woodaaay
Aerospace
- Feb 8, 2009
- 5
Hi guys,
I'm having some trouble getting my head around how to balance the rear carrier in an AT.
I have this standard:
ISO 1940 - Mechanical vibration -- Balance quality requirements for rotors in a constant (rigid) state -- Part 1: Specification and verification of balance tolerances
Is it possible for me to assume that, for balancing purposes, the carrier is in a rigid state? It isn't supported in the same way as what the standard refers to i.e. Internal or External rotor supported by 2 bearings, as at any time it is in contact with sun gears, owc, and carrier shaft. However a preliminary and basic analysis is required.
Any help would be greatly appreciated.
I'm having some trouble getting my head around how to balance the rear carrier in an AT.
I have this standard:
ISO 1940 - Mechanical vibration -- Balance quality requirements for rotors in a constant (rigid) state -- Part 1: Specification and verification of balance tolerances
Is it possible for me to assume that, for balancing purposes, the carrier is in a rigid state? It isn't supported in the same way as what the standard refers to i.e. Internal or External rotor supported by 2 bearings, as at any time it is in contact with sun gears, owc, and carrier shaft. However a preliminary and basic analysis is required.
Any help would be greatly appreciated.