Load Cell

The landing gear wheel spin-up system (English: Wheel Spin-Up System or Pre-Rotation System) is an auxiliary system that controls the rotation of landing gear wheels before they make contact with the runway. The primary purpose of this system is to reduce the speed differential by pre-rotating the wheels prior to touchdown, rather than allowing them to start rotating from rest upon contact with the runway. This minimizes structural stresses, tire wear, and loads on the braking system.

The function of the wheel spin-up system is to reduce the slip ratio between the aircraft’s landing gear wheels and the runway surface at the moment of touchdown. Under normal conditions, landing gear wheels are stationary when they contact the ground and must rapidly accelerate to match the runway’s speed. This speed difference causes high friction, sudden tire heating, and mechanical stress. The wheel spin-up system rotates the wheels to approximately the runway speed before the aircraft lands, thereby reducing this differential.

Wheel spin-up systems typically operate through the following mechanisms:

1. Jet blast systems: Wheels are rotated using pressurized air or gas jets.
2. Electric motor systems: Each wheel is equipped with an electric motor that pre-rotates it prior to touchdown.
3. Mechanical clutch systems: The aircraft’s existing motion energy is transferred to the wheels via a clutch mechanism.

These systems are activated automatically or manually at a specific phase of landing, such as during descent or a predetermined time before touchdown.

• Reduces wheel and tire wear.
• Lowers mechanical shocks at runway contact.
• Extends the lifespan of the braking system.
• Improves landing safety by reducing directional deviations caused by skidding.
• Particularly important for military aircraft with high landing speeds and civil aircraft with expensive landing gear assemblies.

• Commercial passenger aircraft (especially wide-body models).
• Military fighter aircraft and aircraft designed for carrier landings.
• Research and test aircraft for studying landing dynamics.

The implementation of these systems involves certain technical and financial challenges. Factors such as added weight, maintenance costs, and ensuring system reliability can hinder widespread adoption. While some aircraft manufacturers do not offer this system as standard equipment, optional configurations and research-based applications are available.