CN105107954A - End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications - Google Patents

End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications Download PDF

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Publication number
CN105107954A
CN105107954A CN201510580578.3A CN201510580578A CN105107954A CN 105107954 A CN105107954 A CN 105107954A CN 201510580578 A CN201510580578 A CN 201510580578A CN 105107954 A CN105107954 A CN 105107954A
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CN
China
Prior art keywords
counterdie
punch press
flat
face
nose pliers
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
Application number
CN201510580578.3A
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Chinese (zh)
Inventor
张伟强
郑伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang Aircraft Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN201510580578.3A priority Critical patent/CN105107954A/en
Publication of CN105107954A publication Critical patent/CN105107954A/en
Pending legal-status Critical Current

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Abstract

The invention relates to an end partial subsidence forming mold for an aluminum alloy L-shaped angle section part and applications thereof. An upper mold body and a lower mold body which are of a split structure are adopted, and the lower end face of the upper mold body and the upper end face of the lower mold body are fold line end faces of a complementary structure. A baffle is arranged on the side end face of the lower mold body and corresponds to the side end face of the lower mold body in shape, and locating pins are arranged on the baffle. A clamping and locating process is used for inspecting processing of the mold, the geometric shape and the size precision of the part can be guaranteed, the processing cost is low, the efficiency is high, and the end partial subsidence forming mold is suitable for small batch production of airplane parts.

Description

The sagging shaping dies in local, aluminium alloy L shape angle section part termination and application
Technical field
The present invention relates to the sagging shaping dies in local, a kind of aluminium alloy L shape angle section part termination and application, belong to mechanical aviation manufacture field.
Background technology
Aircraft machine aluminium alloy L shape angle section part is aircraft common part, and shape mostly is arc, and part termination, with sinking, needs to form the final accessory size of guarantee part by partial operation.
Summary of the invention
The technical problem to be solved in the present invention is to provide the sagging shaping dies in local, a kind of aluminium alloy L shape angle section part termination and application, realizes local, L shape angle section part termination and sink shaping accurately, meet Element Design and instructions for use.
For overcoming the above problems, concrete technical scheme of the present invention is as follows: sink local, a kind of aluminium alloy L shape angle section part termination shaping dies, the upper die and lower die of split-type structural, patrix lower surface and counterdie upper surface are the broken line end face in complementary structure, the side end face of counterdie is provided with baffle plate, baffle shapes is corresponding with counterdie side end face shape, and baffle plate is provided with alignment pin.
Utilize an application for the sagging shaping dies in local, aluminium alloy L shape angle section part termination, comprise the steps:
1) sagging finishing die is carried out on punch press installation to fix, counterdie and baffle plate flat-nose pliers are fixed on punch press, adjustment punch press and flat-nose pliers position, upper die and lower die and baffle plate die-closed position correct;
2) open punch press patrix is risen, flat-nose pliers is unclamped counterdie and flapper gap are strengthened;
3) press alignment pin and location, counterdie side at the hand-held part in punch press side, part is installed on mould, flat-nose pliers clamping is ensured that parts fixation is firm simultaneously;
6) opening punch press makes patrix decline, and carries out stamping processing, and patrix arrives after minimum point completes punching press and rises;
7) unclamp flat-nose pliers, side shield and counterdie are separated, take out part;
8) part after shaping is tested, after confirming that part is qualified, repeat stamping step, realize processing new part.
The beneficial effect that the present invention brings is: to be sunk to aluminium alloy L shape part termination by the mould of split-type structural and process for stamping and process, geometry and the dimensional accuracy of part can be ensured, processing cost is low, and efficiency is high, is applicable to airplane parts small lot batch manufacture.
Accompanying drawing explanation
Fig. 1 is the structural representation of the sagging shaping dies in local, aluminium alloy L shape angle section part termination.
Fig. 2 is the A-A sectional view of Fig. 1.
Wherein, 1-patrix, 2-counterdie, 3-baffle plate, 4-alignment pin.
Detailed description of the invention
As depicted in figs. 1 and 2, sink local, a kind of aluminium alloy L shape angle section part termination shaping dies, the patrix 1 of split-type structural and counterdie 2, patrix 1 lower surface and counterdie 2 upper surface are the broken line end face in complementary structure, the side end face of counterdie 2 is provided with baffle plate 3, baffle plate 3 shape is corresponding with counterdie 2 side end face shape, and baffle plate is provided with alignment pin.
Utilize an application for the sagging shaping dies in local, aluminium alloy L shape angle section part termination, comprise the steps:
1) sagging finishing die is carried out on punch press installation to fix, counterdie 2 and baffle plate 3 are fixed on punch press with flat-nose pliers, adjustment punch press and flat-nose pliers position, and patrix 1, counterdie 2 and baffle plate 3 die-closed position are correct;
2) open punch press patrix 1 is risen, flat-nose pliers is unclamped counterdie 2 and baffle plate 3 gap are strengthened;
3) press alignment pin and location, counterdie 2 side at the hand-held part in punch press side, part is installed on mould, flat-nose pliers clamping is ensured that parts fixation is firm simultaneously;
6) opening punch press makes patrix 1 decline, and carry out stamping processing, patrix 1 arrives after minimum point completes punching press and rises;
7) unclamp flat-nose pliers, side shield 3 and counterdie 2 are separated, take out part;
8) part after shaping is tested, after confirming that part is qualified, repeat stamping step, realize processing new part.
Above-described is only the preferred embodiments of the present invention.It should be pointed out that for the person of ordinary skill of the art, under the premise without departing from the principles of the invention, some modification and improvement can also be made, also should be considered as belonging to protection scope of the present invention.

Claims (2)

1. the sagging shaping dies in local, an aluminium alloy L shape angle section part termination, it is characterized in that: the upper die and lower die of split-type structural, patrix lower surface and counterdie upper surface are the broken line end face in complementary structure, the side end face of counterdie is provided with baffle plate, baffle shapes is corresponding with counterdie side end face shape, and baffle plate is provided with alignment pin.
2. utilize an application for the sagging shaping dies in local, aluminium alloy L shape angle section part termination described in claim 1, it is characterized in that, comprise the steps:
1) sagging finishing die is carried out on punch press installation to fix, counterdie and baffle plate flat-nose pliers are fixed on punch press, adjustment punch press and flat-nose pliers position, upper die and lower die and baffle plate die-closed position correct;
2) open punch press patrix is risen, flat-nose pliers is unclamped counterdie and flapper gap are strengthened;
3) press alignment pin and location, counterdie side at the hand-held part in punch press side, part is installed on mould, flat-nose pliers clamping is ensured that parts fixation is firm simultaneously;
4) opening punch press makes patrix decline, and carries out stamping processing, and patrix arrives after minimum point completes punching press and rises;
5) unclamp flat-nose pliers, side shield and counterdie are separated, take out part;
6) part after shaping is tested, after confirming that part is qualified, repeat stamping step, realize processing new part.
CN201510580578.3A 2015-09-14 2015-09-14 End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications Pending CN105107954A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510580578.3A CN105107954A (en) 2015-09-14 2015-09-14 End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510580578.3A CN105107954A (en) 2015-09-14 2015-09-14 End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications

Publications (1)

Publication Number Publication Date
CN105107954A true CN105107954A (en) 2015-12-02

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510580578.3A Pending CN105107954A (en) 2015-09-14 2015-09-14 End partial subsidence forming mold for aluminum alloy L-shaped angle section part and applications

Country Status (1)

Country Link
CN (1) CN105107954A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108704976A (en) * 2018-05-03 2018-10-26 合肥江航飞机装备有限公司 A kind of processing method of sagging part
CN110153289A (en) * 2019-06-06 2019-08-23 西北工业大学 A kind of sagging mold of support-adjustable flexibility

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0919721A (en) * 1995-07-07 1997-01-21 Aiko Kk Press device for bending shapes
US6178799B1 (en) * 1999-10-12 2001-01-30 The Boeing Company Forming press and method for shaping angle-section workpieces
CN103157723A (en) * 2011-12-16 2013-06-19 上海外高桥造船有限公司 Angle steel support bending pressed film
CN204338715U (en) * 2014-12-25 2015-05-20 重庆重型汽车集团专用汽车有限责任公司 A kind of angle steel six degree of bending moulds
CN204503994U (en) * 2015-04-09 2015-07-29 哈尔滨建成集团有限公司 A kind of particular manufacturing craft angle steel being bent to U-shaped

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0919721A (en) * 1995-07-07 1997-01-21 Aiko Kk Press device for bending shapes
US6178799B1 (en) * 1999-10-12 2001-01-30 The Boeing Company Forming press and method for shaping angle-section workpieces
CN103157723A (en) * 2011-12-16 2013-06-19 上海外高桥造船有限公司 Angle steel support bending pressed film
CN204338715U (en) * 2014-12-25 2015-05-20 重庆重型汽车集团专用汽车有限责任公司 A kind of angle steel six degree of bending moulds
CN204503994U (en) * 2015-04-09 2015-07-29 哈尔滨建成集团有限公司 A kind of particular manufacturing craft angle steel being bent to U-shaped

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108704976A (en) * 2018-05-03 2018-10-26 合肥江航飞机装备有限公司 A kind of processing method of sagging part
CN110153289A (en) * 2019-06-06 2019-08-23 西北工业大学 A kind of sagging mold of support-adjustable flexibility

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Application publication date: 20151202

RJ01 Rejection of invention patent application after publication