压缩机叶轮用钢——X12Cr13锻件工艺研究

通过对X12Cr13钢中奥氏体与铁素体的相匹配关系的研究,确定出该钢种合理的化学成分和合理的加热及热处理制度,解决了该钢在轧制、锻造等压力加工过程中易产生裂纹的问题。     

压缩机阀片的失效分析与离子渗氮工艺

从断口形貌、渗氮层组织相结构、性能和残余应力的角度出发，对离子渗氮表面强化的30CrMnSiA压编机阀片进行了失效分析。结果表明，阀片的损坏主要以疲劳断裂为主；渗氮层太薄或过渗氮时都将导致阀片过早的疲劳失效；阀片的渗氮层最佳深度为30—80μm。     

运用均衡凝固技术解决压缩机缸体缩孔缩松

利用均衡凝固技术，将大型活塞式压缩机气缸体的原底注工艺改为项注雨淋工艺，并采用冷铁等措施，使项注雨淋方式的下低上高的温度场分布趋势得到明显的加强，改变了先中间后两头的凝固顺序，缸体从总体上形成了从下往上的有利于补缩的凝固顺序，从而有效解决了压缩机缸体缩孔缩松缺陷。数值模拟结果和实际生产结果验证了工艺改进的正确性，而且废品率由原来的10％降低为5％，工艺出品率由原来的75％提高到85％～90％，效果显著。     

广蓄B厂调相压水周期过长探讨及改进

分析了广州蓄能水电厂B厂由于高压气机及高压气系统效率降低导致调相压水周期过长,无法及时转入抽水调相（CP）工况运行的原因。通过处理压水管路漏气点、高压气机漏气、漏油点及将备用高压气机投入运行的技术改造,提高了高压气系统运行效率,满足及时启动CP工况的系统要求。该技术改造缩短单次CP启动高压气机运行时间,实现了高压气系统节能运行,具有一定工程有效性。     

机组控制逻辑图在故障处理中的应用

府谷压气站燃气轮机-压缩机组已经安全运行8年多,由于机组长期运行,设备组件老化,机组出现故障的次数、几率逐步上升,故障处理的难度也在逐渐增加。如何安全、快速、有效的解决机组出现的各种故障,保障机组安全平稳运行显得非常重要。本文仅针对机组逻辑控制图在机组故障处理过程中的应用,以案例的方式详细的阐述了机组故障处理的方法,旨在说明进行机组故障处理时,不同的思路和方法在机组故障处理过程中具有不同的效用,以达到抛砖引玉、拓展思路的目的。     

PLC控制系统在CCPP中的应用

本文主要介绍了重钢集团股份有限公司的CCPP（燃气-蒸汽联合循环发电机组）特点和PLC控制系统在这个项目中应用。PLC控制系统完成了CCPP工程中的燃气轮机、煤压机、余热锅炉、汽轮机等主体系统的主要功能和控制逻辑,在整个项目中起到了举足轻重的作用。     

A new algorithm for sparse interpolation of multivariate polynomials

To reconstruct a black box multivariate sparse polynomial from its floating point evaluations, the existing algorithms need to know upper bounds for both the number of terms in the polynomial and the partial degree in each of the variables. Here we present a new technique, based on Rutishauser’s qd$qd$-algorithm, in which we overcome both drawbacks.     

A bilevel mixed-integer program for critical infrastructure protection planning

Vulnerability to sudden service disruptions due to deliberate sabotage and terrorist attacks is one of the major threats of today. In this paper, we present a bilevel formulation of the r-interdiction median problem with fortification (RIMF). RIMF identifies the most cost-effective way of allocating protective resources among the facilities of an existing but vulnerable system so that the impact of the most disruptive attack to r unprotected facilities is minimized. The model is based upon the classical p-median location model and assumes that the efficiency of the system is measured in terms of accessibility or service provision costs. In the bilevel formulation, the top level problem involves the decisions about which facilities to fortify in order to minimize the worst-case efficiency reduction due to the loss of unprotected facilities. Worst-case scenario losses are modeled in the lower-level interdiction problem. We solve the bilevel problem through an implicit enumeration (IE) algorithm, which relies on the efficient solution of the lower-level interdiction problem. Extensive computational results are reported, including comparisons with earlier results obtained by a single-level approach to the problem.     

On numerical solution of arbitrary symmetric linear systems by approximate orthogonalization

A very important class of inverse problems are those modelled by integral equations of the first kind. These equations are usually ill-conditioned, such that any discretization technique will produce an ill-conditioned system, in classical or least-squares formulation. For such kind of symmetric problems, we propose in this paper a stable iterative solver based on an approximate orthogonalization algorithm introduced by Z. Kovarik. We prove convergence of our algorithm for general symmetric least-squares problems and present some numerical experiments ilustrating its good behaviour on problems concerned with the determination of charge distribution generating a given electric field and gravity surveying, both modelled by first kind integral equations.     

Stirling-type pulse tube refrigerator (PTR) with cold compression: Cold compressor,colder expander

This research paper focuses on the performance prediction and its validation via experimental investigation of a Stirling-type pulse tube refrigerator (PTR) equipped with a cold linear compressor. When the working gas is compressed at cryogenic temperature, the acoustic power (PV power) can be directly transmitted through the regenerator to the pulsating tube without experiencing unnecessary precooling process. The required PV power generated by the linear compressor, furthermore, can be significantly diminished due to the relatively small specific volume of the working gas at low temperature. The PTR can reach lower temperature efficiently with higher heat lift at the corresponding temperature than other typical single-stage Stirling-type PTRs. Utilizing a cryogenic reservoir as a warm end and regulating the entire operating temperature range of the PTR will enable a PTR to operate efficiently under space environment.In this research, the experimental validation as a proof of concept was carried out to demonstrate the capability of PTR operating between 80 K and 40 K. The linear compressor was submerged in a liquid nitrogen bath and the lowest temperature was measured as 38.5 K. The test results were analyzed to identify loss mechanisms with the simple numerical computation (linear model) which considers the dynamic characteristics of the cold linear compressor with thermo-hydraulic governing equations for each of sub components of the PTR. All the mass flows and pressure waves were assumed to be sinusoidal.