Aircraft engine drive shaft compartment assembly and method of assembling an aircraft engine drive shaft compartment assembly

摘要

A drive shaft chamber assembly for a gas turbine engine is disclosed. The drive shaft housing chamber assembly includes a drive shaft housing chamber and an outlet guide vane. The drive shaft storage chamber includes a front surface, a rear surface, and side surfaces on both sides, and is configured to receive at least a part of the radial drive shaft. The outlet guide vane includes a leading edge and a trailing edge. The length of the rear edge portion is substantially equal to the length of the front surface of the drive shaft housing chamber, thereby forming the rear edge portion of the outlet guide vane in a streamlined manner, and the driving shaft housing chamber. Can be matched to the front. [Selection] Figure 1