4046T28G14 Turbine Stator Vane Segment – OEM Hot?Section Component for GE T700 Engines

Description

The 4046T28G14 Turbine Stator Vane Segment is a precision?engineered hot?section component designed for General Electric T700?series engines powering UH?60 Black Hawk and AH?64 Apache helicopters. Classified under NSN 2840?01?184?9842, this stator vane segment channels high?temperature combustion gases toward the turbine rotor, optimizing aerodynamic flow, thermal efficiency, and power output. Manufactured from advanced heat?resistant alloys, it withstands extreme temperatures, oxidation, and sustained mechanical loading within the turbine section. The segment includes contoured airfoils, mounting platforms, and cooling features engineered to maintain structural integrity and consistent airflow during demanding operational conditions.

Key Specs:

Manufacturer: General Electric (CAGE 99207)
NSN: 2840?01?184?9842
Function: Directs combustion gas flow to turbine rotor blades
Category: Turbine stator vane segment, hot?section component
Applications: GE T700?GE?701C/701D engines for UH?60 and AH?64 aircraft
Dimensions: Approx. 6" x 4" x 3" (typical stator vane segment size)
Weight: ~1.2 lbs
Compliance: Built to military?grade and aerospace hot?section performance standards
This stator vane segment ensures efficient turbine operation, stable engine performance, and long?term durability in high?temperature aviation environments.

Features

• Heat?resistant alloy construction for extreme turbine temperatures.
• Aerodynamic vane geometry for optimized gas?flow direction.
• Precision?machined platforms for secure hot?section mounting.
• Engineered to resist oxidation and thermal cycling.
• Supports efficient turbine energy transfer and power output.
• NSN?classified for accurate sourcing and maintenance planning.
• Designed for long?term durability in high?temperature environments.

Frequently Asked Questions