The Aircraft 3.0 πŸ”΅: πŸ”΅✈️ 225. Most important characteristics of Aircraft: Gas Turbine Engine Bearings and Seals 🚁🎞️

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πŸ”΅✈️ 225. Most important characteristics of Aircraft: Gas Turbine Engine Bearings and Seals 🚁🎞️

Aircraft: Gas Turbine Engine Bearings and Seals

Most important characteristics of Aircraft: Gas Turbine Engine Bearings and Seals

The main bearings have the critical function of supporting the main engine rotor. The number of bearings necessary for proper engine support is, for the most part, determined by the length and weight of the engine rotor. The length and weight are directly affected by the type of compressor used in the engine. Naturally, a two-spool compressor requires more bearing support. 


The minimum number of bearings required to support one shaft is one deep groove ball bearing (thrust and radial loads) and one straight roller bearing (radial load only). Sometimes, it is necessary to use more than one roller bearing if the shaft is subject to vibration or its length is excessive. 


The gas turbine rotors are supported by ball and roller bearings, which are antifriction bearings. Many newer engines use hydraulic bearings, in which the outside race is surrounded by a thin film of oil. This reduces vibrations transmitted to the engine.


In general, antifriction bearings are preferred largely because they: • Offer little rotational resistance, • Facilitate precision alignment of rotating elements, • Are relatively inexpensive, • Are easily replaced, • Withstand high momentary overloads, • Are simple to cool, lubricate, and maintain, • Accommodate both radial and axial loads, and • Are relatively resistant to elevated temperatures.


Aircraft: Gas Turbine Engine Bearings and Seals


The main disadvantages are their vulnerability to foreign matter and tendency to fail without appreciable warning. 


Usually the ball bearings are positioned on the compressor or turbine shaft so that they can absorb any axial (thrust) loads or radial loads. Because the roller bearings present a larger working surface, they are better equipped to support radial loads than thrust loads. 


Therefore, they are used primarily for this purpose. A typical ball or roller bearing assembly includes a bearing support housing, which must be strongly constructed and supported in order to carry the radial and axial loads of the rapidly rotating rotor. 


The bearing housing usually contains oil seals to prevent the oil leaking from its normal path of flow. It also delivers the oil to the bearing for its lubrication, usually through spray nozzles. The oil seals may be the labyrinth or thread (helical) type. 



These seals also may be pressurized to minimize oil leaking along the compressor shaft. The labyrinth seal is usually pressurized, but the helical seal depends solely on reverse threading to stop oil leakage. These two types of seals are very similar, differing only in thread size and the fact that the labyrinth seal is pressurized.


Another type of oil seal used on some of the later engines is the carbon seal. These seals are usually spring loaded and are similar in material and application to the carbon brushes used in electrical motors. Carbon seals rest against a surface provided to create a sealed bearing cavity or void; thus, the oil is prevented from leaking out along the shaft into the compressor airflow or the turbine section.


The ball or roller bearing is fitted into the bearing housing and may have a self-aligning feature. If a bearing is self-aligning, it is usually seated in a spherical ring. This allows the shaft a certain amount of radial movement without transmitting stress to the bearing inner race. 


The bearing surface is usually provided by a machined journal on the appropriate shaft. The bearing is usually locked in position by a steel snap ring or other suitable locking device. The rotor shaft also provides the matching surface for the oil seals in the bearing housing. These machined surfaces are called lands and fit in rather close to the oil seal.  


Most important characteristics of Aircraft: Gas Turbine Engine Bearings and Seals



Component NameTypeFunctionSupported LoadsAdvantagesDisadvantagesLubrication/Sealing Mechanism
Ball Bearing

Antifriction/Deep groove

Support the main engine rotor

Both radial and axial (thrust)

Little rotational resistance, precision alignment, inexpensive, easily replaced, withstands high momentary overloads, simple to maintain, heat resistant

Vulnerable to foreign matter, tendency to fail without warning

Cooled and lubricated via oil spray nozzles in the bearing housing

Roller Bearing

Antifriction/Straight roller

Support the main engine rotor (especially if subject to vibration or excessive length)

Radial loads only

Larger working surface for better radial support, precision alignment, inexpensive, easily replaced, heat resistant

Vulnerable to foreign matter, tendency to fail without warning, not equipped for thrust loads

Cooled and lubricated via oil spray nozzles in the bearing housing

Hydraulic Bearing

Antifriction (Newer types)

Outside race surrounded by oil film to support rotor

Reduces vibrations transmitted to the engine

Vulnerable to foreign matter, tendency. to fail without warning

Thin film of oil surrounding the outside race

Labyrinth Seal

Oil Seal

Prevent oil leaking from its normal path of flow along the compressor shaft

Not applicable

Effective leakage prevention when pressurized

Usually pressurized to minimize oil leaking

Carbon Seal

Oil Seal

Prevent oil from leaking out along the shaft into the compressor airflow or turbine section

Not applicable

Creates a sealed bearing cavity or void

Spring loaded; rests against a surface to create a seal

Thread (Helical) Seal

Oil Seal

Prevent oil leaking from its normal path of flow

Not applicable

Simplicity (depends on threading)

Not pressurized; depends solely on reverse threading

Depends on reverse threading to stop oil leakage