CN106270177A - FT15 missile launcher front fairing drawing die - Google Patents
FT15 missile launcher front fairing drawing die Download PDFInfo
- Publication number
- CN106270177A CN106270177A CN201510282776.1A CN201510282776A CN106270177A CN 106270177 A CN106270177 A CN 106270177A CN 201510282776 A CN201510282776 A CN 201510282776A CN 106270177 A CN106270177 A CN 106270177A
- Authority
- CN
- China
- Prior art keywords
- die
- pressing plate
- annular pressing
- bolster
- pair guide
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
FT15 missile launcher front fairing drawing die includes upper bolster (1), die shoe (2), upper padding plate (3), lower bolster (4), upper die and lower die, upper mold includes annular pressing plate (5) and punch (6), lower mold includes die and lower annular pressing plate (7), mould structure design is reasonable, use stability and high efficiency, design size precision is guaranteed, and front fairing outer surface roughness meets design requirement.
Description
Technical field
The present invention relates to missile launcher and produce apparatus field, be specifically related to FT15 missile launcher front fairing drawing die.
Background technology
Missile launcher front fairing is thin wall special-shaped part due to it, and its design size and overall dimensions require extremely strict, then use punching stretch forming, thus need the drawing die of a stability and high efficiency that it is carried out drawing and forming.
Summary of the invention
The purpose of the present invention is aiming at above-mentioned requirement, and provides FT15 missile launcher front fairing drawing die.
The present invention includes upper bolster, die shoe, upper padding plate, lower bolster, upper die and lower die, it is respectively equipped with bearing on upper bolster and die shoe, upper padding plate and lower bolster are mounted by means of bolts on upper bolster and die shoe respectively, upper mold includes annular pressing plate and punch, the outer loop-shaped of punch matches with the interior loop-shaped of upper annular pressing plate, upper annular pressing plate and punch are mounted by means of bolts on upper padding plate respectively, lower mold includes die and lower annular pressing plate, die includes die base plate, left concave template and right concave template, die base plate and lower annular pressing plate are mounted by means of bolts on lower bolster respectively, left concave template and right concave template are mounted by means of bolts on die base plate respectively, and the outer loop-shaped of die matches with the interior loop-shaped of lower annular pressing plate.
It also has a pair guide pillar and a pair guide pin bushing, a pair guide pillar and a pair guide pin bushing to be respectively and fixedly installed on upper bolster and die shoe, and a pair guide pillar lays respectively in a pair guide pin bushing inner ring.
The method have the advantages that: mould structure design is reasonable, using stability and high efficiency, design size precision is guaranteed, and front fairing outer surface roughness meets design requirement.
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram.
Fig. 2 is cavity die structure schematic diagram of the present invention.
Detailed description of the invention
nullSuch as Fig. 1、Shown in 2，The present invention includes upper bolster 1、Die shoe 2、Upper padding plate 3、Lower bolster 4、Upper die and lower die，It is respectively equipped with bearing on upper bolster 1 and die shoe 2，Upper padding plate 3 and lower bolster 4 are mounted by means of bolts on upper bolster 1 and die shoe 2 respectively，Upper mold includes annular pressing plate 5 and punch 6，The outer loop-shaped of punch 6 matches with the interior loop-shaped of upper annular pressing plate 5，Upper annular pressing plate 5 and punch 6 are mounted by means of bolts on upper padding plate 3 respectively，Lower mold includes die and lower annular pressing plate 7，Die includes die base plate 8、Left concave template 9 and right concave template 10，Die base plate 8 and lower annular pressing plate 7 are mounted by means of bolts on lower bolster 4 respectively，Left concave template 9 and right concave template 10 are mounted by means of bolts on die base plate 8 respectively，And the outer loop-shaped of die matches with the interior loop-shaped of lower annular pressing plate 7.
It also has a pair guide pillar 11 and a pair guide pin bushing 12, a pair guide pillar 11 and a pair guide pin bushing 12 to be respectively and fixedly installed on upper bolster 1 and die shoe 2, and a pair guide pillar 11 lays respectively in a pair guide pin bushing 12 inner ring.
Working method: respectively upper bolster 1 and die shoe 2 are fixedly installed on forcing press, stretched blank part first passes through diel punching press out, blank is positioned on recessed annular pressing plate 7 at correct position, start forcing press, upper bolster 1 is pressed down against blank with punch 6, after punch 6 and die are mutually twisted completely, blank between punch 6 and die has just been drawn into design shape, after start forcing press by upper bolster 1 pull-up, take out tensioning member, i.e. complete the drawing and forming of front fairing.
Claims (2)
- null1. FT15 missile launcher front fairing drawing die，It is characterized in that it includes upper bolster (1)、Die shoe (2)、Upper padding plate (3)、Lower bolster (4)、Upper die and lower die，It is respectively equipped with bearing on upper bolster (1) and die shoe (2)，Upper padding plate (3) and lower bolster (4) are mounted by means of bolts on upper bolster (1) and die shoe (2) respectively，Upper mold includes annular pressing plate (5) and punch (6)，The outer loop-shaped of punch (6) matches with the interior loop-shaped of upper annular pressing plate (5)，Upper annular pressing plate (5) and punch (6) are mounted by means of bolts on upper padding plate (3) respectively，Lower mold includes die and lower annular pressing plate (7)，Die includes die base plate (8)、Left concave template (9) and right concave template (10)，Die base plate (8) and lower annular pressing plate (7) are mounted by means of bolts on lower bolster (4) respectively，Left concave template (9) and right concave template (10) are mounted by means of bolts on die base plate (8) respectively，And the outer loop-shaped of die matches with the interior loop-shaped of lower annular pressing plate (7).
- FT15 missile launcher front fairing drawing die the most according to claim 1, it is characterized in that it also has a pair guide pillar (11) and a pair guide pin bushing (12), a pair guide pillar (11) and a pair guide pin bushing (12) are respectively and fixedly installed on upper bolster (1) and die shoe (2), and a pair guide pillar (11) lays respectively in a pair guide pin bushing (12) inner ring respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282776.1A CN106270177A (en) | 2015-05-29 | 2015-05-29 | FT15 missile launcher front fairing drawing die |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282776.1A CN106270177A (en) | 2015-05-29 | 2015-05-29 | FT15 missile launcher front fairing drawing die |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106270177A true CN106270177A (en) | 2017-01-04 |
Family
ID=57634993
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510282776.1A Pending CN106270177A (en) | 2015-05-29 | 2015-05-29 | FT15 missile launcher front fairing drawing die |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106270177A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108080509A (en) * | 2017-12-08 | 2018-05-29 | 四川航天长征装备制造有限公司 | Drop hammer die cavity plate backing plate and application process |
| CN112405791A (en) * | 2020-09-29 | 2021-02-26 | 天津津航技术物理研究所 | Forming die and forming method for biscuit of hyper-hemispherical ceramic fairing |
-
2015
- 2015-05-29 CN CN201510282776.1A patent/CN106270177A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108080509A (en) * | 2017-12-08 | 2018-05-29 | 四川航天长征装备制造有限公司 | Drop hammer die cavity plate backing plate and application process |
| CN112405791A (en) * | 2020-09-29 | 2021-02-26 | 天津津航技术物理研究所 | Forming die and forming method for biscuit of hyper-hemispherical ceramic fairing |
| CN112405791B (en) * | 2020-09-29 | 2021-10-15 | 天津津航技术物理研究所 | Forming die and forming method for biscuit of hyper-hemispherical ceramic fairing |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202779417U (en) | Composite die with upper punch die | |
| JP2014133260A5 (en) | ||
| MX2018010165A (en) | Molded material production method and molded material. | |
| MX2018010129A (en) | Molded material production method and molded material. | |
| MX2018015788A (en) | Blade mould for manufacturing a blade shell part of a wind turbine blade and related method. | |
| MX2018009039A (en) | Press apparatus, and production method for press-molded article. | |
| CN103949539A (en) | Window punching process for clutch gland | |
| CN204867056U (en) | A stamping die for bend for disposable 120 degrees | |
| CN204135174U (en) | A kind of aluminum cylindrical member partial thickening blanking mold | |
| CN106270177A (en) | FT15 missile launcher front fairing drawing die | |
| CN203002943U (en) | Right-handed compound die | |
| CN204747250U (en) | Tensile mould of radome fairing before FT15 missile launcher | |
| CN203764798U (en) | Engineering mould for automated mechanical line-connecting production engineer of vacuum booster housings | |
| CN204584061U (en) | A kind of automobile exhaust pipe end cone drawing die | |
| CN203737742U (en) | Cold extrusion die device for shank gear | |
| CN203417990U (en) | Thin-plate metal part swaging and edge trimming composite forming die | |
| CN203155838U (en) | Blanking and drawing combined continuous stamping die | |
| CN104889238A (en) | Deep drawing shaft sleeve forming process | |
| CN204052614U (en) | A kind of brake(-holder) block press-moulding die | |
| CN103658485A (en) | Valve core forging die | |
| CN205732524U (en) | For the drift that automobile formwork parts piercing and flanging is once-forming | |
| CN104475583A (en) | Necking die for pipe | |
| CN205096346U (en) | Circular stamping die | |
| CN203955905U (en) | A kind of diel that is provided with suspension link flange punch mechanism | |
| CN109967610A (en) | A kind of car roof stiffening plate composable mold |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170104 |
|
| WD01 | Invention patent application deemed withdrawn after publication |