Idle wheel structure of aeroengine accessories case
A technology for aero-engines and accessory casings, applied to transmission parts, transmission boxes, mechanical equipment, etc., can solve problems such as insufficient rigidity of the accessory casing, gear tooth surface eccentric load wear, gear eccentric load wear, etc., to achieve Effects of reducing shell deformation, reducing gyro moment, and increasing shell rigidity
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[0031] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application.
[0032] In order to overcome the problems in the prior art that the rigidity of the case shell at the idler wheel of the accessory case is insufficient and the idler wheel is prone to unbalanced load, the present application provides an idler wheel structure.
[0033] Such as figure 2 As shown, the idler structure of an aero-engine accessory case provided by the present application includes: an idler shaft 21A, a pressure plate 22A, a bearing 25A and a gear ring 26A. Wherein the idler shaft 21A and the pressure plate 22A can constitute the main structure of the idler, the upper end of the idler shaft 21A is inserted into the pressure plate 22A to achieve relative positioning, the pressure plate 22A is connec...
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