Engine bearing cavity cooling structure and engine
By installing a cooling box between the bearing housing and the load-bearing casing and using film cooling holes for cooling, the problem of high temperature in the bearing cavity was solved, resulting in reduced lubricating oil consumption and improved engine reliability.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- 太仓点石航空动力有限公司
- Filing Date
- 2023-07-06
- Publication Date
- 2026-05-29
AI Technical Summary
In the existing technology, the bearing cavity of gas turbines and aero engines is prone to excessively high temperature due to high-temperature heat transfer, resulting in high oil consumption, oil coking, and premature bearing failure. This problem is particularly difficult to solve effectively in small and medium-sized engines where the structural space is limited.
An annular cooling box is installed between the bearing housing and the load-bearing casing. High-pressure cold air in the cooling box is used to cool the bearing cavity, the inner cavity of the load-bearing casing, and the rim sealing cavity through cross-shaped air film cooling holes and through holes, thus isolating heat radiation and carrying away heat.
It effectively reduces bearing cavity temperature, improves lubrication, reduces oil consumption, and enhances engine reliability and safety.
Smart Images

Figure CN116696555B_ABST