Voidable rotor support structure and aero-engine
A technology of rotor support and engine, which is applied in the directions of engine components, machines/engines, blade support components, etc., can solve the problems of stator collision, deformation of rotor 4, and large vibration amplitude of rotor 4, so as to avoid collision and meet the needs of Effects of performance and safety requirements
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[0025] The present invention will be described in detail below. In the following paragraphs, different aspects of the embodiments are defined in more detail. The aspects so defined can be combined with any other aspect or aspects, unless it is clearly indicated that they cannot be combined. In particular, any feature considered to be preferred or advantageous may be combined with one or more other features considered to be preferred or advantageous.
[0026] The terms "first" and "second" appearing in the present invention are only for convenience of description, to distinguish different components with the same name, and do not indicate a sequence or a primary-secondary relationship.
[0027] In the description of the present invention, it should be understood that the terms "front", "rear", "circumferential", "axial" and "radial" indicate the orientation or positional relationship based on the orientation shown in the drawings. The or positional relationship is only for the con...
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