CN213262972U

CN213262972U - Be applied to unmanned aerial vehicle's gesture debugging device

Info

Publication number: CN213262972U
Application number: CN202022410196.5U
Authority: CN
Inventors: 刘丽丽; 左继红
Original assignee: HUNAN RAILWAY PROFESSIONAL TECHNOLOGY COLLEGE
Current assignee: HUNAN RAILWAY PROFESSIONAL TECHNOLOGY COLLEGE
Priority date: 2020-10-20
Filing date: 2020-10-20
Publication date: 2021-05-25
Anticipated expiration: 2030-10-20

Abstract

The utility model discloses a be applied to unmanned aerial vehicle's gesture debugging device, the camera includes a supporting plate, the fixed plate, the bottom plate with place the board, one side is provided with the backup pad on the bottom plate, the opposite side is provided with the fixed plate on the bottom plate, backup pad and fixed plate bottom vertical fixation are on the bottom plate, backup pad and fixed plate top are provided with places the board, it rotates through the pivot and the backup pad that set up to place board one end and is connected, it is fixed with the fixed block to place board other end bottom, one side installs first motor in the backup pad, first motor output end is connected with the lead screw, the lead screw other end passes through the backup pad, there is the thread bush through threaded connection on the lead screw, be provided with the connecting piece between thread bush and the fixed block. Has the advantages that: can simulate and realize unmanned aerial vehicle partial to and space action such as rotation, reach the effect of unmanned aerial vehicle attitude control test, reduce unmanned aerial vehicle test cost.

Description

Be applied to unmanned aerial vehicle's gesture debugging device

Technical Field

The utility model relates to an unmanned air vehicle technique field particularly, relates to a be applied to unmanned aerial vehicle's gesture debugging device.

Background

Along with the development of unmanned aerial vehicle technique, its performance is more and more powerful, and the function is abundant gradually, and research and development cost also risees thereupon. When the research test is carried out, a complex environment or other emergencies are met, and the flight experiment of the unmanned aerial vehicle can pay great cost. Unmanned aerial vehicle and airborne equipment's security obtains the more and more concern of researcher, consequently designs a set and just can carry out the device of debugging with rotatory to unmanned aerial vehicle indoor and be present urgent to solve.

An effective solution to the problems in the related art has not been proposed yet.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a be applied to unmanned aerial vehicle's gesture debugging device to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a posture debugging device applied to an unmanned aerial vehicle comprises a supporting plate, a fixing plate, a bottom plate and a placing plate, wherein the supporting plate is arranged on one side of the bottom plate, the fixing plate is arranged on the other side of the bottom plate, the bottoms of the supporting plate and the fixing plate are vertically fixed on the bottom plate, the placing plate is arranged on the tops of the supporting plate and the fixing plate, one end of the placing plate is rotatably connected with the supporting plate through an arranged rotating shaft, the bottom of the other end of the placing plate is fixedly provided with a fixing block, a first motor is arranged on one side of the supporting plate, the output end of the first motor is connected with a lead screw, the other end of the lead screw is rotatably connected with the fixing plate through an arranged bearing seat, a threaded sleeve is connected onto the lead screw through threads, a connecting piece is arranged between the threaded sleeve and, the top end of the connecting piece is rotatably connected with the fixed block through a fixed shaft, and a sliding rod is connected between the supporting plate and the fixed plate.

Furthermore, a sliding sleeve is sleeved on the sliding rod, the top end of the sliding sleeve is connected with a connecting rod, and the top end of the connecting rod is connected to the threaded sleeve.

Furthermore, a disc is arranged in the middle of the placing plate, a circular groove is reserved in the disc, and a mounting seat is arranged in the groove.

Furthermore, the mounting base is matched with the groove in shape and size, and bolt holes are reserved in the mounting base and are multiple.

Further, place board bottom intermediate position department and install the second motor, the output of second motor is connected with the output shaft.

Furthermore, the top end of the output shaft is connected to the bottom of the mounting seat through a placing plate and a disc.

Compared with the prior art, the utility model discloses following beneficial effect has: through the backup pad that sets up, place board, pivot, fixed block, first motor, lead screw, thread bush, connecting piece and fixed axle, realize the adjustment to placing board inclination, through disc, recess, mount pad, second motor and the output shaft that sets up, realized the rotation of mount pad to can simulate and realize space actions such as unmanned aerial vehicle erroneous tendency and rotation, reach the effect of unmanned aerial vehicle attitude control test, reduced unmanned aerial vehicle test cost.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic structural diagram of an attitude adjustment apparatus applied to an unmanned aerial vehicle according to an embodiment of the present invention;

fig. 2 is according to the utility model discloses an be applied to unmanned aerial vehicle's gesture debugging device's structural section.

Reference numerals:

1. a support plate; 2. a fixing plate; 3. a base plate; 4. placing the plate; 5. a rotating shaft; 6. a fixed block; 7. a first motor; 8. a screw rod; 9. a bearing seat; 10. a threaded sleeve; 11. a connecting member; 12. a fixed shaft; 13. a slide bar; 14. a sliding sleeve; 15. a connecting rod; 16. a disc; 17. a groove; 18. a mounting seat; 19. bolt holes; 20. a second motor; 21. and an output shaft.

Detailed Description

The following, with reference to the drawings and the detailed description, further description of the present invention is made:

referring to fig. 1-2, an attitude adjustment device applied to an unmanned aerial vehicle according to an embodiment of the present invention includes a supporting plate 1, a fixing plate 2, a bottom plate 3 and a placing plate 4, the supporting plate 1 is disposed on one side of the bottom plate 3, the fixing plate 2 is disposed on the other side of the bottom plate 3, bottoms of the supporting plate 1 and the fixing plate 2 are vertically fixed on the bottom plate 3, the placing plate 4 is disposed on top of the supporting plate 1 and the fixing plate 2, one end of the placing plate 4 is rotatably connected to the supporting plate 1 through a rotating shaft 5, the fixing block 6 is fixed at the bottom of the other end of the placing plate 4, a first motor 7 is mounted on one side of the supporting plate 1, an output end of the first motor 7 is connected to a screw rod 8, the other end of the screw rod 8 passes through the supporting plate 1, the other end of, the lead screw 8 is connected with a threaded sleeve 10 through threads, a connecting piece 11 is arranged between the threaded sleeve 10 and the fixed block 6, the bottom end of the connecting piece 11 is rotatably connected with the threaded sleeve 10 through a set fixed shaft 12, the top end of the connecting piece 11 is rotatably connected with the fixed block 6 through the set fixed shaft 12, and a sliding rod 13 is connected between the supporting plate 1 and the fixed plate 2.

Through the above technical scheme of the utility model, the cover has sliding sleeve 14 on the slide bar 13, sliding sleeve 14 top is connected with connecting rod 15, connecting rod 15's top is connected on the thread bush 10, it is provided with disc 16 to place intermediate position department on the board 4, leave circular shape recess 17 in the disc 16, be provided with mount pad 18 in the recess 17, mount pad 18 and recess 17's the big or small looks adaptation of shape, leave bolt hole 19 on the mount pad 18, bolt hole 19 is a plurality of, place board 4 bottom intermediate position department and install second motor 20, the output of second motor 20 is connected with output shaft 21, output shaft 21's top is through placing board 4 and disc 16, output shaft 21's top is connected in mount pad 18 bottom.

When specifically using, unmanned aerial vehicle passes through fixed modes such as bolt and installs on mount pad 18, start first motor 7, first motor 7 control lead screw 8 rotates, make thread bush 10 remove to the right side for lead screw 8, sliding sleeve 14 slides on slide bar 13, thereby make connecting piece 11 take place to deviate from, connecting piece 11 stimulates fixed block 6 and places board 4, make place board 4 also take place to deviate from, the realization is to the adjustment of placing 4 inclination of board, start second motor 20, second motor 20 control output shaft 21 rotates, output shaft 21 rotates and drives mount pad 18 rotatory, thereby can simulate and realize that unmanned aerial vehicle is partial to and space action such as rotation, reach the effect of unmanned aerial vehicle attitude control test, unmanned aerial vehicle testing cost is reduced.

In the description of the present invention, it should be noted that the terms "top", "bottom", "one side", "the other side", "front", "back", "middle part", "inside", "top", "bottom", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, which is only for the convenience of description and simplification of the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention; furthermore, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, as they may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The posture debugging device applied to the unmanned aerial vehicle is characterized by comprising a supporting plate (1), a fixing plate (2), a bottom plate (3) and a placing plate (4), wherein the supporting plate (1) is arranged on one side of the bottom plate (3), the fixing plate (2) is arranged on the other side of the bottom plate (3), the bottoms of the supporting plate (1) and the fixing plate (2) are vertically fixed on the bottom plate (3), the placing plate (4) is arranged on the tops of the supporting plate (1) and the fixing plate (2), one end of the placing plate (4) is rotatably connected with the supporting plate (1) through a rotating shaft (5), a fixing block (6) is fixed at the bottom of the other end of the placing plate (4), a first motor (7) is installed on one side of the supporting plate (1), the output end of the first motor (7) is connected with a screw rod (8), and the other end of the screw rod, the other end of lead screw (8) is rotated through bearing frame (9) that sets up and is connected with fixed plate (2), there is thread bush (10) through threaded connection on lead screw (8), be provided with connecting piece (11) between thread bush (10) and fixed block (6), connecting piece (11) bottom is rotated through fixed axle (12) that sets up and is connected with thread bush (10), connecting piece (11) top is rotated through fixed axle (12) that sets up and is connected with fixed block (6), be connected with slide bar (13) between backup pad (1) and fixed plate (2).

2. The attitude debugging device applied to the unmanned aerial vehicle of claim 1, wherein a sliding sleeve (14) is sleeved on the sliding rod (13), a connecting rod (15) is connected to the top end of the sliding sleeve (14), and the top end of the connecting rod (15) is connected to the threaded sleeve (10).

3. The attitude debugging device applied to the unmanned aerial vehicle of claim 1, wherein a disc (16) is arranged at a middle position on the placing plate (4), a circular groove (17) is reserved in the disc (16), and a mounting seat (18) is arranged in the groove (17).

4. The attitude debugging device applied to the unmanned aerial vehicle of claim 3, wherein the mounting seat (18) is matched with the groove (17) in shape and size, bolt holes (19) are reserved on the mounting seat (18), and the number of the bolt holes (19) is several.

5. The attitude debugging device applied to the unmanned aerial vehicle of claim 1, wherein a second motor (20) is installed at the middle position of the bottom of the placing plate (4), and an output shaft (21) is connected to the output end of the second motor (20).

6. The attitude debugging device applied to the unmanned aerial vehicle of claim 5, wherein the top end of the output shaft (21) passes through the placing plate (4) and the disc (16), and the top end of the output shaft (21) is connected to the bottom of the mounting seat (18).