CN212448161U - Unmanned aerial vehicle control parameter debugging frame - Google Patents
Unmanned aerial vehicle control parameter debugging frame Download PDFInfo
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- CN212448161U CN212448161U CN202021137246.0U CN202021137246U CN212448161U CN 212448161 U CN212448161 U CN 212448161U CN 202021137246 U CN202021137246 U CN 202021137246U CN 212448161 U CN212448161 U CN 212448161U
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Abstract
The utility model provides an unmanned aerial vehicle control parameter debugging frame, including the debugging frame, be equipped with a plurality of debugging frame on the base, the top outside of debugging frame is equipped with supports the slip table, be equipped with electric putter on the debugging frame, electric putter's propulsion end with the below of supporting the slip table is connected, the top central authorities of debugging frame are equipped with the connecting piece, it is equipped with the through-hole to support slip table top central authorities, the upper end of connecting piece is passed the through-hole, the upper end of connecting piece is equipped with the aircraft fixing base, be equipped with unmanned aerial vehicle on the aircraft fixing base, the lower part of debugging frame is equipped with the base. Compared with the prior art, the airplane is arranged on the debugging frame to limit the translational freedom degree of the airplane, but not to limit the rotational freedom degree of the airplane, so that the potential safety hazard in the debugging process is reduced; two debugging modes are provided; the supporting sliding table can lock the attitude of the airplane before the airplane takes off and is unlocked, and the supporting sliding table descends after the airplane takes off, so that the airplane can rotate freely.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to an unmanned aerial vehicle debugging technical field, in particular to unmanned aerial vehicle control parameter debugging frame.
[ background of the invention ]
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, has wide application, and is applied to the industries of police, city management, agriculture, geology, meteorology, electric power, emergency rescue and relief, video shooting and the like.
Unmanned aerial vehicle debugs control parameter at the design in-process to try out reasonable parameter, among the prior art, unmanned aerial vehicle's debugging adopts the form that actual space tried to fly mostly, has certain potential safety hazard like this in the debugging process.
[ Utility model ] content
An object of the utility model is to provide an unmanned aerial vehicle control parameter debugging frame to overcome the problem that there is certain potential safety hazard in the unmanned aerial vehicle debugging process among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme:
the application discloses unmanned aerial vehicle control parameter debugging frame, including debugging frame, base, support slip table, electric putter, aircraft fixing base and connecting piece, be equipped with a plurality of debugging frame on the base, the top outside of debugging frame is equipped with supports the slip table, be equipped with electric putter on the debugging frame, electric putter's propulsion end with the below of supporting the slip table is connected, the top central authorities of debugging frame are equipped with the connecting piece, it is equipped with the through-hole to support slip table top central authorities, the upper end of connecting piece is passed the through-hole, the upper end of connecting piece is equipped with the aircraft fixing base, be equipped with unmanned aerial vehicle on the aircraft fixing base, the lower part of debugging frame is equipped with the base.
Preferably, the connecting piece is of a ball head hinge structure, a ball head seat is arranged in the center of the bottom of the aircraft fixing seat, a fixing plate is arranged below the ball head seat, and a ball head end of the connecting piece penetrates through the fixing plate to be connected with the ball head seat.
Preferably, the connecting piece is of a dead axle hinge structure, the bottom of the airplane fixing seat is provided with a connecting seat matched with the dead axle hinge, a fixing plate is arranged below the connecting seat, and the dead axle end of the connecting piece penetrates through the fixing plate to be connected with the connecting seat.
Preferably, the bottom of the connecting piece is sleeved with a quick-release piece, and the lower end of the quick-release piece penetrates through the through hole to be connected with the debugging frame.
Preferably, the top structure of the aircraft fixing seat is matched with the bottom structure of the unmanned aerial vehicle, and the aircraft fixing seat and the unmanned aerial vehicle are reinforced through an aircraft fixing bandage.
Preferably, the base is provided with a plurality of stable bottom rods, a plurality of stable inclined rods are arranged between the base and the debugging frame, and connecting rods are arranged between the debugging frames.
Preferably, a rubber pad is arranged at the top of the supporting sliding table.
The utility model has the advantages that: compared with the prior art, the utility model provides a pair of unmanned aerial vehicle control parameter debugging frame, it is rational in infrastructure:
(1) the aircraft is arranged on the debugging frame to limit the translational freedom degree of the aircraft, but not to limit the rotational freedom degree of the aircraft, so that the potential safety hazard in the debugging process is reduced.
(2) Two debugging modes are provided, one mode is that a connecting piece adopts a ball joint hinge to allow any axis of the airplane to rotate; the other is that the connecting piece adopts a fixed-axis hinge and only allows the airplane to rotate on one axis.
(3) The supporting sliding table is designed, the attitude of the airplane can be locked before the airplane takes off and is unlocked, and the supporting sliding table descends through the electric push rod after the airplane takes off, so that the airplane can rotate freely.
(4) The quick-release part is designed between the connecting part and the debugging frame, and the quick connection and the fixation between the quick-release part and the debugging frame are realized.
The features and advantages of the present invention will be described in detail by embodiments with reference to the accompanying drawings.
[ description of the drawings ]
Fig. 1 is a schematic diagram of a front structure of an unmanned aerial vehicle control parameter debugging frame of the present invention;
fig. 2 is a schematic structural view of the unmanned aerial vehicle control parameter debugging frame of the present invention;
FIG. 3 is a schematic view of the installation of the connecting member of the present invention using a ball joint hinge;
FIG. 4 is a schematic view of the installation of the connecting member of the present invention using a fixed axis hinge;
FIG. 5 is a schematic view of the front structure of the support slide for limiting;
fig. 6 is a front schematic view of the sliding table of the present invention when the sliding table is released from the position limitation.
In the figure: 1-debugging frame, 2-base, 21-stable low rod, 22-stable inclined rod, 23-connecting rod, 3-supporting sliding table, 31-rubber pad, 32-through hole, 4-electric push rod, 5-airplane fixing seat, 51-ball seat, 52-fixing plate, 53-connecting seat, 54-airplane fixing binding band, 6-unmanned aerial vehicle, 7-connecting piece and 71-quick-dismantling piece.
[ detailed description ] embodiments
In order to make the objects, technical solutions and advantages of the present invention more clear, the present invention is further described in detail through the accompanying drawings and embodiments. It should be understood, however, that the description herein of specific embodiments is only intended to illustrate the invention and not to limit the scope of the invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
Referring to fig. 1 to 6, the embodiment of the utility model provides an unmanned aerial vehicle control parameter debugging frame, including debugging frame 1, base 2, support slip table 3, electric putter 4, aircraft fixing base 5 and connecting piece 7, be equipped with a plurality of debugging frame 1 on the base 2, the top outside of debugging frame 1 is equipped with supports slip table 3, be equipped with electric putter 4 on the debugging frame 1, electric putter 4's the promotion end with the below of supporting slip table 3 is connected, the top central authorities of debugging frame 1 are equipped with connecting piece 7, it is equipped with through-hole 32 to support slip table 3 top central authorities, the upper end of connecting piece 7 is passed through-hole 32, the upper end of connecting piece 7 is equipped with aircraft fixing base 5, be equipped with unmanned aerial vehicle 6 on the aircraft fixing base 5, the lower part of debugging frame 1 is equipped with base 2.
The connecting piece 7 is of a ball head hinge structure, a ball head seat 51 is arranged in the center of the bottom of the aircraft fixing seat 5, a fixing plate 52 is arranged below the ball head seat 51, and the ball head end of the connecting piece 7 penetrates through the fixing plate 52 to be connected with the ball head seat 51. The connecting piece 7 is of a fixed-axis hinge structure, the bottom of the airplane fixing seat 5 is provided with a connecting seat 53 matched with the fixed-axis hinge, a fixing plate 52 is arranged below the connecting seat 53, and the fixed-axis end of the connecting piece 7 penetrates through the fixing plate 52 to be connected with the connecting seat 53. The bottom of the connecting piece 7 is sleeved with a quick-release piece 71, and the lower end of the quick-release piece 71 penetrates through the through hole 32 to be connected with the debugging frame 1.
The top structure of the aircraft fixing seat 5 is matched with the bottom structure of the unmanned aerial vehicle 6, and the aircraft fixing seat 5 and the unmanned aerial vehicle 6 are reinforced through an aircraft fixing bandage 54. The base 2 is provided with a plurality of stable bottom rods 21, a plurality of stable inclined rods 22 are arranged between the base 2 and the debugging frame 1, and a connecting rod 23 is arranged between the debugging frame 1. The top of the support sliding table 3 is provided with a rubber pad 31.
The utility model discloses the working process:
when carrying out the unipolar pivot debugging, it is fixed with unmanned aerial vehicle 6's bottom and aircraft fixing base 5, and consolidate the back with aircraft fixing bandage 54, connect dead axle hinged joint spare 7 on the connecting seat 53 of aircraft fixing base 5 bottom, reuse fixed plate 52 is fixed the back, install connecting piece 7 at debugging frame 1 top through quick detach 71, will support slip table 3 and push away to the top through electric putter 4, make support slip table 3 and aircraft fixing base 5 contactless each other, the unblock aircraft, operation electric putter 4 will support slip table 3 and glide gradually, make the aircraft begin to carry out the unipolar debugging.
When carrying out the qxcomm technology pivot debugging, it is fixed with unmanned aerial vehicle 6's bottom and aircraft fixing base 5, and consolidate the back with aircraft fixing bandage 54, install bulb seat 51 in aircraft fixing base 5 bottom, and be connected bulb seat 51 with bulb hinged joint spare 7, reuse fixed plate 52 is fixed the back, install connecting piece 7 at debugging frame 1 top through quick detach piece 71, will support slip table 3 and push away to the top through electric putter 4, make and support slip table 3 and aircraft fixing base 5 mutual contact, the unblock aircraft, operation electric putter 4 will support slip table 3 and glide gradually, make the unmanned aerial vehicle begin to carry out the qxcomm technology pivot debugging.
In two debugging processes, unmanned aerial vehicle 6 is restricted its translation degree of freedom on debugging frame 1, and does not restrict its rotation degree of freedom to can debug unmanned aerial vehicle 6 under the circumstances of guaranteeing safety
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modification, equivalent replacement or improvement made within the spirit and principle of the present invention should be included in the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle control parameter debugging frame which characterized in that: comprises a debugging frame (1), a base (2), a supporting sliding table (3), an electric push rod (4), an airplane fixing seat (5) and a connecting piece (7), a plurality of debugging frames (1) are arranged on the base (2), a supporting sliding table (3) is arranged on the outer side of the top of each debugging frame (1), an electric push rod (4) is arranged on the debugging frame (1), the propelling end of the electric push rod (4) is connected with the lower part of the supporting sliding table (3), the center of the top of the debugging frame (1) is provided with a connecting piece (7), the center of the top of the supporting sliding table (3) is provided with a through hole (32), the upper end of the connecting piece (7) passes through the through hole (32), the upper end of the connecting piece (7) is provided with an airplane fixing seat (5), be equipped with unmanned aerial vehicle (6) on aircraft fixing base (5), the lower part of debugging frame (1) is equipped with base (2).
2. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: the connecting piece (7) is of a ball head hinge structure, a ball head seat (51) is arranged in the center of the bottom of the airplane fixing seat (5), a fixing plate (52) is arranged below the ball head seat (51), and the ball head end of the connecting piece (7) penetrates through the fixing plate (52) to be connected with the ball head seat (51).
3. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: the connecting piece (7) is of a dead axle hinge structure, a connecting seat (53) matched with the dead axle hinge is arranged at the bottom of the airplane fixing seat (5), a fixing plate (52) is arranged below the connecting seat (53), and the dead axle end of the connecting piece (7) penetrates through the fixing plate (52) to be connected with the connecting seat (53).
4. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: the bottom of the connecting piece (7) is sleeved with a quick-release piece (71), and the lower end of the quick-release piece (71) penetrates through the through hole (32) to be connected with the debugging frame (1).
5. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: the top structure of the aircraft fixing seat (5) is matched with the bottom structure of the unmanned aerial vehicle (6), and the aircraft fixing seat (5) and the unmanned aerial vehicle (6) are reinforced through an aircraft fixing binding belt (54).
6. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: be equipped with a plurality of bottom rod (21) that stabilize on base (2), a plurality of down tube (22) that stabilize between base (2) and debugging frame (1), be equipped with connecting rod (23) between debugging frame (1).
7. The unmanned aerial vehicle control parameter debugging frame of claim 1, characterized in that: and a rubber pad (31) is arranged at the top of the supporting sliding table (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021137246.0U CN212448161U (en) | 2020-06-18 | 2020-06-18 | Unmanned aerial vehicle control parameter debugging frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021137246.0U CN212448161U (en) | 2020-06-18 | 2020-06-18 | Unmanned aerial vehicle control parameter debugging frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212448161U true CN212448161U (en) | 2021-02-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021137246.0U Active CN212448161U (en) | 2020-06-18 | 2020-06-18 | Unmanned aerial vehicle control parameter debugging frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212448161U (en) |
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2020
- 2020-06-18 CN CN202021137246.0U patent/CN212448161U/en active Active
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