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Engine intake manifold machining method

A technology of intake manifold and processing method, which is applied in the direction of metal processing equipment, manufacturing tools, auxiliary devices, etc., can solve problems such as unsatisfactory weight uncertainty, and achieve the effect of easy control of wall thickness

Active Publication Date: 2020-06-09
安徽航瑞航空动力装备有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, for the intake manifold, the weight uncertainty caused by the deviation of the wall thickness of the casting molding process cannot meet the application in new fields, and a new molding method is required to meet the weight requirements of the new field

Method used

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  • Engine intake manifold machining method
  • Engine intake manifold machining method
  • Engine intake manifold machining method

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Embodiment Construction

[0035] Below with reference to the accompanying drawings; through the description of the embodiments, the specific embodiments of the present invention will be described in further detail, the purpose is to help those skilled in the art to have a more complete, accurate and in-depth understanding of the concept and technical solutions of the present invention, and contribute to its implementation.

[0036] It should be noted that, in the following embodiments, the “first” and “second” do not represent an absolute distinction relationship in structure and / or function, nor do they represent a sequential execution order, but only for the purpose of Convenience of description.

[0037] like Figure 1 to Figure 3 As shown, the present invention provides a processing method for an engine intake manifold, comprising the following steps:

[0038] S1. The processing of each component of the intake manifold;

[0039] S2. Assemble the components to form an intake manifold blank;

[0...

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Abstract

The invention discloses an engine intake manifold machining method. The method includes the steps of S1, machining all parts of an intake manifold; S2, splicing the parts to form an intake manifold blank; and S3, machining a flange face and installing holes of the intake manifold blank, wherein the parts of the intake manifold include the first air outlet flange, the second air outlet flange, theintake flange, a first cylinder branch pipe lower half shell body, a second cylinder branch pipe lower half shell body, a third cylinder branch pipe lower half shell body, a fourth cylinder branch pipe lower half shell body, a first cylinder branch pipe upper half shell body, a second cylinder branch pipe upper half shell body, a third cylinder branch pipe upper half shell body, a fourth cylinderbranch pipe upper half shell body, a resonant cavity lower half shell body and a resonant cavity upper half shell body. According to the engine intake manifold machining method, by dividing the intakemanifold into multiple pieces and splicing the pieces after machining to form an assembly piece, the wall thicknesses of all the parts are easy to control, and the light weight of the intake manifoldcan be realized.

Description

technical field [0001] The invention belongs to the technical field of engine production technology, in particular, the invention relates to a processing method of an engine intake manifold. Background technique [0002] In the development of the existing piston engine assembly, the aluminum alloy intake manifold rapid prototype forming methods include investment casting, wood mold casting and other processes, but these forming methods have a significant impact on the wall thickness of the intake manifold during the casting process. There are certain requirements, generally at least 4mm, this wall thickness can avoid the scrapping of parts due to casting defects. [0003] Due to the new application areas of piston engines, there are new requirements for piston engine assemblies - weight targets. In order to meet the weight target requirements of the engine in the new application field, each part of the engine needs to be reduced in weight under the premise of considering it...

Claims

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Application Information

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IPC IPC(8): B23P15/00B23K37/04
CPCB23K37/0435B23P15/00
Inventor 张敏许贡杜宇张辰卿郭变变
Owner 安徽航瑞航空动力装备有限公司