飞机结构英语课件ppt.ppt

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1、飞机结构英语飞机结构英语Compartments Location 2Compartments Location 3Qfurnishing 客客舱设备 Qcockpit 驾驶舱Qstair bay客梯客梯舱Qwing center box中央翼盒中央翼盒 Qcabin客客舱Qaccessory compartment 附件附件舱Qcargo compartment 货舱Qbulk cargo compartment 散装散装货舱45QA.cabin attendant seat 乘乘务员座椅座椅QB.curtain 隔帘隔帘QC.galley/buffet 厨房厨房/餐具柜餐具柜QD.lava

2、tory 厕所所QE.stowage 储藏藏间QF.passenger compartment seat 客客舱座椅座椅QG.floor covering(carpet)地板覆地板覆层（地毯）（地毯）6QH.overhead stowage compartment行李架行李架QJ.lining 衬层、装、装饰板板QK.emergency exit 应急出口急出口QL.passenger service unit 旅客服旅客服务组件件78大家有疑问的，可以询问和交流大家有疑问的，可以询问和交流可以互相讨论下，但要小声点可以互相讨论下，但要小声点可以互相讨论下，但要小声点可以互相讨论下，但要小声点

3、9Qceiling panel 天花板天花板Qcove light panel 拱形灯光盖板拱形灯光盖板Qsidewall panel 侧壁板壁板Qthermal 热量的量的Qacoustic 声音的声音的Qinsulation 隔离隔离层Qinsulation blanket 隔离隔离层101112Qdecorative panel 装装饰板板Qfastener 紧固件固件Qattachment fitting 接接头Qquick release pin 快卸快卸钉1314Qarmrest 扶手扶手Qseat belt 座椅安全座椅安全带Qseat cushion 坐坐垫Qbackrest靠

4、背靠背Qfood tray 餐桌板餐桌板Qlife vest 救生衣救生衣Qpouch 储存袋存袋Qbaggage bar 行李行李围栏Qframework 框架框架Qrecline后靠后靠1516Qcaptain 机机长Qfirst officer 副副驾驶Qoccupant 乘乘员Qoxygen mask 氧气面罩氧气面罩171819Qpartition wall 隔板隔板Qstanchion支柱支柱Qtie down point 系留点系留点20212223Qemergency equipment应急急设备Qescape rope撤离撤离绳Qdescent device emergenc

5、y应急下落装置急下落装置Qsingle/dual lane slide单/双通道滑梯双通道滑梯Qraft救生船救生船24QThe emergency equipment is installed in the aircraft for the safety of the passengers and the crew.Q安装在安装在飞机上的机上的应急急设备为旅客和机旅客和机组乘乘员提提供安全保供安全保护。25QThe cockpit is equipped with adjustable seats for two crew members,a third occupant seat and

6、a folding seat for a fourth occupant.Q驾驶舱安装有两个可安装有两个可调节的机的机组座椅，一个座椅，一个第三乘第三乘员座椅和一个可折叠的第四乘座椅和一个可折叠的第四乘员座椅。座椅。26QFasteners attach the upper part of the decorative panels to the attachment fittings mounted on the aircraft structure.Q紧固件将装固件将装饰板的上部板的上部连接到安装在接到安装在飞机机结构构上的接上的接头上。上。27QAdjust the hinge to g

7、et the dimension C clearance between the lavatory door and the door frame.Q调节铰链以达到以达到厕所所门和和门框之框之间的的间隙尺寸隙尺寸C。28QDO NOT TOUCH THE UNIT UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).Q不要接触部件直到其完全冷却以防不要接触部件直到其完全冷却以防执行行维护任任务时烫伤。29QThe Bulk cargo compartment has tie dow

8、n/attachment points for the door nets and for the nets and straps which keep the bulk cargo in place.Q散装散装货舱安装有安装有连接接门网和散网和散货固定网及束固定网及束带的系留点。的系留点。30QEscape slide inflation is automatic if the door is opened with the Emergency Control Handle(ECH)in the ARMED mode.Q如果如果应急控制手柄（急控制手柄（ECH）在）在ARMED(待命待命)模

9、模式式时舱门打开，撤离滑梯自打开，撤离滑梯自动充气。充气。31QThe thermal insulation is distributed through the pressurized fuselage,and is of different thickness,and installed in different ways.Q隔隔热层分布于整个承分布于整个承压机身，厚度不同，并以机身，厚度不同，并以不同的方式安装。不同的方式安装。32QThe seat pan is spring loaded to return the seat to the retracted position whe

10、n it is not in use.Q当不使用当不使用时座板在座板在弹簧力的作用下回到收起位簧力的作用下回到收起位置。置。33QOpen the doors on coatroom and remove all the equipments to lighten the unit weight and to provide access to the seat track attachments.Q打开衣帽打开衣帽间门，移走所有，移走所有设备以减以减轻部件重量部件重量并得以接近座椅并得以接近座椅导轨连接件。接件。34Aircraft Structure飞机机结构构3536Qstation(S

11、TA)站位站位Qframe(FR)隔框隔框3738Qfuselage机身机身Qradome雷达罩雷达罩Qpressure bulkhead承承压隔框隔框Qnose机机头Qpowerplant动力装置力装置Qpylon发动机吊架机吊架Qwing机翼机翼Qvertical stabilizer垂直安定面垂直安定面Qhorizontal stabilizer水平安定面水平安定面Qtail cone尾尾锥3940Qwindshield风挡Qfixed window固定窗固定窗Qsliding window活活动窗窗Qclearview window活活动窗、窗、观察窗察窗4142Qbelly fair

12、ing机腹整流罩机腹整流罩Qlanding gear bay起落架起落架舱Qpassenger/crew door旅客旅客/机机组门、登机、登机门Qfloor structure地板地板结构构434445Qslat缝翼翼Qflap襟翼襟翼Qtab调整片整片Qspoiler扰流板流板Qaileron副翼副翼Qwingtip翼尖翼尖Qfence翼刀翼刀Qrib肋板肋板Qspar翼梁翼梁Qoverwing翼上的翼上的464748Qrudder方向舵方向舵Qelevator升降舵升降舵Qapron裙板、裙板、围板板Qleading edge前前缘Qtrailing edge后后缘Qspar box梁盒

13、梁盒Qattach fitting接接头4950Qnose cowl进气道、前气道、前环Qlnlet cowl进气道、前气道、前环Qfan cowl风扇罩扇罩Qthrust reverser反推反推Qcommon nozzle尾尾喷管管Qexhaust cone排气排气锥Qduct函道函道5152Qprimary structure主要主要结构构Qsecondary structure次要次要结构构Qconfig构型构型Qdorsal fin背背鳍Qlanding gear door起落架起落架舱门Qcargo door货舱门535455Qtitanium plate钛板板Qsandwich

14、panel夹芯板芯板Qbird impact鸟击Qflight deck驾驶舱Qskin蒙皮蒙皮Qsupport支撑支撑56575859Qlongitudinal joint纵向接向接缝Qcircumferential joint环向接向接缝Qstringer/longeron 长桁桁Qcross beam横梁横梁Qvertical strut立柱立柱Qseat rail/track座椅座椅导轨Qsplice搭接搭接带Qkeel beam龙骨梁骨梁Qcrack stopper止裂板止裂板Qassembly组件件60QThe material,the function and the locat

15、ion of a component have an effect upon the type of protective treatment applied to a component.Q部件的材料、功能和位置决定了用于部件的材料、功能和位置决定了用于该部件上部件上的防的防护处理理类型。型。61QSkin stiffeners make the fuselage skin stronger and are riveted to the skin in areas of high stress(door openings,emergency exits,cabin windows,etc.)

16、.Q蒙皮加蒙皮加强件使机身蒙皮得到加件使机身蒙皮得到加强并且并且铆接在高接在高应力区域（力区域（舱门开口、开口、应急出口、客急出口、客舱窗等）窗等）的蒙皮上。的蒙皮上。62QThe fuselage is a semimonocoque structure,light alloy circular frames and longitudinal stringers support and strengthen the main fuselage skin.Q机身机身为半硬壳半硬壳结构，构，轻质合金的合金的环形隔框和形隔框和纵向向长桁支撑并加桁支撑并加强了主要机身蒙皮。了主要机身蒙皮。63Str

17、ucture Damage结构构损伤64Qscratch划痕划痕Qgouge凿痕痕Qcrack裂裂纹Qdent凹坑凹坑Qdistortion变形形Qcorrosion腐腐蚀Qcorrosion preventive compound防腐防腐剂65Qabrasion磨磨损Qerosion侵侵蚀、风蚀Qcrease折痕折痕Qdebonding脱胶脱胶Qdelamination分分层66QDamage which exceeds the Allowable Damage limits can be repaired by cutting out the damaged area of a struc

18、tural component and inserting or attaching a reinforcing piece.Q超超过可允可允许损伤限制的限制的损伤可以通可以通过切除切除结构构件的件的损伤区域并嵌入或安装一个加区域并嵌入或安装一个加强件来件来进行行修理。修理。67QAll corrosion which you find must be immediately and fully removed,because corrosion which remains will cause new corrosion and further decrease the strength o

19、f the structure.Q被被发现的腐的腐蚀必需立即完全去除，必需立即完全去除，应为余留的余留的腐腐蚀会造成新的腐会造成新的腐蚀并并进一步减弱一步减弱结构构强度。度。68QAfter the corrosion is fully removed the extent of the damage must be examined and compared with the allowable damage limits.Q腐腐蚀完全去除后，必需完全去除后，必需检查损伤程度并与可允程度并与可允许损伤限制限制对比。比。69Structure Repair结构修理构修理7071Qdoubler

20、加加强板板Qpatch补片片Qcutout切口切口Qcutout/cutting line切割切割线Qfastener spacing/pitch紧固件固件间距距Qedge distance/margin(紧固件固件)边距距7273Qfinger doubler指形板指形板Qfiller填片填片Qshim填隙片填隙片Qsplice strap搭接搭接带Qchamfer倒角倒角7475Qflange缘边Qweb腹板腹板Qrepair angle修理角材修理角材7677Qsealant密封密封剂Qinterfay结合面合面Qfillet seal填角密封填角密封Qovercoat保保护层7879Q

21、bend弯曲弯曲Qbend angle弯曲角弯曲角Qbend radius弯曲半径弯曲半径Qsection angle部件角部件角Qsheet thickness板厚板厚8081Qjoggle下陷、折接下陷、折接8283Qpneumatic气气动的的Qsander打磨器打磨器Qstep sanding台台阶打磨打磨Qscarf sanding斜面打磨斜面打磨Qblend out打磨去除打磨去除8485Qdress out(凹坑凹坑)整形整形Qcold form冷成形冷成形Qstop hole止裂孔止裂孔Qheattreatment热处理理86QHeat treatment shall be c

22、arried out uniformly over the whole material and never on a part of the material only.Q应均匀地均匀地对整体材料整体材料进行行热处理，而不可以理，而不可以仅针对材料的一部分。材料的一部分。87QYou can form light-alloy sheet in either its as received condition or heattreated condition.Q可以在收可以在收货状状态或或热处理状理状态下下对轻质合金薄合金薄板板进行成形操作。行成形操作。88QSealing the exter

23、nal joints of the aircraft structure to make sure that water does not go into the structure and to make the structure aerodynamic.Q密封密封飞机机结构的外部接构的外部接缝以确保水分不以确保水分不进入入结构并构并获得得结构的气构的气动性。性。89Structure Material结构材料构材料90Qaluminium alloy铝合金合金Qtitanium alloy钛合金合金Qmonel蒙乃蒙乃尔（铜镍合金）合金）Qcorrosion resistant stee

24、l(CRES)不不锈钢Qcopper铜Qclad金属包金属包层Qunclad/bare非金属包非金属包层QAL Clad Sheet包包铝板板91Qextrusion挤压型材型材Qformed section板弯型材板弯型材Qbar棒料棒料Qtube管料管料Qsheet薄板薄板 (0.25 inch)Qplate 板材板材(0.25 inch)Qforging锻件件92Hat Sectionextrusionformed section93Qcomposite material复合材料复合材料Qglassfiber玻璃玻璃纤维Qcarbonfiber碳碳纤维Qaramidfiber芳芳纶纤维Q

25、honeycomb core蜂蜂窝夹芯芯Qresin树脂脂Qteflon特氟隆特氟隆Qsilicone硅硅树脂脂Qadhesive粘接粘接剂Qadhesive film胶膜胶膜94Qtopcoat面漆面漆Qprimer底漆底漆Qcoating涂涂层、漆、漆层95QCarbonfiber parts may include small quantities of Glassfiber or Aramidfiber used as dielectric coating or galvanic corrosion protection.Q碳碳纤维部件可能会包含少量的玻璃部件可能会包含少量的玻璃纤维或

26、芳或芳纶纤维用作用作绝缘层或或电偶腐偶腐蚀保保护。96QThe floor panels are made of a honeycomb core which is bonded between Glass-fiber Reinforced Plastic(GFRP)sheets.Q地板是由蜂地板是由蜂窝夹芯粘接于玻璃芯粘接于玻璃纤维增增强塑料塑料（GFRP)薄板之薄板之间制成的。制成的。97Fastener紧固件固件98Qrivet铆钉Qsolid rivet实芯芯铆钉Qblind rivet拉拉铆钉Qpin销钉QHi-Lok高高锁钉、海螺、海螺钉Qscrew螺螺钉Qbolt螺栓螺栓Qnut

27、螺帽螺帽Qwasher垫片片99Qlockbolt锁螺栓螺栓Qself-locking自自锁Qnutplate托板螺帽托板螺帽Qclipnut夹板螺帽板螺帽Qcollar螺帽螺帽Qprotruding head凸凸头Qcountersunk head埋埋头Qtension head拉伸拉伸头Qshear head剪切剪切头Qgrip length夹紧长度度100Collar101Solid RivetProtrudingHeadCountersunkHead102Blind RivetProtrudingHeadCountersunkHead103Hi-Lok PinProtrudingHea

28、dCountersunkHead104Lockbolt105Clipnut106Nutplate107Grip Length108QWhen a fastener hole is damaged and outside the tolerances for the original fastener nominal diameter,an oversize fastener must be installed.Q当一个当一个紧固件孔固件孔损伤并且超出原有并且超出原有紧固件固件标称称直径的公差范直径的公差范围时，必需安装一个加大尺寸的，必需安装一个加大尺寸的紧固件。固件。109QWhen an

29、aluminum rivet is upset against a softer material,a washer must be used under the upset head to prevent eruption of the softer material.Q当一个当一个铝铆钉的的镦头形成在形成在较软的材料一的材料一边时，必需在必需在铆钉镦头下使用下使用垫片以防止片以防止较软材料材料胀裂。裂。110QHi-Lok pins installed in aluminum structure shall be installed into interference-fit holes

30、unless otherwise specified on the engineering drawing.Q安装在安装在铝质结构中的高构中的高锁钉应安装在干涉配合安装在干涉配合的孔中，除非工程的孔中，除非工程图纸上有其它上有其它说明。明。111Repair Example修理修理举例例112Q1.Cut out the damaged area of skin and deburr the edges，the minimum radius of skin cutout is 0.5 inch.Q切除蒙皮上的切除蒙皮上的损伤区域并清除区域并清除边缘毛刺，蒙毛刺，蒙皮切口最小半径皮切口最小半径0

31、.5英寸。英寸。113Q2.Performing high frequency eddy current inspection of area around skin cutout and make sure that no crack existing.Q对蒙皮切口周蒙皮切口周边区域做高区域做高频涡流探流探伤检查并并 确定无裂确定无裂纹存在。存在。114Q3.Fabricate a external doubler and a filler from 0.063 inch thick 2024-T3 AL clad sheet and break sharp edges.Q用用0.063英寸

32、厚的英寸厚的2024-T3包包铝板制作一外加板制作一外加强板和一填片并打磨尖板和一填片并打磨尖边。115Q4.Aero chamfer all edges of the external doubler to 0.03 inch thickness using a 10:1 taper.Q按按10:1的斜度的斜度对外加外加强板的所有板的所有边缘做气做气动倒角至倒角至0.03英寸厚。英寸厚。116Q5.Protect reworked area against corrosion and dissimilar metal per SRM chapter 51.Q 按按SRM51章章对修理区域做防腐修理区域做防腐处理和不同金理和不同金 属属间的防的防护。117