Wheel for a lubrication system of a reduction device of a turbine engine of an aircraft
By introducing oil stabilizing grooves and distribution grooves into the lubrication system, the problem of insufficient bag filling caused by oil splashing in the lubrication system is solved, achieving continuous and uniform lubrication and improving the efficiency and life of the deceleration device.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-18
- Publication Date
- 2026-07-17
AI Technical Summary
In the existing lubrication system of the deceleration device of aircraft turbine engine, the oil spray and the impact between the oil in the tank cause splashing, resulting in insufficient filling of the bag, affecting the continuity and uniformity of lubrication, and limiting the amount of oil and lubrication efficiency of the parts to be lubricated.
Design a wheel including an oil stabilizing groove and an oil distributing groove, the stabilizing groove and the distributing groove being separated by a common radial wall, the stabilizing groove receiving oil supplied by an injector and supplying it to the distributing groove via overflow, the distributing groove being connected to different lubrication circuits to ensure maximum oil level and continuous supply.
The design of the stabilizing groove reduces splashing, ensures maximum oil level and continuous lubrication in the distribution groove, and improves the efficiency and service life of the deceleration device.
Smart Images

Figure CN122422679A_ABST
Abstract
Citation Information
Patent Citations
dispositif D'ALIMENTATION EN HUILE POUR UN REDUCTEUR A TRAIN EPICYCLOIDAL.
FR3041054A1
axially-partitioned OIL-DISTRIBUTION WHEEL, AND PLANETARY REDUCTION GEAR COMPRISING SUCH A WHEEL
FR3047279A1
Oil distribution system with at least one first area that is embodied in a rotatable manner and a second area
US20190085972A1