What could cause a low-pressure compressor first stage blade of a low-bypass turbofan engine to bend forward?
I also noticed rotor path rubbing in the 9 to 12 o'clock portion (while usually this can happen only in the 6 o'clock area).
What could cause a low-pressure compressor first stage blade of a low-bypass turbofan engine to bend forward?
I also noticed rotor path rubbing in the 9 to 12 o'clock portion (while usually this can happen only in the 6 o'clock area).
Forward bending of the first stage of the low pressure compressor is usually associated with (soft) Foreign Object Damage (FOD).
Ice and/or large quantities of snow in the engine intake will typically cause forward bending of the leading edge of the tip of the blades.
Damage to GE CF680C2 turbine engine compressor fan blades after snow/ice ingestion
Source: Flight Safety Australia
Damage to Turbomeca gas turbine Arriel 2B turbine engine compressor blades after snow/ice ingestion
Source: Transport Safety Board of Canada, aviation accident investigation report A12P0008