PSEUWord下载.docx
- 文档编号:18181433
- 上传时间:2022-12-14
- 格式:DOCX
- 页数:13
- 大小:425.32KB
PSEUWord下载.docx
《PSEUWord下载.docx》由会员分享,可在线阅读,更多相关《PSEUWord下载.docx(13页珍藏版)》请在冰豆网上搜索。
PSEU是航线可更换组件,包括两个内部电路和一个前部自测试面板,面板下方的红灯指示空地系统的空中模式。
其有以下7个电子接口:
系统1的J1-J4;
系统2的J5-J7。
其在空地系统中的主要功能有:
1.监控起落架压力传感器2.操作空地继电器3.传送空地离散信号除此之外还有以下功能:
1.起落架位置指示与警告2.起落架传输活门控制3.起落架未放下警告4.减速伸出琥珀色灯控制5.起飞音频警告6.门警告
PESU错误灯逻辑:
内部错误形式:
1.软件/硬件错误
2.内部系统的通信
3.供电A/B错误
4.Sensordrive1/2
外部错误:
1.渐进传感器线路
2.LEflapsexternalwiringfaults
3.Externalinputconfigurationfaults
4.Externalinputmonitoringfaults.
AgroundisprovidedforthePSEUwhentheautothrottleswitchpacksarelessthan53degrees.
IfthePSEUsensesanon-dispatchablefault,theamberPSEUlightontheP5panelcomeson30secondsafterlandingwhenboththrustleversarelessthan53degrees.AsignalisalsosenttothemastercautioncardintheFlightRecorderandMachAirspeedWarningmoduleforaPSEUfault.
ThePSEUfaultlightgoesoffwhenthefaultiscorrected
当飞机落地30秒后且所有油门杆角度小于53度时,PSEU琥珀色灯亮为一个不可放行的错误。
同时有个信号传至飞行记录器和马赫配平模块指示一个PSEU错误。
IfthePSEUsensesadispatchablefault,theamberPSEUlightontheP5panelcomeson30secondsafterlanding,whenthrustleversarelessthan53degrees.ThePSEUfaultlightgoesoffwhentheenginesareshutdownortheparkingbrakeisset,eventhoughthedispatchablefaultmaystillbepresent.PSEUBITEdisplaymustbecheckedfortheexistingfault.
Inputsfromthesystem1sensorsgotosystem1intheproximityswitchelectronicsunit(PSEU),andinputsfromsystem2sensorsgotosystem2inthePSEU.BothsystemswithinthePSEUshareinformationthroughacommonbus.
Twolandinggearcompressedsensorsoneachlandinggearsendair/groundpositiontothePSEU.ThePSEUprocessesthesignalsfromthecompressedsensors,operatestheair/groundrelays,andsendstheseoutputstoairplanesystems:
▪Groundmode
▪Airmode
▪Leftgearongroundmode(system1only)
▪Rightgearongroundmode(system2only)
▪Nosegearongroundmode
▪Parkingbrakesetonground(system1only).
System1onlysendsparkingbrakeset,andongroundsignalstothevoicerecorder.Thisletsyouerasethevoicerecorderwhentheparkingbrakeissetandtheairplaneisontheground.
Youcanchangetheoutputofeachair/groundsystemwiththeAIR/GNDOVRDfunctiononthePSEUBITE.Theair/groundsysteminairredlightsandPSEUamberlightcomeonwhenthesystemisintheairmode.
TheBITEdoesnotoperatewhentheforwardaccessdoorisclosed.
ThePSEUsensestheairplaneisinoperationasopposedtomaintenancewhenalltheeightentry,access,serviceandcargodoorsareclosedoreitherengineisrunning.
ThePSEUamberlightontheP5aftoverheadpanelcomesonwhenano-dispatchtypeoffaultisstoredinthememoryofthePSEU.Thelightcomesonwhentheseoccur:
▪Airplaneontheground
▪Boththrustleverslessthan53degrees
▪Morethan30secondsafterlanding.
ThePSEUlightalsocomesonwhenyoupusheitherMASTERCAUTIONlightifadispatchablefaultisstoredinthememoryofthePSEU.ThePSEUthengoesoffwhenyoupushtheMASTERCAUTIONlight.ThePSEUlightalsocomesonifadispatchablefaultisstoredinthememoryofthePSEU.ThePSEUlightwillautomaticallygooffwheneithertheparkingbrakeissetorbothenginesareturnedoff.
ThesearetheitemsinthemainmenuofthePSEUBITE:
▪EXISTINGFAULTS
▪FAULTHISTORY
▪GROUNDTESTS
▪AIR/GNDOVRD
▪OTHERFUNCTIONS.
non-volatilememory(NVM)非易失存储器
TheGROUNDTESTSselectionletsyoudothesetests:
▪LRUreplacementtest
▪PSEUselftest
▪Landinggeartransfervalvetest
▪SPEEDBRAKESEXTENDEDlightoperationtest
▪Takeoffwarningtest
▪PSEUBITEdisplaytest.
TheOTHERFUNCTIONSselectionletsyoudothesefunctions:
▪Takeoffwarningreport
▪Landinggeartransfervalvereport
▪Seesensorinformation
▪MonitorPSEUinputsandoutputs
▪SeePSEUconfiguration
Ifthereisoneormoreexistingfault,thefirstmessageshowsthedispatchstatusoftheairplane
EachPSEUfaultmessagehasasinglemaintenanceaction.ThefaultmessagehasaBITEmessagenumber.ThisistheformatfortheBITEmessagenumbers:
▪Eightcharactersinlength
▪ThefirsttwocharactersaretheATAchapternumberofthesystem
▪Thethirdcharacterisahyphen(-)
▪ThefourthcharacteristhefirstnumberoftheATAsectionnumberofthefaultedsub-system.
Thelastfourdigitsshowthefault:
▪0XXX-powerfaults
▪1XXX-sensorfaults
▪2XXX-discreteinputfaults
▪3XXX-reportfaults
▪4XXX-others
▪5XXX-inputsthathavenocycles(TOWandSPDBRKtests)
▪6XXX-fieldprogrammablegatearray(FPGA)outputloadfaults.
FaultHistory
Thefaulthistoryselectionshowsfaultinformationthatisinthenon-volatilememory(NVM)inthePSEU.MonitorsinthePSEUputdataintheNVMduringtheseconditions:
▪SystemtestswiththePSEUBITE
▪Continuousmonitoring
▪Poweruptests.
TheNVMkeepsdataforthelast64flightlegsoramaximumof256failures.Flightleg0isthecurrentflightleg.Flightleg63isthelastleg.Faultsinflightleg0arefaultsthatoccurredduringthemostrecentflightandthefaultsthatoccurredonthegroundafterthemostrecentflight.TheflightlegstartswhentheairplanegoesfromthegroundtotheairandtheN2enginespeedsignalshowsenginenumberoneoperates.
Tofindfaultinformationfromaspecificflightleg,dothesesteps:
▪Gotothemainmenu
▪UsetheupordownarrowswitchesuntilyouseeFAULTHISTORY?
intheBITEdisplay
▪PushtheYESswitch
▪Usetheupordownarrowswitchesuntilyouseetheflightlegthatyouwant
▪PushtheYESswitch.
TheinformationforMOREDETAILSshowsthephasewhenthefaultoccurred(airorground),andthetypeofthefault.
ThefaulttypesareHARD,INTRMTNT,orREPEATnn:
▪HARDfaultsarefaultsnotclearedpriortotheendoflastflightleg
▪INTRMTNTfaultsarefaultsclearedpriortotheendofthelastflightleg
▪REPEATnnfaultsareintermittentfaultsthatoccurrednntimesduringthelastflightleg.
ThesearethegroundtestsinthePSEUBITE:
▪REPLACETEST
▪SELFTEST
▪LGTVTEST
▪SBRKTEST
▪T/OWARNTEST
▪DISPLAYTEST.
Duringthetest,thedisplayshowsTESTINPROGRESS.Ifthetestpasses,thedisplayshowsTESTPASSED.Ifthetestfails,thedisplayshowsafaultmessage.TheinformationforMOREDETAILS?
isthesameasfortheexistingfaultstest.
DuringtheREPLACETESTandSELFTEST,someoutputsfromthePSEUchange.Airplanesystemsmayoperateautomaticallybecausetheair/groundsystemssendairmodesignalsduringthetests.ObeythesewarningswhenyoudotheREPLACETESTandSELFTEST:
WARNING:
OBEYTHEPROCEDURETHATPREPARESTOPUTTHEAIRPLANEINTHEAIRMODE.INTHEAIRMODE,MANYOFTHEAIRPLANESYSTEMSCANOPERATE.THISCANCAUSEINJURIESTOPERSONSANDDAMAGETOEQUIPMENTCANOCCUR.
KEEPPERSONSANDEQUIPMENTCLEAROFTHEFLIGHTCONTROLSURFACES.THESECOMPONENTSCANMOVESUDDENLYWHENYOUPUTTHEAIRPLANEINTHEAIRMODE.THISCANCAUSEINJURIESTOPERSONSANDDAMAGETOEQUIPMENT.
更换测试REPLACETEST
更换测试进行PSEU的内部自测以及PSEU的相关接口测试,测试过程中需按手册对飞机系统或部件进行操作
更换测试中出现的故障代码及信息在当前故障页面中显示
•自测试SELFTEST
自测试对PSEU本身进行检测,自测试中出现的故障代码及信息同样显示在当前故障页面中
•起落架转换活门测试LGTVTEST
起落架转换活门测试是对起落架转换活门的操作测试,该测试使用主用和备用通道对活门进行操作
若活门作动正常则无故障信息显示,测试通过,否则故障信息显示在当前故障页面中
•速度刹车测试SPDBRKTEST
速度刹车测试显示当前状态下控制琥珀色SPEEDBRAKESEXTENDED指示灯的各个输入变量
若各输入变量正常则测试通过且无故障信息显示,否则显示INTERNALFAULTS
•起飞警告测试T/OWARNTEST
起飞警告测试显示当前状态下起飞警告系统的各个输入变量
•显示测试DISPLAYTEST
显示测试对BITE界面上的各个显示单元进行逐一测试,测试完毕后显示DISPLAYTEST?
TheT/OWARNREPORTfunctionletsyouseewhichconditionscausedthemostrecenttakeoffwarning.
目前737NG飞机可以使用的PSEU主要有两种件号:
285A1600-5和285A1600-4.由于两种件号PSEU灯亮的逻辑不一样,这里分别说明。
(注意:
被锁定的历史故障也会点亮PSEU灯,类似于当前故障)
1)件号为285A1600-4:
a)当系统检测到有可以放行的故障时,在飞机着陆后30S,双发油门小于53度并且按压主警告牌。
那么PSEU灯点亮;
再按压主警告灯可以复位。
即:
如故障没有排除,飞机再次推出时机组会反映有可以复位的PSEU故障。
b)当系统检测到有不可以放行的故障时,在飞机着陆后30S,双发油门小于53度,那么PSEU灯点亮,再按压主警告灯不可以复位
2)件号为285A1600-5:
a)当系统检测到有可以放行的故障时,在飞机着陆后30S,双发油门小于53度那么PSEU灯直接点亮;
双发关车并且停留刹车刹上,PSEU灯熄灭。
如故障没有排除,飞机直到下个起降的着陆后才有可能会再点亮故障灯。
b)当系统检测到有不可以放行的故障时,在飞机着陆后30S,双发油门小于53度那么PSEU灯直接点亮;
双发关车并且停留刹车刹上也不能够使PSEU灯熄灭。
3.PSEU灯亮的保留措施(分三种情况):
1)PSEU灯亮,按压主警告牌能够复位即能熄灭PSEU灯。
那么直接按照C类保留就可以了。
2)PSEU灯亮,按压主警告牌不能够复位即不能熄灭PSEU灯,要求在PSEU灯处贴失效标牌
3)PSEU灯指示失效,包括不能点亮PSEU灯
对于2)和3)要求查看PSEU的具体当前故障信息,来确定是否能够做保留。
为了做当前故障检查,到前电子设备舱接近PESU自检面板。
按压ON/YES按钮,屏幕将显示EXISTINGFAULTS?
再按压YES按钮。
此时屏幕显示当前的故障信息,只要逐项记录信息代码就可以了;
如没有故障信息,屏幕会显示NOFAULTS。
而查找的结果一般有这么几种:
a)无任何故障信息NOFAULTS此时可按MEL32-17保留
b)出现状态信息32-64003DISPATCHFAULT此时可按MEL32-17保留;
若故障信息出现32-62009/32-62010/32-62014中的任意一条,那么按照MEL32-21保留
c)出现状态信息32-64004NODISPFAULT此时不可以保留;
若故障信息同
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- PSEU