1) acops: automatic cpu overheat prevention system,cpu
过热预防系统
2) Thermal protection system
防热系统
1.
Health Monitoring for Thermal Protection Systems on Reusable Launch Vehicles;
重复使用跨大气层飞行器防热系统健康监控技术研究
2.
With the development of reusable launch vehicles, the thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system.
随着可重复使用航天器的发展,热防护系统在向着防热-结构-推进系统一体化设计的方向发展,与此同时,整个防热系统在总起飞重量中所占的重量比例也在降低,而使用温度升高,即要求防热结构日趋先进。
3.
With the development of reusable launch vehicles, thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system.
随着可重复使用航天器的发展,热防护系统向着防热-结构-推进系统一体化设计的方向发展,与此同时,整个防热系统在总起飞重量中所占的重量比例也在降低,而使用温度升高,即要求防热结构日趋先进。
3) preheating system
预热系统
1.
Design of a fuel preheating system for diesel locomotive;
一种内燃机车燃油预热系统设计
2.
A feasible discussion on dry materiel preheating systemin the carbon green anode production;
干料预热系统在炭素生阳极生产中的可行性探讨
3.
In view of the technical problems of preheating system of the gas-burning active lime shaft kiln, the double preheating system is transformed two times so as to make the air and gas preheating effect obvious and the calcine working condition stable and improve the quality of active lime and reduce the heat consumption.
针对活性石灰气烧竖窑预热系统存在的技术问题,通过两次对双预热系统的技术改造,空气、煤气预热效果明显,稳定了煅烧工况,提高了活性石灰质量,降低了热耗。
5) high coolant temperature protection
冷却液过热预防
6) thermal protection system
热防护系统
1.
This paper mainly introduces the application research progress of CFRCMCs in thermal protection system,rocket engine and scramjet.
主要介绍了国外CFRCMCs在热防护系统、火箭发动机和超燃冲压发动机上应用的研究进展。
2.
The combined radiation /conduction heat transfer in thermal protection systems(TPSes)for reusable launch vehicles was analyzed using the APDL language of ANSYS to simulate reentry aerodynamic heating conditions.
针对可重复使用飞行器再入过程中热防护系统的复杂辐射-传导传热问题,采用有限元方法并结合仿真软件ANSYS的参数化分析语言APDL,对可重复使用飞行器热防护系统进行参数化求解,模拟再入条件下热防护系统内部辐射和传导复合换热,预测内部瞬态温度响应。
3.
Thermal protection system (TPS) is one of the key technologies for space vehicle, especially for reusable launch vehicles (RLV).
热防护系统是航天飞行器 ,特别是重复使用运载器的关键技术之一。
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条