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Pre-pressing mold for 2014 aluminum alloy aviation precision wheel hub die forging

A technology for aluminum alloy and die forgings, which is applied in the field of aerospace precision wheel die forgings, can solve the problems of difficult size control and uniformity control of structure and performance, and achieve reasonable filling sequence, reasonable metal flow and improved product quality. Effect

Pending Publication Date: 2020-01-17
SOUTHWEST ALUMINUM GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, the biggest difficulty of hub die forgings is the difficulty of size control and the difficulty of controlling the uniformity of structure and performance

Method used

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  • Pre-pressing mold for 2014 aluminum alloy aviation precision wheel hub die forging
  • Pre-pressing mold for 2014 aluminum alloy aviation precision wheel hub die forging
  • Pre-pressing mold for 2014 aluminum alloy aviation precision wheel hub die forging

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Embodiment Construction

[0032] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0033] Please refer to Figure 3 to Figure 4 , image 3 Schematic diagram of the side view structure of the pre-press die for the 2014 aluminum alloy aviation precision hub die forging provided for the embodiment of the present invention; Figure 4 A schematic cross-sectional structure diagram of a pre-press die for a 2014 aluminum alloy av...

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Abstract

The invention discloses a pre-pressing mold for a 2014 aluminum alloy aviation precision wheel hub die forging. The pre-pressing mold comprises an upper mold and a lower mold, wherein a first groove is formed in the end face of a first protrusion of the upper mold, a second groove is formed in the middle of the first groove, a third protrusion is arranged in the second groove, a first annular gapis formed between the third protrusion and the wall surface of the second groove, a fourth groove for forming a lug embryonic form is arranged on the first protrusion, a mold cavity is arranged on thelower mold, a second protrusion is arranged on the bottom of the mold cavity, a first annular groove and a second annular groove are arranged on the lower mold and surround the mold cavity from the inner part to the outer part, the first annular groove communicates with the mold cavity, the second annular groove communicates with one of the annular grooves, a third groove is formed in the middleof the bottom of the mold cavity, a fifth protrusion is arranged in the third groove, and a second annular gap is formed between the fifth protrusion and the wall surface of the third groove. When thestructure shape of the pre-pressing mold for the 2014 aluminum alloy aviation precision wheel hub die forging enables a pre-pressing piece to be formed, the flowing and filling sequence of metal arereasonable, and thus the product quality is improved.

Description

technical field [0001] The invention relates to the technical field of manufacturing aviation precision wheel hub die forgings, in particular to a pre-pressing mold for 2014 aluminum alloy aviation precision wheel hub die forgings. Background technique [0002] There is a typical specification forging on a large aircraft, which is the largest forging in the high-strength 2014 aluminum alloy aviation precision hub die forging: half wheel (cabin inner) die forging. The half-wheel (cabin inner side) die forging is a precision die forging, which is a disc type die forging. The maximum outer hub size of the part is φ593.3×309.1mm mm, and the maximum outer contour size of the die forging is φ616.5×314.2mm. [0003] Parts inside the half wheel well such as figure 1 and figure 2 as shown, figure 1 The first side view structural schematic diagram of the 2014 aluminum alloy aviation precision hub die forging provided for the embodiment of the present invention; figure 2 The seco...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21J13/02B21J1/04B21K1/40
CPCB21J1/04B21J13/02B21K1/40
Inventor 陈丽芳吴道祥王正安林海涛曾庆华付笑笑
Owner SOUTHWEST ALUMINUM GRP
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