Ropeblock为Sarens超级环轨起重机配备超大吊钩
“巨无霸”履带吊成为核电大件吊装利器
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德马格起重机械(上海)有限公司重磅推出新品——第二代DC环链电动葫芦
德马格起重机械(上海)有限公司重磅推出新品——第二代DC
环链电动葫芦
供稿/德马格起重机械(上海)有限公司;王芝兵采编/邹铁汉;张韦微
【期刊名称】《起重运输机械》
【年(卷),期】2024()7
【摘要】德马格起重机在欧洲最大室内物流展览会LogiMAT2024上发布了风靡全球,且久经实际应用验证的DC系列环链电动葫芦的下一代——DC-II系列。
德马格起重机于20年前首次推出了DC系列环链电动葫芦,现已堪称环链电动葫芦产品的行业标杆。
在开发第二代DC环链电动葫芦时,德马格充分考虑了近年来的发展趋势,以引领该产品系列走向未来。
现场观众可以在LogiMAT2024德马格起重机的展台上了解到最新的起重技术。
【总页数】3页(P2-4)
【作者】供稿/德马格起重机械(上海)有限公司;王芝兵采编/邹铁汉;张韦微
【作者单位】不详
【正文语种】中文
【中图分类】TH2
【相关文献】
1.德马格公司的新型DC环链电动葫芦
2.德马格起重机械（上海）有限公司DC型环链电动葫芦
3.德马格推出DCS-Pro 10变频调速环链电动葫芦系列
4.德马格起
重机械(上海)有限公司环链电动葫芦的迭代创新5.德马格起重机械(上海)有限公司DVR钢丝绳电动葫芦
因版权原因，仅展示原文概要，查看原文内容请购买。
Terex
建筑机械 2016.136企业报道ENTERPRISE在里昂以东的法国城市德希内斯·尚皮埃，新足球体育场的建设倍受瞩目。
为了安装支撑屋顶的钢结构，施工方特别委托Sarens集团承担此重任，Sarens用650t的Terex ® Superlift 3800桁架臂履带式起重机做出响应。
“我们选择这款起重机是因为其灵活性，”Sarens集团的项目经理Sam Voeten对此解释，“对于此项目，我们需要起重机在短半径时具有很大的起重能力，在扩展半径工作时也具有很大的起重能力，不用重新配置吊臂。
Superlift 3800可满足这个要求。
”起重机将从法国北部的瑟堡运往体育场，行程超过800km 。
在1周内由46辆卡车运达体育场内。
Superlift 3800起重机的设计有助于在公路上运输组件。
“所有组件的宽度都不超过3m ，”特雷克斯起重机的产品市场经理Guntram Jakobs解释说，“因此Superlift 3800起重机正是为方便运输而制造的。
它能轻松地运输到全世界任何市场，像嵌入式臂杆和可互换配重块这样的功能可减少货车载荷，并降低运输成本。
”这款履带式起重机的紧凑运输设计也有助于在体育场的作业。
“运输卡车的入口通道高5m 、宽4m ，Superlift 3800起重机较窄的运输尺寸有助于我们将组件运到体育场内进行装配，”Voeten表示。
到现场后，5个工作人员在4天内便完成了起重机和超起的组装。
这款起重机的液压插拔销功能有助于Sarens装配人员快速组装履带和主臂，同时，快速连接系统能够让上车在15min内完成安装。
Guntram Jakobs 解释说，起重机还配有协助装配者的辅助工具。
当装配Superlift 3800桁架臂履带式起重机的吊臂部分时，特雷克斯防坠落保护系统提供了安全保障。
该装置包含一个配有减震器的背心式安全带，为主桁架上工作行走的人员提供绳索保护，在装配者到达地面之前阻止坠落。
和利时电机SYNTRON森创产品说明书
版权申明SYNTRON森创®是北京和利时电机公司（以下简称和利时电机）于2005年推出的产品品牌。
这个品牌浓缩了公司的核心技术和影响力，是公司始终注重自主创新，保持技术优势的体现。
说明书的内容参照了相关法律基准和行业基准。
如对本说明书提供的内容有疑问，请向销售人员咨询，致电客服热线，联系官网客服或致信本公司。
和利时电机保留在不事先通知的情况下，修改本手册中的产品和产品规格参数等权力。
手册请联系销售人员，或在和利时电机的官方网站下载相关手册。
和利时电机具有本产品及其软件的专利权、版权和其它知识产权。
未经授权，不得直接或者间接地复制、制造、加工、使用本产品及其相关部分。
和利时电机具有本使用说明书的著作权，未经许可，不得修改、复制使用说明书的全部或部分内容。
安全有关的符号说明本说明书中与安全有关的内容，使用了下述符号。
标注了安全符号的都为重要内容，请安全注意事项安全注意事项目录 第一章产品概况 ................................................... - 1 -1.1产品概况 ................................................................................................................................ - 1 -1.1.1简介 ........................................................................................................................... - 1 -1.1.2低压伺服驱动器型号命名 ....................................................................................... - 3 -1.1.3低压伺服一体机型号命名 ....................................................................................... - 3 -1.1.4规格和性能 ............................................................................................................... - 4 -1.1.5电机配套 ................................................................................................................... - 4 -1.1.6产品构造 ................................................................................................................... - 5 -1.1.7安装尺寸 ................................................................................................................... - 5 - 第二章准备 ...................................................... - 12 -2.1通讯协议及软件 .................................................................................................................. - 12 -2.2操作面板 .............................................................................................................................. - 13 -2.2.1操作面板介绍 .........................................................................................................- 13 -2.2.2指示灯介绍 .............................................................................................................- 13 -2.2.3数码管 .....................................................................................................................- 13 -2.2.4按键 .........................................................................................................................- 14 -2.2.5键盘操作流程 .........................................................................................................- 15 - 第三章配线 ...................................................... - 16 -3.1接线总图 .............................................................................................................................. - 16 -3.2接线定义 .............................................................................................................................. - 17 -3.2.1 LS-10520M2系列接线定义 ..................................................................................- 17 -3.2.2 LS-10530BA系列接线定义 ..................................................................................- 18 -3.2.3 LS-10530BK系列接线定义 ..................................................................................- 19 -3.2.4 LS-10530D5系列接线定义...................................................................................- 20 -3.2.5 LS-10540D/LS-10550D系列接线定义................................................................- 21 -3.2.6 LS-20530DG系列接线定义..................................................................................- 22 -3.2.7 LS-20520E系列接线定义 .....................................................................................- 23 -3.2.8 LS-20530E / LS-20535E系列接线定义..............................................................- 25 -3.2.9 LS-20540E系列接线定义 .....................................................................................- 27 -3.2.10 DM一体机系列接线（驱动器后置一体机）.....................................................- 29 -3.2.11 SM一体机系列接线（驱动器侧背一体机） .....................................................- 29 -3.2.11.1类型1 ....................................................................................................................- 29 -3.2.11.2类型2 ....................................................................................................................- 32 -3.3其他接线说明 ...................................................................................................................... - 33 -3.3.1 地线连接..................................................................................................................- 33 -目录3.3.2 编码器差分输出接线 ..............................................................................................- 33 -3.3.3 数字输入接线 ..........................................................................................................- 33 -3.3.4 数字输出接线 ..........................................................................................................- 33 -3.3.5 手动控制制动器接线 ..............................................................................................- 34 -3.3.6 位置模式接线 ..........................................................................................................- 34 -3.3.7 内部速度模式接线 ..................................................................................................- 35 -3.3.8 外部速度/转矩模式接线图 .....................................................................................- 35 - 第四章设定 ...................................................... - 36 -4.1电机方向 .............................................................................................................................. - 36 -4.2状态参数 .............................................................................................................................. - 36 -4.3功能参数 .............................................................................................................................. - 37 -4.3.1工作控制模式 .........................................................................................................- 37 -4.3.2系统基本参数控制 .................................................................................................- 37 -4.3.3数字输入端口 .........................................................................................................- 38 -4.3.4内部控制信号 .........................................................................................................- 38 -4.3.5数字输出端口 .........................................................................................................- 41 -4.3.6脉冲端口输入输出 .................................................................................................- 41 -4.3.7目标到达状态判断 .................................................................................................- 42 -4.3.8位置环控制参数 .....................................................................................................- 43 -4.3.9模拟量输入参数 .....................................................................................................- 44 -4.3.10内部速度参数 .........................................................................................................- 45 -4.3.11速度环调节参数 .....................................................................................................- 45 -4.3.12转矩电流指令滤波参数 .........................................................................................- 45 -4.3.13控制限制参数 .........................................................................................................- 46 -4.3.14增益切换 .................................................................................................................- 47 -4.3.15速度模式加减速时间 .............................................................................................- 48 -4.3.16电磁制动器 .............................................................................................................- 48 -4.3.17报警保护配置 .........................................................................................................- 48 -4.3.18通讯参数设置 .........................................................................................................- 50 -4.3.19电流环控制参数 .....................................................................................................- 51 -4.3.20泄放参数配置 .........................................................................................................- 51 -4.3.21历史报警码 .............................................................................................................- 52 -4.4试运行 .................................................................................................................................. - 52 -4.4.1基本流程 .................................................................................................................- 52 -4.4.2JOG模式空载试运行（键盘面板上操作） ........................................................- 54 -4.4.3速度模式空载试运行（总线通讯操作） .............................................................- 54 -目录 第五章调整 ...................................................... - 55 -5.1控制模式的选择 .................................................................................................................. - 55 -5.2输入输出的配置 .................................................................................................................. - 56 -5.2.1输入信号端口分配 .................................................................................................- 56 -5.2.2输出信号端口分配 .................................................................................................- 57 -5.3基本参数 .............................................................................................................................. - 58 -5.3.1伺服使能 .................................................................................................................- 58 -5.3.2急停 .........................................................................................................................- 58 -5.3.3指令取反 .................................................................................................................- 58 -5.3.4零速到达 .................................................................................................................- 59 -5.3.5目标速度到达 .........................................................................................................- 59 -5.3.6速度一致 .................................................................................................................- 59 -5.3.7目标转矩到达 .........................................................................................................- 59 -5.3.8超程 .........................................................................................................................- 60 -5.3.9恢复出厂默认参数 .................................................................................................- 60 -5.4位置模式调整 ...................................................................................................................... - 61 -5.4.1脉冲指令方式的选择 .............................................................................................- 61 -5.4.2脉冲指令窗口滤波器 .............................................................................................- 61 -5.4.3脉冲指令平滑滤波器 .............................................................................................- 62 -5.4.4指令脉冲禁止功能 .................................................................................................- 62 -5.4.5电子齿轮的设定 .....................................................................................................- 62 -5.4.6位置到达信号 .........................................................................................................- 65 -5.4.7位置接近信号 .........................................................................................................- 65 -5.4.8位置超差警告 .........................................................................................................- 66 -5.4.9位置脉冲误差清零 .................................................................................................- 66 -5.5速度模式调整 ...................................................................................................................... - 66 -5.5.1外部模拟量速度模式运行 .....................................................................................- 66 -5.5.2内部速度模式运行 .................................................................................................- 67 -5.5.3加减速时间 .............................................................................................................- 68 -5.5.4零速给定 .................................................................................................................- 69 -5.6转矩模式调整 ...................................................................................................................... - 69 -5.6.1转矩指令增益的调整 .............................................................................................- 69 -5.6.2转矩指令偏移量的调整 .........................................................................................- 69 -5.6.3转矩指令方向的设置 .............................................................................................- 69 -5.6.4转矩指令低通滤波器 .............................................................................................- 69 -5.6.5模拟转矩指令零值箝位 .........................................................................................- 70 -目录5.6.6转矩控制时的速度限制 .........................................................................................- 70 -5.7共振抑制 .............................................................................................................................. - 71 -5.8转矩限制 .............................................................................................................................. - 72 -5.9增益切换 .............................................................................................................................. - 73 -5.10增益调整 .............................................................................................................................. - 75 -5.10.1速度环增益调整 .....................................................................................................- 75 -5.10.2位置环增益调整 .....................................................................................................- 75 -5.10.3增益调整注意事项 .................................................................................................- 75 -5.11电磁制动 .............................................................................................................................. - 76 -5.12编码器的输出 ...................................................................................................................... - 77 -5.13干扰对策 .............................................................................................................................. - 77 -第六章通讯 ...................................................... - 79 -6.1Modbus总线设置 ................................................................................................................ - 79 -6.2CAN总线设置..................................................................................................................... - 79 -6.3通讯协议 .............................................................................................................................. - 79 -第七章故障警告及处理 ............................................ - 80 -7.1报警代码 .............................................................................................................................. - 80 -7.2报警状态指示灯 .................................................................................................................. - 83 -7.3性能异常及解决办法 .......................................................................................................... - 83 -第八章维护与保养 ................................................ - 84 -8.1伺服电机的检查 .................................................................................................................. - 84 -8.2伺服驱动器的检查 .............................................................................................................. - 84 -产品概况第一章产品概况1.1 产品概况1.1.1 简介LS系列低压伺服驱动器（以下简称LS驱动器），是和利时电机根据市场需求推出的新一代高性能、高可靠产品。
世界军用拖车系列130：象房怪兽，三一SAC6000与利勃海尔G-BKF军吊
世界军用拖车系列130：象房怪兽，三一SAC6000与利勃海尔G-BKF军吊“民用车辆是军车的基础”，这么说可能太空洞容易被人误解。
本文通过两种“玻羊车界”从未涉及过的车辆——吊车——三一重工的SAC6000和利勃海尔的G-BKF军用装甲吊车，来浅显的分析一下民用车辆技术对军用车辆发展的重大意义！上图为三一重工的SAC6000提到重型工程车辆，造挖掘机出身的“三一重工”无疑是我国最具有代表性的企业！三一重工所生产的SAC6000型全路面起重机，不仅满足了国内吊装800吨-1000吨级1.5-2兆瓦风力发电机组的需求，其在全球重型起重机界，更是“独孤求败”般的存在！SAC6000售价不菲，属于让托尼·斯塔克或“蝙蝠侠”购买也要皱一下眉头的那种！其整机长宽高尺寸为22.75×3×4米，貌似不是什么庞然大物。
但是作为一种8轴特种用车，其单车质量就有96吨；在进行相关起吊作业时，还可以通过遥控的方式，自行拆卸或安装最高165吨的组合式可变平衡配重。
作为起重机的根本，SAC6000的椭圆型主起重臂长90米，塔臂同样有90米的长度，把主臂展开并加装塔臂情况下，最大起吊高度可达136米！再配合主卷扬单绳136米/分钟的最大起升率，以及副卷扬单绳136米/分钟的最大起升率，能够将80吨的重物起吊至80米高！SAC6000起重机的支腿为“X”型，其支腿最大跨距可达10.8×10.8米。
该吊车搭载一台480千瓦的奔驰V8发动机。
在转场行驶过程中，它那个大吊臂是与车身分开运输的！利勃海尔G-BKF的德语全称为“装甲救援起重机”（GeschutztesBergekranfahrzeug）。
于2017年6月，德国联邦国防军以1.5亿欧元的高价，采购了33台G-BKF和38台G-LTM 1090-4.2移动式起重机，已经在2021年交付完成。
之所以把G-BKF 放到本专题来介绍，是德军特殊的车型概念，影响到德国军队中没有单纯的自行牵引抢救车；因此名为“吊车”的G-BKF实际上可执行“牵引、拖曳、起吊、撤离”等多重任务！因此，利勃海尔G-BKF在车尾左右两侧、工具箱的前方，各装有1个Rotzler TR 200型和1个Rotzler TR 80型液压绞盘。
集装箱门吊技术规格书
项目名称：海安货场轨道式集装箱门式起重机技术规格书上海铁路局2014 道式集装箱门式起重机项目技术规格书型号：吊架下起升重量40.5 吨名称：轨道式集装箱门式起重机目录1 (5)2. 目概略 (5)3. 目技格 (6)3.1 概括 ..................................................... ⋯⋯⋯3.2 使用境参数 .. (6)3.3 性能参数 (7)3.4 主要外件品牌 (8)3.5 准与范 (9)3.6 主要板厚度 (11)3.7 主要零件资料 (11)3.8 主要气的防等 . (11)4. 通用技要求 (12)4.1 固件和接件 (12)螺栓、螺母接 . (12)、接 . (12)承与密封 . (12)4.2 资料与制作工 (12)资料 (12)制作工 . (13)4.3 接 (13)4.4 表面理与涂装 (14)5. 主要零零件技范 (14)5.1 金属构件 (14)金属构件技范 (14)5.1.2 架 . (15)5.1.3 小架 . (15)大均衡梁和台架 (15)5.2 起升机构 (16)5.3 小运行机构 (16)5.4 大行走机构 (17)5.5 平台、通道、梯和杆 . (18)5.6 集装箱吊具和吊具上架 . (18)5.7 (19)5.8 滑 (20)5.9 卷筒 (20)5.10 减速器 (20)5.11 器 (21)5.12 制器 (21)5.13 车轮组及轨道 (21)5.14 缓冲器 (21)5.15 轮边制动器和锚定装置 . (22)5.16 电气房 (22)5.17 司机室 (23)5.18 润滑 (24)5.19 液压系统 (24)6. 电气系统技术规范 (25)6.1 电气派括 (25)6.2 供电 (25)6.3 主要电气设备及电气设计 . (28)主机构电动机 . (28)变频调速系统 . (29)操作联动台 . (29)配电设备 . (30)全机电气保护 . (30)控制屏、自动开关、接触器、继电器 (30)变频调速器 . (30)可编程序控制器（ PLC） (31)6.4 指示灯、报警信号与丈量表计及限位开关与紧停开关 (31)6.5 维修电源 (32)6.6 吊具电缆收放装置 (32)6.7 小车电缆 (32)6.8 机构的安全保护装置 . (33)起升机构联锁 . (33)小车运行机构安全装置 (33)大车行走机构安全装置 (34)紧迫泊车按钮 . (34)6.9 联锁与检测 (35)起升机构联锁 . (35)小车运行机构联锁 (35)大车行走机构联锁 (35)故障显示与检测 . (36)6.10 照明 (36)6.11 电源插座 (37)6.12 通信、广播系统 (37)6.13 电线电缆、布线和端子 . (37)6.13.1 电线电缆 . (37)布线 . (38)端子 . (39)6.14 接地、防雷 (39)6.15 加热器与电阻器 (39)6.16 电气设备安装 (39)7. 信息系统 (40)7.1 起重机 CMS软件及硬件要求 . (32)7.2 文件 ...........................................................7.3 其余要求 .......................................................8. 其余技术要求 (43)8.1 负荷牌、铭牌及标示牌 . (43)8.2 消防器械 (43)9. 技术资料、图纸及随机备件、工具要求 (43)9.1 招标时应供应的技术文件 . (43)9.2 基本方案设计审察应提交资料 . (44)9.3 竣薪资料 (44)9.4 随机备件 (45)9.5 随机工具与仪表仪器 . (45)10 设计审察与施工监造 (46)10.1 基本设计审察 (46)10.2 最后设计审察 (47)10.3 设计审察经过 (47)10.4 施工监理及监造 (47)11. 运输、安装、调试与查收据款 (47)11.1 运输、安装 (47)11.2 调试、试车及查收 (47)调试、试车 . (47)起重机初步查收（交钥匙） (47)起重机最后查收（保修期结束） (48)11.3 技术培训 (48)11.4 质量保证 (48)11.5 交货期 (48)11.6 安全责任 (48)12. 技术规格书附表 (48)12.1 附表目录 (49)附表 1. 主要尺寸和运行参数 (49)附表 2. 随机备品配件清单（单台机） (50)附表 3 随机工具与仪表仪器 (51)1.总则本技术规格书用于上海铁路局铁路货场的共 1 台额定起重量为 40.5 吨（吊架下）的轨道式集装箱龙门起重机（简称门吊）的采买。
北美绳索技术装备标准
北美绳索技术装备标准
北美绳索技术装备标准通常是指由美国国家标准协会（ANSI）和美国登山器材制造商协会（UIAA）制定的相关标准。
这些标准涵盖了各种绳索、安全带、抱索、冰镐、头盔等登山和攀岩装备的设计、测试和认证要求。
此外，美国登山指导协会（AMGA）也会提供有关绳索技术装备的培训和指导标准。
这些标准旨在确保登山和攀岩装备的质量和安全性，以保护登山者和攀岩者的生命和健康。
具体的标准文件可以在 ANSI 和 UIAA 的官方网站上找到，并且这些标准通常会根据行业和技术的发展而不断更新和修订。
黑翼飞行模拟器用户手册说明书
IntroductionThe Blackwing BW 635RG is an ultralight two-seater aeroplane designed for recreational flying and training purposes. It features a sleek and modern design, with a composite airframe and a low-wing configuration. The Blackwing has a cruising speed of up to 120 knots and a range of approximately 700 nautical miles, making it suitable for both short and long-distance flights. The cockpit is equipped with state-of-the-art avionics, including a glass cockpit display and an autopilot system. The Blackwing is also known for its superior handling and stability, making it a popular choice among flying enthusiasts and flight schools. The BW 635RG is powered by the venerable Rotax 915 iS engine.Development Credits:Mal Cartwright Product LeadRuss White3D Modelling, Interior and Exterior TexturingJack Lavigne IntegrationHarry Stringer AnimationPropAir Flight Model and SystemsJordan Gough ManualWith special thanks to our Beta Testers:Rob Abernathy John BurgessNick Cooper John DowMatt McGee Darryl WightmanTable of ContentsIntroduction (2)Development Credits: (2)With special thanks to our Beta Testers: (2)Table of Contents (3)Notes on Hardware (4)Overview (5)Aircraft Limitations (6)Airspeed Limitations (6)Engine Limitations (6)Operating Conditions (6)Fuel (7)Other Limitations (7)Emergency Procedures (8)Engine Failure on the Take-off Roll (8)Engine Failure after Take-off (8)Glide Performance (8)Emergency Landing (9)Spin Recovery (9)Normal Procedures (10)Before Starting Engine (10)Starting Engine (10)Before Taxiing (11)Taxiing (11)Engine Runup (11)Before Take-off (11)Take-Off (12)Initial Climb (12)Cruise Climb (12)Cruise (12)Landing (13)Balked Landing (13)After Landing (13)Securing Aircraft (14)Basic Performance (15)Stall Speeds (15)Take-Off Performance (15)Landing Performance (16)Systems Description (17)Instrument Panel Layout (17)Switch Logic and Electrical System (18)Master Switch (18)Fuel Pump Switch (19)LAND/TAXI Switch (19)Strobe/Nav Switch (19)Electrical System Diagram (20)Engine (21)Propeller (21)Fuel (21)Notes on HardwareDue to the unusual 3-position switches in this aircraft, conventional hardware 2position toggle switches (eg. strobe or nav light switches) cannot be translated tothe single 3-position switch which combine these.Additionally, as this aircraft utilises a single level power control (throttle), conventional throttle/prop/mixture hardware may interfere with the function of this system, and not work as intended. It is recommended to place your propeller and mixture levers in the IDLE position, and not move them while the engine is running.OverviewThe Orbx BW 635RG has been developed using official documentation and Computer Aided Design (CAD) resources from Blackwing Sweden. As a result, the aeroplane has been created through masterful modelling, texturing, systems integration, and flight model development.Figure 1 – Aircraft 3-viewAircraft DimensionsLength 6.6m Height 2.2m Wingspan8.4mWeightsBasic Empty Weight 375kg Maximum Take-off Weight 600kg Maximum Fuel Capacity (Litres)130LThe content in this manual and the operation of the BW 635RG in Microsoft Flight Simulator strictly must not be used as reference material in any form for operating the real aircraft.Aircraft LimitationsAirspeed LimitationsAirspeed Description Airspeed (KIAS) RemarksVne Never Exceed Speed 157 Must not exceed this speed in any operation.Va Manoeuvring Speed 109 If full or abrupt control deflection is made, the airframe may be overstressed.Vfe1 Max flap extended speed20 degrees90 Maximum speed for flaps 20°Vfe2 Max flap extended speed35-45 degrees 70 Maximum speed for flaps 35-45°Vlo Maximum landing gearoperating speed 70Do not extended or retract the landing gearabove this speed.Vle Maximum landing gear extended speed 90 Do not exceed this speed with the landing gearalready down.Vs0 Stall speed flaps/gearextended 38 Stall speed with gear down/flaps >0° and in level flight at MTOWVs1 Stall speed clean 49 Stall speed flaps retracted, gear up and in level flight at MTOWEngine LimitationsEngineEngine Manufacturer Rotax Engine Model Rotax 915 iSMaximum Power Take-off (Max 5 min.) 141 hp Continuous 135 hpMaximum RPM Take-off (Max 5 min.) 5800 Continuous 5500Critical Altitude 15000ft AMSL Maximum OperatingAltitude23000ft AMSL Operating ConditionsAerobatic manoeuvres, flight in IFR conditionsand flights in icing conditions are prohibited inthis aircraft.FuelFuel TanksLeft Right Litres US Gal Litres US GalTotal Fuel in Tank 67.5 17.8 62.5 16.5Unusable Fuel 2.5 0.7 2.5 0.7 Total Useable Fuel in Tanks 66.5 17.6 61.5 16.2Other LimitationsMaximum demonstrated crosswind for the BW 635RG is 20 knots.Emergency ProceduresNote: The following procedures have been modified to be suitable for simulation. It does not cover emergencies that are a) not simulated and b) not reasonable. Checklist items from the real procedures have been omitted and these procedures must not under any circumstances be used for training purposes.Engine Failure on the Take-off RollThrottle: IDLEIgnition: OFFFuel Pump: MAIN (DOWN POS)Brakes: APPLYWhen stopped: SECURE AIRCRAFTEngine Failure after Take-offNose: IMMEDIATELY LOWERAirspeed: 65 KNOTSLanding Area: DETERMINE WITHIN 30° OF NOSEFlaps: USE AS REQUIREDLanding Gear: USE DESCRETIONFuel Selector: OFFIgnition: OFFMaster Switch: OFFGlide PerformanceThe BW 635RG, the approximate performance for a glide is 65 KIAS which willgive approximately a 545ft/min rate of descent in the clean configuration.Glide performance will degrade significantly on extension of flaps and landinggear.Emergency LandingAirspeed: 65 KIASField: PICK BEST OPTIONLanding Gear: USE DISCRETION DEPENDING ON FIELD TYPEFlaps: AS REQUIREDFuel Selector: OFFIgnition: OFFFuel Pump: MAIN (down)Master Switch: OFF BEFORE LANDINGSpin RecoveryThrottle: IDLEControl Stick: AILERON NEUTRALRudder: FULL OPPOSITE TO DIRECTION OF ROTATIONControl Stick: POSITIVELY FORWARD OF NEUTRALRudder: NEUTRAL WHEN ROTATION STOPSControl Stick: SMOOTHLY PULL OUT OF DIVEWARNING:INTENTIONAL SPINS ARE NOT APPROVED INTHIS AIRCRAFT.Normal ProceduresNote: The pre-flight inspection portion of the normal procedures has been removed due to impracticality in the simulator.Before Starting EngineIgnition: OFFMaster Switch: OFF (down)Backup Battery: OFF/AUTO (down)Landing Gear Lever: DOWNCircuit Breakers: INCanopy CLOSED (CLICKING THE LATCHON THE INSIDE LEFT SIDEWALL.) Starting EngineParking Brake: HOLD TOE BRAKES AND ENGAGE PARKINGBRAKEMaster Switch: ENGINE START (middle position)Fuel Selector: SETFuel Gauge: CHECKFuel Pump: BOTH (up)Ignition: BOTHNav Lights: STROBE (middle position)Throttle: SET ½-1 INCH OPENIgnition: STARTOil Pressure: GREEN WITHIN 10 SECWarnings: NONEBefore TaxiingMaster Switch: NORMAL OPERATION (up)Altimeter: SETAvionics: SETParking Brake: DISENGAGETaxiingInstruments: CHECKED (COMPASS/HSI/BALL/ATT) Engine RunupParking Brake: ENGAGERPM: 2500 RPMFuel Pump: CYCLE, CHECK FUEL PRESSUREIdle: CHECK IDLE 1800 +/- 100 RPM Before Take-offCanopy: CLOSED AND LOCKEDFlaps: 1 STAGE (20°)Elevator Trim: SET FOR TAKE-OFFEngine Instruments: NORMALLanding Light: ON (up)Controls: FULL FREE AND CORRECT MOVEMENTParking Brake: DISENGAGETake-OffThrottle: FULLControls: NEUTRAL45 Knots: ROTATEAccelerate: NOSE ON HORIZON, ACCEL TO 80 KIASPositive Rate of Climb: GEAR UPLanding Light: OFF (down)Flaps: RETRACT ABOVE 500’ AGLInitial ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 90 KIASFuel Pump: MAIN (down) ABOVE 500’ AGL Cruise ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 130 KIASCruiseThrottle: 55-75% PowerAirspeed: 120-157 KIAS (<130 KIAS IN TURB)LandingFuel: QTY CHECKEDFuel Selector: FULLEST TANKFuel Pump: BOTH (up position)Airspeed: 90 KIASFlaps: EXTEND FLAP 1 <90 KIASDownwind Airspeed: 65 KIASLanding Gear: DOWN @ 65 KIAS; CHECK 3 GREENLanding Light: ON (up position)Base Leg: EXTEND FLAP 2 < 65 KIASFinal Approach Airspeed: 60 KIASBalked LandingThrottle: SMOOTHLY INCREASEAirspeed: 60 KIASTrim: COURSE TRIM TO RELIEVE PRESSUREFlaps: RETRACT TO POSITION 1 (20°)Gear: UPTrim: TRIM FOR CLIMBAfter LandingFlaps: RETRACTExterior Lights: AS REQ’DFuel Pump: MAIN (down)Securing AircraftParking Brake: ENGAGEDThrottle: IDLESwitches: ALL OFF EXCEPT ACL AND MASTERIgnition: OFFNav Lights: OFF (down)Master Switch: OFFBasic PerformanceStall SpeedsMTOW 600kg | CG 32% MAC | Power Idle | Level FlightFlap Position Stall Speed (KIAS) 0° 49 20° 44 35° 39 45°38Take-Off PerformanceMTOW | ISA CONDITIONS | SEA LEVEL | FLAPS 1 (20°) | MTOW (600kg)Cruise PerformanceRunway Surface Ground RollOver 50ft Obstacleft mft mPaved Runway328 100 656 200 Unpaved (Grass) Runway 361110689208Pressure Altitude Power (%) TAS Fuel Flow LPH MAP (inHg) Endurance(hr)Range (nm) 500055 161 19.7 30 5.8 941 65 170 23.3 34.1 4.9 827 7517826.937.44.1738Landing PerformanceMTOW | ISA CONDITIONS | FLAPS 2 (35°) | MTOW (600kg) | Speed 1.3 x VsoRunway Surface Ground Roll Over 50ft Obstacle ft m ft mPaved Runway 525 160 951 290 Unpaved (Grass) Runway 558 170 984 300Systems Description Instrument Panel LayoutSwitch Logic and Electrical SystemThe electrical switches in the BW 635RG are 3-position switches. These are generally known as “DOWN”, “MIDDLE” and “UP”. They are briefly explained below.Master SwitchThe MASTER switch functions in a unique way, with the following switch logic:1.When the MASTER switch is DOWN, all battery power is off. There will beno electrical power provided to the aircraft.•Note: The engine CANNOT be shut down when the master switch isoff. Electrical power must be present for the engine to turn off.2.When the MASTER switch is in the MIDDLE (Engine Start) position, limitedsystem functionality will be present. The backup battery will be activatedand power the following systems:•Primary Flight Display•Compass•AHRS (Attitude Heading Reference System)•Radio3.When the MASTER switch is UP (Normal Operation), full electrical supplywill be provided to the aircraft. The following systems will be powered on: •Note: the engine CANNOT be started with the MASTER switch in theUP position. If the engine won’t start, check the switch is in theMIDDLE position•Multi-Function Display•Transponder•Autopilot•Audio panel•STBY instruments•Pitot Heat•Main battery is disconnected from running engine. Alternatorprovides power.See Section NORMAL PROCEDURES for positioning of the MASTER switch.Fuel Pump SwitchThe Fuel Pump switch also has some advanced logic to it, due to two fuel pumpsbeing present, however, to put it simply, it operates in the following way:1.In the DOWN position, the main fuel pump is in use.2.In the MIDDLE position, the auxiliary fuel pump is in use.3.In the UP position, both fuel pumps will be on.LAND/TAXI SwitchThe LAND/TAXI switch powers the Taxi and Landing lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the taxi light will switch on when the landinggear is extended.3.In the UP position, the Landing Light will switch on when the landinggear is extended.Strobe/Nav SwitchThe Strobe/Nav switch powers the Navigation (Red/Green) and Strobe (flashingwhite) lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the STROBE light will be on.3.In the UP position, both the strobe and Nav lights will be on.Electrical System DiagramThe BW 635RG’s electrical system is modelled in the following way in Microsoft Flight Simulator.Because the starter system is connected to the BACKUP BUS, this means you cannot start the engine with the MASTER switch in the UP position, due to the BACKUP BUS being disconnected from the circuit once the MAIN BAT BUS is powered.Page 21 of 21User Guide v1.0 –RevisionEngineThe BW 635RG is powered by the Rotax 915iS. The Rotax 915iS is a four-stroke, four-cylinder, fuel-injected, turbocharged aircraft engine with a maximum power output of141 horsepower. The engine utilizes electronic fuel injection (EFI) technology toprovide precise fuel delivery and improved fuel efficiency. It also features a modernliquid-cooling system and a dual electronic ignition system for reliable performance.The Rotax 915iS engine has a maximum operating RPM of 5,200, with a recommended continuous operation range of 5,000 RPM or less.PropellerThe propeller is a 3-blade wood-composite design, which is hydraulically adjustable for operation at various pitch angles, controlled independently of the pilot. The propeller is linked to the engine through an electronically controlled governor, where RPM isadjusted in accordance with the position of the throttle control. This pitch curve cannot be adjusted in flight, however is designed to ensure maximum performance in allphases of flight.FuelBoth wings have fuel tanks, which are fed to the engine via electric fuel pumps. Fuelsystem information is fed via sensors to the Garmin avionics suite and can be viewedon the displays inside the cockpit.AIRPLANE WEIGHTSBasic Empty Weight……………………….…375 KgMaximum Takeoff Weight…………………..600 KgMaximum Fuel Weight………………………...95 Kg Maximum Landing Weight………………….600 Kg TANK USABLE FUEL LEFT WING TANK67.5 litres 17.8 US Gallons RIGHT WING TANK62.5 litres 16.5 US Gallons TOTAL 130 litres34.3 US GallonsFUEL CAPACITY AIRSPEEDS Never Exceed Speed ……….…………….173 KIAS Max Structural Cruising Speed…………..156 KIAS Maneuvering Speed MTOW……………….109 KIAS Initial Climb………………………………………80 KIASBest Angle Climb……………………………….75 KIASBest Rate of Climb……………………………..90 KIASMax Flap Ext 20°……………………..............90 KIASMax Flap Ext 35-45°……………………………70 KIASMax Landing Gear Operation……………….70 KIASMax Landing Gear Extended………………..90 KIASPlanned Cruise TAS………………………….130 KIASFinal Approach Speed………………………..60 KIAS POWERPLANT LIMITATIONSENGINE LIMITS (RPM)Take-off (5 Minutes)………....5800 RPM Max Continuous……………….5500 RPMALTITUDE LIMITSMaximum Operating Altitude………………23 000ftFor Microsoft Flight Simulator Use Only0-12023 Orbx Simulation Systems Pty. Ltd BW 635RG QUICK REFERENCESHEETIssued: 21 Apr 2023Revised: 21 Apr 20230-2PROCEDURESBEFORE STARTING ENGINEPreflight Inspection………………………….COMPLETECrew Briefing………………………………….COMPLETEIgnition…………………………………………………….OFFMaster Switch…………………………………………..OFFBackup Battery …..…………………………….OFF/AUTOLanding Gear Lever………………………………..DOWNCircuit Breakers…………………………………………..IN Canopy………………………………………………CLOSED STARTING ENGINEArea……………………………………………………..CLEARParking Brake……………….HOLD TOE BRAKES ANDENGAGEMaster Switch …..……………….ENGINE START (MID)Fuel Selector…………………………………………….SETFuel Pump………………………………………BOTH (UP)Ignition………………………………………………….BOTHExternal Lights……………………………………..AS REQThrottle ………………………..………..Τ12-1 INCH OPENIgnition………………………………………………….START AFTER START Oil Pressure.…………………………………………RISING Master Switch ……………………………..NORMAL (UP)Radios………………………………………………………SET Altimeter…………………………………………………..SET ATIS and Clearance…………………………..OBTAINEDBEFORE TAXIBrakes/Park Brake ………………………….DISENGAGEFlight Instruments……………………………..CHECKEDCompass…………………………………………CHECKED BEFORE TAKEOFFCanopy/Harnesses………………………………SECURE Flaps…………………………………….……1 STAGE (20°)Trim ..……………………………………SET FOR TAKEOFF Flight Instruments………………………………………SET Engine Instruments………………CHECKED NORMAL Avionics…………………………………………………….SET External Lights………………………………………AS REQ Flight Controls…………..FULL, FREE AND CORRECT Takeoff Safety Brief………………………….DELIVERED TAKEOFFBrakes/Park Brake………………………….DISENGAGEPower…………SMOOTHLY INCREASE TO MAXIMUM45 knots………………………………………………ROTATEAccelerate……….…NOSE ON HORIZON, TO 80 KTSPositive Rate of Climb………………………….GEAR UPLanding Light.……………………………….OFF (DOWN)Flaps ………………………..RETRACT ABOVE 500’ AGLMEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd ENGINE RUN UP Parking Brake ……………………………………..ENGAGE Engine Instruments……………………………CHECKED Engine RPM…………………………………SET 2500 RPM Fuel Pump…………………………………………….CYCLE Idle …………………..…..CHECK IDLE 1800 ±100RPM Navigation Equipment …..…………………………….SETFor Microsoft Flight Simulator Use OnlyIssued: 21 Apr 2023Revised: 21 Apr 2023AFTER TAKEOFF Engine Instruments……………………..WITHIN LIMITS Climb Speed…………………………………………90 KIAS Fuel Pump………….MAIN (DOWN ) ABOVE 500’ AGL0-3CRUISEPower….……………………………………….SET 55-75%Airspeed…..……….120-157KTS (<130KTS IN TURB.)DESCENTAltimeter…………………………………………………..SETFuel Selector………………………………FULLEST TANKPower Lever………………….AS REQUIRED FOR RODApproach Brief………………………………PLETE BEFORE LANDINGBrakes……………………………………………………..OFFFuel ………….………………………………QTY CHECKEDFuel Selector………………………………FULLEST TANK Fuel Pump……….………………………………BOTH (UP)LANDINGDOWNWINDAirspeed….………………………………………….90 KIASFlaps….………………………………………STAGE 1 (20°)Airspeed………….………………………………….65 KIASLanding Gear…..…………………….DOWN @ 65 KIASCHECK 3 GREENLanding Light………………………………………ON (UP)BASEFlaps…………………………… STAGE 2 (35°) < 65 KIASFINALAirspeed………….………………………………….60 KIASTouchdown ……………………….MAIN WHEELS FIRSTStick………………………………………………FULL BACK Brakes…………………………………………………..APPLYAFTER LANDING Flaps………………………………………………..RETRACT Landing Lights…………………………………………..OFFFuel Pump….………………………………MAIN (DOWN)SHUTDOWNParking Brake ……………………………………..ENGAGE Throttle……………………………………………………IDLE Switches….………………………….OFF EXCL. MASTERIgnition..…………………………………………………..OFFLights….……………………………………….OFF (DOWN)Master Switch..……………………………..OFF (DOWN)MEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd For Microsoft Flight Simulator Use OnlyPROCEDURESIssued: 21 Apr 2023Revised: 21 Apr 2023。
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Ropeblock为Sarens超级环轨起重机配备超大吊钩
荷兰制造商Ropeblock（中文名：神固）为Sarens公司的超级环轨起重机SGC- 120配套生产了世界上最大的吊钩。
商务经理Wim Fabricius介绍了公司为满足所有用户而制定的目标。
Ropeblock的产品广泛应用于工程、工业、海洋、船舶、石油、煤矿、水电、钢铁等领域。
这家公司成立于1993年，之后成长为世界起重行业内的一家高品质公司。
公司核心业务来自于精益求精。
荷兰神固的产品主要有吊钩、滑车、滑轮、应力释放器、索节等产品。
在严苛的测试和可追溯的质量产品体系下，可以设计生产制造出满足行业内绝大多数的标准和规定的产品。
在业内仅有的对所有出厂的吊钩产品均进行全检（材料检测、磁粉探伤检测、超声波探伤检测以及预拉伸测试后复检），保证每一个交付到客户手里的产品都安全合格。
为陆基卷扬机构起重机制造世界最大吊钩是Ropeblock公司取得的许多业绩之一。
对Ropeblock来说，几乎可以参与任何大型起重类的项目，在2014年，荷兰神固成功的攻克业内难题，可以研发设计制造起重量达到10,000T的吊钩。
Ropeblock生产的吊钩不仅限于超大的起重量的吊钩，还为许多起重机生产商提供常用吨位的吊钩滑车总成。
Ropeblock拥有研发、设计、制造和供应特种Overhaul Ball式的吊钩，用于低温环境和极深水下环境作业。
由于产品具有水下4000m深度起重作业的良好记录，许多活跃在海洋和油气行业的公司选择Ropeblock作为它们最恶劣环境下起重作业元件的唯一供应商，与NOV、麦基嘉、TTS等国际一流产品有深度的合作关系。
Ropeblock向Sarens提供的SWL为3,200T的双钩吊钩总成，是当时陆地上单机起重量最大的履带式起重机。