风机技术
風機技術
풍궤기술
COMPRESSOR,BLOWER & FAN TECHNOLOGY
2013年
3期
74-78
,共5页
柴油加氢离心压缩机%喘振工况%氢气组分变化%防喘振曲线修正
柴油加氫離心壓縮機%喘振工況%氫氣組分變化%防喘振麯線脩正
시유가경리심압축궤%천진공황%경기조분변화%방천진곡선수정
diesel hydrogenation centrifugal compressor%anti-surge%change of hydrogen component%correction of anti-surge curve
由于压缩机混合气中氢气组分变化偏离设计值,致使柴油加氢循环氢离心机组原设计防喘振曲线不能满足生产的需要,导致机组运行中采用防喘振阀门回流的方法维持生产,负荷较高大部分循环气处于自循环状态,且无法保证反应系统所需氢气。压缩机处于高负荷下运行,使得汽轮机负载高,造成不必要的损失。对此具体分析了其原因,通过实测喘振点,修正了由于气体组分发生变化的防喘振曲线,解决了加氢装置运行的瓶颈,为用户实现有效氢量增加25%,直接节约动力成本260万/年。
由于壓縮機混閤氣中氫氣組分變化偏離設計值,緻使柴油加氫循環氫離心機組原設計防喘振麯線不能滿足生產的需要,導緻機組運行中採用防喘振閥門迴流的方法維持生產,負荷較高大部分循環氣處于自循環狀態,且無法保證反應繫統所需氫氣。壓縮機處于高負荷下運行,使得汽輪機負載高,造成不必要的損失。對此具體分析瞭其原因,通過實測喘振點,脩正瞭由于氣體組分髮生變化的防喘振麯線,解決瞭加氫裝置運行的瓶頸,為用戶實現有效氫量增加25%,直接節約動力成本260萬/年。
유우압축궤혼합기중경기조분변화편리설계치,치사시유가경순배경리심궤조원설계방천진곡선불능만족생산적수요,도치궤조운행중채용방천진벌문회류적방법유지생산,부하교고대부분순배기처우자순배상태,차무법보증반응계통소수경기。압축궤처우고부하하운행,사득기륜궤부재고,조성불필요적손실。대차구체분석료기원인,통과실측천진점,수정료유우기체조분발생변화적방천진곡선,해결료가경장치운행적병경,위용호실현유효경량증가25%,직접절약동력성본260만/년。
Due to the hydrogen gas component changing in the compressor mixture deviates from the design values, it had caused the original design anti-surge curve of diesel hydrogenation recycle hydrogen centrifugal compressor unit cannot meet the requirement of production, and the means of adopting anti-surge valve reflux will be used to maintain production in the unit operating. The load was higher, most of circulating gas was in the state of self-circulation, and the required hydrogen gas in reaction system cannot be ensured. The compressor will be running with high load, which made the turbine with high load and caused unnecessary losses. This paper had analyzed the reason, and based on actual measuring surge points, corrected the anti-surge curve caused by the change of gas component. Then the problem in hydrogenation unit running was solved, which increased 25% of effective hydrogen and saving power costs 2.6 million per year directly for users.