Casing boss channel machining method based on characteristics

A processing method and channel technology, applied in the CAM field, can solve problems such as low programming efficiency, insufficient flexibility, and poor quality, and achieve the effects of high computing efficiency, high accuracy rate, and strong flexibility

Active Publication Date: 2014-12-17
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0004] The present invention aims at the lack of processing mode for the channels between the bosses of the aero-engine case in the current CAM system, that is, the combination of plunge milling rough machining and layer milling finish machining, and the existing machining programming efficiency is low, the quality is poor, and the flexibility is insufficient. To solve this problem, a feature-based machining method for the channel between the bosses of the aero-engine casing is proposed. It first reads the casing model and the feature recognition results of the casing, automatically constructs the processing area of ​​the channel between the bosses, and then according to the machining resource library Data, you can choose to automatically generate or manually input the rough and finish machining process information of the channel between the machining bosses, and automatically and quickly generate the rough machining plunge milling trajectory and finishing trajectory

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  • Casing boss channel machining method based on characteristics
  • Casing boss channel machining method based on characteristics
  • Casing boss channel machining method based on characteristics

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Embodiment Construction

[0049] The technical solution of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0050] The present invention aims at the lack of a systematic processing mode for the channel between the bosses of the aero-engine casing in the current CAM system, that is, the combination of rough machining with plunging milling and finishing with layer milling, and the low efficiency, poor quality, and insufficient flexibility of existing machining programming. To solve this problem, a feature-based machining method for the convex channel of aero-engine casing is proposed. First read the casing model and casing feature recognition results, automatically build the processing area of ​​the channel between the bosses, and then according to the data in the processing resource library, you can choose to automatically generate or manually input the rough and fine roughness and fineness of the channel between the bosses t...

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Abstract

A casing boss channel machining method based on characteristics is characterized by including casing model and casing boss characteristic information, establishing a boss channel machining region automatically, selecting automatically generating or manually inputting machining process information of machined boss characteristics, and finally generating rough and fine machining tracks automatically. The method can be applied to rough and fine machining of boss channels, the cutter track calculating efficiency is high, the correct rate is high, the flexibility is high, the programming workload of engineering staffs is reduced greatly, single or batched multiple boss channels can be machined, and the different requirements of the engineering staffs can be met.

Description

technical field [0001] The invention relates to a CAM technology, in particular to a CAM technology of an aero-engine casing, in particular to a CAM processing method based on a feature extraction channel between bosses of the casing. Background technique [0002] The aero-engine is the power source of the aircraft. With the increasing thrust-to-weight ratio of the aero-engine, not only higher requirements are put forward for the structural design of the aero-engine case, but also higher challenges are put forward for the manufacture of the case. At present, the case Titanium alloys, high-temperature alloys and other high-temperature-resistant and difficult-to-cut materials are mostly used; in terms of structure, the hub surface is the main body, and the cylindrical island bosses are divided in the circumferential direction. The thinnest part of the part is only 2-3mm thick, which is a multi-island complex thin-walled structure. pieces. In the CNC machining of the casing, d...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/4097
Inventor 李迎光郝小忠马斯博刘旭
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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