Preparation method of high-temperature alloy four-layer lattice lightweight structure

A high-temperature alloy and lightweight technology, which is applied in metal processing equipment, welding equipment, manufacturing tools, etc., can solve the problems that it is difficult to fully utilize the high-strength and light-weight characteristics of the lattice structure, and achieve good mechanical properties and high welding rate. Effect

Active Publication Date: 2020-04-28
AEROSPACE HIWING HARBIN TITANIUM IND
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  • Abstract
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AI Technical Summary

Problems solved by technology

The introduction of the lattice structure will bring about a more significant weight reduction effect, but the current research on the lattice structure is limited to medium and thick plate materials due to the influence of material properties, and it is difficult to fully utilize the high-strength and light-weight characteristics of the lattice structure

Method used

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  • Preparation method of high-temperature alloy four-layer lattice lightweight structure
  • Preparation method of high-temperature alloy four-layer lattice lightweight structure
  • Preparation method of high-temperature alloy four-layer lattice lightweight structure

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Embodiment Construction

[0034] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0035] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0036] Such as Figure 1-Figure 4 As shown, a method for preparing a superalloy four-layer lattice lightweight structure comprises the following steps:

[0037] Step 1. Process the hollowed diamond grid structure of the middle laminate: use laser cutting or machining to process the GH4169 superalloy plate into a hollow diamond grid structure according to the design pattern; complete the hollow diamond grid structure of the middle laminate After the structure, use a belt machine or a white steel knife to remove the cutting burrs; the thickness of the middle laminate is 1mm;

[0038] Step 2. Process the skin panel: use laser cutting or machining to process the GH4169 superalloy plate int...

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Abstract

The invention provides a preparation method of a high-temperature alloy four-layer lattice lightweight structure. The preparation method comprises the steps of 1, machining hollowed-out rhombus grid structures of middle layer plates; 2, machining a skin panel; 3, removing surface oxidation films of the skin panel and the two middle layer plates through acid pickling, and cleaning acid, alkali andgreasy dirt remaining on the surface of the skin panel and the surfaces of the two middle layer plates through ethyl alcohol; 4, coating the plate surfaces of the two middle-layer plates with solder resist; 5, carrying out diffusion bonding of the skin panel and the middle layer plates; 6, performing superplastic forming; and 7, taking a formed prefabricated blank out of a superplastic forming mold, and machining the GH4169 high-temperature alloy four-layer lattice lightweight structure through a machining method. The four-layer ultrathin lattice structure rudder airfoil prepared through the method is made of GH4169 high-temperature alloy and has the advantages of good machinability and weldability, the ultrathin lattice structure has the advantage of light weight, and the four-layer rudder airfoil is high in degree of symmetry and better in mechanical property.

Description

technical field [0001] The invention belongs to the field of GH4169 superalloy structure forming, and in particular relates to a method for preparing a superalloy four-layer lattice lightweight structure. Background technique [0002] The GH4169 superalloy is a nickel-based superalloy that is precipitated and strengthened by body-centered four-room γ” and face-centered cubic γ’ phases. It has good comprehensive properties in the temperature range of -253-700 ° C, and the area service strength below 650 ° C It ranks first among deformed superalloys, and has good fatigue resistance, radiation resistance, oxidation resistance, corrosion resistance, good processing performance, welding performance and long-term organizational stability, and can manufacture various parts with complex shapes. In the , nuclear energy and petroleum industries, it has been widely used in the above temperature range. [0003] As an important lightweight structure, the lattice structure is widely used...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P15/00B23K20/14B23K20/02
CPCB23P15/00B23K20/14B23K20/023
Inventor 崔庆龙刘仲权丁锐杨小克贺晓峰杨敏赵倩倩丛宇鹏王好强张群
Owner AEROSPACE HIWING HARBIN TITANIUM IND
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