Reliability simulation method related to failure of multiple components of typical mechanism of aero-engine
An aero-engine and failure-related technology, which is applied in the field of reliability simulation related to multi-component failure of typical aero-engine mechanisms, can solve problems such as affecting calculation efficiency and initial state difficulties, and achieve the effect of improving calculation efficiency and reducing calculation costs.
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[0045] In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as there is no conflict with each other.
[0046] like figure 1 As shown, the present invention is a reliability simulation method related to the failure of multiple components of a typical mechanism of an aero-engine, and the content of the invention is explained by taking the stator blade adjustment mechanism as an example, including the following steps:
[0047] Step S1: Determine random variables and distribution types according to the ...
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