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Method for generating wing by adopting active structure rigidity method

A technology of structural rigidity and rigidity, which is applied in the field of generating wings by using the active structural stiffness method, can solve the problems of insufficient scientific and rigorous design methods and ideas of structural stiffness, structural instability, and increased design workload, etc., to shorten the model development cycle , Improving the level of structural design and the effect of improving the quality of structural design

Inactive Publication Date: 2013-05-15
BEIHANG UNIV
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0006] (1) The number of structural components increases, and the continuity of the structure is not good, which leads to a decrease in structural stiffness, discontinuous distribution of structural stiffness, and difficulty in controlling the distribution of stiffness
[0007] (2) The number of connectors and connecting surfaces of the structure increases, and the connection relationship of the structure is complicated. In this way, the stiffness characteristics of the structure will change greatly at the structural connection, which will cause the internal force transmission and structural deformation of the structure to change, making the overall structure large variations in stiffness and local stiffness
[0008] (3) The deformation and rotation angle of the structure are only given vague expressions in the aircraft design specifications and airworthiness regulations, such as "the deformation should not be too large", but the specific size or percentage is not clearly given. bring some difficulties
[0010] (5) For large aircraft, there are also factors closely related to structural stiffness such as structural instability and large openings that need to be considered, and these factors will affect the quality of structural design
[0011] Through the previous analysis of the structural stiffness design, it can be seen that the structural stiffness design is related to many actual performances and functions of the structure and even the product, and the passive or semi-passive structural stiffness design invisibly increases the design workload and at the same time Affect design progress and increase design overhead
More importantly, the methods and ideas of passive structural stiffness design are not scientific and rigorous enough, and have a certain degree of blindness

Method used

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  • Method for generating wing by adopting active structure rigidity method
  • Method for generating wing by adopting active structure rigidity method
  • Method for generating wing by adopting active structure rigidity method

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Embodiment Construction

[0030] The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0031] Active structural stiffness design should run through the entire product development process, and the design requirements for structural stiffness should be clearly put forward for each design stage of the product. Since it is an active structural stiffness design, it is necessary to analyze the structural stiffness design problems clearly in advance, rather than remedial the structural stiffness afterwards. Since it is necessary to clarify the structural stiffness problem in advance, it is necessary to carry out effective structural stiffness analysis and calculation in the early stage of aircraft structure design, that is, in the phase of aircraft program demonstration and program design, to provide support for subsequent structural design. basis and guidance. Compared with passive structural stiffness design methods, active structural stiff...

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Abstract

The invention discloses a method for generating a wing by adopting an active structure rigidity method. The method is characterized by comprising the following steps of: 1, determining rigidity index; 2, designing a structure; and 3, comparing errors. In the initial stage of the active structure rigidity design method, the rigidity index is considered into the structure design, thus blindness of passive and half-passive structure rigidity designs can be avoided; according to the active structure rigidity designing method, the structure design level of products can be improved, the structure design quality is improved, the type researching period is shortened, the type researching cost is reduced; according to the active structure rigidity designing method, an optimal structure according with the requirement can be designed according to the demands, the designing method is more scientific and rigorous; and according to the active structure rigidity design, the structure design level of the product can be improved, the structure design quality is improved, the type researching period is shortened, and the type researching cost is reduced. More importantly, according to the active structure rigidity design, the structure design idea is more scientific and rigorous.

Description

technical field [0001] The invention belongs to the technical field of aerospace and relates to a method for generating wings by adopting an active structure stiffness method. Background technique [0002] Stiffness is the ability of a material, component or structure to resist deformation under the action of an external force. Structural stiffness design includes a wide range of content, and stiffness is related to many factors such as material, force form, geometric shape, and boundary conditions. From the effect of load, structural stiffness can be divided into tension and compression stiffness, bending stiffness, shear stiffness and torsional stiffness. Different connection forms, combination methods, force transmission routes, and working environments of structures have different stiffness characteristics. The complexity of stiffness design brings many structural stiffness problems. [0003] The structural design should meet the strength and stiffness design requirem...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 何景武夏盛来黑丽洁张佳佳李喜茹
Owner BEIHANG UNIV
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