052/052B Class Destroyers
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Mysterre
Banned Idiot
re: PLAN Type 052 Class Destroyer
The real question is: was it quad-packed or single-packed? A quad-packed ARH missile with a range of 50km would be a massive force multiplier for the 054A.
Yes, high firing rate, omnidirectional launch, multiple missile types, and elimination of single point-of-failure breakdowns.
re: PLAN Type 052 Class Destroyer
The Engine Powers 052C & D
GT25000燃气轮机第二阶段国产化研制工作，综合国产化率达到98.1%
2010年7月，国家能源局正式授牌成立国家能源燃气轮机技术研发中心（以下简称“研发中心”）。研发中心依托中国船舶重工集团公司第七○三研究所建设，研究方向和目标为：建成船舶和中小型工业燃气轮机的研究设计平台、试验验证平台、应用评估平台；加强关键技术研究，研制两型高性能母型机，突破先进燃气轮机部件及整机设计的各项核心技术；逐步衍生发展型号产品，研制具有市场竞争力的七型舰船和中小型工业燃气轮机型号产品；基本形成具备自主创新、持续发展的舰船和中小型工业燃气轮机研发体系。
自成立以来，研发中心积极开展基础设施及实验平台建设，已经取得卓有成效的成果。在基础设施建设方面。研发中心在哈尔滨总部已建有功能完备的基础和公用设施，包括燃油系统、天然气系统、循环水系统、压缩空气系统、供电系统等，具备2600吨燃油和9000立方米/小时天然气两种燃料系统，50MW供电、13500t/h循环水、24t/h化学水等系统能力。在实验平台建设方面。研发中心已建成燃气轮机大型综合技术实验室、关键部件实验室、整机试验台等，基本满足30MW级燃气轮机部件和整机试验的条件。其中，综合技术和关键部件实验室可开展燃气轮机部件模化和全尺寸试验。包括全台压气机试验台、高压单管燃烧室试验台、涡轮试验台、喷嘴试验台、燃油系统、滑油系统及关键部件试验台、叶片强度振动试验台等。在整机试验方面，整机试验台可进行30MW级燃气轮机单机试验，34MW燃气轮机联合循环发电上网试验。目前，研发中心在无锡分部已建有两个30MW级燃气轮机整机试验台。在哈尔滨总部，已建有一个驱动用燃气轮机整机试验台和一个燃气轮机发电机组试验台。另外，研发中心在无锡分部，正在建设燃气轮机并车试验台，可进行4台25MW级燃气轮机并车装置试验。
依托强大的研发团队，研发中心在重点技术领域开展了一系列研究工作，取得了突破性进展。一是关键设备燃驱压缩机组国产化研制。研发中心主要科研工作是重新设计低排放燃烧室及其燃料系统、燃气发生器改型、高速动力涡轮、监控系统以及其它成套系统的研制、机组联调试验、工业应用考核试验等。国产化率62%的“产品一”于2011年10月27日通过了国家能源局、中国工业机械联合会及中国石油组织的“天然气长输管线30MW级燃驱压缩机组（产品一）新产品鉴定会”，标志着 “产品一”的研制任务全部完成。100%国产化的“产品二”正在进行样机制造。二是装备型号研制及预先研究项目。第一，研发中心全面完成GT25000燃气轮机第二阶段国产化研制工作，综合国产化率达到98.1%（超过任务书规定的95%指标），技术性能指标达到了技术规格书规定的要求，并按试验大纲完成1000小时可靠性试验及300小时补充试验考核。2011年12月26日，该项目通过了 “GT25000燃气轮机第二阶段国产化研制鉴定会”。研发中心正在进行第三阶段国产化研制，主要目的是提高机组可靠性。GT25000国产机组已经开始批量供货，截止2011年底已经完成12台机组的供货。第二，某型涡轮增压机组是船用增压锅炉装置的关键设备，由多级轴流式压气机、烟气涡轮、辅助汽轮机、齿轮箱、调控及保护系统集成一起构成，国内过去没有先例。研发中心承担了该机组的研制、总装集成和试验等方面工作。完成8台装备机组陆上试验和2台科研机组研制和试验。第三，综合电力系统演示验证—20MW级船用燃气轮机发电模块。研发中心计划2012年完成燃气轮机发电模块试验，2013年完成综合电力系统试验。三是车船动力专项（MPRD）燃气轮机技术基础研究。研发中心目前承担的MPRD计划船舶燃气轮机基础科研项目共6项。2012年2月16日，引进机总体逆向设计及试验验证、引进机关键部件逆向设计及试验验证、S-S循环燃机总体技术及试验验证三个项目通过了国防科工局组织的验收会议。现阶段，舰船全电力系统燃机发电模块技术正在进行整机试验验证的准备工作，间冷热循环（IC）总体性能与结构技术及试验验证正在按任务书要求开展课题的研究工作。四是国家863计划10MW高温气冷实验堆氦气透平压缩机组研制。该课题为国家“863”能源领域重点项目。该项目研制包括高低压压气机、涡轮等设计和制造，机组不同运行工况的分析，定子密封试验、高低压压气机性能试验、机组空载机械运转试验、堆上运行验证试验等。研发中心已完成了高温气冷堆闭式循环氦气轮机的设计研究和加工总装工作；已完成压气机试验件的设计和试验台适应性改造工作，正在进行压气机试验件制造工作。五是F级中低热值燃料燃气轮机关键技术与整机设计技术研究。研发中心承担了本项目F级中低热值燃料燃气轮机的压气机的、高温透平冷效、单喷嘴燃烧室的实验研究以及中低热值燃气轮机透平设计等工作。该项目正在按计划实施。
研发中心在人才队伍建设、标准制修订和技术创新以及国际合作等方面也取得了重要成果。在人才队伍建设方面。目前研发中心拥有一支以4位院士为领军人才，由200多名专业细分、结构层次合理、年龄梯队化的高水平科研人员组成的专业功底深厚、具有创新精神的专家队伍。为加快人才队伍建设，研发中心通过高薪聘请国际化专业人才、与高等院校联合培养后续青年人才队伍等措施，促进人才快速成长。在标准制修订和技术创新方面。研发中心成立近两年主持和参加制定的国际、国家、行业标准4项。申请专利数43个，专利授权数21个。目前拥有的全部有效发明专利数6个，获国家自然科学、技术发明、科技进步奖项目数2项。在国际合作方面。研发中心与俄罗斯相关科研单位开展了功率为25000kW的燃气轮机装置轴流式低压压气机的叶片系统改进的相关研究工作。
研发中心与日立公司签署燃气轮机的合作协议，确定了集各自所长的联合体合作模式。根据用户需求，联合体可提供发电机组成套供货、电站设计以及工程总承包等多种方案。另外，为充分发挥调动产、学、研等各方优势和积极性，研发中心已建成开放式的国家级燃气轮机技术研发平台。
研发中心将按照《国家能源科技“十二五”规划》的发展目标和任务要求，深入贯彻落实科学发展观，以“重大技术研究、重大技术装备、重大示范工程及技术创新平台”四位一体的国家能源科技创新体系为指导，进一步开展以下工作：一是完成30MW级驱动用燃气轮机、20MW船用燃气轮机发电模块研制以及GT25000燃气轮机低工况性能改进；二是完成40MW级GT25000IC燃气轮机关键技术研究和部件试验；三是完成GT30-J型母型机研发，改进完善形成CGT30产品；四是完成GT10-J型母型机的设计；五是开展基础及关键技术研究，建立、补充和完善设计规范、设计软件和数据库，初步形成工程可用的设计体系；六是完善燃气轮机研发的部件、整机试验条件；七是完善加工制造条件，提高总装集成和维修保障的能力；八是开展高温冷却叶片的共性制造.
Auto Translation:
GT25000 gas turbine domestic development of the second phase of work, comprehensive localization rate of 98.1%
In July 2010, the National Energy Board formally awarding the establishment of a National Energy gas turbine technology R & D Center (hereinafter referred to as "R & D Center). R & D center based on the construction of seventy-three Institute of China Shipbuilding Industry Corporation, the research direction and goals: study design platform built ships and small and medium-sized industrial gas turbines, test verification platform, application evaluation platform; strengthen key technology research, the development of two types of female high-performance machine, the core technology breakthrough in advanced gas turbine engine components and machine design; gradually derivative development models, the development of seven type ships with market competitiveness and small and medium-sized industrial gas turbine models; basically formed with independent innovation sustainable development of ships and small and medium-sized industrial gas turbine research and development system. Since its inception, the R & D center and actively carry out the construction of infrastructure and experimental platform has achieved fruitful results. In infrastructure building. Headquarters in Harbin, the R & D center has a full-featured foundation and utilities, including the fuel system, natural gas system, circulating water system, compressed air system, power supply system, with 2600 tons of fuel oil and 9000 m3 / h of natural gas the two fuels system, 50MW supply, 13500t / h circulating water, 24t / h chemical water system capabilities. In the experimental platform building. The R & D center has been built gas turbine large integrated technology lab, the key components of the laboratory, the whole test bench, basically meet the 30MW-class gas turbine components and machine test conditions. Which comprehensive technology and key components of the laboratory to carry out modeling of gas turbine engine components and full-scale test. Including the compressor test rig of the Taiwan high-pressure single-tube combustor test rig, turbine test bench, nozzle test bench, fuel system, oil system and key components of test bench, blade strength vibration test stand. In terms of the whole test, the whole test rig 30MW gas turbines stand-alone test, 34MW gas turbine combined cycle power generation Internet test. Currently, the R & D center in Wuxi segment has two 30MW gas turbines machine test stand. Headquarters in Harbin, the drive has built a gas turbine machine test stand and a gas turbine generator test bench. In addition, the R & D center in Wuxi Branch, is building the gas turbine and vehicle test-bed, four 25MW gas turbines and car device test. Relying on strong R & D team, R & D center has carried out a series of research in key technology breakthrough has been made. One key equipment burning drive compressor group domestic development. The main research work of the R & D center is the re-design of the low-emission combustion chamber and its fuel system, modification of the gas generator, high-speed power turbine monitoring system, and other sets of system development, the FBI of the unit test, industrial applications assessment test. Localization rate of 62% of the "product" on October 27, 2011 by the National Energy Bureau, China Machinery Industry Federation and the China Petroleum Institute "long distance gas pipelines 30MW grade fuel to drive the compressor group (a) new product appraisal meeting marked "a research task is completed. 100% localization "product" ongoing prototyping. Equipment models developed and pre-research project. First, the R & D center is fully completed GT25000 gas turbine domestic development of the second phase of work, comprehensive localization rate of 98.1% (more than 95% of the mission statement provides indicators), technical performance indicators have reached the specified requirements of the technical specifications, press the test the outline supplementary test assessment completed 1000 hours of reliability testing and 300 hours. December 26, 2011, the project through the "GT25000 gas turbine domestic development of the second phase of appraisal meeting. The R & D center of ongoing domestic development of the third phase, the main purpose is to improve the reliability of the unit. The GT25000 made units have begun to bulk supply, the supply of 12 units have been completed as of the end of 2011. Second, a certain type of turbo unit is the key equipment of the marine supercharged boiler device, constituted by the multi-stage axial compressor, gas turbine, auxiliary steam turbine, gearbox, regulation and protection system integrated with domestic no precedent in the past . The R & D center is charged with the work of the unit's development, final assembly and integration and test. Complete equipped units onshore test and research unit development and testing. Third, integrated power system demonstration-20MW-class marine gas turbine power generation module. R & D center planned 2012 completion of the gas turbine power generation module test, complete integrated power system test in 2013. Third, the basic research of special travel power gas turbine technology (MPRD). The MPRD currently undertaken by the R & D center plans to ship gas turbine the basis of a total of six research projects. February 16, 2012, the introduction of the machine overall reverse design and experimental verification, the introduction of key components of reverse design and experimental verification, the SS cycle gas turbine overall technical and experimental verification three projects through the organization's acceptance of the National Defense Science and Industry Bureau meeting. At this stage, ready to ship the whole electricity system gas turbine power generation module technology the ongoing machine test validation, the overall performance and structure between the hot and cold cycles (IC) and the experimental verification is required by task book research work carried out subject. National 863 Program 10MW high temperature gas-cooled reactor helium turbine compressor units developed. The subject of the national "863" key projects of the energy field. Development of the project, including the design and manufacture of high and low pressure compressor and turbine unit operating conditions analysis, stator seal test, high and low pressure compressor performance test, the unit no-load mechanical operation test heap run verification tests. The R & D center has completed the design of the HTGR closed-cycle helium turbine research and processing of final assembly work; has completed the design of the compressor test pieces and test bench adaptability transformation, ongoing compressor the test parts manufacturing work. Fifth Class F key technology of the low calorific value fuel gas turbine and aircraft design, technology research. R & D center is charged with the the Project F grade, low calorific value fuel gas turbine compressor, high temperature turbine cold efficiency, the experimental study of the combustion chamber of the single nozzle and low calorific value gas turbine turbine design work. The project is being implemented as planned. R & D centers in qualified personnel, and amend standards and technological innovation as well as international cooperation has achieved important results. qualified personnel. The R & D center has a leading talent four academicians, broken down by more than 200 professional, reasonable structure level, age echelon of high-level research staff consisting of professional deep innovative team of experts to accelerate the talent team construction, research and development centers through high salaries to hire international professionals to jointly develop future youth talent, and institutions of higher learning and other measures to promote the rapid growth of talent. research and development center was established nearly two years to host and participate in the development in the revision of the standard and technical innovation. international, national, industry-standard 4. patent number 43 and 21, the number of patents. 6 currently has an effective number of invention patents, won the national natural science, technological invention, scientific and technological progress awards 2 projects in International cooperation in R & D centers to carry out related research units and the Russian gas turbine device power 25000kW axial low pressure compressor blade system improvements research and R & D center of the cooperation agreement signed with Hitachi gas turbine, determine the set of their talents the Commonwealth cooperation mode according to user needs, the Commonwealth can provide generators composed of sets of supply, power plant design and engineering general contracting and other programs. addition, to give full play to the advantages of the parties and the enthusiasm of the mobilization of industry, academia, research, research and development The center has been built national open gas turbine technology research and development platform. c I3 n5, & v8 t; g. C2 T! Y R & D center in accordance with the National Energy Technology "12th Five-Year Plan for the development of objectives and mission requirements, thoroughly implement the implement the scientific concept of development, "significant technical study of major technical equipment, major demonstration projects and technology innovation platform" four in one of the National Energy Technology Innovation System to further carry out the following work: First, the completion of a 30MW-class drive with a gas turbine, 20MW marine gas turbine power generation module developed low condition GT25000 gas turbine performance improvements; complete 40MW-level GT25000IC gas turbine key technology research and component testing; GT30-J female R & D machine is completed and improved the the perfect formation CGT30 products; Fourth completed GT10 -J-the female machine design; basic and key technology research, establish, supplement and perfect the design specification, design, and database software, the initial formation of the engineering design system available; six perfect components of the gas turbine research and development, the whole test conditions; seven perfect manufacturing conditions, and improve the ability of the final assembly and integration and maintenance support; eight high temperature cooling blades in common manufacturing
The Engine Powers 052C & D
GT25000燃气轮机第二阶段国产化研制工作，综合国产化率达到98.1%
2010年7月，国家能源局正式授牌成立国家能源燃气轮机技术研发中心（以下简称“研发中心”）。研发中心依托中国船舶重工集团公司第七○三研究所建设，研究方向和目标为：建成船舶和中小型工业燃气轮机的研究设计平台、试验验证平台、应用评估平台；加强关键技术研究，研制两型高性能母型机，突破先进燃气轮机部件及整机设计的各项核心技术；逐步衍生发展型号产品，研制具有市场竞争力的七型舰船和中小型工业燃气轮机型号产品；基本形成具备自主创新、持续发展的舰船和中小型工业燃气轮机研发体系。
自成立以来，研发中心积极开展基础设施及实验平台建设，已经取得卓有成效的成果。在基础设施建设方面。研发中心在哈尔滨总部已建有功能完备的基础和公用设施，包括燃油系统、天然气系统、循环水系统、压缩空气系统、供电系统等，具备2600吨燃油和9000立方米/小时天然气两种燃料系统，50MW供电、13500t/h循环水、24t/h化学水等系统能力。在实验平台建设方面。研发中心已建成燃气轮机大型综合技术实验室、关键部件实验室、整机试验台等，基本满足30MW级燃气轮机部件和整机试验的条件。其中，综合技术和关键部件实验室可开展燃气轮机部件模化和全尺寸试验。包括全台压气机试验台、高压单管燃烧室试验台、涡轮试验台、喷嘴试验台、燃油系统、滑油系统及关键部件试验台、叶片强度振动试验台等。在整机试验方面，整机试验台可进行30MW级燃气轮机单机试验，34MW燃气轮机联合循环发电上网试验。目前，研发中心在无锡分部已建有两个30MW级燃气轮机整机试验台。在哈尔滨总部，已建有一个驱动用燃气轮机整机试验台和一个燃气轮机发电机组试验台。另外，研发中心在无锡分部，正在建设燃气轮机并车试验台，可进行4台25MW级燃气轮机并车装置试验。
依托强大的研发团队，研发中心在重点技术领域开展了一系列研究工作，取得了突破性进展。一是关键设备燃驱压缩机组国产化研制。研发中心主要科研工作是重新设计低排放燃烧室及其燃料系统、燃气发生器改型、高速动力涡轮、监控系统以及其它成套系统的研制、机组联调试验、工业应用考核试验等。国产化率62%的“产品一”于2011年10月27日通过了国家能源局、中国工业机械联合会及中国石油组织的“天然气长输管线30MW级燃驱压缩机组（产品一）新产品鉴定会”，标志着 “产品一”的研制任务全部完成。100%国产化的“产品二”正在进行样机制造。二是装备型号研制及预先研究项目。第一，研发中心全面完成GT25000燃气轮机第二阶段国产化研制工作，综合国产化率达到98.1%（超过任务书规定的95%指标），技术性能指标达到了技术规格书规定的要求，并按试验大纲完成1000小时可靠性试验及300小时补充试验考核。2011年12月26日，该项目通过了 “GT25000燃气轮机第二阶段国产化研制鉴定会”。研发中心正在进行第三阶段国产化研制，主要目的是提高机组可靠性。GT25000国产机组已经开始批量供货，截止2011年底已经完成12台机组的供货。第二，某型涡轮增压机组是船用增压锅炉装置的关键设备，由多级轴流式压气机、烟气涡轮、辅助汽轮机、齿轮箱、调控及保护系统集成一起构成，国内过去没有先例。研发中心承担了该机组的研制、总装集成和试验等方面工作。完成8台装备机组陆上试验和2台科研机组研制和试验。第三，综合电力系统演示验证—20MW级船用燃气轮机发电模块。研发中心计划2012年完成燃气轮机发电模块试验，2013年完成综合电力系统试验。三是车船动力专项（MPRD）燃气轮机技术基础研究。研发中心目前承担的MPRD计划船舶燃气轮机基础科研项目共6项。2012年2月16日，引进机总体逆向设计及试验验证、引进机关键部件逆向设计及试验验证、S-S循环燃机总体技术及试验验证三个项目通过了国防科工局组织的验收会议。现阶段，舰船全电力系统燃机发电模块技术正在进行整机试验验证的准备工作，间冷热循环（IC）总体性能与结构技术及试验验证正在按任务书要求开展课题的研究工作。四是国家863计划10MW高温气冷实验堆氦气透平压缩机组研制。该课题为国家“863”能源领域重点项目。该项目研制包括高低压压气机、涡轮等设计和制造，机组不同运行工况的分析，定子密封试验、高低压压气机性能试验、机组空载机械运转试验、堆上运行验证试验等。研发中心已完成了高温气冷堆闭式循环氦气轮机的设计研究和加工总装工作；已完成压气机试验件的设计和试验台适应性改造工作，正在进行压气机试验件制造工作。五是F级中低热值燃料燃气轮机关键技术与整机设计技术研究。研发中心承担了本项目F级中低热值燃料燃气轮机的压气机的、高温透平冷效、单喷嘴燃烧室的实验研究以及中低热值燃气轮机透平设计等工作。该项目正在按计划实施。
研发中心在人才队伍建设、标准制修订和技术创新以及国际合作等方面也取得了重要成果。在人才队伍建设方面。目前研发中心拥有一支以4位院士为领军人才，由200多名专业细分、结构层次合理、年龄梯队化的高水平科研人员组成的专业功底深厚、具有创新精神的专家队伍。为加快人才队伍建设，研发中心通过高薪聘请国际化专业人才、与高等院校联合培养后续青年人才队伍等措施，促进人才快速成长。在标准制修订和技术创新方面。研发中心成立近两年主持和参加制定的国际、国家、行业标准4项。申请专利数43个，专利授权数21个。目前拥有的全部有效发明专利数6个，获国家自然科学、技术发明、科技进步奖项目数2项。在国际合作方面。研发中心与俄罗斯相关科研单位开展了功率为25000kW的燃气轮机装置轴流式低压压气机的叶片系统改进的相关研究工作。
研发中心与日立公司签署燃气轮机的合作协议，确定了集各自所长的联合体合作模式。根据用户需求，联合体可提供发电机组成套供货、电站设计以及工程总承包等多种方案。另外，为充分发挥调动产、学、研等各方优势和积极性，研发中心已建成开放式的国家级燃气轮机技术研发平台。
研发中心将按照《国家能源科技“十二五”规划》的发展目标和任务要求，深入贯彻落实科学发展观，以“重大技术研究、重大技术装备、重大示范工程及技术创新平台”四位一体的国家能源科技创新体系为指导，进一步开展以下工作：一是完成30MW级驱动用燃气轮机、20MW船用燃气轮机发电模块研制以及GT25000燃气轮机低工况性能改进；二是完成40MW级GT25000IC燃气轮机关键技术研究和部件试验；三是完成GT30-J型母型机研发，改进完善形成CGT30产品；四是完成GT10-J型母型机的设计；五是开展基础及关键技术研究，建立、补充和完善设计规范、设计软件和数据库，初步形成工程可用的设计体系；六是完善燃气轮机研发的部件、整机试验条件；七是完善加工制造条件，提高总装集成和维修保障的能力；八是开展高温冷却叶片的共性制造.
Auto Translation:
GT25000 gas turbine domestic development of the second phase of work, comprehensive localization rate of 98.1%
In July 2010, the National Energy Board formally awarding the establishment of a National Energy gas turbine technology R & D Center (hereinafter referred to as "R & D Center). R & D center based on the construction of seventy-three Institute of China Shipbuilding Industry Corporation, the research direction and goals: study design platform built ships and small and medium-sized industrial gas turbines, test verification platform, application evaluation platform; strengthen key technology research, the development of two types of female high-performance machine, the core technology breakthrough in advanced gas turbine engine components and machine design; gradually derivative development models, the development of seven type ships with market competitiveness and small and medium-sized industrial gas turbine models; basically formed with independent innovation sustainable development of ships and small and medium-sized industrial gas turbine research and development system. Since its inception, the R & D center and actively carry out the construction of infrastructure and experimental platform has achieved fruitful results. In infrastructure building. Headquarters in Harbin, the R & D center has a full-featured foundation and utilities, including the fuel system, natural gas system, circulating water system, compressed air system, power supply system, with 2600 tons of fuel oil and 9000 m3 / h of natural gas the two fuels system, 50MW supply, 13500t / h circulating water, 24t / h chemical water system capabilities. In the experimental platform building. The R & D center has been built gas turbine large integrated technology lab, the key components of the laboratory, the whole test bench, basically meet the 30MW-class gas turbine components and machine test conditions. Which comprehensive technology and key components of the laboratory to carry out modeling of gas turbine engine components and full-scale test. Including the compressor test rig of the Taiwan high-pressure single-tube combustor test rig, turbine test bench, nozzle test bench, fuel system, oil system and key components of test bench, blade strength vibration test stand. In terms of the whole test, the whole test rig 30MW gas turbines stand-alone test, 34MW gas turbine combined cycle power generation Internet test. Currently, the R & D center in Wuxi segment has two 30MW gas turbines machine test stand. Headquarters in Harbin, the drive has built a gas turbine machine test stand and a gas turbine generator test bench. In addition, the R & D center in Wuxi Branch, is building the gas turbine and vehicle test-bed, four 25MW gas turbines and car device test. Relying on strong R & D team, R & D center has carried out a series of research in key technology breakthrough has been made. One key equipment burning drive compressor group domestic development. The main research work of the R & D center is the re-design of the low-emission combustion chamber and its fuel system, modification of the gas generator, high-speed power turbine monitoring system, and other sets of system development, the FBI of the unit test, industrial applications assessment test. Localization rate of 62% of the "product" on October 27, 2011 by the National Energy Bureau, China Machinery Industry Federation and the China Petroleum Institute "long distance gas pipelines 30MW grade fuel to drive the compressor group (a) new product appraisal meeting marked "a research task is completed. 100% localization "product" ongoing prototyping. Equipment models developed and pre-research project. First, the R & D center is fully completed GT25000 gas turbine domestic development of the second phase of work, comprehensive localization rate of 98.1% (more than 95% of the mission statement provides indicators), technical performance indicators have reached the specified requirements of the technical specifications, press the test the outline supplementary test assessment completed 1000 hours of reliability testing and 300 hours. December 26, 2011, the project through the "GT25000 gas turbine domestic development of the second phase of appraisal meeting. The R & D center of ongoing domestic development of the third phase, the main purpose is to improve the reliability of the unit. The GT25000 made units have begun to bulk supply, the supply of 12 units have been completed as of the end of 2011. Second, a certain type of turbo unit is the key equipment of the marine supercharged boiler device, constituted by the multi-stage axial compressor, gas turbine, auxiliary steam turbine, gearbox, regulation and protection system integrated with domestic no precedent in the past . The R & D center is charged with the work of the unit's development, final assembly and integration and test. Complete equipped units onshore test and research unit development and testing. Third, integrated power system demonstration-20MW-class marine gas turbine power generation module. R & D center planned 2012 completion of the gas turbine power generation module test, complete integrated power system test in 2013. Third, the basic research of special travel power gas turbine technology (MPRD). The MPRD currently undertaken by the R & D center plans to ship gas turbine the basis of a total of six research projects. February 16, 2012, the introduction of the machine overall reverse design and experimental verification, the introduction of key components of reverse design and experimental verification, the SS cycle gas turbine overall technical and experimental verification three projects through the organization's acceptance of the National Defense Science and Industry Bureau meeting. At this stage, ready to ship the whole electricity system gas turbine power generation module technology the ongoing machine test validation, the overall performance and structure between the hot and cold cycles (IC) and the experimental verification is required by task book research work carried out subject. National 863 Program 10MW high temperature gas-cooled reactor helium turbine compressor units developed. The subject of the national "863" key projects of the energy field. Development of the project, including the design and manufacture of high and low pressure compressor and turbine unit operating conditions analysis, stator seal test, high and low pressure compressor performance test, the unit no-load mechanical operation test heap run verification tests. The R & D center has completed the design of the HTGR closed-cycle helium turbine research and processing of final assembly work; has completed the design of the compressor test pieces and test bench adaptability transformation, ongoing compressor the test parts manufacturing work. Fifth Class F key technology of the low calorific value fuel gas turbine and aircraft design, technology research. R & D center is charged with the the Project F grade, low calorific value fuel gas turbine compressor, high temperature turbine cold efficiency, the experimental study of the combustion chamber of the single nozzle and low calorific value gas turbine turbine design work. The project is being implemented as planned. R & D centers in qualified personnel, and amend standards and technological innovation as well as international cooperation has achieved important results. qualified personnel. The R & D center has a leading talent four academicians, broken down by more than 200 professional, reasonable structure level, age echelon of high-level research staff consisting of professional deep innovative team of experts to accelerate the talent team construction, research and development centers through high salaries to hire international professionals to jointly develop future youth talent, and institutions of higher learning and other measures to promote the rapid growth of talent. research and development center was established nearly two years to host and participate in the development in the revision of the standard and technical innovation. international, national, industry-standard 4. patent number 43 and 21, the number of patents. 6 currently has an effective number of invention patents, won the national natural science, technological invention, scientific and technological progress awards 2 projects in International cooperation in R & D centers to carry out related research units and the Russian gas turbine device power 25000kW axial low pressure compressor blade system improvements research and R & D center of the cooperation agreement signed with Hitachi gas turbine, determine the set of their talents the Commonwealth cooperation mode according to user needs, the Commonwealth can provide generators composed of sets of supply, power plant design and engineering general contracting and other programs. addition, to give full play to the advantages of the parties and the enthusiasm of the mobilization of industry, academia, research, research and development The center has been built national open gas turbine technology research and development platform. c I3 n5, & v8 t; g. C2 T! Y R & D center in accordance with the National Energy Technology "12th Five-Year Plan for the development of objectives and mission requirements, thoroughly implement the implement the scientific concept of development, "significant technical study of major technical equipment, major demonstration projects and technology innovation platform" four in one of the National Energy Technology Innovation System to further carry out the following work: First, the completion of a 30MW-class drive with a gas turbine, 20MW marine gas turbine power generation module developed low condition GT25000 gas turbine performance improvements; complete 40MW-level GT25000IC gas turbine key technology research and component testing; GT30-J female R & D machine is completed and improved the the perfect formation CGT30 products; Fourth completed GT10 -J-the female machine design; basic and key technology research, establish, supplement and perfect the design specification, design, and database software, the initial formation of the engineering design system available; six perfect components of the gas turbine research and development, the whole test conditions; seven perfect manufacturing conditions, and improve the ability of the final assembly and integration and maintenance support; eight high temperature cooling blades in common manufacturing
antiterror13
Brigadier
re: PLAN Type 052 Class Destroyer
the translation really gave me a bad headache :-(
the translation really gave me a bad headache :-(
re: PLAN Type 052 Class Destroyer
That's the set up I would prefer too, and I think it's perfectly feasible to do. The document said there will be three module types, large, medium, and small; they are to house missile canisters size up to 9m, 7m, and 3.3m respectively. My interpretation is that if our preferred configuration is possible then it doesn't have to specify three different modules, instead it could have said simply that the module can accommodate 9m, 7m, and 3.3m missile canisters. Of course that's how I interpreted it, maybe I'm being overly literal and the document's wording is relatively generic. The module referred in the document is the structure supporting 8 "compartments (cells)," since the canisters are self sustained the cell concept is quite different from the HQ16 cell which is a full housing with exhaust systems, in this case it's pretty much just scaffolding.
The missiles cannot be launched simultaneously, the continuous launch rate of this particular VLS is less than one missile per second, the launch control system can manage the launch of four missiles, in missile interception they are most likely bottlenecked by illumination channels instead of the VLS.
Mysterre
Banned Idiot
re: PLAN Type 052 Class Destroyer
Possibly the author of the document is merely unimaginative. If all we are talking about is scaffolding, which makes sense for a module without a common vent system, then this scaffolding could easily be constructed to house cells of different lengths.
re: PLAN Type 052 Class Destroyer
Yeah it should be completely doable, the standard is probably too generic to include such design details.
Yeah it should be completely doable, the standard is probably too generic to include such design details.