CN211219370U - Guided missile wing's fixed-position welding frock - Google Patents
Guided missile wing's fixed-position welding frock Download PDFInfo
- Publication number
- CN211219370U CN211219370U CN201921973486.1U CN201921973486U CN211219370U CN 211219370 U CN211219370 U CN 211219370U CN 201921973486 U CN201921973486 U CN 201921973486U CN 211219370 U CN211219370 U CN 211219370U
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- Prior art keywords
- pedestal
- positioning
- slide
- guided missile
- sliding
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- Expired - Fee Related
Links
- 238000003466 welding Methods 0.000 title claims abstract description 27
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 28
- 230000007246 mechanism Effects 0.000 claims abstract description 9
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a positioning welding tool for guided missile wing panels, which comprises a pedestal, wherein a positioning cavity for positioning welding of the wing panels is arranged on the table top of the pedestal along the axis direction, and a plurality of groups of fixing mechanisms capable of fixing the wing panels in the positioning cavity are arranged at intervals on the table top of the pedestal; each group of fixing mechanisms comprises two fastening components which are symmetrically arranged along the axis of the pedestal, the table top of the pedestal is provided with a plurality of sliding chutes which are communicated with the positioning cavity and symmetrically arranged along the axis of the pedestal, and each sliding chute is in one-to-one corresponding sliding fit with the fastening components; fastening components includes the slide, and the slide is located the spout, and one side face threaded connection of slide towards the location chamber has the bolt, and the one end that the location chamber was kept away from to the slide is equipped with the fixed plate, and the face threaded connection of fixed plate has the screw rod. This guided missile fin's fixed-position welding frock carries out the fixed-position fast to the web and the gusset of fin and presss from both sides tightly, realizes the quick fixed-position welding of fin, compares traditional manual positioning accuracy height, the simple operation.
Description
Technical Field
The utility model relates to a welding frock technical field specifically is a guided missile fin's fixed-position welding frock.
Background
In missile parts, missile wings play an important role in the flying of missiles. The welding of traditional guided missile fin adopts artifical fixed back spot welding, owing to adopt manual operation, is difficult for accurate location, leads to the fin processingquality not good, and workman's technical merit differs moreover, and the product differentiation is great, and machining efficiency is low, and it is inconvenient to use.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome current defect, provide a guided missile fin's fixed-position welding frock, carry out the fixed-position clamp fast to the web and the gusset of fin and press from both sides tightly, realize the quick fixed-position welding of fin, it is high to compare the manual positioning accuracy of tradition, the simple operation can effectively solve the problem in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: a positioning welding tool for a wing piece of a missile comprises a pedestal, wherein a positioning cavity for positioning welding of the wing piece is formed in the table top of the pedestal along the axis direction, and a plurality of groups of fixing mechanisms capable of fixing the wing piece in the positioning cavity are arranged on the table top of the pedestal at intervals; each group of fixing mechanisms comprises two fastening components which are symmetrically arranged along the axis of the pedestal, the table top of the pedestal is provided with a plurality of sliding chutes which are communicated with the positioning cavity and symmetrically arranged along the axis of the pedestal, and each sliding chute is in one-to-one corresponding sliding fit with the fastening components;
fastening components includes the slide, and the slide is located the spout, and one side face threaded connection of slide orientation chamber has the bolt, and the one end that the chamber was kept away from to the slide is equipped with the fixed plate, and the face threaded connection of fixed plate has the screw rod, and the one end of screw rod is contradicted with the terminal surface of pedestal, and the other end of screw rod is equipped with the knob.
Preferably, the positioning cavity comprises a first rectangular groove and a second trapezoidal groove communicated with the first rectangular groove.
Preferably, the two opposite side surfaces of the sliding plate are respectively provided with a semicircular sliding part, and the two opposite side walls of the inner cavity of the sliding groove are provided with guide grooves matched with the sliding parts.
Preferably, four corners of the table board of the table seat are provided with mounting threaded holes.
Preferably, the bolt is a hexagon socket head cap screw.
Compared with the prior art, the beneficial effects of the utility model are that: this guided missile fin's fixed position welding frock, the location intracavity is arranged in to the web of fin, twists the knob and makes two fastening components relative movement of symmetry, and two fastening components centre gripping fix the gusset and make its perpendicular to web, then twist the bolt, and the bolt moves down and compresses tightly the web and be fixed in the location chamber end to the realization is tight to the location of web and gusset, then spot welding, realizes the quick tack welding of fin, compares traditional manual positioning accuracy height, the simple operation.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the present invention;
FIG. 3 is a schematic structural view of the fastening assembly of the present invention;
FIG. 4 is a schematic view of the slide plate and the chute of the present invention;
FIG. 5 is a schematic view of a missile wing.
In the figure: the device comprises a mounting threaded hole 1, a positioning cavity 2, a first rectangular groove 201, a second trapezoidal groove 202, a pedestal 3, a fastening assembly 4, a sliding plate 401, a bolt 402, a knob 403, a fixing plate 404, a screw 405 and a sliding groove 5.
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. 1-5, the present invention provides a technical solution: a guided missile wing piece positioning and welding tool comprises a pedestal 3, wherein mounting threaded holes 1 are formed in four corners of a table top of the pedestal 3, so that the fixed mounting is facilitated, a positioning cavity 2 for positioning and welding wing pieces is formed in the table top of the pedestal 3 along the axis direction, the positioning cavity 2 comprises a first rectangular groove 201 and a second trapezoidal groove 202 communicated with the first rectangular groove 201 and is used for placing the wing pieces, and a plurality of groups of fixing mechanisms capable of fixing the wing pieces in the positioning cavity 2 are arranged on the table top of the pedestal 3 at intervals; each group of fixing mechanisms comprises two fastening components 4 symmetrically arranged along the axis of the pedestal 3, the table top of the pedestal 3 is provided with a plurality of sliding grooves 5 communicated with the positioning cavity 2 and symmetrically arranged along the axis of the pedestal 3, each sliding groove 5 is in one-to-one corresponding sliding fit with the fastening components 4, and the two fastening components 4 which are arranged in sliding symmetry can clamp and fix the rib plate of the wing plate and can ensure that the rib plate is kept in a state of being perpendicular to the web plate;
the fastening assembly 4 comprises a sliding plate 401, the sliding plate 401 is located in a sliding chute 5, two opposite side surfaces of the sliding plate 401 are respectively provided with a semicircular sliding part, two opposite side walls of an inner cavity of the sliding chute 5 are provided with guide grooves matched with the sliding parts, one side surface of the sliding plate 401 facing a positioning cavity 2 is in threaded connection with a bolt 402, the bolt 402 is an inner hexagon bolt, the bolt 402 is screwed, a plurality of groups of bolts 402 move downwards and press a web plate at the bottom of the positioning cavity 2 to realize the positioning and pressing of the web plate, one end of the sliding plate 401 far away from the positioning cavity 2 is provided with a fixing plate 404, the surface of the fixing plate 404 is in threaded connection with a screw rod 405, one end of the screw rod 405 is abutted against the end surface of the pedestal 3, the other end of the screw rod 405 is provided with a knob 403, the screw rod 405 drives the sliding plate 401 to move by screwing the knob 403, the inner, realize the quick tack welding of fin, it is high to compare traditional manual positioning accuracy, the simple operation.
The working principle is as follows: when the wing plate fixing device is used, a web plate of a wing plate is placed in the positioning cavity 2, then a rib plate of the wing plate is placed perpendicular to the web plate, then the knob 403 is screwed, the knob 403 drives the screw rod 405 to rotate, the screw rod 405 drives the sliding plates 401 to move, the two symmetrical sliding plates 401 move relatively and clamp and fix the rib plate, then the bolt 402 is screwed, and the bolt 402 moves downwards to press the web plate, so that the web plate and the rib plate are fixed, and then spot welding positioning is performed.
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 (5)
1. The utility model provides a guided missile wing's fixed-position welding frock, includes pedestal (3), its characterized in that: the table-board of the table-board (3) is provided with a positioning cavity (2) for positioning and welding the fins along the axis direction, and the table-board of the table-board (3) is provided with a plurality of groups of fixing mechanisms at intervals, wherein the fixing mechanisms can fix the fins in the positioning cavity (2); each group of fixing mechanisms comprises two fastening components (4) symmetrically arranged along the axis of the pedestal (3), the table top of the pedestal (3) is provided with a plurality of sliding grooves (5) communicated with the positioning cavity (2) and symmetrically arranged along the axis of the pedestal (3), and each sliding groove (5) is in one-to-one corresponding sliding fit with the fastening components (4);
fastening components (4) include slide (401), slide (401) are located spout (5), and slide (401) have bolt (402) towards one side face threaded connection who fixes a position chamber (2), and the one end that fixes a position chamber (2) was kept away from in slide (401) is equipped with fixed plate (404), and the face threaded connection of fixed plate (404) has screw rod (405), and the one end of screw rod (405) is contradicted with the terminal surface of pedestal (3), and the other end of screw rod (405) is equipped with knob (403).
2. The guided missile wing positioning and welding tool as claimed in claim 1, wherein the tool comprises: the positioning cavity (2) comprises a first rectangular groove (201) and a second trapezoidal groove (202) communicated with the first rectangular groove (201).
3. The guided missile wing positioning and welding tool as claimed in claim 1, wherein the tool comprises: the two opposite side faces of the sliding plate (401) are respectively provided with a semicircular sliding part, and the two opposite side walls of the inner cavity of the sliding groove (5) are provided with guide grooves matched with the sliding parts.
4. The guided missile wing positioning and welding tool as claimed in claim 1, wherein the tool comprises: four corners of the table board of the table seat (3) are provided with mounting threaded holes (1).
5. The guided missile wing positioning and welding tool as claimed in claim 1, wherein the tool comprises: the bolt (402) is a hexagon socket head cap screw.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921973486.1U CN211219370U (en) | 2019-11-15 | 2019-11-15 | Guided missile wing's fixed-position welding frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921973486.1U CN211219370U (en) | 2019-11-15 | 2019-11-15 | Guided missile wing's fixed-position welding frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211219370U true CN211219370U (en) | 2020-08-11 |
Family
ID=71917500
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921973486.1U Expired - Fee Related CN211219370U (en) | 2019-11-15 | 2019-11-15 | Guided missile wing's fixed-position welding frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211219370U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117428680A (en) * | 2023-12-06 | 2024-01-23 | 丹阳丹金航空材料科技有限公司 | Missile wing mold processing |
-
2019
- 2019-11-15 CN CN201921973486.1U patent/CN211219370U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117428680A (en) * | 2023-12-06 | 2024-01-23 | 丹阳丹金航空材料科技有限公司 | Missile wing mold processing |
| CN117428680B (en) * | 2023-12-06 | 2024-06-04 | 丹阳丹金航空材料科技有限公司 | Missile wing mold processing |
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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: 20200811 |