In order to strengthen emission controlling of the carburetor motorcycle engines,the metering characteristics of carburetor are adjusted,combustion chamber as well as intake and exhaust ducts are further optimized,and secondary air injection system and oxidation type catalytic converter.
为此,通过化油器燃油供给特性的调整及燃烧室与进排气道结构优化,采用二次空气喷射系统和催化转化器,运用曲轴箱闭式通风装置减低曲轴箱窜气污染物,将现行生产的各种化油器式中小排量摩托车排气污染物控制在GB14622-2002排放限值内,实现摩托车发动机排放控制的强化。
In order to enhance the air compensating effect of the secondary air injection system, a model for a motorcycle engine is set up and the performances of the model JS125-12A are calculated and analyzed by using the engine performance analyzing software package of AVL BOOST.
为了提高二次空气喷射系统的补气效果,建立了摩托车发动机模型,应用内燃机性能分析软件AVLBOOST,对JS125-12A型摩托车发动机进行性能计算,并与试验值进行了对比分析。
The structure and recondition of the secondary air injection system;
二次空气喷射系统结构与检修
secondary air injection relief valve
二次空气喷射减压阀
Computation of three-dimensional flow field in secondary gas injection for thrust vectoring nozzle
气体二次喷射矢量喷管三维流场计算
Analysis of Second Gas Injection Affecting Factor on SRM Thrust Vector Control
气体二次喷射SRM推力矢量控制影响因素分析
external air (injection) manifold
外装式空气喷射总管
air injection diesel engine
空气喷射柴油发动机
steam-jet air ejector
蒸汽喷射式空气抽逐器
compression operated fuel injection system
压缩空气燃油喷射系统
A study for thrust vector control of aerospike nozzle based on second injection
塞式喷管二次喷射推力矢量控制研究
Unsteady characteristic research of startup process of secondary hot gas injection thrust vector control system
燃气二次喷射推力矢量控制系统启动过程非定常效应研究
Injection characteristics of the supercritical jet fuel injected into the atmospheric environment
超临界航空煤油喷射到大气环境的喷射特性
exhaust pulse air injection
(抽吸式) 排气脉冲空气喷射
To spout moist air from the blowhole.Used of a whale.
喷水鲸鱼通过鼻子喷射出满是水的空气
pulse air induction reactor (PAIR)
脉冲负压空气喷射净化器
To spout moist air from the blowhole.
鲸鱼通过鼻子喷射出满是水的空气。
Thoroughly clean the area around the injector with compressed air.
用压缩空气彻底清理喷射器周围区域。
propels a projectile by compressed air.
通过压缩空气来喷射子弹的枪支。
Until the World War 2，the jet is used.
直到二次世界大战才使用喷气式飞机。
The jet flow radiation computational method of axis-symmetry nozzle and rectangle nozzle are also discussed.
研究了轴对称喷管和二元矩形喷管喷气流辐射的计算方法。