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A kind of forging process method of tc18 titanium alloy large-scale bundled bearing forgings

A technology of TC18 and process method, which is applied in the direction of manufacturing tools, metal processing equipment, forging/pressing/hammer devices, etc. It can solve the problems of high design index requirements, difficulty in ensuring the uniformity of bar structure, and large deformation resistance in the two-phase area.

Active Publication Date: 2021-11-02
天津航天长征技术装备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The phase transition point of TC18 titanium alloy is low, the deformation resistance in the two-phase area is large, the forgeability of large-sized billets is relatively difficult, and the uniformity of the bar structure is not easy to ensure. , the weight of the intermediate billet is nearly 2 tons, which intensifies the difficulty of controlling the uniformity of the billet during the preparation process
Due to the complex shape of forgings, many edges and corners, and poor filling performance of titanium alloy, there are problems of poor filling or even missing corners in some positions during hot die forging
In addition, the product design index requirements are high, and the longitudinal mechanical properties require Rm≥1080MPa, Rp0.2≥1010MPa, A≥8%, Z≥20%, aKU≥25J / cm2, and its low-magnification structure and high-magnification structure must meet GJB2744A- Organizational rating requirements in 2007, there are certain technical challenges for oversized forgings of bundled supports

Method used

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  • A kind of forging process method of tc18 titanium alloy large-scale bundled bearing forgings
  • A kind of forging process method of tc18 titanium alloy large-scale bundled bearing forgings
  • A kind of forging process method of tc18 titanium alloy large-scale bundled bearing forgings

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Embodiment 1

[0044] Taking the heavy-duty launch vehicle TC18 bundled support forging product as an example, the size specification is 1210mm×1260mm×550mm.

[0045] Step (1): Multi-fire forging billet

[0046] (1) Ingot billet forging: place a TC18 titanium alloy round ingot with a size of Φ650×1500mm in a high-temperature electric furnace and heat it to 1100-1200°C, and after a certain period of time, carry out upsetting and elongation deformation on a forging press The amount of single upsetting and elongating deformation is controlled at 40% to 50%;

[0047] (2) Multi-fire reversing upsetting deformation: The phase transition point of the ingot is measured to be 860°C. Alternate multi-fire reversing upsetting deformation is carried out above the phase transition point and below the phase transition point. The initial forging temperature of the billet heating temperature for phase zone forging is controlled at 900-1100°C, and the initial forging temperature of two-phase zone forging bel...

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Abstract

A forging process method for a TC18 titanium alloy large-scale bundled support forging, the steps of which are: (1) multi-fire forging to make a billet: (1) ingot forging; (2) multi-fire reversing upsetting deformation; ( 3) Bar forging; (4) Blank preparation; (2) Hot die forging: (1) Die preheating; (2) Forging main body forming; (3) Forging forming optimization; (3) Forging heat treatment and detection analysis: (1) Machining before heat treatment; (2) Double annealing heat treatment; (3) Detection and analysis. The multi-fire forging of the invention increases the forgeability and uniformity of the structure of the intermediate blank, and the quasi-beta hot die forging obtains a relatively ideal basket structure and excellent comprehensive performance of the TC18 titanium alloy.

Description

technical field [0001] The invention relates to the technical field of thermal processing and forming, in particular to a forging process method of a TC18 titanium alloy large binding support forging. Background technique [0002] my country's aerospace model products are developing in the direction of large-scale, the requirements for lightweight structures are getting higher and higher, and the requirements for materials are constantly improving. The binding support is a key load-bearing component in the rocket body structure. It is used to connect the rocket core stage and the booster. In the early days, the binding support was mostly made of high-strength steel alloy. As the demand for rocket weight reduction becomes more and more urgent, it has gradually been adopted in recent years. High-strength titanium alloy replaces high-strength steel materials. The nominal chemical composition of TC18 titanium alloy is Ti-5Al-5Mo-5V-1Cr-1Fe, which is a α-β type two-phase titaniu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21J5/02B21J5/06B21J5/08B21K29/00
CPCB21J5/02B21J5/06B21J5/08B21K29/00
Inventor 张曼曼王恒强张文学魏瑞刚姚梦刘浩付敏敏宫成呼啸白景彬黄德超汪永阳
Owner 天津航天长征技术装备有限公司
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