CN215036717U - Positioning device for airplane wing - Google Patents
Positioning device for airplane wing Download PDFInfo
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- CN215036717U CN215036717U CN202120444258.6U CN202120444258U CN215036717U CN 215036717 U CN215036717 U CN 215036717U CN 202120444258 U CN202120444258 U CN 202120444258U CN 215036717 U CN215036717 U CN 215036717U
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- mount pad
- rotating plate
- rotor plate
- aircraft wing
- positioning device
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Abstract
The utility model discloses an aircraft is positioner for wing includes frame, left mount pad, right mount pad, rotor plate, rotation drive arrangement and positioning mechanism, a left side mount pad with right side mount pad be the interval with install in the frame, the rotor plate is located a left side mount pad with between the mount pad of the right side, one side of rotor plate rotationally with left side mount pad is connected, the opposite side of rotor plate rotationally with right side mount pad is connected, positioning mechanism install in be used for fixing on the rotor plate work piece on the rotor plate, rotation drive arrangement install in left side mount pad, the rotor plate install in rotation drive arrangement's output, the rotor plate is in rotation drive arrangement's drive is rotated down. The utility model discloses an aircraft is positioner for wing has that production efficiency is high, with low costs and the high advantage of accuracy.
Description
Technical Field
The utility model relates to the field of machining, especially, relate to an aircraft is positioner for wing.
Background
The aircraft is the flight device commonly used, in the aircraft wing manufacturing's of aircraft in-process, often need process a plurality of positions of aircraft wing, processing such as radian especially, however current frock clamp often can only fixed position to can only process the upper surface of aircraft wing, and can not process to the side etc. if will process just must adopt the assembly to other anchor clamps on, so not only inefficiency and with high costs, and easy because many times the clamping and the precision that leads to processing is low, the event can't satisfy current production demand.
Accordingly, there is a need for a positioning device for an aircraft wing that overcomes the above-mentioned deficiencies.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a positioner is used to aircraft wing that production efficiency is high, with low costs and the accuracy is high.
In order to realize the above-mentioned purpose, the utility model discloses an aircraft is positioner for wing, it includes frame, left mount pad, right mount pad, rotor plate, rotation drive arrangement and positioning mechanism, a left side mount pad with right side mount pad be the interval ground install in the frame, the rotor plate is located a left side mount pad with between the mount pad of the right side, one side of rotor plate rotationally with left side mount pad is connected, the opposite side of rotor plate rotationally with right side mount pad is connected, positioning mechanism install in be used for fixing on the rotor plate work piece on the rotor plate, rotation drive arrangement install in left side mount pad, the rotor plate install in rotation drive arrangement's output, the rotor plate is in rotation drive arrangement's drive is down rotated.
Preferably, one side of the rotating plate is rotatably connected with the left mounting seat through a left bearing.
Specifically, one side of the rotating plate is provided with a left connecting plate which is used for being connected with the left bearing.
Preferably, the other side of the rotating plate is rotatably connected with the right mounting seat through a right bearing.
Specifically, the other side of the rotating plate is provided with a right connecting plate for connecting with the right bearing.
Preferably, the positioning mechanism comprises a left pressing piece and a right pressing piece, and the left pressing piece and the right pressing piece are spaced and oppositely mounted on the left side and the right side of the rotating plate.
Specifically, the left pressing piece comprises a left pressing driving device and a left pressing head, the left pressing driving device is installed on the rotating plate, the left pressing head is installed at the output end of the left pressing driving device, and the left pressing head is driven by the left pressing driving device to lift so as to press or loosen a workpiece on the rotating plate.
Specifically, the right pressing piece comprises a right pressing driving device and a right pressing head, the right pressing driving device is installed on the rotating plate, the right pressing head is installed at the output end of the right pressing driving device, and the right pressing head is driven by the right pressing driving device to lift so as to press or loosen a workpiece on the rotating plate.
Specifically, the left pressing piece and the right pressing piece jointly enclose a quadrilateral structure.
Preferably, the positioning device for the aircraft wing further comprises a position detection device for detecting the position of the workpiece.
Compared with the prior art, the positioning device for the aircraft wing of the utility model combines a left mounting seat, a right mounting seat, a rotating plate, a rotating driving device, a positioning mechanism and the like together, the left mounting seat and the right mounting seat are installed on the frame at intervals, the rotating plate is arranged between the left mounting seat and the right mounting seat, one side of the rotating plate is rotatably connected with the left mounting seat, the other side of the rotating plate is rotatably connected with the right mounting seat, so that the rotating plate can rotate relative to the left mounting seat and the right mounting seat, the positioning mechanism is installed on the rotating plate and is used for fixing a workpiece on the rotating plate, thereby fixing the workpiece on the rotating plate by utilizing the positioning mechanism, further leading the rotating plate to form a processing area for processing, the rotating driving device is installed on the left mounting seat, the rotating plate is installed at the output end of the rotating driving device, the rotating plate rotates under the driving of the rotating driving device, the workpiece on the rotating plate is rotated by means of rotation of the rotating plate, in other words, a plurality of angles and positions of the workpiece can be processed by only once positioning, and the adjusting is flexible, the processing efficiency is high, the cost is low, and the accuracy is high.
Drawings
Fig. 1 is a schematic structural view of the positioning device for aircraft wing of the present invention in the front view direction.
Fig. 2 is a schematic structural view of the positioning device for aircraft wing according to the present invention in the downward direction.
Detailed Description
In order to explain technical contents, structural features, and objects and effects of the present invention in detail, the following description is given in conjunction with the embodiments and the accompanying drawings.
Referring to fig. 1 to 2, a positioning device 100 for an aircraft wing of the present invention includes a frame 1, a left mounting seat 2, a right mounting seat 3, a rotating plate 4, a rotation driving device 5 and a positioning mechanism 6, wherein the frame 1 is a plate-shaped structure, the left mounting seat 2 and the right mounting seat 3 are installed on the frame 1 at intervals, the left mounting seat 2 and the right mounting seat 3 are oppositely disposed, the rotating plate 4 is disposed between the left mounting seat 2 and the right mounting seat 3, one side of the rotating plate 4 is rotatably connected to the left mounting seat 2, the other side of the rotating plate 4 is rotatably connected to the right mounting seat 3, such that the rotating plate 4 can rotate relative to the left mounting seat 2 and the right mounting seat 3, the positioning mechanism 6 is installed on the rotating plate 4 and is used for fixing a workpiece 200 on the rotating plate 4, such that the positioning mechanism 6 fixes the workpiece 200 on the rotating plate 4, and the rotating plate 4 forms a processing area for processing, rotation drive arrangement 5 installs in left mount pad 2, and rotor plate 4 installs in rotation drive arrangement 5's output, and rotor plate 4 rotates under rotation drive arrangement 5's drive, borrows the rotation that borrows rotor plate 4 to make work piece 200 on the rotor plate 4 rotate, in other words, only need once fix a position can process a plurality of angles and a plurality of positions of work piece 200, and it is nimble to adjust, machining efficiency is high, with low costs and the accuracy is high. More specifically, the following:
referring to fig. 1 to 2, one side of the rotating plate 4 is rotatably connected to the left mounting base 2 through a left bearing 7, so that the rotating plate 4 can rotate smoothly, and a left connecting plate 8 for connecting with the left bearing 7 is disposed on one side of the rotating plate 4, so that the components are more compact and the connection is more stable. The opposite side of rotor plate 4 passes through right bearing 9 and right mount pad 3 rotatable coupling to realize rotor plate 4's smooth and easy rotation, the opposite side of rotor plate 4 is equipped with the right connecting plate 10 that is used for being connected with right bearing 9, thereby makes between each part compacter and connect more stably.
Referring to fig. 1 to 2, the positioning mechanism 6 includes a left pressing member 61 and a right pressing member 62, and the left pressing member 61 and the right pressing member 62 are spaced apart and oppositely mounted on the left and right sides of the rotating plate 4, so as to position the workpiece 200 by pressing and prevent the workpiece from moving during rotation. For example, the left pressing member 61 includes a left pressing driving device 611 and a left pressing head 612, the left pressing driving device 611 is installed on the rotating plate 4, the left pressing head 612 is installed at an output end of the left pressing driving device 611, the left pressing head 612 is driven by the left pressing driving device 611 to lift and lower to press or release the workpiece 200 on the rotating plate 4, the right pressing member 62 includes a right pressing driving device 621 and a right pressing head 622, the right pressing driving device 621 is installed on the rotating plate 4, the right pressing head 622 is installed at an output end of the right pressing driving device 621, and the right pressing head 622 is driven by the right pressing driving device 621 to lift and lower to press or release the workpiece 200 on the rotating plate 4. Preferably, the left pressing member 61 and the right pressing member 62 together form a quadrilateral structure, so as to better realize good and stable positioning of the workpiece 200.
Referring to fig. 1 to 2, the positioning device 100 for an aircraft wing of the present invention further includes a position detection device 11 for detecting the position of the workpiece 200, the position detection device 11 detects the position of the workpiece 200 at any time, and if there is a deviation in the position of the workpiece 200, an alarm is issued, so as to effectively ensure the processing accuracy of the workpiece 200.
In summary, referring to fig. 1 to 2, a detailed description is made of the working process of the positioning device 100 for an aircraft wing according to the present invention:
the workpiece 200 is placed on the rotating plate 4, the left pressing head 612 descends and presses one side of the workpiece 200 under the driving of the left pressing driving device 611, the right pressing head 622 descends and presses the other side of the workpiece 200 under the driving of the right pressing driving device 621, so that the positioning of the workpiece 200 is realized, and the rotating plate 4 rotates under the driving of the rotating driving device 5, so that multiple angles of the workpiece 200 can be machined.
By combining a left mounting seat 2, a right mounting seat 3, a rotating plate 4, a rotating driving device 5, a positioning mechanism 6 and the like together, wherein the left mounting seat 2 and the right mounting seat 3 are arranged on a frame 1 at intervals, the rotating plate 4 is arranged between the left mounting seat 2 and the right mounting seat 3, one side of the rotating plate 4 is rotatably connected with the left mounting seat 2, the other side of the rotating plate 4 is rotatably connected with the right mounting seat 3, so that the rotating plate 4 can rotate relative to the left mounting seat 2 and the right mounting seat 3, the positioning mechanism 6 is arranged on the rotating plate 4 and is used for fixing a workpiece 200 on the rotating plate 4, so that the workpiece 200 is fixed on the rotating plate 4 by the positioning mechanism 6, further the rotating plate 4 forms a processing area for processing, the rotating driving device 5 is arranged on the left mounting seat 2, the rotating plate 4 is arranged at the output end of the rotating driving device 5, and the rotating plate 4 rotates under the driving of the rotating driving device 5, the rotation of the rotating plate 4 enables the workpiece 200 on the rotating plate 4 to rotate, in other words, a plurality of angles and a plurality of positions of the workpiece 200 can be processed only by once positioning, and the adjustment is flexible, the processing efficiency is high, the cost is low, and the accuracy is high.
The above disclosure is only a preferred embodiment of the present invention, and certainly, the scope of the present invention should not be limited thereto, and therefore, the scope of the present invention is not limited to the above embodiments.
Claims (10)
1. The utility model provides an aircraft is positioner for wing, its characterized in that, includes frame, left mount pad, right mount pad, rotor plate, rotation drive arrangement and positioning mechanism, a left side mount pad with right side mount pad be the interval with install in the frame, the rotor plate is located a left side mount pad with between the right side mount pad, one side of rotor plate rotationally with left side mount pad is connected, the opposite side of rotor plate rotationally with right side mount pad is connected, positioning mechanism install in be used for fixing on the rotor plate work piece on the rotor plate, rotation drive arrangement install in left side mount pad, the rotor plate install in rotation drive arrangement's output, the rotor plate is in rotation drive arrangement's drive is down rotated.
2. The aircraft wing positioning device of claim 1, wherein one side of the rotating plate is rotatably coupled to the left mounting bracket by a left bearing.
3. The aircraft wing positioning device of claim 2, wherein one side of the rotating plate is provided with a left connecting plate for connection with the left bearing.
4. The aircraft wing positioning device of claim 1, wherein the other side of the rotating plate is rotatably coupled to the right mounting base by a right bearing.
5. The aircraft wing positioning device of claim 4, wherein the other side of the rotating plate is provided with a right connecting plate for connection with the right bearing.
6. The aircraft wing positioning device of claim 1, wherein the positioning mechanism comprises a left press and a right press, the left press and the right press being spaced apart and oppositely mounted to the left and right sides of the rotating plate.
7. The aircraft wing positioning device of claim 6, wherein the left stitching member comprises a left stitching drive device and a left pressing head, the left stitching drive device is mounted on the rotating plate, the left pressing head is mounted at an output end of the left stitching drive device, and the left pressing head is driven by the left stitching drive device to lift and lower so as to press or release a workpiece on the rotating plate.
8. The aircraft wing positioning device of claim 6, wherein the right stitching member comprises a right stitching drive device and a right pressing head, the right stitching drive device is mounted on the rotating plate, the right pressing head is mounted at an output end of the right stitching drive device, and the right pressing head is driven by the right stitching drive device to lift and lower so as to press or release the workpiece on the rotating plate.
9. The aircraft wing positioning device of claim 6, wherein the left compression element and the right compression element together define a quadrilateral configuration.
10. The aircraft wing positioning device of claim 1, further comprising a position detection device for detecting the position of the workpiece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120444258.6U CN215036717U (en) | 2021-03-01 | 2021-03-01 | Positioning device for airplane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120444258.6U CN215036717U (en) | 2021-03-01 | 2021-03-01 | Positioning device for airplane wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215036717U true CN215036717U (en) | 2021-12-07 |
Family
ID=79254107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120444258.6U Active CN215036717U (en) | 2021-03-01 | 2021-03-01 | Positioning device for airplane wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215036717U (en) |
-
2021
- 2021-03-01 CN CN202120444258.6U patent/CN215036717U/en active Active
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