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
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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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