‘壹’ 空气压缩机论文
一、概述
可编程控制器（PLC）是一种新型的通用控制装置，他将传统的继电器控制技术、计算机控制技术和通信技术融为一体，专为工业控制而设计，具有功能强、通用灵活、可靠性强、环境适应性好、编成简单、使用方便、体积小、重量轻、功耗低等一系列优点。近年来，随着可编程控制器的日渐成熟，越来越多设备的控制都采用PLC控制器来代替传统的继电器控制，并取得了很好的经济效益。
空气压缩机使矿山生产重要的四大固定设备之一，它生产压缩空气，用以带动凿岩机、风动装岩机等设备及其他风动工具。其能否安全运行直接影响着煤矿生产的产量和效益问题。影响其安全生产的要素主要有空压机的超温、超压、断水、断油等因素。
随着煤矿现代化的发展，矿山对矿山设备的要求越来越高,建设本质安全性矿山已成为煤矿生产建设的核心。矿山设备不断更新，不断进步，可靠性、易操作性、可监视性、易维护性等已是最基本的要求了。用继电器搭成的控制电路具有可靠性差、不易维护、不易监视，已不能适应当前的要求。现在迫切需要可靠性高、易维护、易操作、可监视并且价格不高这样的控制器来代替继电器搭成的电路。随着电子技术、软件技术、控制技术飞速发展，可编程控制器（PLC）发展迅猛，性能很高，价格较为合理，与继电器搭的控制电路比具有非常大的优势。许多矿山设备已选用了PLC来代替比较重要的设备控制。传统的保护主要采用分离仪表，其可靠性差、集程度低、费用高，不能有效的满足矿山设备投入的经济性和安全性的要求。
本文笔者采用可编程控制器（PLC）作为核心控制器，通过检测仪器为PLC提供控制中所需要的信号参数对空压机进行自动巡回检测控制。进行监控的主要参数有空压机高低压缸温度、润滑油温度、电动机温度、风包温度、出水温度；高低压缸压力、风包压力、润滑油压力；高/低压、中/后冷却水断水检测等参数。
二、控制功能和控制原理
1. 保护控制功能
⑴、 电机电流和电压的检测。
⑵、 一二级缸、油压、风包压力检测。
⑶、 一二级排气温度、油温、电机温度检测。
⑷、 电动机的延时启动。
⑸、 电机的无水运转。
2. 保护控制原理
在启动主机之前先将水源电磁阀和放空电磁阀都打开，在冷却水压和流量达到规定值条件下，可以进行空压机的空载起动，然后延时自动关闭放空电磁阀，空压机进行正常运行。启动时允许低油压启动，设置一定时间后对油压进行监控。在停机时，按复位按钮放空电磁阀打开，经30秒延时后切断主电源。实现空压机的停机，同时关闭水源电磁阀和放空电磁阀。在保户状态时，以上监控参数有一个在设定范围内发生故障，产生报警信号，同时打开放空电磁阀，压缩机减载运行，延时30秒故障不消除自动机停机。
⑴. 控制分布图
1-1压缩机控制分布图
⑵. 控制通讯原理
现场总线PROFIBUS可以实现数字和模拟输入/输出、智能信号装置和过程调节装置与可编程控制器PLC和PC之间的数据传输，把I/O通道分散到实际需要的现场设备附近。PROFIBUS一方面覆盖了传感器/执行器领域的通信要求，另一方面又具有单元级领域的所有通信网络通信功能。他支持高速的循环数据通信，以满足了实时监控的要求。
1-2系统控制通讯图
三、信号采集S7-200为每个本机数字量输入提供脉冲捕捉功能。脉冲捕捉功能允许PLC捕捉到持续时间很短的脉冲。而在扫描周期的开始，这些脉冲不是总能被CPU读到。当一个输入设置了脉冲捕捉功能时，输入端的状态变化被锁存并一直保持到下一个扫描循环刷新。这就确保了一个持续时间很短的脉冲被捕捉到并保持到S7-200读取输入点。
本设计需对下列参数进行采集：
(1)、压力信号分别为1级缸、2级缸及储风缸压力、润滑油压力4点；
(2)、温度信号为1级缸排气温度、2级缸进气温度、风包温度、油温、电机温度以及冷却水出口温度共6点；
(3)、电量信号为主电机电流1点，电源电压1点，共2个点。
(4)、流量检测有高低/压端2点，中/后冷2点共4点。
采集参数总计为4+6+2+4=16个。
对上述参数采集后，首先判断有关参数是否异常，然后形成动态数据表格进行实时巡回显示，并存储起来而供以后进行随机查询。
四、系统软件设计
本系统主要是以保护为主，根据《煤矿安全规程》的要求和空压机的保护原理，其控制的软件设计流如下。
五、结束语
该系统主要是以S7-200 为核心控制器，PROFIBUS作为通讯桥梁，通过检测元件为控制其提供检测信号，以此达到保护控制的目的。在本文的编写过程中，得到了张集矿机电科多位领导的大力支持，在此致以诚挚的谢意！同时感谢西门子（中国）有限公司自动化驱动集团提供的大量资料。
‘贰’ 制冷压缩机的科技论文的撰写思路
摘要 随着时代的不断发展，制冷技术也在不断的发展，自然界的客观规律是热量传递总是从高温物体传向低温物体，直到温度相等。但是在消耗功可使低温物体传热量到高温物体，人工制冷就是使热量从低温物体传递到高温物体的技术。制冷技术的应用也日益的广泛，现已渗透到人们生活生产各个领域中，并在改善人们的生活质量方面发挥着巨大作用。在此简单介绍制冷技术及应用。 关键词：吸附制冷 磁制冷 循环系统 热电制冷 环保 节能 1 吸附制冷技术 吸附式制冷技术非常适用于太阳能和地热能等可再生能源的应用和余热、废热的回收,这也是其与压缩式制冷技术竞争的主要优势之一。 1. 1 原理
‘叁’ 如何写关于压缩机，泵的论文
全封闭制冷压缩机的发展趋势 【摘要】 详细介绍了全封闭制冷压缩机的发展趋势和前景。引用大量的数据证明各种压缩机的发展空间和必然性。从而为各行业使用制冷压缩机提供了可靠的数据和指导说明。 【关键词】 电磁振动式压缩机；电动式压缩机；发展趋势 0引言 发表职称论文，就找ABC论文坊： http://www.lwabc.net 制冷压缩机质量的好坏将直接影响着电冰箱、空调器等小型制冷设备的制冷效果、使用寿命、噪音和震动等多种性能。就制冷压缩机的工作原理与结构而言，形式多样，性能各异。现在生产的小型制冷设备采用的全封闭式压缩机，按其结构特性可分为电磁式和电动式两大类。而电动式又可分为往复活塞式、旋转活塞式和涡旋式3种类型。以上几种全封闭制冷压缩机的性能特点。 l 电磁振动式压缩机 电磁振动式压缩机有以下3种：11动圈式电磁振动型；2)动铁芯式电磁振动型；3)悬吊动磁铁式电磁振动型。其中，动圈式在全封闭式制冷压缩机中被实际应用，它是利用通以交流电流的线圈产生的交变磁场与永久磁场之间相互作用，直接驱动活塞作往复运动的压缩 机。其特点是结构简单、零部件少、加工精度要求不高、容易制造。因此从20世纪50年代开始就用于容积较小的电冰箱。ABC论文坊但从另一方面，由于电源频率变化引起的制冷量变化大，且50 Hz和60 Hz不能通用，存在着因排气、吸气压力引起行程变化等问题，使活塞行程的长短随负荷的变化而改变，同时机内弹簧作高频谐振，易产生弹性疲劳，因此一般只适用于生产100 W 以下的压缩机。而动铁芯式和悬吊动磁铁式电磁振动型由于只在研究阶段还没有实际应用。故此不作介绍。 2 电动式压缩机 2．1 往复活塞式压缩机 按其结构分为滑管式和连杆式压缩机两类。 2．1．1 滑管式压缩机 滑管式压缩机产生于20世纪60年代，它是往复活塞式压缩机的一种类型。其特点是结构简单，工艺性好，成本较低，对零部件的加工精度要求不高，制造和装配都比较容易，所以发展较快。目前这类压缩机在国内外的电冰箱生产中应用比较普遍。缺点是活塞与缸壁间的侧力较大、磨擦功耗大、能效比偏低，因此目前滑管式压缩机正在进入衰退期，将逐渐被连杆式压缩机或旋转式压缩机所取代。 2．1．2 连杆式压缩机 连杆式压缩机也属往复活塞式，是电冰箱采用时间较早的一种。在20世纪5O年代以前生产的电冰箱几乎都是采用连杆式压缩机。其特点是运转比较平稳、噪声低、磨损小、使用寿命长、能效比较高、工作可靠、综合性能优良。但由于零部件形状复杂，加工精度要求较 高，工艺难度较大，因此其发展一度受到限制，在电冰箱及其它小型制冷设备中被滑管式和旋转式压缩机所取代。近几年来随着机械工业的不断发展，对其结构进行了多方面的技术改进。目前连杆式压缩机又成为电 www.lwabc.net 冰箱压缩机的主导产品。总需求是有较大的提升【1_。近年来世界各电冰箱生产大国，尤其是日本、意大利、美国等国对往复式压缩机的制造技术进行了多方面的改造，从而使连杆式压缩机的各项性能都有了很大的提高。因此，有重新成为电冰箱压缩机主导产品的趋势。 2_2 旋转式压缩机 旋转式压缩机的电机无需将转子的旋转运动转换为活塞的往复运动，而是直接带动旋转活塞作旋转运动来完成对制冷剂蒸气的压缩。这种压缩机更适合于小型空调器，特别是在家用空调器上的应用更为广泛。如美国通用电器公司和沃普公司生产的旋转式压缩机都设计了较好的防过热和润滑装置。它采用把冷凝器处的部分制冷液用配管引至压缩室，使之在气缸内喷射的冷却方式，提高了冷却效果。为了防止把大量的制冷液直接吸人气缸内，产生液击，在吸气回路的压缩机前部设有气液分离器，润滑油和制冷液一旦进入器内 则制冷液在气液分离器内蒸发，压缩机吸人的是气体；润滑油从气液分离器下方的小孔中缓缓地连续 少量进入压缩机，用这种方法防止液击[21。油泵给油的方法是在转轴下端装设两个齿轮状的叶轮，它与转轴一同转动。对油施加离心力，从转轴中心孑L把油导向上方。另外，在轴的外表面上开有螺旋状的油槽，实现对轴承部位的给油。作为安全措施。在压缩机顶部装有过 负荷继电器，这种继电器是用感温板感受压缩机内部高压气体的温度，当达到一定的温度后，继电器动作，压缩机停止运转，用这种方法防止电动机烧毁，因此说旋转式压缩机是一种很有发展前景的压缩机。其主要优点是：由于活塞作旋转运动，压缩工作圆滑平稳，平衡性能好，另外旋转式压缩机没有余隙容积，无再膨胀气体的干扰，因此具有压缩效率高、零部件少、体积小、重量轻、平衡性能好、噪音低、防护措施完备和耗电量小等优点。缺点是压缩机对材质、加工精度、热处理、装配工艺及润滑系统要求较高，由于要靠运动间隙中的润滑油进行密封，为从排气中分离出油，机壳内须做成高压，因此，电动机、压缩机容易过热，如果不采取特殊的措施。在大型压缩机和低温用压缩机中是不能使用的。由于它比其它类型的压缩机有较明显的优势，所以它得到广泛了推广应用。如国产上菱BCD一180 W、阿里斯顿BCD-220 W 等电冰箱都采用了旋转式压缩机。尤其在家用空调器上的应用就更为普遍，从发展的趋势看旋转式压缩机今后有可能成为市场的主导产品。 2．3 涡旋式压缩机 涡旋式压缩机是20世纪8O年代发展起来的新型产品。它效率高，噪声低，体积小，重量轻，不需要排气阀组，工作的可靠性及容积效率都较高，允许气体制冷剂中带少量液体，输气效率高，气体泄漏少，可较好地运用于小型热泵系统、小型空调等。综上所述，几种压缩机的性能特点，我们不难看出经多年的技术改造，连杆式压缩机在一定的时期内仍有明显的优势，而旋转式压缩机则是一种新型的产品，特别是在空调器上的应用更为广泛，必将成为制冷产业的主导产品。通过对往复式和旋转式压缩机的性能试验比较可知，往复式和旋转式压缩机，启动后排气、吸气压力的时间变化特性不同，电动机上的负荷转矩由吸、排气压力的大小确定，在往复式的情况下，投入运转几分钟内至十几分钟后，排气压力出现峰值，对于电动机，为了承受这个尖峰负荷，需要比稳定运转时所需转矩大得多f2～4倍)[31。而旋转 式压缩机，由于不存在刚刚启动后的峰值，所以，只要有一般稳定运转时所需的转矩即可，因此可以实现电动机的小型化，这也是它今后发展优势所在。 参考文献 [1]胡鹏程，赵清．电冰箱、空调器的原理和维修【M】．北京：电子工业出版社．1995：1 14—148． [2]吴业正．制冷原理及设备【M】(第2版)．西安：西安交通大学出版社．2006． [3]赵春怡，王志强．活塞式单机双级制冷压缩JJL[M]．北京：机械工业出版社．2003．
‘肆’ 哪位大侠可以给我发一个《输气站场压缩机的日常操作与维修》的论文啊 大学毕业论文那种
草 雷哥 我也需要啊
‘伍’ 急求3L-15/12型空气压缩机的毕业设计论文的cad图纸. 类似的也行
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‘陆’ 跪求《离心压缩机二段冷却期设计》 相关论文 英语原文及翻译
可以帮你下载英文原版论文。
‘柒’ 空气压缩机2016年毕业论文
空气压缩机的， 能聊来；。
‘捌’ 求一篇压缩机方面的英文论文（最好是隔膜压缩机的）3000字以上
The Basics
A jet engine can be divided into several distinct sections: intake, compressor, diffuser, combustion chamber, turbine, and exhaust. These sections are much like the different cycles in a four-stroke reciprocating engine: intake, compression, power and exhaust. In a four-stroke engine a fuel/air mixture is is brought into the engine (intake), compressed (compression), and finally ignited and pushed out the exhaust (power and exhaust). In it's most basic form, a jet engine works in much the same way.
* Air comes in the front of the engine where it enters the compressor. The air is compressed by a series of small spinning blades aptly named compressor blades and leaves at a high pressure. The pressure ratio between the beginning and end of the compressor can be as much as 48:1, but almost always 12:1 or more.
* The air now enters the diffuser, which is nothing more than an area where the air can expand and lower it's velocity, thus increasing its pressure a little bit more.
* The high pressure air at the end of the diffuser now enters the combustion chamber where it is mixed with fuel, ignited and burned.
* When the fuel/air mixture burns, the temperature increases (obviously) which makes the air expand.
* This expanding gas drives a set of turbine blades located aft of the combustion chamber. At least some of these turbine blades are connected by a shaft to the compressor blades to drive them. Depending on the type of engine, there may be another set of turbine blades used to drive another shaft to do other things, such as turn a propeller or generator.
* The left over energy not extracted by the turbine blades is pushed out the back of the engine (exhaust section) and creates thrust, usually used to drive an airplane forward.
The types of jet engines include:
* Turbojet
* Turbofan
* Turboprop
* Turbo shaft
Turbojet
The turbojet is the simplest of them all, it is just as described in "The basics" section. This style was the first type of jet engine to be used in aircraft. It is a pretty primitive style used mostly in early military jet fighters such as the F-86. Its use was discontinued, for the most part, in favor of the more efficient turbofans. Actually, I should clarify that. Each type of engine is most efficient under certain conditions. Turbojets are most efficient at high altitudes and speeds above the speed of sound. See the diagram at the end of this page for relative efficiencies of each style engine.
Turbofan
Turbofans make up the majority of jet engines being proced and used today. A turbofan engine uses an extra set of turbine blades to drive a large fan, typically on the front of the engine. This fan differs from a propeller in that there are many small blades and they are inside of a ct. The fan sits just in front of the normal intake, some of the air driven by this fan will enter the engine, while the rest will go around the outside. The amount of air that bypasses the engine is different for each type of airplane. The different styles are called high and low bypass engines. Bypass ratio is the ratio of how much air goes through the fan, to how much goes through the engine. Typical bypass ratios would be 1:1 for a low bypass and 5:1 or more for a high bypass. Low bypass engines are more efficient at higher speeds, and are used on planes such as military aircraft, while high bypass engines are used in commercial airliners.
Turboprop
Turboprops are similar to turbofans in that they incorporate an extra set of turbine blades used to drive the propeller. Unlike the turbofan engines, nearly all the thrust proced by a turboprop is from the propellor, hardly any thrust comes from the exhaust. These engines are used mostly on smaller and slower planes such as commuter aircraft that fly to the smaller airports. As you can see from the efficiency chart below, turboprops are very efficient over a fairly wide range of speeds. They would probably be used more often on large transport aircraft, except for one problem: they have propellors. The general public does not like propellors, as they appear to be old-fashioned and unsafe. However, the military knows better and uses them on several large transport aircraft.
Turbo shaft
Turbo shaft engines are very similar to turboprop engines, but instead of driving a propellor, they are used to drive something else. Many helicopters use them to drive their rotors, and airliners and other large jets use them to generate electricity. Also, the Alaska Pipeline uses them at the pump stations to pump oil.
Overall
Overall the big difference between these engines is how they take a chunk of air and move it. Newton's third law states that Force equals mass times acceleration. Applying this to turbine engines: the turboprop takes a large chunk and accelerates it a little bit, while the turbojet takes a small chunk and accelerates the heck out of it, and the turbofan is somewhere in between these two.
These different methods of moving air also have to do with how much noise each engine makes. The turbojet makes the most noise because there is a large difference in velocities of the blast of air coming out the exhaust and the surrounding air. The air from the fan on a turbofan engine "shields" the blast in the center by having the slower moving air from the fan surround it. Then the turboprop is the quietest of all because the air it's moving is relatively slow.
A pressure - volume diagram (or a P-V diagram) is a useful tool in thermodynamics. In this case, it relates the pressure and volume of the gas moving through the engine at different stages. A P-V diagram can also be helpful in finding the work output of an engine. Work equals the integral of pressure with respect to volume. Or is simpler form, work equals the area enclosed in the diagram above. The above cycle is the Brayton cycle, or the cycle used by aircraft gas turbine engines.
Explanation of the above cycle:
* Air enters the inlet at point 1 at atmospheric pressure.
* As this air passes through the compressor (from point 1 to 2), the pressure rises adiabatically (no heat enters or leaves the system).
* Now the air enters the combustion chamber (from point 2 to 3), is mixed with fuel, and burned at a constant pressure.
* Finally, the air goes through the turbine and out the exhaust (point 3 to 4) where the gases expand and do work. Thus, the pressure drops and the volume increases.
The Compressor
There are two main styles for turbine compressors: the axial and the centrifugal.
The Axial Compressor
* The axial type compressor is made up of many small blades, called rotor vanes, arranged in rows on a cylinder whose radius gets larger towards the back (as can be seen from the above picture). These blades act much like small propellors.
* In between these rotor vanes are stator vanes which stay in a fixed spot and straighten the air coming out of the previous stage of rotor vanes before it enters the next stage.
* On some newer engines, the angle of these stator vanes can be adjusted for optimum efficiency.
* Each stage (1 row of rotor and stator vanes) generally provides for a pressure rise of about 1.3:1 (so after the first stage, the pressure would be 1.3 above atmospheric, after the second it would be 1.69, 2.2, etc...).
The Centrifugal Compressor
* Air enters the centrifugal compressor at the front and center. The blades then sling the air radially outwards where it is once again collected (at a higher pressure) before it enters the diffuser.
* Pressure rise per stage is usually about 4 to 8:1 (higher than axial). These can be sombined in series (that is the exit of the first leads to the entrance of the next) to proce a greater pressure rise. But more than two stages is not practical.
- Jet engines are rated in "pounds of thrust," while turboprops and turboshaft engines are rated in "shaft horsepower" (SHP). This is because it is difficult to hook up a dynamometer (power measuring device) to the column of air coming out of a jet engine, while it is easy to hook one to the shaft of a turboprop.
- An equivalent measure to horsepower is thrust horsepower (THP). THP = (Thrust x MPH) / 375. or THP = SHP x 80% in the case of turboprop engines (the 80% is because the propeller "slips" a little in flight).
- Exhaust gases exit the exhaust at upwards of 1000 mph or more and can use 1000 gallons of fuel/hour or more.
- Turbine engines run lean. Unlike gasoline engines, turbines take in more air than they need for combustion.
- Fuel can be injected into the exhaust section to burn with this unused air for extra thrust. This is called an afterburner.
- A water/methanol mixture can be injected into the intake to increase the air density, and thus increase thrust.
- Turbine engines can be built on a small scale as well. The turbine pictured below has a diameter of 4mm and runs at 500,000 rpm. It was built by at MIT for purposes of powering an aircraft with a wing span of about 5 inches that was projected to fly about 35 - 70 mph with a range of about 40 - 70 miles.
micro turbine
- The ignition system on turbine engines is only necessary for starting, afterwards it is self sustaining. In jets, the ignition system is also turned on for added saftey in "critical" stages of flight, such as takeoff and landing.
- A device similar to a spark plug is used for the ignition process, but it has a larger gap. The spark is about 4 to 20 Joules (watts/second) at about 25000 volts and occurs between 1 and 2 times per second.
- Turbine engines will run on just about anything, they prefer Jet-A (AKA diesel, kerosene, or home heating oil), but can burn unleaded, burbon, or even very finely powdered coal!
- The above snowmachine uses an Allison turbine engine, a very common engine in helicopters (such as the Bell 206 Jet Ranger shown below). A lot of horsepower can be put into a small package! Note the intake and compressor are at the front of the engine, then the two side tubes take the compressed air and bring it around back to the combustion chamber and turbine and the exhaust exits out the middle. There are many engines out there with strange configurations like this.
Communications Technology
Your Rights and what the Data Protection Commissioner can do to help
Right of Access
The personal information to which you are entitled is that held on
computer or in a manual filing system that facilitates access to
information about you. You can make an access request to any
organisation or any indivial who has personal information about you.
For example, you could make an access request to your doctor, your
bank, a credit reference agency, a Government Department dealing with
your affairs, or your employer.
If you find out that information kept about you by someone else is
inaccurate, you have a right to have that information corrected (or
"rectified"). In some circumstances, you may also have the information
erased altogether from the database - for example, if the body keeping
the information has no good reason to hold it (i.e. it is irrelevant
or excessive for the purpose), or if the information has not been
obtained fairly. You can exercise your right of rectification or
erasure simply by writing to the body keeping your data.
In addition, you can request a data controller to block your data i.e.
to prevent it from being used for certain purposes. For example, you
might want your data blocked for research purposes where it held for
other purposes.
If an organisation holds your information for the purposes of direct
marketing (such as direct mailing, or telephone marketing), you have
the right to have your details removed from that database. This right
is useful if you are receiving unwanted "junk mail" or annoying
telephone calls from salespeople. You can exercise this right simply
by writing to the organisation concerned. The organisation must write
back to you within 40 days confirming that they have dealt with your
request.
Right to complain to the Data Protection Commissioner
What happens if someone ignores your access request, or refuses to
correct information about you which is inaccurate? If you are having
difficulty in exercising your rights, or if you feel that any person
or organisation is not complying with their responsibilities, then you
may complain to the Data Protection Commissioner, Mr Mead, who will
investigate the matter for you. The Commissioner has legal powers to
ensure that your rights are upheld.
The Data Protection Commissioner will help you to secure your rights:
* with advice and information
* by intervening directly on your behalf if you feel you have not
been given satisfaction
* by taking action against those failing to fulfil their
obligations.
SEE APPENDIX 2 FOR CASE STUDY
Ergonomics
Ergonomics (from Greek ergon work and nomoi natural laws) is the study
of designing objects to be better adapted to the shape of the human
body and/or to correct the user's posture. Common examples include
chairs designed to prevent the user from sitting in positions that may
have a detrimental effect on the spine, and the ergonomic desk which
offers an adjustable keyboard tray, a main desktop of variable height
and other elements which can be changed by the user.
Ergonomics also helps with the design of alternative computer input
devices for people who want to avoid repetitive strain injury or
carpal tunnel syndrome. A normal computer keyboard tends to force
users to keep their hands together and hunch their shoulders. To
prevent the injuries, or to give relief to people who already have
symptoms, special split keyboards, curved keyboards,
not-really-keyboards keyboards, and other alternative input devices
exist.
Ergonomics is much larger than looking at the physiological and
anatomical aspects of the human being. The psychology of humans is
also a key element within the ergonomics discipline. This
psychological portion of ergonomics is usually referred to as Human
factors or Human factors engineering in the U.S., and ergonomics is
the term used in Europe. Understanding design in terms of cognitive
workload, human error, the way humans perceive their surrounds and,
very importantly, the tasks that they undertake are all analysed by
ergonomists.
[IMAGE]
With video conferencing consideration should be taken in positioning
of camera and screens so as to avoid neck strain.
Codec
1. (COder/DECoder or COmpressor/DECompressor) Hardware or software
that encodes/compresses and decodes/decompresses audio and video
data streams. The purpose of a codec is to rece the size of
digital audio samples and video frames in order to speed up
transmission and save storage space. The goal of all codec
designers is to maintain audio and video quality while compressing
the binary data further. Speech codecs are designed to deal with
the characteristics of voice, while audio codecs are developed for
music. Codecs may also be able to transcode from one digital
format to another; for example, from PCM audio to MP3 audio.
The codec algorithms may be implemented entirely in a chip or entirely
in software in which case the PC does all of the processing. They are
also commonly implemented in both hardware and software where a sound
card or video capture card performs some of the processing, and the
main CPU does the rest.
When analog signals are entered into a computer, cellphone or other
device via a microphone or video source such as a VHS tape or TV,
analog-to-digital converters create the raw digital audio samples and
video frames. Speech, audio and video codecs are typically lossy
codecs that compress data by altering the original format, which is
why "codec" means "encoder/decoder" and "compressor/decompressor." If
a codec uses only lossless compression in which the original data is
restored exactly, then it would not be a coder/decoder. This is a
subtle point, but the two meanings of the acronym have been confusing.
LAN
A local area network (LAN) is a computer network covering a local
area, like a home, office or small group of buildings such as a
college. The topology of a network dictates its physical structure.
The generally accepted maximum size for a LAN is 1000m2. LANs are
different from personal area networks (PANs), metropolitan area
networks (MANs) or wide area networks (WANs). LANs are typically
faster than WANs.
The earliest popular LAN, ARCnet, was released in 1977 by Datapoint
and was originally intended to allow multiple Datapoint 2200s to share
disk storage. Like all early LANs, ARCnet was originally
vendor-specific. Standardization efforts by the IEEE have resulted in
the IEEE 802 series of standards. There are now two common wiring
technologies for a LAN, Ethernet and Token Ring. Wireless technologies
are starting to evolve and are convenient for mobile computer users.
A number of network protocols may use the basic physical transport
mechanism including TCP/IP. In this case DHCP is a convenient way to
obtain an IP address rather than using fixed addressing. LANs can be
interlinked by connections to form a Wide area network. A router is
used to make the connection between LANs.
WAN
WANs are used to connect local area networks together, so that users
and computers in one location can communicate with users and computers
in other locations. Many WANs are built for one particular
organisation and are private, others, built by Internet service
providers provide connections from an organisation's LAN to the
Internet. WANs are most often built of leased lines. At each end of
the leased line, a router connects to the LAN on one side and a hub
within the WAN on the other. A number of network protocols may use the
basic physical transport mechanism including TCP/IP. Other protocols
including X.25 and ATM. Frame relay can also be used for WANs.
Ethernet
Ethernet is normally a shared media LAN. All stations on the segment
share the total bandwidth, which is either 10 Mbps (Ethernet), 100
Mbps (Fast Ethernet) or 1000 Mbps (Gigabit Ethernet). With switched
Ethernet, each sender and receiver pair have the full bandwidth.When
using Ethernet the computers are usually wired to a hub or to a switch.
This constitutes the physical transport mechanism.
Fiber-optic Ethernet (10BaseF and 100BaseFX) is impervious to external
radiation and is often used to extend Ethernet segments up to 1.2
miles. Specifications exist for complete fiber-optic networks as well
as backbone implementations. FOIRL (Fiber-Optic Inter Repeater Link)
was an earlier standard that is limited to .6 miles distance.
‘玖’ 论文关于离心空气压缩机
离心机就是以压缩机本体转速来作为基础的，产生风量提高空气压力的，具体可以参照IHI牌子的离心空压机
‘拾’ 压缩机模拟的论文能投到sci吗
学术论文具有四大特点：①学术性 ②科学性 ③创造性 ④理论性
一、学术性
学术论文的科学性，要求作者在立论上不得带有个人好恶的偏见，不得主观臆造，必须切实地从客观实际出发，从中引出符合实际的结论。在论据上，应尽可能多地占有资料，以最充分的、确凿有力的论据作为立论的依据。在论证时，必须经过周密的思考，进行严谨的论证。
二、科学性
科学研究是对新知识的探求。创造性是科学研究的生命。学术论文的创造性在于作者要有自己独到的见解，能提出新的观点、新的理论。这是因为科学的本性就是“革命的和非正统的”，“科学方法主要是发现新现象、制定新理论的一种手段，旧的科学理论就必然会不断地为新理论推翻。”（斯蒂芬·梅森）因此，没有创造性，学术论文就没有科学价值。
三、创造性
学术论文在形式上是属于议论文的，但它与一般议论文不同，它必须是有自己的理论系统的，不能只是材料的罗列，应对大量的事实、材料进行分析、研究，使感性认识上升到理性认识。一般来说，学术论文具有论证色彩，或具有论辩色彩。论文的内容必须符合历史 唯物主义和 唯物辩证法，符合“实事求是”、“有的放矢”、“既分析又综合” 的科学研究方法。
四、理论性
指的是要用通俗易懂的语言表述科学道理，不仅要做到文从字顺，而且要准确、鲜明、和谐、力求生动。
1.表论文的过程 投稿-审稿-用稿通知-办理相关费用-出刊-邮递样刊一般作者先了解期刊，选定期刊后，找到投稿方式，部分期刊要求书面形式投稿。大部分是采用电子稿件形式。 2.发表论文审核时间一般普通刊物（省级、国家级）审核时间为一周，高质量的杂志，审核时间为14-20天。 核心期刊审核时间一般为4个月，须经过初审、复审、终审三道程序。 3.期刊的级别问题 国家没有对期刊进行级别划分。但各单位一般根据期刊的主管单位的级别来对期刊划为省级期刊和国家级期刊。省级期刊主管单位是省级单位。国家级期刊主管单位是国家部门或直属部门。