HOW TO DO RLA STUDY OF TURBINE




 

Turbine is the most critical equipment operated in hi temperature and speed. Stress is developed due to fluctuation in temperature and frequent start// stop of the machine. If the operating temperature and differential temperature go beyond permissible limit , stress is developed.In real life situation, a component experiences combination of loading patterns whereby its life is consumed by a combination of creep damage, low cycle fatigue damage and crack propagation. Minor's sum is used to determine the life of the component under various kinds of loading patterns expected to be encountered by the component during its life span. The testing plan (typical) for turbine as per below fig.

Components

Inspection

Point/Area/Zone

Evaluation

Rotor

VI, PT, MT

All Surface

Crack,Erosion Corrosion

DI

Shroud Clearance

Creep

UT

Blade Groove

Crack, SCC

RT

High Temp. Surface

Softening

Replica

Blade Groove

SCC, Fatigue

Casing

VI, PT, MT

All Surface

Crack

RT

High Temp. Surface

Softening

RT, MT

Casing Bolt of HP Part

Creep, Softening

M.S.V

G.V

VI, PT, MT

All Surface

Crack

RT

High Temp. Surface

Softening

Replica

High Temp. Surface

Creep

RT, MT

Casing Bolt of HP Part

Creep, Softening


Inspection Points for Replication & Hardness in Turbine Rotor (Typical)

Inspection Points for Replication & Hardness in CV

Universal Turbo Tech ServiceCA And RLA Studies by NDT Tests in Hyderabad | ID: 20311134912

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