1)regulated two-stage turbocharging system可调二级增压系统
1.Thermodynamic analysis was conducted on a regulated two-stage turbocharging system of a heavy-duty vehicle.针对重型车用、带有调节阀的可调二级增压系统的涡轮级进行了热力学分析,推导了涡轮级绝热效率的计算公式,给出了高、低压涡轮流量和膨胀比的计算方法。
2)two stage turbocharging system二级增压系统
1.In order to study the performances of two stage turbocharging system,the special two-stage turbocharging system test bench was set up and the compressor performance experiment was carried out.为了研究所匹配的二级增压系统的性能,在专门的二级增压系统试验台架上进行了二级压气机性能试验。
2.To study centrifugal two stage turbocharging system s surge and the affecting factors,a test bench special for two stage turbocharging system is set up.为研究径流式二级增压系统的喘振及其影响因素,建立了二级增压系统压气机性能试验台架。
英文短句/例句
1.Design and Experiments for a Regulated Two-Stage Turbocharging System with a Wastegate Valve带有放气阀的二级增压系统的设计与试验
2.Configuration and Performance Comparisons between Regulated Two-Stage Turbocharging Systems with Different Valves带不同类型调节阀的二级增压系统结构与性能对比
3.The Comparison Research on Two-staged and Three-staged Sequential Turbocharging System两级和三级相继涡轮增压系统比较研究
4.ESSENTIAL MODEL FOR CYCLE DESIGN AND ALTITUDE PERFOR-MANCE ANALYSIS OF THE TWO-STAGE TURBOCHARGING SYSTEM OF GASOLINE AEROENGINES航空汽油机双级涡轮增压器系统的基本模型
5.Selection of Pilot Buses in Secondary Voltage Control of Power System;电力系统二级电压控制中枢节点的选择
6.Study on Secondary Voltage Coordinated Control Based on Multi-Intelligent System基于多智能系统的二级电压协调控制研究
7.PROGRESSING RESEARCH OF QUASI TWO STAGE COMPRESSION HEAT PUMP SYSTEM COUPLED WITH EJECTOR准二级压缩—喷射复合热泵系统的研究进展
8.Squeezing Properties of Two-Mode Squeezed Light Field Interacting with Two-Level Atoms二能级原子双模光场系统中光场压缩性质
9.Analysis of Operation Condition of Compression-Ejector Double-Stage Refrigeration System太阳能压缩-喷射二级制冷系统的运行工况分析
10.Eperimental Study and Construction of Solar Powerd Compression-Ejector Double-Stage Refrigeration System太阳能压缩-喷射二级制冷系统的系统构建与实验研究
11.Analyses of Fluctuation of Pressure on High-pressure System of Two Intensifiers双增压器增压系统中压力波动的分析
12.secondary signal system二级信号系统 次级信号系统
13.triple action skid control brake system三级降压防滑制动系统
14.Experimental Study and Optimized Design on the Quasi Two-Stage Compression Heat Pump System Coupled with Ejector;准二级压缩-喷射复合热泵系统的试验研究与优化设计
15.Simulation and Experiment Study on the Quasi Two-Stage Compression Heat Pump System Coupled with Ejector;准二级压缩—喷射复合热泵系统的性能模拟与实验研究
16.Study on Characteristics of the Ejector in Quasi Two-Stage Compression Heat Pump Coupled with Ejector准二级压缩—喷射复合热泵系统用喷射器的性能研究
17.Atomic Functor Squeezing of the System of Optical Field Interacting with Moving Two-Level Atom光场与运动二能级原子相互作用系统的原子算符压缩
18.cylinder scavenging and supercharging system气缸扫气和增压系统
相关短句/例句
two stage turbocharging system二级增压系统
1.In order to study the performances of two stage turbocharging system,the special two-stage turbocharging system test bench was set up and the compressor performance experiment was carried out.为了研究所匹配的二级增压系统的性能,在专门的二级增压系统试验台架上进行了二级压气机性能试验。
2.To study centrifugal two stage turbocharging system s surge and the affecting factors,a test bench special for two stage turbocharging system is set up.为研究径流式二级增压系统的喘振及其影响因素,建立了二级增压系统压气机性能试验台架。
3)two stage turbocharging system二级涡轮增压系统
4)Regulated two-stage turbo charging二级可变增压
5)single type supercharging system单级增压系统
6)two-stage supercharging二级增压
1.According to the performance characteristic of small UAV powered by the piston devices,a method matching small UAV\'s two-stage supercharging system was designed for realization at high altitude.分析了新一代无人机动力的发展,针对小型无人机的活塞式动力装置的性能特点,提出了一种小型无人机二级增压系统匹配的高空实现方法。
延伸阅读
火箭发动机推进剂增压系统火箭发动机推进剂增压系统propellant pressurizing system of rocket engine huo)iQn fudongli tuilinli zengya xitong火箭发动机推进剂增压系统(Pl”Pel-lant Pressurizing system of rocket engine)给液体火箭发动机泵压式输送系统的推进齐」贮箱增压的全套装置。用犷保初I几发动机工作时推进剂的额定流量;}功比离心泵发生气蚀;增加推进剂贮箱的轴向承载能力。常用的有4种:①贮气增压系统。由高压气瓶组、减压器、管路、加温器等组成。这种增压系统利用贮存在导弹或火箭土气瓶内的高压气体，经降压后直接或用发动机涡轮废气加温后给推进剂贮箱增压。系统结构较简单，但质量较重。为减轻导弹或火箭上气源的质量，在导弹或火箭起一飞之前常采用地面气源为推进剂贮箱增压。②自生增压系统。由限流嘴、换热器、管路等组成。它利用低沸点推进剂经换热器加热汽化的气体给推进剂自身增压，或利用主推进剂燃烧产生的富氧或富燃燃气经换热器降温后，分别给氧化剂贮箱或燃烧剂贮箱增压。增压气体来源于推进剂自身。系统结构较简单，质量较轻。③冲压气流增压系统。由冲压活门、气体管路等组成。它利用导弹或火箭飞行时的外界气流给推进剂贮箱增压，只适用于在稠密大气层内的飞行阶段，增压压力不够稳定。④化学增压系统。由喷嘴、压力信号器、电动活门、液体管路、气体管路等组成。它利用少量的燃烧剂或氧化剂，分别喷人氧化剂贮箱或燃烧齐lJ贮箱，进行有限度的化学反应，产生燃气给推进剂增压。系统结构较简单，适用于双组元自燃推进剂，增压压力不易控制。随着火箭推进技术的发展，冲压气流增压系统已不再应用，贮气增压系统、自生增压系统和化学增压系统仍在广泛应用。 (郑坚)
