LRR025CRP2612NNN3K2BGA6NAAANNNNNN axial piston pumps

LRR025CRP2612NNN3K2BGA6NAAANNNNNN axial piston pumps play a crucial role in the functionality of aircraft landing gear systems, contributing to the safety and efficiency of an aircraft’s operation. These pumps are designed to generate hydraulic pressure, which is essential for the precise movement and control of landing gear during both landing and take-off procedures.

Model Code :LR-R-025C-RP-26-12-NN-N-3-K2BG-A6N-AAA-NNN-NNN
Model Code :LRR025CRP2612NNN3K2BGA6NAAANNNNNN

The primary function of piston pumps in landing gear systems is to facilitate the extension and retraction of the landing gear. When an aircraft prepares for landing, the pilot activates the landing gear switch, which signals the hydraulic system to engage. The piston pump then draws hydraulic fluid from the reservoir and pressurizes it, directing the fluid into the actuators connected to the landing gear. This pressurized fluid enables the actuators to extend the landing gear, ensuring a smooth transition from the aircraft’s body to the ground.

Model No.ldent No. :83064609

LRR025CRP2612NNN3K2BGA6NAAANNNNNN axial piston pumps.One of the key advantages of piston pumps is their ability to deliver a consistent and controllable flow of hydraulic fluid. They can operate at high pressures, which is essential for overcoming the forces that are generated when landing gear is deployed or retracted. Additionally, piston pumps can be designed to have variable flow rates, allowing the hydraulic system to adapt to different operational requirements, such as slowing down or speeding up the deployment of the landing gear.

In emergencies, piston pumps also enhance the reliability of landing gear systems. Many aircraft are equipped with a backup hydraulic system, often powered by additional piston pumps, ensuring that the landing gear can still be operated even if the primary system fails. This redundancy is vital for maintaining safety and providing pilots with options in critical situations.