1) ejection ram (of press)
脱模活塞<压机>
2) ejection ram
脱模活塞
3) ammonia piston compressor
活塞氨压机
4) piston compressor
活塞压缩机
1.
The dynamic analysis to the itinerary and volume of piston compressor s cylinder by using PRO/E Mechanism;
基于PRO/E Mechanism的活塞压缩机气缸行程容积动态分析
2.
The paper aims at the problem of movement interfere check for crankguide in piston compressor design,puts forward the method to carry out motion simulation for piston compressor using the Pro/MECHANISM module of Pro/E,and introduces the actual operation process.
针对活塞压缩机设计中的曲柄连杆机构运动干涉检查问题,提出利用Pro/E的机构分析模块Pro/MECHANISM实现其运动仿真,并介绍了具体的操作方法,显示出利用Pro/E软件进行压缩机设计的优势。
3.
It gives the method of setting up the parameterized standard part database by using the family table function of Pro/E,and introduces the actual operation process of setting up the standard part database for piston compressor cylinder flange.
比较了AutoCAD和Pro/E在建立标准件库方面的功能差异的基础上,提出利用Pro/E的族表功能建立参数化标准件库的方法;并以活塞压缩机气缸法兰标准件为例,介绍了具体的操作过程。
5) reciprocating compressor
活塞压缩机
1.
Study of pressure between stages calculational methods for pressure between stages of reciprocating compressor under variable operating condition;
活塞压缩机变工况下级间压力计算方法的研究
2.
The overall rule and performance of water-injection internal cooling in the reciprocating compressors was studied when crank angle equals to 180 degrees using the mathematical models in the reference~([1]).
运用文献[1]中建立的数学模型,以内止点喷水为例研究了活塞压缩机喷水内冷却过程的一般规律和性能,分析了喷液直径与喷液量对压缩机耗功、排气温度及吸气量的影响,同时也讨论了喷水内冷却过程中的传热传质性能。
3.
Proceed from thermody namic calculation of the reciprocating compressor,analyze the influence of intake and discharge pressure on reciprocating compressor′s discharge volume and power consuming.
从活塞压缩机热力计算入手,分析吸、排气压力对活塞压缩机排气量及功耗的影响,并通过试验验证理论公式推导的正确性,为进一步提高活塞压缩机的性能提供理论基础及设计依据。
6) piston-compressor
活塞压缩机
1.
0,and set up a parametric design system of the piston-compressor parts.
0来开发Solidworks,建立一个活塞压缩机零件的参数化建模体系,并通过实例说明具体设计的方法,达到缩短活塞压缩机设计周期的目的。
2.
The motion emulate of the piston-compressor guarantees the rationality and the dependability of the compressor structure from the athletic angle.
活塞压缩机的运动仿真从运动的角度保证了所设计的压缩机结构的合理性和可靠性。
3.
By comparing crankle-framework with the crankshaft-framework of piston-compressor,the article proposes specific theory analysis about crankle and crankshaft under pressure,summarizing the superiority of crankle,providing theory evidence for crankle instead of crankshaft and giving the proof of improving performance of crankle.
通过对活塞压缩机的曲柄轴结构和曲拐轴结构的对比 ,对其受力状况进行了具体的理论分析 ,总结出曲拐结构的优越性 ,为曲拐结构代替曲柄结构所带来的优越性提供理论依据 ,并为进一步提高曲拐性能提供佐证。
补充资料:活塞式航空发动机(见航空发动机)
活塞式航空发动机(见航空发动机)
piston aeroengine
huosaishi hQngK。,;,,。一口,活塞式航空发动机(piston aeroengine)~,、八中二九士几
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