G.E.® 4128T14P01 Stage 2 Compressor Vane Shroud is a critical component for GE aircraft engines, designed to support stationary vanes, direct airflow, and prevent leakage within the compressor section, ensuring optimal engine performance.
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Overview
4128T14P01 Compressor Vane Shroud is specifically engineered to guide and direct airflow from previous stages onto the rotor blades. By decreasing the velocity of the air, it effectively increases its static pressure, enhancing the overall efficiency of the compressor. This component plays a vital role in maintaining the performance of the engine by ensuring that the airflow is managed effectively, contributing to optimal energy extraction and operational reliability. The shroud is constructed from high-strength materials to withstand the demanding conditions of gas turbine operation.
Features & Benefits
Supports stationary vanes for effective airflow management
Prevents leakage within the compressor section
Increases static pressure by decreasing airflow velocity
Constructed from high-strength materials for durability
Enhances overall engine performance and efficiency
Technical Information
FAA Approval Code
PC
Condition
New
CAGE Code
99207
Country of Origin
United States
Harmonized Tariff Schedule Code
8411917010
Lead Time (Days)
5
Shelf Life
No
Forecasted
Yes
Dimensions (L x W x H)
9 x 5.50 x 1.42 INH
Package Weight
0.18 LB
Shipping Details
Hazmat Code
ZND
ECCN
9A991.d
Schedule B
8411917010
8130-3 Eligible
Yes
Hazmat
No
Part Explosive
No
Item Replacement History
4128T14P01=CISHROUD: VANE,COMPRESSOR,STG 2, ONLY SOH AVAILABLE
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Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
