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
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。
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。
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。
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。
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。
The article briefly introduces the box cooler and thermal antifouling system(TAS)with their application in the 6800 DWT MPV.
结合6800t多用途船的实例对箱式冷却器在现代船舶中的使用情况作简单介绍,并对热防污系统(TAS)的应用作简要推介。
The unique function of the thermal protection system(TPS) is to maintain the vehicle structural temperature within allowable limit during re-entry aerodynamic heating, which is critical to a new generation of reusable launch vehicles(RLV).
先进热防护系统(TPS)的设计是决定可重复使用运载器(RLV)成败的关键技术之一。
Such aircrafts suffer extremely thermal environment during flight, so the forecast of aerodynamic heating and thermal protection system (TPS) design is one of the key technologies of hypersonic vehicle design and manufacture.
由于高速飞行器的气动加热与热防护系统的热响应是耦合的,通过数值方法进行气动热与热结构的耦合分析,需要对飞行器进行整体建模分析,涉及高温空气的化学非平衡边界层传热,湍流模型和复杂结构传热模型,需要耗费大量的计算机资源和时间;采用风洞进行试验且不说耗费惊人的人力和财力,仅建造能模拟马赫数10以上的飞行条件的风洞就是一个巨大的挑战。
It can simulate not only the thermal /pressure condition subjected by the outer surface of TPS but also the vacuum pressure subjected by the inner surface of TPS.
介绍了一种能模拟可重复使用运载器热防护系统内、外表面气动热和压力环境的热真空模拟试验装置,该装置不仅能模拟TPS外表面所受气动热和气动压力条件,还能模拟TPS内表面的真空压力环境。
Conceptual Research of Leading Thermal Protection System With Unified Heat Management
统一热管理的疏导式防热系统概念研究
Health Management for Thermal Protection System on RLV and Landing Gear Design for an UAV;
RLV防热系统健康管理及某型无人机起落架设计
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
Research on Erodible Mechanism and Protected Technology of Steel in Oil Field Hot Water System;
油田热水系统钢材的腐蚀与防护研究
Design and Analysis of Metallic Thermal Protection System Attachment;
金属热防护系统连接结构设计与分析
Research on Thermal Insulating Mechanism and Thermal Insulating Efficiency of Thermal Insulations of Metallic Thermal Protection System;
金属热防护系统隔热材料的隔热机理及隔热效率研究
Three-dimensional conjugate heat transfer simulation for the surface temperature of wing hot-air anti-icing system
三维内外热耦合计算热气防冰系统表面温度
Parallel One-dimensional Model for Transient Thermal Analysis of Metallic Thermal Protection System
金属热防护系统瞬态热分析的并联一维模型
A Study on Numerical Simulation Method for Transient Heat Transfer in Metallic Thermal Protection Systems
金属热防护系统瞬态传热数值模拟方法研究
Dynamic supervise control network to prevent stealing heat in central heating system
集中供热系统中防止“窃热”行为的动态监控网络
Reusable Launch Vehicle Thermal Protection System Performance Study;
可重复使用运载器热防护系统性能分析研究
Design of Structural Parameters about Honeycomb Sandwich on ARMOR Thermal Protection Systems
ARMOR热防护系统蜂窝夹层板结构参数设计
Safety and preventive measure for molten salt heating system in alumina refinery
氧化铝厂熔盐加热系统的安全防范措施
Research on Vehicle Collision Avoidance System Based on Infrared Imaging Sensor
基于热红外成像传感器的汽车防撞系统研究
Study of Thermo-Mechanical Coupled Computation for Thermal Protection System of Reusable Launch Vehicle;
可重复使用运载器热防护系统热/力耦合数值计算研究
Simulation and Test of Aeroheating and Thermal Response of TPS for Hypersonic Vehicle
高超声速飞行器气动加热与热防护系统性能的仿真与试验研究
Diagnosis and Preventing from Gas Explosion in End-port Regenerative Furnace
热煤气蓄热式马蹄焰玻璃熔窑系统煤气“放炮”原因分析及预防
Analysis of diathermancy about unglued structure of thermal protection systems of reusable launch vehicles
可重复使用运载器热防护系统胶层脱胶传热分析