The transient thermal analysis of the main thrust ball bearing was performed during fuelcut off for an aeroengine oil system.
对在航空发动机滑油系统断油时的主推力球轴承瞬态热进行了分析。
2
Control strategy for engine running control such as starting, idling, smart power output, decrease fuelcut off, limp home and over-speed protection are designed.
设计了发动机的起动、怠速、智能功率、减速断油和跛行回家等柴油机运行控制策略。
3
Mechanical efficiency obtained by the new method is compared with that obtained by conventional individual cylinder fuelcut method and a good agreement is achieved.