A kind of numerical control processing method of aircraft model

An aircraft model and processing method technology, applied in toy aircraft, toys, entertainment and other directions, can solve problems such as aircraft model flutter, achieve the effects of high processing quality, improve production efficiency, and ensure consistency

Inactive Publication Date: 2017-07-28
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The object of the present invention is to provide a kind of numerical control processing method of aircraft model, and this method has solved the problem of flutter in the numerical control processing of aircraft model

Method used

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  • A kind of numerical control processing method of aircraft model
  • A kind of numerical control processing method of aircraft model
  • A kind of numerical control processing method of aircraft model

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Embodiment 1

[0032] A numerical control machining method for an aircraft model, specifically implemented according to the following steps:

[0033]Step 1. Analyze the overall structural characteristics of the aircraft;

[0034] figure 1 It is the schematic flow chart of the processing method of embodiment 1 aircraft model;

[0035] figure 2 It is the structural representation of embodiment 1 aircraft model, wherein 1. fuselage, 2. wing, 3. vertical tail, 4. horizontal tail, 5. missile and pylon, 6. pitot tube;

[0036] image 3 It is the back schematic diagram of the craft boss structure design of embodiment 1 aircraft model, 7. rectangular craft boss, 8. cylindrical craft boss; image 3 The middle d represents the distance between the two inlets;

[0037] Figure 4 is the front schematic diagram of the structural design of the aircraft model of embodiment 1, h 1 Rectangular process boss height dimension, h 2 Tail height dimension.

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Abstract

The invention discloses a numerical control machining method of an airplane model. The method specifically comprises the following steps that firstly, the airplane model is partitioned according to structural characteristics; secondly, back faces of the airplane model are independently machined according to partitions in the first step, and process bosses are machined on the back faces of the airplane model; thirdly, the front faces of the airplane model are independently machined according to the partitions in the first step; and fourthly, the process bosses on the back faces of the airplane model are cut away, or the machined process bosses on the back faces of the airplane model are machined into airspeed heads, surface treatment is carried out by waxing polishing paste or applying a grinding agent, and the machining of the airplane model is finished. According to a method for vibration restraining of numerical control machining of an airplane, the problem that complex airplane curved surfaces and airplane thin-wall pieces vibrate during numerical control machining is solved, the consistency of the profile machining quality and the exterior surface size is guaranteed, and meanwhile production efficiency is improved.

Description

technical field [0001] The invention belongs to the technical field of model processing methods, and relates to a numerical control processing method of an aircraft model. Background technique [0002] The development of simulation models has a long history. In the records of ancient Chinese history books, there are many descriptions about simulation models. In modern archaeological excavations in my country, some ceramic and wooden simulated military models have also been unearthed, such as the earliest ship model in China—a military model of a ceramic canoe found in the Neolithic site of Hemudu in Yuyao, Zhejiang, and Terracotta Warriors and Horses of Qin Shihuang unearthed in Xi'an. The most attractive part of the model collection is not only to test the hands-on ability, but also to see whether there is sufficient background knowledge and understanding of military history. After an airplane model is released and sold, with the progress of time and the continuous improve...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P15/00
CPCA63H27/00B23P15/00
Inventor 田卫军任军学李郁姚倡锋冯亚洲周金华
Owner NORTHWESTERN POLYTECHNICAL UNIV
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