09-06-2023 дата публикации
Номер: CN116242623A
Принадлежит:
The invention belongs to the technical field of engine tests, and particularly relates to a similar design method of a power turbine rotor simulation tester. The method comprises the following steps: determining a rotor supporting form of a real power turbine rotor structure to be simulated, the position of a turbine blade disc, a rotor critical rotating speed and strain energy distribution; giving an initial structure scheme of the power turbine rotor tester meeting the structure and dynamics requirements, and adopting a rotor structure supported by two fulcrums with a cantilever disc; acquiring a fulcrum load, a rotor critical rotating speed and strain energy distribution of the power turbine rotor tester, comparing the fulcrum load, the rotor critical rotating speed and the strain energy distribution with a real power turbine rotor structure, and when a comparison error exceeds a set value, adjusting a fulcrum, a cantilever disc and the rotor structure; and whether the elastic support ...
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