Large titanium alloy blade upsetting blank manufacture mold with heads on two ends, and blank manufacture method thereof

A technology for titanium alloy and blades, which is applied to large-scale titanium alloy blade top forging billet molds and the field of billet making. Gather instability and fold burrs to ensure the effect of stability and reliability

Active Publication Date: 2020-09-18
AECC AERO SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a large-scale titanium alloy blade head forging billet mold and its billet making method with two ends, so as to solve the problem that the existing billet dies cannot meet the batch production requirements and the quality of the finished billet is poor

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  • Large titanium alloy blade upsetting blank manufacture mold with heads on two ends, and blank manufacture method thereof
  • Large titanium alloy blade upsetting blank manufacture mold with heads on two ends, and blank manufacture method thereof
  • Large titanium alloy blade upsetting blank manufacture mold with heads on two ends, and blank manufacture method thereof

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Embodiment Construction

[0056] The principles and features of the present invention are described below in conjunction with the accompanying drawings, and examples are only used to explain the present invention, and are not intended to limit the scope of the present invention.

[0057] Such as Figure 1 to Figure 2 As shown, a large-scale titanium alloy blade with heads at both ends is an upset blank die, including a large-end gathering forming mechanism and a small-end gathering forming mechanism. The large-end gathering forming mechanism is used for the forming operation of the large end of the blank, and the small-end gathering forming mechanism is used for the forming operation of the small end of the blank.

[0058] The bulk gathering and forming mechanism includes a bulk back gauge 1 and a bulk first gathering module 2, a bulk secondary gathering module 3, a bulk tertiary gathering module 4 and a bulk Forming module 5. Through the structure of three gathering modules and one forming module, t...

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Abstract

The invention discloses a large titanium alloy blade upsetting blank manufacture mold with heads on two ends. The mold comprises a large head gathering and shaping mechanism and a small head gatheringand shaping mechanism, wherein the large head gathering and shaping mechanism comprises a large head backward blocking base as well as a first large head gathering module, a second large head gathering module, a third large head gathering module and a large head shaping module which are successively disposed on the large head backward blocking base from top to bottom; and the small head gatheringand sharing mechanism comprises a small head backward blocking base as well as a first small head gather module, a second small head gathering module and a small head shaping module which are successively disposed on the small head backward blocking base from top to bottom. Through design of a specific three gatherings + one integration processing structure for a blank large head end, and designof a specific two gatherings + one shaping processing structure for a small head end, blade end shaping blank manufacture is realized. With the more exquisite gathering processing structure, occurrence of defects such as gathering instability and burr folding caused by excessive deformation can be avoided effectively, and batched production demands can be satisfied reliably.

Description

technical field [0001] The invention relates to the technical field of titanium alloy blade upsetting billet making, in particular to a large titanium alloy blade upsetting die with heads at both ends and a billet making method thereof. Background technique [0002] Titanium alloy is a new type of metal structure material developed after World War II. Its main features are small specific gravity and high strength, so it has high specific strength, good heat resistance and corrosion resistance, and is widely used in the aviation industry. However, the deformation resistance of titanium alloy is large, the forging interval is narrow, and it is sensitive to the change of process parameters such as forging speed and deformation amount. A certain type of engine has a large titanium alloy blade with two heads at both ends. The ends are large, the blade body is wide, long and thin, and the cross-sectional area of ​​the axis varies greatly. It is difficult to realize the blanking of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21J13/02B21K3/04
CPCB21J13/02B21K3/04
Inventor 姜仕林袁本福
Owner AECC AERO SCI & TECH CO LTD
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