Rolls-Royce M250-10577 Stage 2 C20/C20R Turbine Nozzle is engineered to optimize airflow and efficiency in M250 series gas turbine engines, directing combusted hot gases from the first turbine stage to the second-stage turbine blades.
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Overview
M250-10577 Turbine Nozzle plays a crucial role in controlling the flow of combusted hot gases after their expansion in stage 1. It directs these gases onto the second stage through a set of stationary vanes, effectively acting as a control valve for the engine. As the hot, high-pressure gases travel through the second stage nozzle, they expand, resulting in changes in acceleration, pressure, and temperature necessary to drive the turbine blades. This nozzle is specifically designed to achieve optimum flow control while dissipating excess heat, ensuring the turbine operates under optimal conditions and efficiency. The stationary vanes are constructed from super-alloys, allowing them to manage the flow of hot gases while withstanding extreme temperatures and thermal stress. It is designed for use in the Rolls-Royce M250-C20 and M250-C20R engine models.
Features & Benefits
Optimizes airflow and efficiency in gas turbine engines
Directs combusted hot gases to enhance turbine performance
Acts as a control valve for effective gas flow management
Constructed from super-alloys for durability under extreme conditions
Ensures optimal operation conditions and efficiency
Technical Information
NIIN
015943997
NSN
2840-01-594-3997
FSCG
2840
FSCG Category
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
FAA Approval Code
PC
Condition
New
CAGE Code
63005
Country of Origin
United States
Harmonized Tariff Schedule Code
8411997010
Lead Time (Days)
285
Shelf Life
No
Forecasted
Yes
Dimensions (L x W x H)
9 x 9.50 x 5
Package Weight
2.86 LB
Shipping Details
Hazmat Code
ZND
ECCN
9A991.c
Schedule B
8411997010
8130-3 Eligible
Yes
Hazmat
No
Part Explosive
No
Item Replacement History
23084490=64NOZZLE: TURBINE,STG2,C20/C20R, USE M250-10577=64
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