组合发动机
- 网络Combined engine;TBCC
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一种新型吸气式与火箭组合发动机(LOCE)及先进天地往返运输系统的发展
A new type of airbreathing rocket combined engine ( loce ) and the development on Advanced Earth to orbit transportation systems
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导弹与固体火箭-冲压组合发动机协调设计
The integrated design of missile with solid rocket - ramjet combination
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液化空气循环对组合发动机性能影响的研究
Influence of Air Liquefaction Cycle on Performance of Combined Cycle Engine
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一种组合发动机变几何进气道流场特性研究
Study of flow characteristics for a variable geometry inlet on combined engine
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某组合发动机进气道抽吸作用分析
Analysis of Suction Roles for Supersonic Inlet on Combined Engine
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涡扇-冲压组合发动机性能计算模型及性能分析研究
A Model for Performance Analysis of a Turbofan-Ramjet Combined Engine
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吸气式组合发动机初步方案氢供应调节系统概念研究
A Conceptual Investigation on Hydrogen Supply Adjustment System of Air breathing Combined Engine
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涡轮-冲压组合发动机技术发展浅析
Development Study on Turbine Based Combined Cycle Engine Technology
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涡轮冲压组合发动机一体化数值模拟涡轮增压器与高压共轨柴油机的匹配研究
Research on the Calibration between Turbochargers and High Pressure Common Rail Diesel Engine
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吸气式组合发动机进口转换阀门通用特性的计算
Transforming bridge a calculation of characteristics of a transition valve for airbreathing engine
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组合发动机空气预冷换热器动态特性的数值分析
Numerical analysis of dynamic characteristics of air precooled heat exchanger for compound engine
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组合发动机系统控制方程(1)
Control Equations of Combination Engine System ( 1 )
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固冲组合发动机进气道设计
The design of inlet for combined rocket-ramjet engine
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组合发动机混合动力电动汽车燃油经济性的分析
Analysis of Combination Engine HEV on Fuel Economy
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燃烧过程中使用的燃料种类数及氧化剂种类数均没有限制。还假设了一个组合发动机作为例题。
There is no limit to the number of fuel and oxidant species used simultaneously .
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基于推力连续准则的小型涡轮冲压组合发动机模态转换过程分析
Analysis of mode transition with thrust smoothing of small turbine / ramjet combined cycle engine
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基于模块化合成程序的研究思想,采用数值模拟技术研究了涡轮冲压组合发动机性能。
Based on a modular structure program , the performance characteristic of turbo-ramjet is simulated by numerical method .
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对某组合发动机进气道设计马赫数下的三维流场进行了数值模拟。
The 3-D flow field in a inlet of combined engine with suction at different positions is numerically analyzed .
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在涡扇发动机基础上,以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。
Based on a turbofan engine , the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine .
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在高超声速推进系统中,涡轮冲压组合发动机由于有着宽广的飞行范围,良好的比冲性能,受到世界各国的普遍重视。
As a hypersonic propulsion system , turbo-ramjet received recognition because of the widely flight envelope and excellent performance such as Isp .
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作为未来航天运输系统的动力装置,吸气式组合发动机需要一个特殊的氢供应及管理系统。
As a power plant of future space transportation system , air breathing combined engine needs a special hydrogen supply and management system .
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目前,高超声速飞行器的推进系统主要有三种类型:火箭发动机、冲压发动机和组合发动机。
There are three different types of propulsion system in hypersonic aircraft , such as rocket engine , ramjet engine and combination engine .
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本文给出了一组能够描述各种组合发动机系统工作过程的通用方程组。
A set of general equations which can describe the operating process of all kinds of combination engine systems is given in this paper .
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吸气式高超声速技术是指飞行马赫数大于5、以吸气式发动机及其组合发动机为动力、在大气层和跨大气层中实现高超声速远程飞行的飞行器技术。
Airbreathing hypersonic technology studies the technology of flight vehicle for long-distance hypersonic flight in atmosphere layer or trans-atmosphere layer at flight Mach number above 5 .
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完全氢膨胀循环吸气式组合发动机性能优越,结构简单,循环布局合理。
The absolute hydrogen expansion turbine cycles of air-breathing combined turbo-ramjet engines has the advantages of good performances , simple constructions and reasonable arrangement of cycles .
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对滑跃式高超音速巡航飞行器的动力技术进行了初步研究,分析了采用火箭基组合循环发动机(RBCC)方案所需的燃料消耗。
Finally dynamic technology of soaring hypersonic cruise vehicle was preliminarily investigated . The fuel consumption of rocket based combined cycle ( RBCC ) for the soaring hypersonic cruise vehicle was analyzed .
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涡轮基组合循环发动机性能数值模拟
Numerical simulation of performance for turbine based combined cycle propulsion system
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深冷涡喷火箭组合循环发动机初步分析
Primary analysis of deep cooled turbojet liquid rocket engine combined cycle
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火箭基组合循环发动机引射模态流动分析
Flow analysis and validation of rocket ejector mode for rocket based combined cycle
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组合式发动机进气道的冷却研究
Investigation on the enhanced cooling of combined ramjet engine inlet of space craft