and the top end of the rotating column (18) is fixedly connected with a coupler (19).

7. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the outer circumference of installing disc (1) is provided with U type frame (20), U type frame (20) equidistance is provided with six, and the first half and the aircraft frame fixed connection of U type frame (20).

8. A rotary single lens oblique photography mechanism for an aircraft according to claim 7, wherein: the bottom of the inner surface of the U-shaped frame (20) is rotatably connected with steel balls (21), and an annular groove (22) matched with the steel balls (21) is formed in the periphery of the bottom of the mounting disc (1).

9. A rotary single lens oblique photography mechanism for an aircraft according to claim 1, wherein: the process of the push-type screw motor (8) is provided with three rotation positions of the three gears corresponding to the mirror frame (6), and the included angles between the three rotation positions of the mirror frame (6) and the horizontal plane are 67.5 degrees, 45 degrees and 22.5 degrees respectively.