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A 3D coordination method for aircraft products

A coordination method and aircraft technology, applied in special data processing applications, instruments, electrical and digital data processing, etc., can solve the problems of a large number of coordination records, occupying the designer's time, data deviation, etc., to facilitate data management and traceability , avoid omissions and improve efficiency

Active Publication Date: 2017-05-17
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In recent years, major aircraft research companies both at home and abroad have adopted electronic prototypes that establish three-dimensional solid models of parts to replace coordination diagrams, but the traditional two-dimensional method is still followed for the coordination record sheet that expresses the interface between disciplines.
This mixed coordination method of 2D and 3D interrupts the transmission of digital design data. In the process of converting 3D to 2D and 2D to 3D, problems such as data deviation and loss are likely to occur, and due to the large number of coordination records , drawing, printing and implementation all take up a lot of time for the designer

Method used

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  • A 3D coordination method for aircraft products
  • A 3D coordination method for aircraft products
  • A 3D coordination method for aircraft products

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0051]Taking the professional coordination of accessories, pipelines and rear fuselage structure of the hydraulic system in the detailed preliminary design stage of aircraft products as an example, the following three-dimensional coordination model between the system and the structure is established:

[0052] 1. According to the electronic prototype, put the profile surface of the oil return hydraulic oil filter of the hydraulic system in the three-dimensional coordination model according to the placement position (see attached figure 2 The cylindrical surface in the middle); establish the surface connecting the oil return hydraulic oil filter with the structure installation (see attached figure 2 The support-shaped surface in ) is used to express the connection area and connection form between the oil return hydraulic oil filter and the structure;

[0053] 2. Fill in the attribute information one by one, including the name of the oil return hydraulic oil filter (return oil ...

Embodiment 2

[0060] Taking the coordination between landing gear door locks and hydraulic conduits in the detailed preliminary design stage of an aircraft product as an example, a three-dimensional coordination model among system accessories is established as follows:

[0061] 1. According to the position of the interface between the landing gear door lock and the hydraulic conduit on the aircraft, establish the profile surface at the interface between the two accessories, which is used to represent the position, shape and size of the hydraulic joint of the landing gear door lock; establish the above The geometric surface connected between the two is used to express the connection information, see the attached Image 6 ;

[0062] 2. Express the attribute information of the landing gear door lock in words, including name, model, weight, and material; express the sealing requirements, clearance requirements, working pressure, and working fluid at the hydraulic conduit of the landing gear doo...

Embodiment 3

[0065] Taking the coordination between the vertical tail structural components and the rear fuselage structural components in the detailed preliminary design stage of aircraft products as an example, the following three-dimensional coordination model between structural components is established:

[0066] 1. According to the location of the centralized joint between the vertical tail and the rear fuselage on the aircraft, establish the contour surface of the centralized joint to express the relative position and connection form of the joint between the vertical tail and the rear fuselage. The vertical tail adopts double ears Ear piece, the rear fuselage adopts a single ear piece, and each group of joints is connected by two sets of bolts. For the form, material selection, bolt position, size and material selection of the ear piece, please refer to the attachment Figure 8 ;

[0067] 2. Establish the geometric surface of the connection area between the root of the vertical tail ...

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Abstract

The invention belongs to the field of airplane design and relates to establishment of a method for conducting three-dimensional coordination on all systems of an airplane product in the detailed initial design stage. The method is characterized by comprising the steps that firstly, coordination of all specialties of the airplane product is divided into three types; secondly, three types of three-dimensional coordination models are established respectively; thirdly, mutual coordination is conducted between the specialties to confirm data. By means of the method, the whole course data transmission in the developing process of large industrial products such as airplanes is achieved, and thus the transmission of the coordination data is accurate and fast; the geometric models expressed with points, lines and planes which occupy quite little resources and quite small space are adopted in the three-dimensional coordination models to specially express the coordination information between the specialties, and the expressed content is concise and clear; the standardized three-dimensional coordination models enable coordination elements to be completely expressed, and missing and incompletion of the coordination elements are effectively avoided; the three-dimensional coordination models facilitate the concentrated expression of the coordination elements; state control is adopted in the three-dimensional coordination models, and thus data management and tracing are facilitated.

Description

technical field [0001] The invention belongs to the field of aircraft design, and relates to the creation of a method for three-dimensional coordination between various systems of aircraft products in the detailed preliminary design stage. Background technique [0002] For traditional aircraft, in the detailed preliminary design stage, the coordination between various disciplines uses two-dimensional coordination diagrams, coordination records and coordination minutes to record the coordination content between disciplines. The main basis for detailed design. Because aircraft products involve coordination among many disciplines, the content is very complex. An aircraft model often requires thousands or even tens of thousands of coordination sheets, and hundreds of large coordination maps need to be drawn at the same time. Drawing coordination diagrams and coordination records takes up a lot of time for designers, and the coordination workload is huge. According to statistic...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 许平樊海东毕世权苏智星
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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