CN212287536U - Positioning device for processing composite material component of aircraft - Google Patents
Positioning device for processing composite material component of aircraft Download PDFInfo
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- CN212287536U CN212287536U CN202020821968.1U CN202020821968U CN212287536U CN 212287536 U CN212287536 U CN 212287536U CN 202020821968 U CN202020821968 U CN 202020821968U CN 212287536 U CN212287536 U CN 212287536U
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- clamping plate
- plate
- workbench
- fixedly connected
- clamping
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- 239000002131 composite material Substances 0.000 title claims abstract description 11
- 230000007246 mechanism Effects 0.000 claims abstract description 24
- 238000003754 machining Methods 0.000 claims abstract 6
- 238000001125 extrusion Methods 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 230000003111 delayed effect Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a positioning device for processing aircraft composite material components, which comprises a workbench, wherein both sides of the bottom end of the workbench are fixedly connected with side plates, the bottom end parts of the two side plates are fixedly connected with bottom feet, an adjusting mechanism is arranged between the two side plates, the adjusting mechanism is positioned below the workbench, a first clamping plate and a second clamping plate are symmetrically arranged on the adjusting mechanism, a first opening and a second opening are arranged on the workbench, the first clamping plate and the second clamping plate respectively pass through the workbench through the first opening and the second opening, a placing groove is arranged on the workbench between the first clamping plate and the second clamping plate, the opposite sides of the upper ends of the first clamping plate and the second clamping plate are respectively and fixedly connected with a first transverse plate and a second transverse plate, the first transverse plate is inserted in the second transverse plate, the utility model can extrude and clamp four sides of a processed piece, thereby the processed piece can be positioned and fixed rapidly, the stability of the machined part is ensured, and the smooth proceeding of the machining process is further ensured.
Description
Technical Field
The utility model relates to a positioner is used in processing of aircraft combined material subassembly belongs to positioner technical field.
Background
A personal aircraft is any flying object made by humans, capable of flying off the ground, flying in space, and controlled by humans, that is provided for personal use. With the popularity of aircraft, personal aircraft are certainly the direction of future development. Light and flexible low-altitude and low-speed aircraft are the development direction of personal aircraft.
In the processing process of the aircraft and the component, the aircraft and the component need to be fixed by using the fixing device, the aircraft and the component cannot be well and quickly positioned by using the conventional fixing device in the fixing process, and time is delayed, so that the processing process is delayed, and the processing efficiency is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft is positioner for combined material subassembly processing to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a positioning device for processing an aircraft composite material assembly comprises a workbench, wherein two sides of the bottom end of the workbench are fixedly connected with side plates, the end parts of the bottom ends of the two side plates are fixedly connected with bottom feet, an adjusting mechanism is arranged between the two side plates, the adjusting mechanism is positioned below the workbench, a first clamping plate and a second clamping plate are symmetrically arranged on the adjusting mechanism, the workbench is provided with a first opening and a second opening, the first clamping plate and the second clamping plate respectively penetrate through the workbench through the first opening and the second opening, a placing groove is arranged on the workbench between the first clamping plate and the second clamping plate, the opposite sides of the upper ends of the first clamping plate and the second clamping plate are respectively and fixedly connected with a first transverse plate and a second transverse plate, the first transverse plate is inserted into the second transverse plate, and the first transverse plate and the second transverse plate are both provided with extrusion mechanisms.
Preferably, the adjusting mechanism comprises a screw rod, a control block and two cross rods, the screw rod is arranged between the side plates and is rotatably connected with the two side plates, the end part of the screw rod, extending out of one of the side plates, is fixedly connected with the control block, the cross rods are arranged on two sides of the screw rod, the cross rods are fixedly connected to opposite sides of the two side plates, and the first clamping plate and the second clamping plate are sleeved on the screw rod and the two cross rods.
Preferably, the first clamping plate and the second clamping plate are both in threaded connection with the screw, the internal threads on the first clamping plate and the second clamping plate are opposite in direction, and the first clamping plate and the second clamping plate are both in sliding connection with the two cross rods.
Preferably, two the extrusion mechanism all includes bolt, stripper plate, cushion and two telescopic links, equal threaded connection has the bolt on first diaphragm and the second diaphragm, two the shank of bolt wall tip all rotates and is connected with the stripper plate, two stripper plate bottom tip all bonds and has the cushion, two the stripper plate respectively with first diaphragm bottom and two telescopic links of second diaphragm bottom fixedly connected with.
Preferably, a plurality of clamping blocks are fixedly connected to opposite sides of the first clamping plate and the second clamping plate.
Preferably, the first transverse plate and the second transverse plate are connected in a sliding manner.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the rotation control block, the control block drives the screw rod and rotates, because the internal thread on first grip block and the second grip block is the opposite phase each other and turns to, consequently first grip block and second grip block can be along screw rod removal in opposite directions, carry out centre gripping and location to the machined part both sides in the standing groove through a plurality of grip blocks of first grip block and second grip block offside, can fix a position the machined part is quick, make the machined part can be more stable process, adaptability is stronger.
2. The two bolts are rotated, the wall ends of the two bolt rods drive the corresponding extrusion plates to move downwards, the upper sides of the machined parts are extruded, the machined parts are further clamped, and the stability of the machined parts is guaranteed.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the extruding mechanism of the present invention;
3 FIG. 3 3 3 is 3 a 3 schematic 3 view 3 of 3 the 3 structure 3 of 3 the 3 A 3- 3 A 3 surface 3 of 3 the 3 present 3 invention 3; 3
Fig. 4 is a schematic top view of the present invention.
In the figure: 1. a work table; 2. a side plate; 3. footing; 4. an adjustment mechanism; 41. a control block; 42. a screw; 43. a cross bar; 5. a first clamping plate; 6. a clamping block; 7. a placement groove; 8. an extrusion mechanism; 81. a bolt; 82. a telescopic rod; 83. a pressing plate; 84. a rubber pad; 9. a second transverse plate; 10. a first transverse plate; 11. a second clamping plate; 12. a first opening; 13. a second opening.
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. 1-4, the present invention provides a technical solution: a positioning device for processing an aircraft composite material assembly comprises a workbench 1, wherein two sides of the bottom end of the workbench 1 are fixedly connected with side plates 2, the bottom end parts of the two side plates 2 are fixedly connected with bottom feet 3, an adjusting mechanism 4 is arranged between the two side plates 2, the adjusting mechanism 4 is positioned below the workbench 1, a first clamping plate 5 and a second clamping plate 11 are symmetrically arranged on the adjusting mechanism 4, a first opening 12 and a second opening 13 are arranged on the workbench 1, the first clamping plate 5 and the second clamping plate 11 respectively penetrate through the workbench 1 through the first opening 12 and the second opening 13, a placing groove 7 is arranged on the workbench 1 between the first clamping plate 5 and the second clamping plate 11, a first transverse plate 10 and a second transverse plate 9 are fixedly connected to opposite sides of the upper ends of the first clamping plate 5 and the second clamping plate 11 respectively, the first transverse plate 10 is inserted into the second transverse plate 9, extruding mechanisms 8 are arranged on the first transverse plate 10 and the second transverse plate 9, can extrude and the centre gripping four sides of machined part to make the machined part can be quick fix a position and fix, guarantee the stability of machined part, and then guarantee that the course of working goes on smoothly.
The opposite sides of the first clamping plate 5 and the second clamping plate 11 are fixedly connected with a plurality of clamping blocks 6, the first transverse plate 10 is connected with the second transverse plate 9 in a sliding manner, workpieces in the placing groove 7 are clamped and positioned through the plurality of clamping blocks 6, the workpieces can be quickly positioned, the workpieces can be processed more stably, the adaptability is stronger, the two extrusion mechanisms 8 comprise bolts 81, extrusion plates 83, rubber pads 84 and two telescopic rods 82, the bolts 81 are in threaded connection with the first transverse plate 10 and the second transverse plate 9, the extrusion plates 83 are in rotary connection with the end parts of the rod walls of the two bolts 81, the rubber pads 84 are bonded with the end parts of the bottom ends of the two extrusion plates 83, the two telescopic rods 82 are respectively and fixedly connected with the bottom ends of the first transverse plate 10 and the bottom end of the second transverse plate 9, the two bolts 81 are rotated, the rod walls of the two bolts 81 drive the corresponding extrusion plates 83 to move downwards, the upper side of a workpiece is extruded, the workpiece is further clamped, the stability of the workpiece is ensured, the adjusting mechanism 4 comprises a screw 42, a control block 41 and two cross rods 43, the screw 42 is arranged between the two side plates 2, the screw 42 is rotatably connected with the two side plates 2, the end part of one end of the screw 42 extending out of one side plate 2 is fixedly connected with the control block 41, the two sides of the screw 42 are respectively provided with the cross rods 43, the two cross rods 43 are respectively and fixedly connected with the opposite sides of the two side plates 2, the first clamping plate 5 and the second clamping plate 11 are respectively sleeved on the screw 42 and the two cross rods 43, the first clamping plate 5 and the second clamping plate 11 are respectively in threaded connection with the screw 42, the internal threads on the first clamping plate 5 and the second clamping plate 11 are oppositely turned, the first clamping plate 5 and the second clamping plate 11 are respectively in sliding connection with the two cross rods 43, the control block, because the internal threads on the first clamping plate 5 and the second clamping plate 11 are opposite to each other and turn to, consequently first clamping plate 5 and second clamping plate 11 can move along screw rod 42 in opposite directions, carry out centre gripping and location to the machined part both sides in the standing groove 7 through a plurality of grip blocks 6 of first clamping plate 5 and second clamping plate 11 opposite side, can fix a position the machined part is quick, make the machined part can be more stable process, the adaptability is stronger.
Specifically, when the utility model is used, a workpiece is placed in the placing groove 7, the control block 41 is rotated, the control block 41 drives the screw rod 42 to rotate, because the internal threads on the first clamping plate 5 and the second clamping plate 11 are opposite to each other, the first clamping plate 5 and the second clamping plate 11 can move along the screw rod 42 in opposite directions, the two sides of the workpiece in the placing groove 7 can be clamped and positioned by the clamping blocks 6 on the opposite sides of the first clamping plate 5 and the second clamping plate 11, the workpiece can be quickly positioned, when the first clamping plate 5 and the second clamping plate 11 move in opposite directions, the first transverse plate 10 extends into the second transverse plate 9, the two bolts 81 are rotated, because the two bolts 81 are rotatably connected with the two extrusion plates 83, and then the four telescopic rods 82 are matched, the rod wall ends of the two bolts 81 can drive the corresponding extrusion plates 83 to move downwards to extrude the upper side of the workpiece, further carry out the centre gripping to the machined part, make the machined part can be more stable process, adaptability is stronger.
In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second", "third", "fourth" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated, whereby the features defined as "first", "second", "third", "fourth" may explicitly or implicitly include at least one such feature.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
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 (6)
1. The positioning device for processing the composite material assembly of the aircraft comprises a workbench (1) and is characterized in that two sides of the bottom end of the workbench (1) are fixedly connected with side plates (2), two bottom end parts of the side plates (2) are fixedly connected with bottom feet (3), an adjusting mechanism (4) is arranged between the two side plates (2), the adjusting mechanism (4) is positioned below the workbench (1), a first clamping plate (5) and a second clamping plate (11) are symmetrically arranged on the adjusting mechanism (4), a first opening (12) and a second opening (13) are arranged on the workbench (1), the first clamping plate (5) and the second clamping plate (11) respectively penetrate through the workbench (1) through the first opening (12) and the second opening (13), a placing groove (7) is arranged on the workbench (1) between the first clamping plate (5) and the second clamping plate (11), the clamping device is characterized in that opposite sides of the upper ends of the first clamping plate (5) and the second clamping plate (11) are fixedly connected with a first transverse plate (10) and a second transverse plate (9) respectively, the first transverse plate (10) is inserted into the second transverse plate (9), and the first transverse plate (10) and the second transverse plate (9) are provided with extrusion mechanisms (8).
2. The aircraft composite component machining positioning device of claim 1, wherein: adjustment mechanism (4) include screw rod (42), control block (41) and two horizontal poles (43), two be equipped with screw rod (42) between curb plate (2), screw rod (42) rotate with two curb plate (2) and are connected, the one end tip fixedly connected with control block (41) that one of them curb plate (2) is stretched out in screw rod (42), screw rod (42) both sides all are equipped with horizontal pole (43), two the equal fixed connection in two curb plate (2) opposite sides in horizontal pole (43), screw rod (42) and two horizontal poles (43) are all established to first grip block (5) and second grip block (11) cover.
3. The positioning device for the machining of composite aircraft material components according to claim 2, characterized in that: the first clamping plate (5) and the second clamping plate (11) are in threaded connection with the screw rod (42), internal threads on the first clamping plate (5) and the second clamping plate (11) are in opposite directions, and the first clamping plate (5) and the second clamping plate (11) are in sliding connection with the two cross rods (43).
4. The aircraft composite component machining positioning device of claim 1, wherein: two extrusion mechanism (8) all include bolt (81), stripper plate (83), cushion (84) and two telescopic links (82), equal threaded connection has bolt (81) on first diaphragm (10) and second diaphragm (9), two bolt (81) pole wall tip all rotates and is connected with stripper plate (83), two stripper plate (83) bottom tip all bonds cushion (84), two stripper plate (83) bottom fixedly connected with two telescopic links (82) in bottom with first diaphragm (10) bottom and second diaphragm (9) respectively.
5. The aircraft composite component machining positioning device of claim 1, wherein: the opposite sides of the first clamping plate (5) and the second clamping plate (11) are fixedly connected with a plurality of clamping blocks (6).
6. The aircraft composite component machining positioning device of claim 1, wherein: the first transverse plate (10) is connected with the second transverse plate (9) in a sliding mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020821968.1U CN212287536U (en) | 2020-05-18 | 2020-05-18 | Positioning device for processing composite material component of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020821968.1U CN212287536U (en) | 2020-05-18 | 2020-05-18 | Positioning device for processing composite material component of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212287536U true CN212287536U (en) | 2021-01-05 |
Family
ID=73968655
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020821968.1U Expired - Fee Related CN212287536U (en) | 2020-05-18 | 2020-05-18 | Positioning device for processing composite material component of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212287536U (en) |
-
2020
- 2020-05-18 CN CN202020821968.1U patent/CN212287536U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210105 |