22座神州飞碟(B级)设计说明书
星河动力航天产品手册说明书
北京市亦庄开发区中航技广场 **************************公司介绍Company overview星河动力（北京）空间科技有限公司是国内首家将商业组网卫星送入500km太阳同步轨道、首家实现连续发射成功、首家掌握一箭多星发射能力的民营商业火箭公司。
总部位于北京经济技术开发区（亦庄），由航天系统内资深工程师组建，从事低成本商业航天发射业务的民营航天公司。
公司致力于研发下一代可重复使用商业运载火箭，为国内外小卫星发射市场提供低成本、高可靠、快响应的进入太空系统化解决方案。
公司核心产品包括“智神星”系列中型重复使用液体运载火箭、“谷神星”系列小型运载火箭等。
公司研发团队由来自航天系统的资深技术和管理专家组成，在系统工程、火箭推进、航天电子、化学工程、结构力学等相关领域拥有一流的技术实力和丰富的研制经验。
公司成员作为分系统负责人参与过10余型火箭及发动机研制，成功执行过上百次发射任务。
（1） 在固体运载火箭技术方向，公司聚焦于低成本、高可靠的推力矢量控制四级固体商业运载火箭，该类型火箭具有技术成熟、发射成本低、可靠性高、准备周期短、保障依托少等优点,主要面向300kg 以下的低轨微小卫星发射、低轨星座补网发射等市场。
（2） 在重复使用液体运载火箭方向，公司聚焦于重复使用液氧/煤油商业运载火箭，该火箭具有安全性强、可靠性高、成本低、可重复使用等优点，可大幅度降低卫星发射成本，主要满足低轨星座组网和大型载荷发射需求。
体系完善、专业齐备、专利布局完整，有效支撑火箭研发高效开展专业完善、能力过硬、勇于创新、善于管理的专业化研制团队研制团队R&D team· 数百人的核心研发团队，由来自航天系统的资深技术和管理专家组成，在系统工程、火箭推进、航天电子、化学工程、结构力学等相关领域拥有一流的技术实力和丰富的研制经验。
·团队成员曾参与研发过20余个弹/箭型号，执行过上百次发射任务，获得过近百项国家/国防科技奖。
ufo手感飞行器说明书
ufo手感飞行器说明书
1、三种飞行方式说明。
左上方，该通道用于飞行器的三种飞行模式选择。
定点向前飞行、定点飞行、自由飞行（无光流作用，完全由油门和pithch和rol控制）。
2、四轴需要准备什么零件。
无刷电机、电子调速器、螺旋桨（4个，需要2个正浆，2个反浆）、飞行控制板、电池（11.1v航模动力电池）、遥控器（最低四通道遥控器）机架（非必选）、充电器（尽量选择平衡充电器）。
3、四轴零件之间的接线。
4、电调的正负极需要并联（红色连一起，黑色连一起），并接到电池的正负极上；电调3根黑色的电机控制线，连接电机。
5、电调有个BEC输出，用于输出5v的电压，给飞行控制板供电，和接收飞行控制板的控制信号，遥控接收器连接在飞行控制器上，输出遥控信号，并同时从飞行控制板上得到5v供电。
宇通客车产品手册说明书
S VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-TRAILERS FLA KS A-TRAILERS B-TRAILERS EXTENDABLES TRAYS SKELS DROP-DECK TLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-LERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDABLES TRAYS SKE DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOV I-TRAILERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDABLES TRAYDROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIM• UTES & VANS • PANTECHS • MINI BUSES • TRAYS & HIAB • PRIME MOVERS• SEMI TRAILERS• FLAT DECKS• A & B TRAILERS• EXTENDABLES• SKELS• DROP DECKS•TAUTLINERSUtes1T UteVans1T Van1.5T vanMini Buses (drivers available)s8 seater Mini Bus12 seater Mini Bus14 seater Mini Bus25 seater Mini BusLuggage TrailersPantechs3T Pantech with tail lift (auto or manual)6T Pantech with full tail lift6T Pantech with walk up board8T Pantech with tuck away tail lift8T Pantech with walk up board Tautliners6T Tautliner - 10 pallet with tail lift6T Tautliner - 10 pallet without tail lift8T Tautliner - 12 pallet with tuck away tail lift 8T Tautliner - 12 pallet without tail lift8T Tautliner - 14 pallet with full tail lift8T Tautliner - 14 pallet without tail lift12T Tautliner - 14 pallet with full tail lift 12T Tautliner - 14 pallet without tail lift Trays2T Tray with drop sides3T Tray with tail lift & gates6T Tray with or without gates8T Tray with or without gates12T Tray with container pins Prime MoversSingle rated with sleeperBDouble rated with sleeperBrand new Kenworths & Argosys available in automatic or manualHiab8T Tray with front mounted craneSemi TrailersFlat Decks40’ Flat Deck Tri Axle45’ Flat Deck Tri AxleExtendables19 mtr Flat Deck extendable18 mtr Drop Deck extendable21mtr Flat Extendable Tri AxleSkels40’ Skel with 3 way pins40’ Retractable Skel Tri axleOpen Drop Decks45’ Open Drop Deck with 3 way pins - With or without gatesTautliners45’ Flat Tautliner45’ Drop Deck Tautliner with mezz floor 45’ Drop Deck TautlinerA TrailersA Flat with container pinsA Drop Deck with mezzanine floorA+B SetsFlat open setsFlat Tautliner setsDrop deck Tautliner setsECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-TRAILERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDAB RAYS SKELS DROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-TRAILERS FLAT-DECKS A-TRAILERS B-T XTENDABLES TRAYS SKELS DROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-TRAILERS FLAT-DECKS A -TRAILERS B-TRAILERS EXTENDABLES TRAYS SKELS DROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEM RAILERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDABLES TRAYS SKELS DROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERSShort or long term hireSouthern Cross Truck Rentals offer shortor long term rentals. Our vehicles can be hired as needed – hourly, daily, weekly or monthly.24 Hour emergency service Southern Cross Truck Rentals provides24 hour roadside assistance. In caseof emergency, breakdown or accident involving your hire vehicle call 4633 6100.1800TRUCKHIRE mobile AppIf you’re in and out of the office, why not download our App from the App Store for a quick quote.One way rentalsSouthern Cross offers One Way rentals from Sydney to most capital cities.Call us or visit our website to see our One Way deals.Corporate cardOur CorporateCard offers asignificant discountto businesses whichhave a large fleetor contracted drivers. To find out more about our Corporate Card contact our Sales Department.Truck & Driver Hire Equipment GuideLet us do the driving for youSouthern Cross Truck & Bus Driver Hiresupplies both truck & bus drivers.Depending on your job, you can choose tohire Southern Cross Truck & Bus Driver Hiredrivers either at an hourly or project rate.Included in your price are all drivers’workers’ compensation and travelrequirements and, having a fleet of over140 vehicles at our disposal, we can easilysupply vehicles should you require.S VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-TRAILERS FLA KS A-TRAILERS B-TRAILERS EXTENDABLES TRAYS SKELS DROP-DECK TLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOVERS SEMI-LERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDABLES TRAYS SKE DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIME-MOV I-TRAILERS FLAT-DECKS A-TRAILERS B-TRAILERS EXTENDABLES TRAYDROP-DECKS TAUTLINERS UTES VANS PANTECHS TAUTLINERS PRIMFor more informationCall 02 4633 6100or visit .auSouthern Cross Truck Rentals149 Smeaton Grange Road, Smeaton Grange NSW 2567• Long & short term hire • Vehicle relocations • Vehicle delivery• Vehicle pick up • One way rentals • Corporate card• Driver hire (LR to MC)• Truck & driver hire。
22(B)型客车落成作业指导书(209T型)
6.测量转向架上部与车体下部各零部件的垂直距离：在转向架横梁内侧≥50mm（手制动拉杆及托除外），横梁外 侧≥75mm。线管及空气制动管与轮缘距离须大于 100mm。 7.同一轴箱两钢弹簧高度差不得超过 6mm。 8.测量支持环下部与轴箱弹簧座的间隙，最小不得小于 5mm。 9.纵向牵引拉杆紧固后，测量摇枕两端与构架两侧间隙之差不大于 5mm。 10.测量各垂下品与轨面距离不小于 50mm。电气装置不小于 100mm，闸瓦插销不小于 25mm。 11.测量钩舌与钩腕内侧面距离，锁钩位置时应不大于 130mm，开钩位置时应不大于 245mm。钩舌与上钩耳间隙不 大于 6mm。 12.在锁钩位置时，往上托起钩锁铁，其移动量不大于 15mm。 13.检查钩提杆与下锁销连杆之距离须不小于 15mm，钩提杆须正位，与提杆座凹槽间隙不大于 2mm。 14.钩身上部与冲击座下部间隙为 20～48mm，磨耗板厚度应为 3～12mm。 15.车钩摆块吊有效长度之差不大于 2mm；摆块吊与吊座各接触安装面间隙不大于 2mm。 16.转向架上各配线须安装牢固并留有适当的余量，车辆运行中不被拉张，不磨碰。
支柱定位套和各圆弹簧的
图7
位置是否正确，杜绝转向架
内外侧或一、二位反位。
4.6.1 转向架吊起后，工作
者须指挥行车将转向架位
图8
序号 作业项目
9
22B 客车落成作业指导书（209T 型）
工具及材料
作业程序及标准
作业图示
置调整到安全通道正中间
稳定后，方可进行转运。转
运途中跟随清道并保持一
定安全距离。【图 8】
工具及材料
作业程序及标准
作业图示
生紧急情况，可以通过点击
架车机主控制柜停止键以
22型客车
22C型客车与22型客车之间的区别主要在车体的材质，车体材质采用耐候钢。
客车改造
20世纪90年代开始，符合翻新条件的22型客车进行了翻新改造（铁道部将部分22型客车进行翻新改造，型号 是为22B）继续用于慢车和短途车。部分22型客车翻新改造后车窗结构改为单元式。
23型客车（不包括23型餐车）是在YZ22型客车基础上的改进型，即YZ23型。1961年由四方机车车辆厂进行改 进，车厢取暖方式由温水循环取暖改为大气压式蒸汽取暖。
23型餐车是在CA22型餐车（四方机车车辆厂设计）不合理的平面结构改进而成的。分别由唐山机车车辆厂、 南京浦镇车辆厂设计制造。
31型是市郊用车，只有YZ31型硬座客车一种。其座位布局与地铁列车相仿。车门位于两个转向架之间，不同 于标准22型的两端位车门。
22型客车
中国铁路第二代主型铁路客车
01 简介
03 主要车种 05 改进型客车
目录
02 生产 04 同系列客车 06 客车改造
22型客车是中国铁路第二代主型铁路客车，曾经在中国铁路客运中长期占据着主导地位。于1956年开始设计、 试制，1959年生产，1994年停止生产。
简介
22型客车车体长23.6m，车宽3.105m，车高4.28米。车体采用有中梁薄壁筒体整体承载式全钢焊接结构。钢 骨架加外包板的全金属结构，在钢骨架外焊有金属板，形成一个封闭壳体，俗称薄壁筒型结构车体；为增加结构 的强度和刚度，壳体内采用了墙板压筋方式增加结构的强度和刚度，形成整体承载，两端有密闭式通过台。先后 采用202型（四方机车车辆厂研制，H型构架，摇动台式摇枕弹簧悬挂装置）/206型（四方机车车辆厂研制，侧部 中梁下凹的U型构架，带横向拉杆的小摇动台式摇枕弹簧悬挂装置）/209型（浦镇车辆厂在205型转向架基础上研 制，H型构架，摇动台式摇枕弹簧悬挂装置）转向架，构造速度100km/h，22B型为120km/h。22型客车车体优点 是结构比较合理、制造检修方便、安全可靠。以后内墙板和保温层又广泛采用了塑料贴面板和硬质聚苯乙烯泡沫 塑料，具有不吸潮，不需包装，耐碰撞，制造工艺简单等优点。22型客车采用独立温水取暖装置。22型客车车窗 是双扇单层玻璃向上开启的样式，隔音性能和密封效果较差。22型客车都不带空调，除了某些卧铺车以及后来曾 出现过YZ22型空调客车以外。
F22B技术资料
F22B正时记号拆装一、拆卸注：曲轴的正常转向为逆时针。
在拆卸凸轮轴正时皮带之前必须先卸下平衡器轴皮带。
1．拆卸：■下防溅罩■辅助传动皮带■PAS泵（不断开软管）■凸轮轴盖■正时皮带上盖[1]2．使曲轴转至1号缸的TDC处[2]，使得凸轮轴正时标记[3]与气缸头的上表面对齐[3]，且凸轮轴齿带轮的“UP”标记在顶部[4]。
3．用07JAB-0010200号工具07MAB-PY30100会皮带轮固定工具拧松并卸下曲轴皮带螺栓[5]。
4．撑起发动机5．拆卸■曲轴皮带轮[6] ■左发动机安装架■机油量尺和套管■调节螺母的橡皮密封件[7] ■正时皮带下盖[8]6．检查曲轴齿带轮正时标记对正[9]。
7．在[15]处安装6mm的螺栓，并轻轻拧紧。
8．拧松张紧轮固定螺母[10]，将张紧轮从皮带上取下，轻轻拧紧螺母。
9．卸下平衡器轴皮带和平衡器皮带曲轴齿带轮。
10．卸下正时皮带。
二、安装1．确保曲轴[9]和凸轮轴正时标记[3]和[4]对正。
注：使凸轮轴齿带轮标记[3]与气缸头上表面对齐。
2．从曲轴齿带轮开始，顺时针安装正时皮带，确保曲轴和凸轮轴齿带轮间的皮带张紧。
拧松张紧轮固定螺母[10]，使张紧轮可以转动，再拧紧螺母。
3．暂时装上曲轴皮带轮[6]和平衡器皮带曲轴齿带轮。
4．使曲轴逆时针缓缓转5或6整圈以安好皮带。
5．确保正时标记[3]，[4]和[9]对齐。
6．拧松张紧轮固定螺母[10]，使曲轴逆时针缓缓转动直到凸轮轴齿带轮过正时标记[3]3齿。
7．将张紧轮固定螺母[10]拧紧至44Nm。
8．使曲轴逆时针缓缓转至第一缸的TDC处，确保曲轴正时标记[9]和凸轮轴正时标记[3]和[4]对正。
9．假如不对正，则重复皮带安装和张紧程序。
10．拧紧6mm螺栓[15]以锁住正时皮带张紧轮臂。
11．使后平衡器轴正时标记[11]对正。
12．卸下活塞[12]，插入07LAG-PT20100号平衡器轴锁定销钉[13]。
13．使前平衡器轴齿带轮与正时标记[14]对正，卸下曲轴皮带轮[6]。
神州飞碟
神州飞碟是游乐设备中刺激又好玩的一款游乐设备，它是一个大转盘，自身会旋转，还会顺着月牙形轨道来回滑行，乘客就是坐在转盘边缘，背对转盘中心，这个过程有如天空高速飞翔一般刺激。
神州飞碟主要技术参数
整机尺寸：转盘直径6m
乘员人数：22p
功率：25kw
工作电源：50hz/380v
运行速度：9-12圈/分
占地面积：25*11米(含围栏)
神州飞碟是由机械、气动与油压和电气系统组成，河南世奇游乐设备厂的神州飞碟不但性能优异，操作简单，而且以新颖的造型、华丽迷人的彩灯装饰、逼真刺激的空战音响效果吸引众多的游客，是一项极佳的投资选择。
航天器部件终端带说明书
Y o u r C o n n e c t o r C o n s u l t a n t S i n c e1962M85049/128EMI/RFI ShieldTermination BandsKey Benefits of Termination Bands:►Easy to Terminate►Secure Tension Lock System►For Cost Effective ApplicationsSPACECRAFT C OMPONENTS T ERMINATION B ANDSThese Bands are commonly used to attach a braid or a shield to a backshell. They come in two shapes: Coiled or flat.To provide our customers with a cost effective solution, Spacecraft Components now manufactures Termination Bands and is qualified to the M85049/128 specification.Shown below is a summary of the various bands and their respective tools.ELECTRO- ADAPTER SHAPE SIZE SCP P/N MILITARY REFERENCE MILITARY TOOL NON MILITARY APPLICATIONSELECTRO-ADAPTER TOOLDANIELS TOOL214LF002Flat .245 x 14.0SCPSE-02F M85049/128-1M81306/2-01▲EAK214-25▲DBS-1101▲214L0002CoiledSCPSE-02CM85049/128-2BAND-IT ®SHAPE SIZE SCP P/N MILITARY REFERENCE MILITARY TOOLSNON MILITARY APPLICATIONSBAND-IT ®TOOLSDANIELS TOOLS GLENAIR TOOLSA10089Flat .242 x 14.25SCPBE-02F M85049/128-3M81306/1-01●A40199●DBS-2100●600-058●A10088Coiled SCPBE-02C M85049/128-4A11086Flat .242 x 18.00SCPBE-02FL18♦N/A A31189*Flat .120 x 8.125SCPBE-04F M85049/128-7M81306/1-02●A30199●DBS-2200●600-061●A31188*Coiled SCPBE-04C M85049/128-8A31089*Flat.120 x 14.30SCPBE-03FN/A* Mini Band♦ Two-piece construction GLENAIR SHAPE SIZE SCP P/N MILITARY REFERENCE MILITARY TOOLS NON MILITARY APPLICATIONSGLENAIR TOOLSBAND-IT ® TOOLSDANIELS TOOLS600-052Flat .242 x 14.25SCPBE-02F M85049/128-3M81306/1-01●600-058●A40199●DBS-2100●600-052-1Coiled SCPBE-02C M85049/128-4600-090Flat .242 x 18.0SCPBE-02FL18♦N/A M81306/1-01●600-058●A40199●DBS-2100●600-090-1Coiled SCPBE-02CL18♦600-057*Flat .120 x 8.125SCPBE-04F M85049/128-7M81306/1-02●600-061●A30199●DBS-2200●600-057-1*Coiled SCPBE-04C M85049/128-8600-083*Flat .120 x 14.30SCPBE-03F N/A600-083-1*CoiledSCPBE-03C* Mini Band♦ Two-piece constructionBand-It ® and Glenair bands work in the DBS or STS Tools, but two operations are required (terminate and fold-over) rather than the one operation (terminate/trim). DBS or STS-1101, and 1201 tools include both the termination tool and the secondary roll-over tool.SUNBANK SHAPE SIZE SCP P/N MILITARY REFERENCE MILITARY TOOLS NON MILITARY APPLICATIONSSUNBANK TOOLSDANIELS TOOLSS 3175F2Flat .245 x 14.00SCPSE-02F M85049/128-1M81306/2-01▲STS-1101▲DBS-1101▲S 3175-2Coiled SCPSE-02C M85049/128-2S 3175F3*Flat .118 x 14.25SCPSE-03F N/A M81306/2-02▲STS-1201▲DBS-1201▲S 3175-3*Coiled SCPSE-03C S 3175F4*Flat .118 x 9.50SCPSE-04F M85049/128-5M81306/2-02▲STS-1201▲DBS-1201▲S 3175-4*CoiledSCPSE-04CM85049/128-6* M ini BandDBS or STS-1101 and 1201 tools include both the termination tool and the secondary roll-over tool.MILITARY REFERENCEMILITARY TOOLS NON MILITARY APPLICATIONSMILITARY SHAPE SIZE SCP P/N Band-It®Daniels GlenairSunbank M85049/128-1Flat .245 x 14.00SCPSE-02F M81306/2-01▲–DBS-1101▲–STS-1101▲M85049/128-2Coiled SCPSE-02C M85049/128-3Flat .245 x 14.25SCPBE-02F M81306/1-01●A40199●DBS-2100●600-058●–M85049/128-4Coiled SCPBE-02C M85049/128-5Flat .118 x 9.50SCPSE-04F M81306/2-02▲–DBS-1201▲–STS-1201▲M85049/128-6Coiled SCPSE-04C M85049/128-7Flat .115 x 8.125SCPBE-04F M81306/1-02●A30199●DBS-2200●600-061●–M85049/128-8CoiledSCPBE-04C●One Step Tool ▲ Two Step Tool3040 Clayton StreetPhone: 702.851.7600 Email:************************North Las Vegas, NV 89032 Fax: 702.851.7620 Web: ® B and-It ® is a registered trademark of Band-It-IDEX, Inc., a division ofIDEX Corporation, of which Spacecraft Components Corp. is not affiliated..098 MAXØ1.120SCPSE-03C.198 ±.031.080 REF.118 ±.010.015 REF14.24 ±.060SCPSE-03FSCPSE-03F & SCPSE-03C TERMINATION TOOLS:DANIELS': DBS-1201▲ SUNBANK: STS-1201▲ M81306/2-02▲ ▲ Two Step Tool.098 MAXØ1.120M85049/128-6*SCPSE-04C M85049/128-8*SCPBE-04CØ0.860.198 ±.031.080 REF.118 ±.010.015 REF9.56 – 9.44M85049/128-5*SCPSE-04F.195 ±.031.053 REF.090 REF.115 ±.010.015 REF8.18 – 8.062.031 REFTAIL LENGTH INDICATOR MARKM85049/128-7*SCPBE-04FM85049/128-5 & M85049/128-6SCPSE-04F & SCPSE-04C TERMINATION TOOLS:DANIELS': DBS-1201▲ SUNBANK: STS-1201▲ M81306/2-02▲M85049/128-7 & M85049/128-8 SCPBE-04F & SCPBE-04C TERMINATION TOOLS:BAND-IT ®: A30199●DANIELS: DBS-2200●GLENAIR: 600-061●M81306/1-02● ● One Step Tool ▲ Two Step ToolM85049/128MINI-BANDS (.115 WIDE)MINI-BANDS (.115 WIDE)M85049/128-83040 Clayton StreetPhone: 702.851.7600 Email:************************North Las Vegas, NV 89032 Fax: 702.851.7620 Web: * M 85049/128-5, -6, -7, -8 are proposed.® Band-It ® is a registered trademark of Band-It-IDEX, Inc., a division of IDEX Corporation, of which Spacecraft Components Corp. is not affiliated..140 MAX.150 MAXØ1.750M85049/128-2SCPSE-02CM85049/128-4SCPBE-02CØ1.750.328 ±.031.100 REF.245 ±.010.019 REF14.31 – 13.94M85049/128-1SCPSE-02F.350 ±.031.130 REF.156 REF.245 ±.010.020 REF14.31 – 14.192.031 REFTAIL LENGTH INDICATOR MARKM85049/128-3SCPBE-02FM85049/128-1 & M85049/128-2 SCPSE-02F & SCPSE-02C TERMINATION TOOLS:DANIELS': DBS-1101▲ SUNBANK: STS-1101▲ M81306/2-01▲M85049/128-3 & M85049/128-4 SCPBE-02F & SCPBE-02C TERMINATION TOOLS:BAND-IT ®: A40199● DANIELS: DBS-2100●GLENAIR: 600-058●M81306/1-01● ● One Step Tool ▲ Two Step ToolM85049/128QUARTER-INCH TERMINATION BANDS (.245 WIDE)M85049/128-2M85049/128-4The termination of EMI/RFI shielding materials is a specialized sci-ence in today’s aerospace wiring systems. Application tooling is a critical factor in the overall performance of the wiring system components.DMC has worked closely with the world’s leading connector acces-sory manufacturers to develop the necessary tooling and acces-sories to meet the stringent demands of aerospace and defense system contractors. The resulting products afford the user many benefits which include:COMPATIBILITY with all currently available termination bands and systems.RELIABILITY through the use of commercially proven components and tool design practice.QUALITY & REPEATABILITY which are assured by a tension system.SERVICE & CALIBRATION – All tools produced by DMC are adjustable, and may be easily checked and set by the user. Also, expendable components such as cut-off blades are available for simple replacement by the user.LONG SERVICE LIFE – Properly maintained band applica-tion tools will produce thousands of reliable terminations.AFFORDABILITY – DMC tools continue to be the most cost effec-tive method to produce reliable wiring system shield termina-tions.Models are available for .250 in. (6.350 mm) and .125 in. (3.175 mm) wide bands from all current suppliers to M85049/128.THE PNEUMATIC BAND APPLICATION TOOL...is a cost effective system that speeds production and im-proves ergonomic conditions which are present when manual tools are used. Band tension is precisely applied by a depend-able pneumatic system which is consistent and repeatable.The tension system of the pneumatic band tool is adjustable, and can be checked by use of the verifcation devices avail-able from DMC. (See pages 68-69.)The cutter blade and other components of the DMC Pneu-matic Band tools are interchangeable with the same serieshand tools. The rugged design and field replaceable blades make the PBT/PMBT series the best choice for production ap-plications where EMI/RFI bands are used to terminate wire harness shielding.THE HAND OPERATED BAND APPLICATION TOOL (REFERENCE AS81306/2)is an excellent choice for many production and maintenance operations. Like the power driven models, they too can be calibrated by the user to provide reliable terminations throughout the service life.The lightweight construction and small “nose” pro-file enable the user to apply termination bands in even the tightest of working areas.EMI/RFI Band Application Tooling byBackshells for Banding, Over Molding or Shrink BootsConnectors withIntegrated Backshells for Banding, Over Moldingor Shrink BootsAS50151 – All Series, Crimp or SolderAS95234 – Reverse Bayonet, Crimp or Solder MIL-DTL-26482 – All Series, Crimp or Solder MIL-DTL-38999 – Series I, II & IIISee Calalog 601 for details.SCPB00SV AS95234(REVERSE BAYONET)SC50SV AS50151(MS 3450)SC76SV MIL-DTL-26482Series 2(MS3476)SC3924SV MIL-DTL-38999Series III (D38999/24)3040 Clayton StreetPhone: 702.851.7600 Email:************************North Las Vegas, NV 89032 Fax: 702.851.7620 Web: SF-403NOV.2014SCP 50151 Style ConnectorsAS95234 Reverse Bayonet ConnectorsSCPT 26482 Style SC1 38999 Series I SC2 38999 Series II SC39 38999 Series IIISCPB SeriesConnector AccessoriesConnectors with Integrated BackshellsHeadquarters3040 Clayton StreetPhone: 702.851.7600 Email:************************North Las Vegas, NV 89032Fax: 702.851.7620 Web: Italy OfficeSpacecraft Components , Sp A Milan, Italy+39 (335] 719.4512Arizona Office2432 W. Peoria Ave.Suite 1192Phoenix, AZ 85029Tel: 602.944.2351Fax: 602.997.0373South Carolina Office 25 Woods Lake Rd., Suite 403Greenville, SC 29607Tel: 954.748.4540Fax: 954.748.4128Florida Office4577 Nob Hill Road Suite 106Sunrise, FL 33351Tel: 954.748.4540Fax: 954.748.4128Try Our Other Connector ProductsGet All of OurCatalogs & Product Brochures on One DiscY o u r C o n n e c t o r C o n s u l t a n t S i n c e 1962COMPILED AND PRODUCED BY SPACECRAFT COMPONENTS CORP.©2014 SPACECRAFT COMPONENTS CORP ., NORTH LAS VEGAS, NV 89032。
航天器操作手册
航天器操作手册1. 简介本航天器操作手册旨在为操作员提供必要的指导和信息，以确保顺利、安全地操作航天器。
请严格按照本手册所述的操作步骤执行，并遵循任何特定的引导或警告。
2. 航天器控制系统2.1 主控制面板航天器的主控制面板位于驾驶舱内，用于控制各个航天器系统。
在操作之前，确保熟悉主控制面板上各个按钮和开关的功能，并遵循正确的操作顺序。
2.2 航天器动力系统航天器的动力系统包括发动机和推进器。
在启动动力系统之前，请确保已经进行了正确的预检和安全检查，并按照指令操作控制面板以启动或停止动力系统。
2.3 航天器导航系统航天器的导航系统用于确定位置、速度和航向。
在操作过程中，及时校准导航系统以确保航天器的精确导航。
3. 航天器起飞和降落操作3.1 起飞准备在执行起飞操作之前，需进行以下准备工作：- 检查航天器系统状态；- 校准导航系统；- 确定起飞路线和高度；- 预检动力系统。
3.2 起飞过程- 启动动力系统；- 缓慢推进推进器，使航天器逐渐升空；- 根据导航系统的指示调整航向和高度。
3.3 降落操作- 根据导航系统的指示确定降落目标；- 控制推进器并调整航向，确保航天器平稳降落。
4. 紧急情况处理4.1 呼吸系统失效若发生呼吸系统失效的情况，立即执行以下步骤： - 穿戴氧气面罩；- 尽快寻找并更换故障呼吸设备。
4.2 火灾若发生火灾，立即执行以下步骤：- 封闭相关区域，防止火势蔓延；- 使用灭火器或其它灭火装置进行火灾扑灭。
4.3 外部攻击在遭遇外部攻击时，应采取以下措施：- 启动防御系统，确保航天器安全；- 寻找安全避难所，并保持常规通讯以获取支持。
5. 维护和修理定期进行航天器的维护和修理是确保其性能和可靠性的关键。
在进行维护和修理时，请遵循相关的操作流程和安全指南，并确保具备必要的工具和设备。
6. 结束操作在结束操作前，请进行以下步骤：- 关闭动力系统；- 离开驾驶舱时，确保航天器处于安全状态。
v22飞机参考资料
2005年5月20日。
美国空军在凯特兰空军基地组建了第一个V-22倾转旋翼机训练中队，围绕V-22用于运送特种作战部队的设计初衷展开系统训练。
2005年6月。
美国海军陆战队VMX-22作战试验与评估中队的全部8架“鱼鹰”集中在美国海军LHD 5“巴丹”号两栖攻击舰上。
进行最后阶段的作战评估试验……这一系列事件标志着这种研制期长达25年的新型作战飞机真正投入了部署。
V一22有着独特而优异的性能.但在技术上仍然存在着较严重的问题，对此。
我国专家将进行详尽的分析。
美国研制的V一22“鱼鹰”倾转旋翼机，是一款颇受媒体关注的多功能垂直/短距起降航空器。
其新颖的构思、优异的性能和宽广的适用范围，给人留下了深刻印象。
但这种先进的三军通用型飞机的称谓却值得商榷，所采用的技术和总体设计方案也有许多需要改进的地方。
关于V-22的称谓严格地讲，V一22“鱼鹰”一类的飞行器不应叫做“倾转旋翼机”。
虽然相对干正常的飞行状态(发动机、螺旋桨处在与飞机纵轴平行的位置)，V一22的螺桨旋翼在短距起降、垂直起降、悬停、过渡飞行等状态时的确是“倾转”的，但它们并非单独偏转，而是随着发动机舱的转动而转动。
因此，该机种的准确名称应该是“采用倾转发动机技术”的直升飞机。
美国人之所以将“鱼鹰”定义为倾转旋翼机，是沿用了贝尔直升机公司对XV-3的叫法。
1955年8月试飞成功的XV-3垂直起降研究机，是一架真正意义上的倾转旋翼飞行器。
该机的动力装置是一台450马力的涡轴发动机，飞行时，发动机输出的功率通过一个横轴传给设在左右翼尖上的螺桨旋翼，使之能够同步对转、产生拉力。
两副工作中的螺桨旋翼可由一套特殊的操纵机构控制，在水平和垂直位置间来回转动，以改变拉力矢量的方向，从而构成“直升机状态”、“定翼机状态”和“过渡飞行状态”。
试飞结果表明，XV-3能够在10秒钟之内完成90。
的飞行姿态转换。
1973年，应美国陆军和航空航天局的要求，贝尔公司结合XV-3倾转旋翼机的设计经验，研制了一种采用低桨盘载荷旋翼和倾转发动机技术的垂直起降航空器一一xV-15试验机。
Lockheed Martin Boeing F A-22 Raptor 2商业机舱系统说明书
Lockheed Martin/Boeing F/A-22 Raptor2 EATON Aerospace Group C5-24D April 2014The F/A-22 Raptor replaced the venerable F-15 Eagle as America's premier front-line fighter jet, starting in 2005. It is the air-dominance fighter of the 21st century. "The Raptor is a flexible, adaptable, versatile combat aircraft capable of seeing all, knowing all, and shaping all that occurs on or above the battlefield," says Chief Test Pilot Bret Luedke, one of the pilots responsible for flight-testing the F/A-22. "And do all that while flying supersonic and all but invisible to radar," he added. Eaton, a recognized leader in the design and manufacture of hydraulics, fuel, conveyance and actuation products, was chosen to provide key products for the F/A-22. The 4100 psi (28,300 kPa) hydraulic system on the F/A-22 incorporates Eaton's main engine-driven pumps, auxiliary power pump, air recharge compressor motor, gun drive motor, fuel transfer motor, and main and side weapons bay door motors.The F/A-22 employs a hydraulic gun drive, which is comprised of two discrete component subassemblies integrated into one assembly. This provides mechanical rotary power to the gun when commanded by electric signal or manual input. The fuel transfer motor, a variable displacement 4000 psi (27,600 kPa) inline hydraulic motor, is used in combination with a centrifugal fuel pumping element to provide a fuel pressure compensated fuel boost pump. The 5.9 gpm (22.33 L/min.) hydraulic motor/fuel pump is used on the F/A-22 to boost fuel from the main fuel tanks to the main fuel pumps at essentially constant fuel pressure. This is the first time that avariable displacement motor has been used to provide pressure compensation for a centrifugal fuel pump.With the auxiliary power unit, emergency power is provided by a 27 gpm (102 L/min.), 6,000 rpm, variable displacement, 4000 psi (27,600 kPa), pressure-compensated inline piston pump with an electrical depressurization valve (EDV). Design features include a one-piece housing and solenoid valve with pigtail for vibration isolation from the pump.Eaton's components provide fluid control and actuation for the rudder control, landing gear, electronic warfare emergency power generator, and nose wheel steering systems. The rudder shuttle valve is designed for use at up to 4100 psi (28,300 kPa) operating pressure, and automatically shuttles hydraulic power to the aircraft's rudder system from one of twoindependent hydraulic systems by utilizing the differential pressure between the two independent system pressures to initiate the shuttle. Eaton also provides the hydraulic motor/control valve packages for the weapons bay doors. These consist of a one-piece aluminum manifold within which the hydraulic motor and various control valve components are mounted and interconnected. The heart of the package is an Eaton fixed displacement and variable displacement hydraulic motor, which is configured as a cartridge. The manifolds also provide the hydraulic interface between the side weapons bay door/main weapons bay door (SWBD/MWBD) and aircraft hydraulic supply systems. Hydraulic-mechanical powerconversions for the side weapons bay door and the main weapons bay door are provided by the fixed displacement hydraulic motor and variable displacement hydraulic motor. Speed and direction for both the SWBD and MWBD arecontrolled by the flow limiter/directional control valve, which is a 4-way variable position, slide, and sleeve type metering valve that is spring centered to its normally-closed position where the control ports are overlapped.Eaton is also providing the electro-mechanical seat actuator for the aircraft's Advanced Concept Ejection System (ACES II). As well, Eaton also supplies Aeroquip ® Kevlar ® hoses, Rynglok ® tube fittings, high performance fuel tubes, mini-modular cooling couplings, cockpit air couplings, rotomold ducting, landing gear swivels and E-Seals.Aircraft systems monitoring components such as Eaton's Tedeco ® oil level sensors, debris screen chip collectors, and a Lubriclone ® air/oil separator system can be found on this versatile aircraft as well. The oil level sensor can detect three levels of oil: full, add, and low. Magnetic reed switches have a redundant circuit for high reliability. A reservoir pickup tube is installed in the Airframe Mounted Accessory Drive (AMAD) to assure proper oil flow with minimum air intrusion when the aircraft becomes inverted. Its magnetic chip collector is located in the lubricating fluid flow of the AMAD and traps ferrous wear debris of magnetic attraction, preventing the particles from causing damage to key components. The analysis of these particles may provide an early warning of abnormal wear or breakdown of components within the AMAD, thus increasing its life.The Lockheed Martin F/A-22 Raptor is a swept-winged fighter with blended engine intake/wing leading edge root extension. The aircraft is powered by two Pratt & Whitney F119-PW-100afterburning turbofans, each fitted with a two-dimensional thrust-vectoring nozzle.The advanced tactical fighter's engines produce more thrust than any current fighter engine, especially in the military power regime, allowing the F/A-22 to cruise efficiently in excess of Mach 1.5 without the use of fuel-guzzling afterburners. Thiscapability greatly expands the F/A-22's operating envelope in both speed and range over current fighters.It’s key feature is an advanced avionics architecture using the most advanced fiber-optic and digital electronic flight and weapon and control system in development. All weapons are carried internally.The F/A-22 is intended for an air superiority role,providing much greater range, payload, time on station, and agility than the F-15 and F-16 fighters of today. A combination of improved sensor capabilities, improved situational awareness and improved weapons provides first-kill opportunity. The F/A-22 features a sophisticated sensor suite that allows the pilot to track, identify, and shoot opposing aircraft at beyond-visual-ranges while having the ultimate in close-in dog-fight capabilities. No other aircraft has had thiscombination of characteristics.Lockheed Martin/Boeing F/A-22 Raptor Component & Systems Overview Eaton’s Aerospace Group Product CapabilitiesLockheed Martin/Boeing F/A-22 Raptor Component & Systems OverviewEngine Solutions1. M agnetic Chip Collector2. L ubriclone3. M ini-Modular CoolantCouplings4. O il Level Sensor Motion Control5. M ain Weapons Bay DoorMotor/Package6. S ide Weapons Bay DoorMotor/Package7. Gun Drive Motor8. Landing Gear Sequence Valve9. Landing Gear Control10. Landing Gear Brake Swivels11. Rudder Shuttle ValveHydraulic Systems12. M ain Engine-Driven Pump13. Rynglok Tube Fittings14. Reservoir Pick Up Tube15. Kevlar Hose Assemblies16. S tainless Steel ReinforcedHose Assemblies17. Auxiliary Power Unit Pump18. Utility Isolation Valve19. E lectronic WarfareControl Valve20. Pressure Switches21. P ressure TransducerFuel & Interting22. Fuel Transfer Motor23. M ain EngineFuel Line Assemblies1738221823612415141613975101112192120EATON Aerospace Group C5-24D April 2014 34 EATON Aerospace GroupC5-24D April 2014Mini ModularCoolant CouplingsEaton's miniature modular self-sealing coolant couplings are used extensively in the F/A-22 to help keep the aircraft's state of the art electronic systems cool. These couplings weredeveloped in response to today's need for liquid flow through avionics packaging technologies. The design of these couplings provide unequaled performance in pressure drop and superior reliability in sealing out dust, particulates and foreign matter, while preventing fluid leakage during connection/ disconnection of system components.Kevlar ® Reinforced Hose AssembliesEaton's Aeroquip product line Kevlar ® hose assemblies are utilized extensively throughout the F/A-22 aircraft to optimize weight reduction throughout the hydraulic system. The AE319 and AE355 hose assemblies are rated to 4000 psi (27,600 kPa) and are used in the low pressure hydraulic return system. The AE319 is a heavy duty hose and is used in areas that experience moresevere service.2055 Series Coolant Couplings Eaton's 2055 series push-pull coolant couplings are usedexclusively throughout the F/A-22 PAO coolant system. The 2055 Series were specifically designed for light weight, low profiledemanding applications like thatneeded on the F/A-22.Rynglok ® T ube FittingsThe fittings for the F/A-22 are the 4000 psi (27,600 kPa) titanium and the low pressure aluminum Rynglok ® fittings. The titanium, axial swage fittings provide the link to join fluid delivery tubing, while minimizing system weight. Fittings include permanent and arc seal connections in straight elbow and tee configurations.Stainless Steel Reinforced Hose AssembliesStainless steel reinforced hose assemblies for the F/A-22 include the 666 smooth bore, medium pressure hose assemblies and the AE641 convoluted hose assemblies which are used in the low pressure return side of the hydraulic system and in the fuel system.Eaton's Aeroquip wire reinforced medium pressure hose assemblies are rated for pressures up to 1500 psi (10,343 kPa) and feature a wire reinforced, Teflon ® hose with light weight, low profile crimp fittings.Convoluted hose assemblies provide increased flexibility and are excellent for use in areas that require a tight bend.ECS Air ValvesCockpit video display units are kept cool using Aeroquip ECS Air Valves. The valves are made from lightweight injection-molded nylon material and aluminum castings. Internal valving automatically closes upon removal of the video display units and creates an equivalent pressure drop across the valve that simulates the pressure drop as if the video display unit were still installed.Landing Gear Brake Swivels These 4,000 psig (27,600 kPa) operating pressure swivels are used on the F/A-22 landing gear system to help deliver fluid to the aircraft's braking system. Manufactured from high strength 7075 aluminum material to help keep weight to a minimum, these swivels are capable of a full 360 degrees of rotation.Rotomold DuctingEaton's center console and canopy defog ducts provide environmentally controlled air to the cockpit. These ducts are made of seamless lightweight rotationally-molded nylon material. There is one each of these ductsper aircraft.EATON Aerospace Group C5-24D April 20145Landing Gear Sequence Valve The landing gear sequencevalve is used to control hydraulic pressure and fluid flow forsequencing the main landing gear with the main landing gear door. A pneumatically actuated override feature is provided for emergency operation, which interconnects both the "DOWN" and "LG EXT" ports. Since there is no direct pressure source, the operating pressure comes from either the "DOWN" or "UP" hydraulic command lines via a logic circuit which consists of four miniaturized check valves.Electronic Warfare Control ValveThe solenoid controlled pilot-operated spool valve provides two independent spools forcontrolling hydraulic pressure and return fluid flow for extension and retraction of two hydraulic actuators. There are two of these valves per aircraft.Main EngineFuel Line AssembliesFuel is supplied to each of the engines in the F/A-22 via two main engine fuel line assemblies. Each assembly is three inches in diameter, and approximately two to three feet long. The fuel lines are made from aluminum material and each contains three articulating ball joints. Each ball joint is capable of 20 degrees ofangular movement.Rudder Shuttle ValveThe rudder shuttle valve isdesigned for use up to 4100 psi (28,300 kPa) operating pressures. It automatically shuttles hydraulic power to the aircraft's rudder system from one of twoindependent hydraulic systems by utilizing the differential pressure between the two independent system pressures to initiate the shuttle. The valve is electrically operated through a 28 solenoid valve for primary system isolation and has a return system check valve and flow limiter for downstream functions.Side Weapons Bay Door (SWBD) Motor/Control Valve PackageThis motor/control valve package is used to control and limit the flow of hydraulic fluid to the 4000 psi (27,600 kPa) fixed displacement hydraulic motor (FDHM), which in turn will be used to drive the geared rotary actuator to position the side weapons bay door of the aircraft.Main Weapons Bay Door (MWBD) Motor/Control Valve PackageThis motor/control valve package is used to control and limit the flow of hydraulic fluid to the 4000 psi (27,600 kPa) variable displacement hydraulic motor (VDHM), which in turn is used to drive the geared rotary actuator to position the main weapons bay door of the aircraft.E-SealsThe lower exit duct seal is a metallic E-Seal that is installed between the primary heatexchanger and the exit duct of theF/A-22 aircraft.Utility Isolation ValveThe utility isolation valve provides emergency tow brake operation for the F/A-22 aircraft. During emergency stop conditions, the solenoid-operated, two-position, three-way valve is commanded open to provide hydraulic system 2-reservoir accumulator pressureto the aircraft’s brake circuit.6 EATON Aerospace GroupC5-24D April 2014Oil Level SensorEaton's oil level sensor senses three levels of oil - full, add, and low. Magnetic reed switches have a redundant circuit for highreliability.Reservoir Pickup T ubeInstalled in the Airframe Mounted Assembly Drive (AMAD) to assure proper oil flow with minimum air intrusion when the aircraft becomes inverted.Landing Gear Door Sequence ValveThe landing gear door sequence valve is a mechanically-operated, two-position, four-way hydraulic sequence valve that controls hydraulic supply and return fluid flow for sequencing the main landing gear door with the main landing gear.Solenoid Operated Switching ValveThe hydraulic switching valve control module, is a 6-way 2-position, solenoid-operated, non-interflow type, selectorvalve, with position indicator. The function of the switching valve is to direct pressure and return fluid flow from a secondary hydraulic system of the aircraft (System 1), during maintenance of the aircraft, to power utility functions normally dedicated to the primary system (System 2) for these functions.Magnetic Chip Collector The 1D7092 and 1D7093magnetic chip collector is located in the lubricating fluid flow of the Airframe Mounted Accessory Drive (AMAD) and traps ferrous wear debris by magnetic attraction. This prevents the particles from causing damage to the drive components. The analysis of these particles may provide an early warning ofabnormal wear or breakdown of components within the AMAD,this increasing its life.Pressure SwitchEaton's pressure switches are used for main engine and Auxiliary Power Unit (APU) pump pressure indication/monitoring.Pressure T ransducer Eaton's pressure transducer monitors hydraulic system pressure in the aircraft.EATON Aerospace Group C5-24D April 20147Main Engine Driven Pump Hydraulic power for the F/A-22 is provided for all flight control and utility functions by four 72 gpm (273 L/min.) 4411 rpm, variable displacement, 4100 psi (28,300 kPa), pressure-compensatedeleven-piston pumps. Each pump is equipped with an Electrical Depressurization Valve (EDV)and features a one-piece housing, 11 piston-rotating group, and solenoid valve. Displacement is 4.1 cu. in/rev. (67.15 ml/rev.). Dry weight is 34 lbs (15.42 kg).Gun Drive MotorThe hydraulic gun drive employs a 4000 psi (27,600 kPa), 7250 rpm, fixed displacement inline hydraulic motor and control valve which is integrally mounted to automatically control hydraulic motor speed, acceleration and deceleration. Valves are also included to allow control of the gun port and purge door actuators. Displacement is 0.642 cu. in/rev. (10.5 ml/rev.). Dry weight is 16.25 lbs (7.37 kg).Lubriclone ®Separates entrained air from the scavenged lube system oil by centrifugal force. Uniqueinternal design affords separation efficiencies up to 99%. Wearparticles are also directed to an area where a debris monitor can readily capture and indicate their presence.Auxiliary Power Unit Pump Emergency power is provided by a 27 gpm (102 L/min.), 6,000 rpm, variable displacement, 4000 psi (27,600 kPa), pressure-compensated inline piston pump with electrical depressurization valve (EDV). Design features include a one-piece housing and solenoid valve with pigtail for vibration isolation from pump. Displacement is1.12 cu. in/rev. (18.35 ml/rev.). Dry weight is 14.1 lbs.Side Weapons Bay Door Motor Hydraulic mechanical power conversion for the side weapons bay doors is provided by two 4000 psi (27,600 kPa), 11,200 rpm fixed displacement motors. Displacement is .36 cu. in/rev. (5.89 ml/rev.). Dry weight is 3.11 lbs (1.41 kg). The motor is integrated with the Motor/Control Valve Package.Fuel T ransfer MotorThis variable displacement 4000 psi (27,600 kPa) inline hydraulic motor is used in combination with a centrifugal fuel pumping element to provide a fuel pressure compensated fuel boost pump package. The 5.8 gpm (21.96 L/min.) hydraulic motor/fuel pump is used on the F/A-22 to boost fuel from the main fuel tanks to the main fuel pumps at essentially constant fuel pressure. This is the first time that avariable displacement motor has been used to provide pressure compensation of a centrifugal fuel pump. Displacement is0.13 cu. in/rev. (2.13 ml/rev.). Dry weight is 9 lbs (4.08 kg).High Pressure Actuator Pump Eaton's Model 841200 highpressure actuator pump provides the "fueldraulics" on the Pratt & Whitney F119 engine, which is the most advanced engine inproduction and is used on the U.S.Air Force's F-22 Raptor.Eaton Aerospace Group9650 Jeronimo Road Irvine, CA 92618tel: (949) 452-9500fax: (949) 452-9555 /aerospace Copyright © 2014 Eaton All Rights Reserved Form No. C5-24DApril 2014。
22座(B级)神州飞碟使用维护说明书
FD22神州飞碟（B级）使用维护说明书（版本：A）编制/日期：审核/日期：批准/日期：广东ABC游乐设备有限公司目录第1节设备概述 (1)第2节设备安装与调试 (5)第3节操作规程及注意事项 (6)第4节常见故障及排除方法 (9)第5节操作、维修及救援人员 (10)第6节设备日检、月检、年检 (13)第7节设备的使用、保养与维护 (18)第8节日常润滑部位及要求 (22)第9节使用寿命与易损件、标准机械电气零部件清单 (25)第10节乘客须知 (27)第11节应急措施 (29)第12节售后服务 (32)第13节警告 (33)附件1 神州飞碟运行日记营业检查表 (34)附件2 神州飞碟维修保养记录表 (36)附件3 年度无损检测综合表 (37)附件4 高强螺栓测位置图 (42)附件5 电气原理图 (44)第1节设备概述1.1 基本简介“神州飞碟”是我公司参照国外同类设备并加以改进研发的一项大型游乐项目。
该设备的特点是外观华丽、玩法奇特。
可同时容纳22人乘坐的仿真飞碟，坐落在弯月型的导轨钢架上，乘客以骑跨式乘坐该设备。
设备整体配备彩色灯光装饰。
飞碟转动时配以灯光的变幻，使飞碟成为游乐园中一处光彩夺目的景观。
在设备运动模式上突破了传统设备单一的运动模式，飞碟沿着钢架导轨做高速上冲下荡的同时，飞碟转盘自身也正反交替旋转，使乘客感觉到无与伦比的兴奋与刺激。
1.2 设备运行原理神州飞碟是依据《特种设备安全监察条例》、《游乐设施安全技术监察规程（试行）》、《游乐设施安全规范》（GB8408-2208)、《滑行车类游艺机通用技术条件》（GB/T18159-2208)等标准进行设计，符合相关规范的要求。
保证了该设备运行平稳、噪音小、乘坐舒适、造型美观、运行可靠。
工作原理：本设备以电动机为动力源，飞碟沿导轨左右摆动由电机经过两级减速后驱动摩擦轮带动飞碟底盘实现。
飞碟转盘做旋转运动通过旋转减速机驱动回转支承带动转盘旋转来完成。
Airbus 产品指南说明书
Aircraft GuideData about hundreds of jets, turboprops and helicoptersAS SOON AS itS FiRSt owner departs from the man-ufactu r e r ’s delive r y cente r , a new ai plane technically becomes used (or preowned). Fo r va r ious r easons, how-ever , 10 year s after an air -cr aft’s final pr oduction date is gene ally conside ed them ilestone separating “newer” used business ai c aft f om “older” ones.In deciding which a ircraft to cover, we went well past this 10-year mark to p rovide i nfor mation on all business ai r planes and helicopte r s manufactu r ed since 1997. This means our list includes some models manufactured befor e that year , as long as they we r e still being p r o-duced as r ecently as 1997. As a rule, a long production run is indicative of a success-ful aircraft.We have not listed new models that, at p ess time, had yet to receive final certi-fication.n Source: Conklin & de Decker. *Textron acquired Beechcraft in March 2014, merging it with Cessna Aircraft to create Textron Aviation. N/A = not availableDassault Falcon 7XBombardier Global 6000Emivest SJ30Nextant 400XT Bombardier Challenger 300continued on next pageFalcon 2000SGENERAL SPECSUSED PRICESAirplane and some helicopter selling prices are based on the latest edition of the Aircraft Bluebook Price Digest. Additional h elicopter pricing data is from helicopter appraisers HeliValues.PASSENGER/PILOT SEATING The typical passenger seating on the aircraft is not the maximum certified seats. These numbers may vary for different operations (corporate, c ommercial, EMS, etc.). Maximum n umber of passengers is as certified. Pilot seating is typical (i.e., two pilots may be indicated even if aircraft is single-pilot certified).CABIN DIMENSIONSCabin volume is the interior volume, with headliner in place, without seats or other furnishings. Cabin width, height and length are based on a completedi nterior. Width and heightare the maximum within thatcabin space. In “cabin-class” aircraft, the length is measured from the cockpit divider to the aft p ressure b ulkhead (or aft cabin bulkhead, if unpressurized). For small-cabin aircraft, the distance is from the cockpit firewall to the aft bulkhead.WEIGHTSMax takeoff weight (mtow)is specified during aircraft certification. Fuel capacity is in gallons based on 6.7 pounds per gallon (jet fuel). Max payload with full fuel is the useful load minus the usable fuel. The useful load is based on the maximum ramp weight minus the basic operating weight.PRODUCTION STARTED/ENDED Year of the first delivery to the year of the last serial-number delivery.NUMBER BUILTTotal number produced, which may include converted aircraft.Source: Conklin & de Decker. *Textron acquired Beechcraft in March 2014, merging it with Cessna Aircraft to create Textron Aviation. N/A = not availableExtra 500Dornier SeastarJET AND TURBOPROP RANGEThe maximum IFR range withall passenger seats occupied,using the NBAA IFR alternate fuelreserve calculation for a200-nm alternate.HELICOPTER RANGEFor all helicopters, the maximumVFR range with all passengerseats occupied.SPECIFIC RANGEThe distance an aircraft can travelfor a given amount of fuel used.Based on nautical miles traveledper pound of fuel burned.CRUISE SPEEDSLong-range cruise speed isthe speed required to achievemaximum range (best fueleconomy). High-speed cruise(aka maximum cruise speed)is top speed at a gross weightcorresponding to four passengers(turbine aircraft) or twopassengers (piston aircraft) andhalf of total fuel.SERVICE CEILINGFor airplanes, this is the highestaltitude at which a 100-fpm rateof climb is possible at maximumtakeoff weight with all enginesrunning. For helicopters, this isthe maximum certified altitudefor operation.BALANCED FIELD LENGTH (BFL)BFL is the distance obtained bydetermining the decision speed(V1) at which the takeoff distanceand the accelerate-stop distanceare equal (multi-engine airplanesonly). BFL is based on a dry sea-level runway, no wind, NBAA IFRreserves and 86 degrees F.LANDING DISTANCEThis is computed using the landingdistance from 50 or 35 feet abovethe ground at sea level (dependson certification criteria) multipliedby 1.667. No credit is given forthrust reversers. Configuration iswith four passengers and NBAAIFR fuel reserve on board.Source: Conklin & de Decker N/A = not availableAgustaWestland AW139Eurocopter EC 135MD Helicopters 530FRobinson R66Enstrom 480B。
神州号双层内燃动车组
神州号双层内燃动车组神州号双层内燃动车组编辑词条B 添加义项神州号双层内燃动车组神州号动车组属于NZJ2型动力集中式双层内燃动车组，由大连机车车辆厂、长春客车厂与四方机车车辆厂及北京铁路局联合研制，分双层空调硬座车和双层空调软座车两个车种。
总体列车由动车+10辆双层拖车+动车组成。
子弹头列车的车头采用了目前世界上较先进的分布式计算机控制系统，可以避免因一个地方发生故障而导致“全身瘫痪”。
自动监控系统可显示列车运行的重要参数，驾驶员一目了然。
列车装用的新型准高速转向架确保安全，空气弹簧减震使列车平稳，即使在高速运行中发生意外紧急刹车，列车仍旧平稳如常，还有全球卫星定位系统等其他现代化设施。
神州号一共有机车5组（10个机车头），拖车4组（40个车厢）。
原配属北京铁路局。
现2.5组机车头，2组拖车（20个车厢）配属原南宁铁路局；2.5组机车头，2组拖车（20个车厢）配属武汉铁路局。
2000年10月18日起，神州号动力集中式双层内燃动车组在京山线北京-天津之间开行。
自2007年4月18日起，津京间开行动车组列车后，部分神州号车底城际特快列车T537/8次、T539/40次、T543/4次、T545/6次、T549/50次、T551/2次、T553次停运。
自2007年4月23日起，往返于北京和天津间2对神州号车底城际特快列车T561次(原T535次)北京西至天津北、T562次(原T536次)泰达至北京西、T565次(原T547次)北京西至泰达、T566次(原T548次)天津北至北京西在开行5天之后停运。
自2007年7月24日起，神州号列车因将要调配给南方铁路局使用，京津之间的T563/4次、T591/2次、T593/4次、A221/2次、A223/4次列车、天津—泰达的N213/4次列车停运。
至此，京津之间的神州号列车完全停运。
————————2007年8月，原柳州铁路局、武汉铁路局接收神州号动车组。
2007年8月18日起，原柳州铁路局开行南宁－柳州N725/6次，南宁－桂林N721/2次神州号列车。
20座高空揽月(B级)使用维护说明书
20座（B级）高空揽月使用维护说明书编制：审核：批准：郑州ABC游乐设备有限公司2019年08月郑州ABC游乐设备有限公司敬告用户尊敬的用户：感谢您购买本公司的产品！在您使用本产品前，请务必仔细阅读本说明书。
设备操作和维修人员不仅要了解和掌握本说明书的内容，还应根据国家相关部门针对游乐设备安全经营颁布的法规，结合本单位的具体情况编制此设备的安全、经营操作和维修规程，建立岗位责任制。
设备操作人员要根据国家质量监督检验检疫总局，国质检锅（2001）202号文件之规定取证上岗。
对于未经取证上岗人员的操作或虽有上岗证，但未按本说明书要求进行操作而引发的人身伤害事故或设备故障，本公司概不负责。
对于非专业的维修保养或在维修保养时使用了非正宗的备件而造成的不良后果，用户自行负责。
目录1 设备概述 (1)2 主要参数 (1)3 结构原理与安全措施 (2)4 安装与调试 (3)5 操作与运行 (5)6 游客须知 (6)7 紧急救援措施 (7)8 维护与保养 (10)9 润滑 (11)10 设备的维修及检查 (12)11 整机及关键零部件的设计寿命 (12)12 外购件使用要求 (12)13 常见故障及排除方法 (12)14 易损零部件及更换周期 (13)15 备件清单 (13)16 辅助工程 (13)郑州ABC游乐设备有限公司侧视图正视图图1 设备简图GKLY 高空揽月使用说明书1 设备概述“高空揽月”游艺机属观览车类游乐设备，是公园游乐设备中的大型游乐设备，游客乘坐的吊箱在强离心力作用下，高速旋转翻飞，仿佛被入超越时空的天体，翻江倒海、天旋地转，惊心动魄的刺激，风驰快感，令人回味无穷。
高空揽月卓越的创新设计，符合现代人的娱乐心理和刺激需求，是年轻人的佳选择，是假日里好选择。
游客在极速地上摆与下落过程中，尽情寻求惊险与刺激，在紧张生活之余，追求另一种快感。
本设备按照《游乐设施标准》(GB 8408-2008)和《观览车类游艺机通用技术条件》(GB/T18164-2008)及《游乐设施安全技术监察规程（试行）》(国质检锅〔2003〕34号)等文件设计制造的。
设备简介[模版]
![设备简介[模版]](https://img.taocdn.com/s3/m/cf6fca220a4e767f5acfa1c7aa00b52acfc79c06.png)
设备简介[模版]第一篇：设备简介[模版]1、飓风飞椅简介飓风飞椅是乘人沿固定倾角立柱升降的同时而旋转的游乐设备，设备采用液压程序控制，游客乘坐于吊椅中，在设备运转时，时而飘然升空、时而伴随轻微的失重感下降，超重、失重、离心作用适度，由于设备外观配有多种动物装饰图案及多种颜色的彩灯并随设备旋转，人感到有悠闲自得的仙境之感，又刺激，游客乘坐时其乐无穷，深受游客，特别是青少年及儿童的喜爱。
刺激指数：4星2、神州飞碟简介神州飞碟（旋转飞碟）是我公司在原设备基础上，参照国内外同类设备加以改进，自主开发的一种新型的大型游乐项目。
该设备的最大特点是突破了原游乐设施单一运转方式，将旋转运动与滑行运动有机结合，设备运转时，乘客沿弯月型轨道来回往复滑行，同时自身也飞速旋转，使人感觉上下翻飞、眼花缭乱、非常刺激。
设备第二特点是座椅由传统座舱式改为骑跨式。
且设备外观装饰华丽，玩法独特，当设备运转时，轨道上彩色灯光变幻，使整个设备气势宏大，该设备是游客最喜爱的项目之一。
刺激指数：4星3、太空飞车简介CA型太空飞车是在专用轨道上滑行的新型游艺机。
它由三组摩擦轮以摩擦驱动形式的将飞车送上最高点，以一定的初速度向下自由滑行，轨道高低起伏，运动速度适宜。
不论男女老幼，安坐其中，有如太空历险，够刺激绝无恐慌之感。
车身配以造型新颖美观的玻璃钢外壳，深受游客欢迎。
刺激指数：3星半4、海盗船简介海盗船是一种绕水平轴摆动的游乐设备，游客乘坐时，船时而上升，时而下降，超重与失重交替体验，设备配有仿真的海盗造型，置身其中，犹如在波涛汹涌的大海中行舟，令人惊心动魄，回味无穷，深受游客特别是青少年朋友的喜爱。
刺激指数：4星半5、自控飞机简介自控飞机是根据战场上飞机交战情景设计的一种游乐设备，可安置于公园、渡假村等场所，游客可控制飞机升降，配有各种枪炮音乐，游客乘座时，如亲临战场一样。
设备造型美观、色彩鲜艳、操作简便，适应各年龄的游客乘坐，是各种游乐场所最吸引人的项目之一。
航天器卫星装配说明书
航天器卫星装配说明书一、引言在航天科技快速发展的背景下，航天器卫星的装配工作显得尤为重要。
为了确保卫星的正常运行，我们编制了本说明书，旨在提供详细的装配指导，确保装配过程的准确性和安全性。
二、装配前准备1. 确定装配场地：选择一个干燥、洁净、通风良好的场地进行装配，以防止灰尘和湿气对卫星零部件的损坏。
2. 准备装配工具：根据卫星装配所需，准备各种所需工具，并保证其完好无损。
3. 确认装配顺序：仔细研读卫星组装图纸和相关材料，确定装配的顺序和步骤，确保有序进行。
三、卫星组装与连接1. 安装卫星主体框架：根据组装图纸指导，将卫星主体框架中的各个部件按照顺序安装，注意紧固螺栓的扭矩要求，以确保安装牢固。
2. 连接航天器系统：根据设计要求，连接卫星各个系统，如能源系统、通信系统和导航系统等。
确保系统之间的连接紧密稳固，不影响各自的正常运行。
3. 电路板焊接与安装：根据电路板设计图纸和焊接工艺要求，对卫星电路板进行焊接和安装。
焊接时需注意温度控制和焊接质量，安装时需保持电路板与框架之间的良好接触。
四、卫星测试与调试1. 电气测试：使用专业设备对卫星的电气系统进行测试，包括电压、电流等参数的检测，以确保电路工作正常。
2. 功能测试：按照卫星功能要求，进行功能性测试，包括通信功能、控制功能等。
测试过程中记录测试数据，确保卫星功能正常。
3. 温度与压力测试：使用相应设备对卫星在不同温度和压力环境下的工作性能进行测试，以验证卫星的适应性和可靠性。
4. 开关与控制测试：对卫星的各类开关和控制装置进行测试，确保卫星在操作过程中的灵活性和可控性。
五、卫星装配的注意事项1. 安全操作：在装配过程中，必须穿戴好安全防护装备，如手套、护目镜等，保证人员的安全。
2. 严格质量控制：根据质量控制要求，对装配过程中的每一个环节进行严格控制，确保关键零部件的质量和装配的准确性。
3. 清洁环境：维持装配场地的清洁，定期清理装配过程中产生的杂物和灰尘，以保证卫星装配质量。
- 1、下载文档前请自行甄别文档内容的完整性，平台不提供额外的编辑、内容补充、找答案等附加服务。
- 2、"仅部分预览"的文档,不可在线预览部分如存在完整性等问题,可反馈申请退款(可完整预览的文档不适用该条件!)。
- 3、如文档侵犯您的权益，请联系客服反馈,我们会尽快为您处理(人工客服工作时间：9:00-18:30)。
`FD22神州飞碟(B级)设计说明书（版本：A）编制/日期：审核/日期：批准/日期：广州ABC游乐设备有限公司目录第1节概述 (1)第2节总体方案设计 (4)第3节导轨设计 (7)第4节转盘部分设计 (9)第5节底盘部分设计 (12)第6节动力系统设计 (15)第7节. 电气系统设计 (16)第8节.安全设施 (25)第9节.主要受力部位及加强措施 (28)第10节标准件和外购件的选用 (30)第11节乘客须知 (33)第1节概述“神州飞碟”是我公司参照国外同类设备并加以改进研发的一项大型游乐项目。
该设备的特点是外观华丽、玩法奇特。
可同时容纳22人乘坐的仿真飞碟，坐落在弯月型的导轨钢架上，乘客以骑跨式乘坐该设备。
设备整体配备彩色灯光装饰。
飞碟转动时配以灯光的变幻，使飞碟成为游乐园中一处光彩夺目的景观。
在设备运动模式上突破了传统设备单一的运动模式，飞碟沿着钢架导轨做高速上冲下荡的同时，飞碟转盘自身也正反交替旋转，使乘客感觉到无与伦比的兴奋与刺激。
“神州飞碟”主要由：导轨、底盘、转盘、站台、控制及传动系统等组成。
该设备的导轨轨道由钢板中频热弯而成，转盘骨架由100×50×4的矩形管组焊而成，承重轮及侧护轮均由轮毂外挂高强度聚氨酯制成。
座椅外形由玻璃钢制成，内糊铁件，用螺栓固定在转盘上。
座椅靠背压杠通过棘爪棘轮机构来实现压杠的开合。
1.1主要技术参数1.2工作条件和工作环境(1)使用环境温度：0～40℃；(2)使用环境相对湿度：不大于90％(在最高温度为40°C时，相对湿度不得超过50%)；(3)安装地区地震烈度：≤8度；(4)安装地区海拔高度：≤3000m；(5)当遇到：雷电、雨、雪、雾、结霜、主结构裹冰时停用；(6)当风速大于15m/s时停用。
1.3设计依据：本产品依据市场需求，参考国外同类产品，采用变频器控制+电机+减速机作为动力源，整机符合下列规范和标准：(1)《特种设备安全监察条例》`(2)《大型游乐设施设计文件鉴定规则（试行）》(3)《游乐设施安全技术监察规程（试行）》(4)GB8408-2208《游乐设施安全规范》(5)GB6988.7-1986《电气制图逻辑图》(6)GB16754-2208《机械安全急停设计原则》(7)GB5226《工业机械电气设备》(8)GB14048《低压开关设备和控制设备》(9)GB/T18159-2208《滑行车类游艺机通用技术条件》(10)GB50054-2211《低压配电设计规范》(11)GB50009-2212《建筑结构载荷规范》(12)GB50017-2203《钢结构设计规范》(13)GB50169-2206《电气装置安装工程接地装置施工及验收规范》第2节总体方案设计工作原理：本设备以电动机为动力源，飞碟沿导轨做左右摆动由电机经过两级减速后驱动摩擦轮带动飞碟底盘实现。
飞碟转盘做旋转运动通过旋转减速机驱动回转支撑带动转盘旋转来完成。
“神州飞碟”主要由：导轨、底盘、转盘、站台、控制及传动系统等组成。
见图1 。
图1 神州飞碟外观图主要部件设计使用寿命：注：（1）设备上的高强度螺栓副（包括8.8级以上螺母、垫圈）经过检查，出现失效情况应及时更换。
滚轮、轴承、轴套、密封圈等易磨损零件磨损后应及时更换。
（2）底盘及转盘上的关键件必须每年进行探伤检查，出现问题及时更换。
（3）神州飞碟上所有零部件必须严格按照《设备日检、月检、年检的内容和要求》做好日常检修、调整和维护保养，出现问题及时解决，保证设备最大的使用年限和安全运营。
2.1结构特点：该设备采用钢结构导轨，重量轻，刚性好。
转盘上座舱为圆周均布，转盘结构绕中心平面对称，正常运转时偏载荷较小，设备整体稳定性好。
底盘采用钢结构骨架，既减轻自重又具有较好的抗弯、抗扭的性能。
2.2总体方案的拟定神州飞碟的运行特点就是底盘沿导轨的左右摆动及转盘的旋转。
根据设计内容和需求确定设计方案：沿导轨做左右摆动由电机经过两级减速后驱动摩擦轮带动飞碟底盘实现。
转盘旋转通过旋转减速机驱动回转支撑带动转盘旋转来实现，座椅靠背压杠通过棘轮棘爪机构实现压杠的开合，总体电气执行采用PLC控制。
2.3主要技术参数说明2.3.1轨道高度及运行高度（1）该设计符合《关于调整大型游乐设施分级并做好大型游乐设施检验和型式试验工作的通知》中关于滑行车类B类产品的规定。
（2）考虑设备构件的强度及安全装置的设计制约，设备轨道高度7.6m，运行高度8m。
2.3.2最大摆动和旋转速度（1）考虑安全因素，神州飞碟沿导轨做左右摆动滑行的最大速度设定为11.3m/s。
（2）考虑人的承受能力，转盘旋转速度不宜过大，设定在7.4rpm以内，以免引起身体的不适。
（3）能够满足游乐设备的设计要求，满足乘客的娱乐要求。
2.3.3运行周期（1）考虑设备构件的强度及安全装置的设计制约，运行周期设定为180s。
（2）考虑人的承受能力，运行时间不能太长，以免引起身体不适。
（3）够满足游乐设备的设计要求，使乘客体验到娱乐的惊险与刺激，又留恋忘返。
第3节导轨设计3.1导轨钢结构（1）根据运行特点，设备沿导轨做左右摆动滑行，导轨轨道采用厚度10mm 的方板，中频热弯并焊接而成。
（2）导轨结构沿中心平面对称，整体稳定性好，抗风暴的能力强。
（3）根据刚度、强度要求，并结合经济上的考虑，参考国外同类产品的结构。
导轨支腿采用150×5的方管，导轨支腿与导轨轨道通过高强螺栓连接。
（4）考虑运输、安装方便，导轨分5节，节与节间用钢结构专用高强度螺栓连接，以增加设备的刚性。
（5）导轨各支腿之间通过拉筋连接，拉筋由方管和钢板焊接而成，增加结构稳定性。
（6）零部件进行有限元分析，选取较大的安全系数，确保设计安全可靠，万无一失。
图2 导轨及立柱第4节转盘部分设计4.1转盘的设计:（1）根据运行特点，转盘沿中心轴旋转，偏载较小。
（2）几何中心线与主体重心重合质量分布均匀，运行平稳。
（3）零部件进行有限元分析，选取较大的安全系数，确保设计安全可靠，万无一失。
图3 转盘4.2转盘框架的设计:（1）根据刚度、强度要求，转盘框架选用矩形管100×50×5。
（2）考虑运输、安装方便，转盘框架分3部分，各部分间用高强度螺栓连接。
图4 转盘框架4.3座椅及座椅骨架的设计:（1）座椅外壳玻璃钢材质，颜色鲜明，外形美观。
座椅骨架和框架通过螺栓连接，有效保证了乘客安全。
（2）座椅靠背压杠符合人机工程学原理，保证了乘客的安全性和舒适性。
（3）安全压杠附有软材料，让乘客坐着舒适又安全。
（4）座椅靠背压杠通过两套棘轮棘爪机构来实现压杠的开合。
操作省力，安全性好。
（5）座椅骨架结构采用40×3和30×3的方管，安全系数高，可靠性好。
图5 座椅及座椅骨架第5节底盘部分设计5.1底盘的设计:（1）根据运行特点，底盘沿导轨做左右滑动。
（2）底盘上设计有防翻轮及防翻保险架，能有效保证乘客安全。
（3）为保证回转部分稳定有效，回转支承选用012.40.900.001，与转盘通过螺栓连接。
（3）零部件进行有限元分析，选取较大的安全系数，确保设计安全可靠，万无一失。
图6 底盘5.2底盘骨架的设计:（1）根据刚度、强度要求，底盘骨架选用22#工字钢焊件而成。
（2）轮组连接处选用方管及筋板加强，保证连接安全可靠。
图7 底盘骨架5.3承重轮的设计:（1）承重轮轮子采用聚氨酯材料，运行稳定，耐磨性好。
（2）承重轮与底盘连接位置可回转，保证在运行过程中，承重轮始终贴合导轨。
图8 承重轮第6节动力系统设计6.1机械传动总体设计飞碟沿导轨左右摆动：摆动电动机驱动→链轮减速→摩擦轮→飞碟左右摆动飞碟转盘旋转：旋转电机→减速机→回转支撑→转盘正反转动6.2动力系统元器件设计根据设备运行需求，左右摆动主电机采用37kW，4级交流异步电动机。
旋转电机采用5.5kW，4级交流异步电动机。
第7节.电气系统设计7.1 简述该设备在电路及控制设计上采用目前较为流行的交流变频调速度传动技术。
左右摆动主电机采用37kW，4级交流异步电动机传动，变频驱动器采用DS7-G045/P055-T4变频器，其主要特点具有较好的人机界面、参数保护、故障自诊断、电源缺相及低电压、过电流、电机过载、等多重保护，可在控制端子输入信号的控制下方便可靠地完成电机的正反转、停止、改变加减速时间及电机旋转速度等功能。
旋转电机采用 5.5kW，4级交流异步电动机传动，变频器采用D900-7R5G/011P-T4 7.5kW，变频器控制电机的平滑启动、变向控制带动转盘无冲击正反交替旋转及慢速定位停止。
系统控制器采用信捷XC系列PLC 可编程控制器：型号XC3-32R-E。
其抗干扰能力强，工作稳定。
由PLC根据摆动电机正反转及转盘正反转的需要，给变频器控制端子发出运行指令，并采集变频器输出信号，达到稳定控制目的。
由于左右摆动的高度及时间不同，主电机的工作状态特别，同过PLC接收到的摆动电机正反转状态信号有程序控制达到电机低速启动，高速摆动的不同速度变化需要。
同时系统设计了正反转检测互锁装置，使电机在变向时减少冲击，有效地保护了电机及传动机构。
在安全上设置了站台、安全压背检测与车体的联锁保护，只有在站台踏板处于收回状态下，安全门关闭，同时安全压背压到一定位置后，才能启动设备。
为了防止车体摆动过高冲顶，设计了左右摆动极限位置行程开关，提高了安全性。
此外，安全上还设置了急停按钮，使操作人员在设备故障情况下及时切断设备电源，保证安全。
另外系统还设置了支架彩灯及转盘彩灯装置，增加了设备的美观及娱乐性。
车体电源由四根安装在圆弧导轨上的安全滑触线提供，转盘电机电源及转盘彩灯电源由装在转盘上的集电滑环提供。
本机采用自动工作方式，由PLC 控制，时间约3分钟。
运行时间长短可由操作人员按实际情况调整。
7.2 电路主要设计参数、计算、选型电源输入电压：三相380V （三相五线制）电源输入电流：160A设备的动力功率参数如下：车体摆动电机：37kW AC 3～380V 1台转盘旋转电机：5.5kW AC 3～380V 1台彩灯、控制回路和插座等用电：1.5kW设备总功率： N P =37+5.5+1.5=44kW由功率公式: N N N N N I U P ηλ3=其中为功率因数，取值0.85; 为效率，取值0.90;设备总电源的额定工作电流：I N =N P ÷(√3U N λN ηN )=44÷(√3×0.38×0.85×0.90)≈87A依据GB5226.1-2208文件说明， 过负荷保护电器的动作特性，应符合下列公式的要求： I b ≤I n ≤I zN λN ηI2≤1.45I z式中：I b——回路计算电流（A）；I n——熔断器熔体额定电流或断路器额定电流或整定电流（A）；I z——导体允许持续载流量（A）；I2——保证保护电器可靠动作的电流（A）。