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Preparation method of gas turbine swirler

A gas turbine and cyclone technology, which is applied in the field of precision machining, can solve the problems of difficulty in ensuring the roughness of the inner wall in the hollow blade, affecting product performance, etc., and achieve the effects of shortening the processing cycle, excellent tensile strength performance, and reducing costs.

Active Publication Date: 2021-11-19
XIAN YUANHANG VACUUM BRAZING TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention is to provide a preparation method of a gas turbine swirler to solve the problem in the prior art that the production and processing by casting is not easy to ensure the roughness of the inner wall of the hollow blade, so as to affect the performance of the product

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  • Preparation method of gas turbine swirler
  • Preparation method of gas turbine swirler
  • Preparation method of gas turbine swirler

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Embodiment Construction

[0045] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0046] In describing the present invention, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", The orientations or positional relationships indicated by "top", "bottom", "inner", "outer", etc. are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying References to devices or elements must have a particular orientation, be constructed, and operate in a particular orientation and therefore should not be construed as limiting the invention.

[0047] The terms "first" and "second" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance or implicitly specifying the quantity of indicated ...

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Abstract

The invention belongs to the technical field of precision machining, and discloses a preparation method of a gas turbine swirler, which is characterized in that the gas turbine swirler is decomposed into three parts, namely an inner ring, an outer ring and blades, then the inner ring, the outer ring and the blades are independently formed by adopting a machining method, and then the inner ring, the outer ring and the blades are connected by adopting a brazing method. In order to guarantee the brazing quality, a mounting head is machined on the heads of the blades a blade-shaped groove is correspondingly machined in the inner ring, a bayonet is correspondingly machined in the outer ring, then the outer ring, the blades and the inner ring are tensioned through an assembly tool to guarantee that brazing faces are tightly attached, spot welding is used for positioning, and the blades are conveyed into a furnace to be subjected to vacuum brazing after being completed. The roughness of the inner wall of the hollow blade is guaranteed by splitting the structure of the swirler and combining with independent machining, the tensile strength performance of brazing seams between the blades and the inner ring and the brazing seams between the blades and the outer ring is excellent under the room temperature and high temperature environment, the strength performance is better than that of base metal, the performance of the base metal cannot be lost, and the machining period is effectively shortened.

Description

technical field [0001] The invention belongs to the technical field of precision machining, and relates to a preparation method of a gas turbine cyclone. Background technique [0002] In the field of energy and electric power, the material of the gas turbine engine swirler is a deformed superalloy, the blades on the swirler are hollow blades, and there are small holes in the air film on the blades. In the prior art, production and processing are carried out by casting, but it is not easy Ensure the roughness of the inner wall in the hollow blade, so as to affect the product performance. Moreover, separate mold opening is required for single-piece production, which has a long cycle and high cost. In view of this, it is necessary to provide a preparation method that can ensure the roughness of the inner wall of the hollow blade and ensure the performance of the product. Contents of the invention [0003] The present invention provides a preparation method of a gas turbine ...

Claims

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Application Information

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IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor 任耀文康路路王程成琚明
Owner XIAN YUANHANG VACUUM BRAZING TECH
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