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LEAP-1A/1C Aircraft Engine Component High-Pressure Turbine Locator

The Secondary Rear-End High-Pressure Turbine Locator is an essential component in the LEAP-1A and LEAP-1C aircraft engines. It ensures the precise alignment and stability of the high-pressure turbine under extreme conditions. This component plays a crucial role in improving fuel efficiency, enhancing engine performance, and reducing maintenance costs. Built with advanced materials, it withstands high temperatures and high pressures, making it critical for engine reliability and longevity.

LEAP-1A/1C Components: Secondary Rear-End High-Pressure Turbine Locator (140 TO GE)

Secondary Rear-End High-Pressure Turbine Locator is a vital aircraft engine component in the LEAP-1A and LEAP-1C engines. It ensures the precise positioning and stability of the high-pressure turbine under extreme conditions. This component plays a key role in enhancing fuel efficiency, reducing maintenance, and improving engine performance.

What Is the Secondary Rear-End High-Pressure Turbine Locator?

This aircraft jet engine component ensures accurate alignment of the high-pressure turbine in the hot section of engine. It helps maintain the turbine's stability during engine operation.

It operates in an environment of high temperature and high pressure. This makes it essential for maintaining engine reliability and performance.

  • Precise Alignment: Ensures the turbine's optimal rotation, minimizing vibration and wear.

  • Supports High Temperatures: Made from advanced materials like ceramic composites or titanium alloys.

  • Enhances Durability: Reduces strain on the turbine, extending its working life.

How It Works in the Engine

The air intake system efficiently channels air into the engine. This ensures that the turbines, which drive the aircraft, operate at peak performance. Especially during the critical moments when the engine starts. This precise flow of air is essential for the engine’s ability to generate thrust and power the aircraft.

The Secondary Rear-End High-Pressure Turbine Locator functions within the gas turbine system. It stabilizes the turbine as air passes through the combustion chamber. It distributes load evenly and prevents misalignment.

It maintains stability at high speed. This ensures that the fuel burns efficiently in the combustion chamber. This boosts the overall engine performance.

Key Benefits

Improves Fuel Efficiency

The locator optimizes the turbine's alignment, enabling smooth airflow and reducing drag. This boosts fuel efficiency, helping airlines lower operating costs.

Supports High Pressure and High Temperatures

Built to withstand high pressure and hot section conditions, this component ensures reliable performance even in extreme environments.

Reduces Maintenance Costs

By minimizing wear on the turbine blades and associated parts, it lowers maintenance and replacement frequency.

Enhances Engine Safety

A stable turbine reduces the likelihood of mechanical failures, ensuring the safety of both passengers and crew.

Where It Fits in the LEAP-1A/1C Engines

The LEAP-1A and LEAP-1C are turbofan engines designed for aircraft like the Airbus A320neo and COMAC C919. These engines are well-known for their fuel efficiency and advanced engineering. The Secondary Rear-End High-Pressure Turbine Locator plays a critical role ensuring engine works efficiently under all conditions.

Additional LEAP-1B Components from Liyan International

LEAP-1A/1C Aircraft Engine Component High-Pressure Turbine Locator

At Liyan International, we supply a range of high-quality components of aircraft engine, including the following LEAP-1B components:

  • Front Transition Duct Hanger (288 TO GE): Supports airflow transition in the front section.

  • Front-End Support Ring (158 TO GE): Stabilizes the engine’s front section.

  • Fan Front Support (533 TO SF): Maintains balance and stability of the fan blade.

  • Secondary Rear-End High-Pressure Turbine Locator (140 TO GE): Precisely positions the turbine’s rear section.

  • Rotating Ring Stages 2/3/4/5 (TO SF): Enhances turbine rotation across multiple stages.

  • Bearing 4 Front-End Seal Ring (235 TO GE): Protects front-end bearings from leakage.

  • Bearing 4 End Stop Ring (242 TO GE): Secures the bearing assembly.

  • Retaining Ring Stages 2/3/5 (173/165/150 TO SF): Holds turbine components firmly in place.

Advanced Materials and Durability

The Secondary Rear-End High-Pressure Turbine Locator is crafted from innovative materials like ceramic composites and titanium alloys. These materials ensure high durability, resistance to wear, and low weight. They are critical for maintaining fuel efficiency in modern jet engines.

Why Choose Liyan International for Aircraft Engine Parts?

At Liyan International, we specialize in providing high-quality engine components for turbofan engines.

Our products, including parts for the LEAP-1A, LEAP-1C, and LEAP-1B, help ensure top-tier engine performance. Our products are engineered to meet the highest industry standards, ensuring performance, reliability, and longevity.

Benefits of Our Components:

  • Precision Manufacturing: Each part is crafted with exacting standards for seamless integration.

  • Durability: Designed to withstand high pressure and high temperatures.

  • Cost-Effective Solutions: Lower maintenance and functioning costs for airlines.

A Future of Efficient Aviation

The Secondary Rear-End High-Pressure Turbine Locator is more than just a component of aircraft engine. It represents a leap forward in aviation efficiency and eco-friendliness. By stabilizing turbines that propel the aircraft, it helps airlines reduce emissions, save fuel, and maintain reliability.

For high-quality aircraft engine components, trust Liyan International. Contact us today to learn more about our innovative solutions for the aviation industry.


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