CN203652103U - Die forging structure of titanium alloy rocker arm - Google Patents

Die forging structure of titanium alloy rocker arm Download PDF

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Publication number
CN203652103U
CN203652103U CN201320797841.0U CN201320797841U CN203652103U CN 203652103 U CN203652103 U CN 203652103U CN 201320797841 U CN201320797841 U CN 201320797841U CN 203652103 U CN203652103 U CN 203652103U
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China
Prior art keywords
forging
titanium alloy
die forging
forge piece
die
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Expired - Lifetime
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CN201320797841.0U
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Chinese (zh)
Inventor
陈瑞钢
洪鑫
崔慧然
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Wuxi Turbine Blade Co Ltd
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Wuxi Turbine Blade Co Ltd
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Priority to CN201320797841.0U priority Critical patent/CN203652103U/en
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Abstract

The utility model provides a die forging structure of a titanium alloy rocker arm, which solves the problem that two high tendons of a forge piece are likely to collapse at corners during die forging with an existing die forging structure, and has the advantages that the die forging technical flow is effectively shortened and the production efficiency is improved. The structure comprises a forge piece body, wherein the upper and lower molded surfaces of the forge piece body are symmetrical and high tendons are arranged on the longitudinal sides of the upper and lower molded surfaces. The structure is characterized in that the parting surface of the forge piece body is located below the symmetrical central line of the upper and lower faces of the forge piece body.

Description

A kind of titanium alloy rocking arm die-forged part structure
Technical field
The utility model relates to the structure design field of die-forged part, especially relates to the structure design field of titanium alloy die forging part, is specially a kind of titanium alloy rocking arm die-forged part structure.
Background technology
A kind of titanium alloy rocker component for aircraft system, its appearance profile is of a size of 396mm × 206mm × 140mm(length × wide × height), structure is shown in Fig. 1, the principal feature of this member is that the height to width ratio of two sides side plate 1 is 8:1, belong to complex structural member, and its material is TC4 titanium alloy, belongs to difficult-to-deformation material.The common forging structure of this member is shown in Fig. 2 and Fig. 3, on the Joint face of a pattern 5 and forging of its forging 4, symmetrical center line 11 below overlaps, this forging carries out die forging on 180MN flypress, forming speed is 50mm/sec, in die forging process, often there will be following problem: when (1) carries out titanium alloy product production on flypress, blank and counterdie are long contact time, temperature drop is very fast, therefore counterdie metal flow difficulty in production process, counterdie die cavity is difficult for filling, thereby cause the high muscle 2 of the structural twice of forging, 3 fill difficulty at die forging process, easily produce the angle of collapsing, (2) in contour forging technique, for solving the angle problem of collapsing of the high muscle of above-mentioned twice, Forging Technology adopts the be shaped mode of twice die forging of preforming and finish-forging, and its production efficiency is low.In Fig. 3,6 patrixes that are forging die, 7 counterdies that are forging die, H0 is the height of the high muscle 2,3 of forging, and H is forging thickness, and h is the height between forging body Joint face of a pattern and forging lower plane A.
Summary of the invention
For the problems referred to above, the utility model provides a kind of titanium alloy rocking arm die-forged part structure, it can solve the high muscle of twice that adopts the die forging of existing forging structure to add forging in man-hour and easily produce the problem at angle of collapsing, thereby effectively shortens contour forging technique flow process, enhances productivity.
Its technical scheme is such, it comprises forging body, the upper and lower profile symmetry of described forging body, the upper and lower profile of described forging longitudinally both sides is respectively arranged with high muscle, it is characterized in that: the Joint face of a pattern of described forging body is positioned at the below of the symmetrical center line of described forging body above and below.
It is further characterized in that: the height h of described forging body Joint face of a pattern and described forging lower plane is 0.2 times ~ 0.4 times of described forging thickness H.
The utility model titanium alloy rocking arm die-forged part structure, the more existing forging structure of its forging body Joint face of a pattern Joint face of a pattern moves down, be conducive to the high muscle of counterdie position cavity filling, and the height h that controls forging body Joint face of a pattern and described forging lower plane is 0.2 times ~ 0.4 times of described forging thickness H, thereby can reduce the temperature drop that reduces forging contact time of forging and forging die counterdie, thereby reduce the impact of temperature drop on forging tissue in die forging process, further guarantee the cavity filling of the high muscle of forging counterdie position, forging can put in place at a fire time internal shaping, thereby it is inferior to have reduced the fire that is shaped, improve capacity utilization rate, effectively improve production efficiency.
Accompanying drawing explanation
Fig. 1 is the titanium alloy rocking arm product schematic diagram after the utility model forging process;
Fig. 2 is the conventional forging structural representation of Fig. 1 product;
Fig. 3 is the Joint face of a pattern schematic diagram of Fig. 2 forging;
Fig. 4 is the utility model forging structural representation;
Fig. 5 is the Joint face of a pattern schematic diagram of the utility model forging.
The specific embodiment
See Fig. 4 and Fig. 5, the utility model forging structure comprises forging body 8, the upper and lower profile symmetry of forging body 8, the upper and lower profile of forging longitudinally both sides is respectively arranged with high muscle 9, the Joint face of a pattern 10 of forging body is positioned at the below of the symmetrical center line 11 of forging body above and below, and the height h of forging body Joint face of a pattern 10 and forging lower plane A is 0.2 times ~ 0.4 times of forging thickness H.In Fig. 5,12 is the patrix of the utility model forging forging die, and 13 is counterdie.

Claims (2)

1. a titanium alloy rocking arm die-forged part structure, it comprises forging body, the upper and lower profile symmetry of described forging body, the upper and lower profile of described forging longitudinally both sides is respectively arranged with high muscle, it is characterized in that: the Joint face of a pattern of described forging body is positioned at the below of the symmetrical center line of described forging body above and below.
2. a kind of titanium alloy rocking arm die-forged part structure according to claim 1, is characterized in that: the height h of described forging body Joint face of a pattern and described forging lower plane is 0.2 times ~ 0.4 times of described forging thickness H.
CN201320797841.0U 2013-12-09 2013-12-09 Die forging structure of titanium alloy rocker arm Expired - Lifetime CN203652103U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320797841.0U CN203652103U (en) 2013-12-09 2013-12-09 Die forging structure of titanium alloy rocker arm

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320797841.0U CN203652103U (en) 2013-12-09 2013-12-09 Die forging structure of titanium alloy rocker arm

Publications (1)

Publication Number Publication Date
CN203652103U true CN203652103U (en) 2014-06-18

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320797841.0U Expired - Lifetime CN203652103U (en) 2013-12-09 2013-12-09 Die forging structure of titanium alloy rocker arm

Country Status (1)

Country Link
CN (1) CN203652103U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640691A (en) * 2013-12-09 2014-03-19 无锡透平叶片有限公司 Titanium alloy rocker die forging structure
CN112570564A (en) * 2020-12-11 2021-03-30 南通高扬电机有限公司 Stamping tool for motor special-shaped shaft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640691A (en) * 2013-12-09 2014-03-19 无锡透平叶片有限公司 Titanium alloy rocker die forging structure
CN112570564A (en) * 2020-12-11 2021-03-30 南通高扬电机有限公司 Stamping tool for motor special-shaped shaft

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GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20140618

CX01 Expiry of patent term