Air pump for aero-engine

By designing the injector nozzle with the nozzle facing the connecting rod in the air pump, the problem of insufficient output pressure during splash lubrication is solved, and the effect of maintaining the output air pressure stabilization when the air pump uses a small amount of lubricating oil is achieved, which improves the reliability of the air pump.

CN119664628APending Publication Date: 2025-03-21CHONGQING ZONGSHEN AERO ENGINE MFG CO LTD
1 Cites 0 Cited by

Patent Information

Application Number
CN202411981275.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-12-31
Publication Date
2025-03-21

AI Technical Summary

Technical Problem

Existing air pumps used in aircraft engines are prone to insufficient output pressure when using splash lubrication.

Method used

An air pump is designed, which includes a cylinder block provided with a pump chamber, a piston and a connecting rod are provided in the pump chamber, and an injector nozzle with a nozzle facing the connecting rod is connected to the cylinder block, and the cross-sectional area of ​​the oil passage at the nozzle of the fuel injector is between 1.1-1.8 square millimeters.

Benefits of technology

The lubricant is sprayed directly towards the connecting rod through the fuel injector, forming an oil mist, which improves the lubrication effect, so that the air pump can maintain the stability of the output air pressure while using a small amount of lubricant, and the output air pressure is maintained between 4.5-6bar, improving the reliability of the air pump.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

The air pump for the aero-engine comprises a cylinder body provided with a pump cavity, a piston and a connecting rod are arranged in the pump cavity, an oil nozzle with a nozzle facing the connecting rod is connected to the cylinder body, and the cross sectional area of an oil duct at the nozzle of the oil nozzle ranges from 1.1 square millimeters to 1.8 square millimeters. According to the scheme, the problem that in the prior art, when an air pump for an aero-engine adopts splash lubrication, the output pressure is prone to being insufficient is solved.
Need to check novelty before this filing date? Find Prior Art