Leading edge configuration for compressor blades of gas...

Details Leading edge configuration for compressor blades of gas... Leading edge configuration for compressor blades of gas...

2006-12-18

2010-06-29

Kershteyn, Igor (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Removable auxiliary attachment to work surface

C416S22300B, C416S224000, C416S235000, C416S23600R

Reexamination Certificate

active

07744346

ABSTRACT:
In a supersonic area, on a leading edge (2) of a compressor blade (1) for a gas turbine engine, a replaceable, longitudinally elastically deformable leading edge rail (7) with slender tip (11) and limited weight is positively held in a locating groove (3) and at a stop (6) and elastically locked by the curved blade form. While the maintenance effort is reduced, safe operation and long service life of the compressor (fan) are ensured.

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