1.2 座舱系统
-welcome to your second lesson trainee
欢迎来到第二节训练课
-today we'll familiarize you with the cockpit of the ka-50
今天我们将熟悉K50的座舱
-the cockpit consists of several instrument panels that house gauges and
indicators that display information on current flight parameters.aircraft
systems.status engine states,flight controls and system warming indicators.
驾驶舱由多个仪表板,压力表,飞行信息指示系统,飞行系统,引擎状态,飞行控制及警告
指示系统.
-the primary flight controls are the cyclic control stick,the collective
control stick and the rudder pedals.
主飞行控制系统有周期变距杆,杆距和飞行脚舵共同组成.
-the collective control stick controls the collective pitch of all of the
rotor blades simultaneously and equally,thereby increasing of decreasing the
amount of lift generated by the rotor disk.the cyclic control stick controls
the swash plate,this creates propulsion and determines the direction of the
helicopter's movement.the actual pitch of any single rotor blade at any
given moment is the summation of the collective and cyclic pitch.the rudder
pedals are used to control the helicopter's direction in horizontal axis
(yaw)
总杆量控制总体螺旋桨的俯仰角度,用以控制升降机产生增加或下降的力.周期变距杆用
于控制飞机的移动.二者共同完成飞行中控制.脚舵用于控制水平转向(偏航)的控制.
-the primary flight instruments are located on the forward panel,beneath the
antiglare shiled.
主飞行仪器被固定在前面板上,并附有保护物.
-the attitude director indicator(ADI),also referred to as the "artificial
horizon" indicates the helicopter's orientation relative to the horizon.it
also shows deviation form the assigned flight path in horizontal and
vertical axis.
姿态方位仪,也被称为人工地平线表明直升机相对于地平线的方向.也被用于表明垂直水
平方向上的相对于地平线的偏差.
-the horizontal situation indicator(HSI) indicates the helicopter's heading
navigation data,and the helicopter's position in horizontal space relative
to the assigned couse line or navigation points.these can include
waypoints,target points,or airfields.the HSI is helpful when navigating a
route or retuning to base.
水平方位仪(HSI),用于反应飞行的水平状态,用于反应和预设导航点的关系.包含路径点
,目标点机场等.HSI在预设导航和返航基础都是非常有帮助的.
-the rotor blade pitch indicator is used to monitor the pitch angle of the
rotor blades.
螺旋桨叶指示用于指示螺旋桨叶仰俯的程度,
-the barometric altimeter indicates the aircraft's current altitude above
sea level(ASL).the altimeter dial has two hands
ne full rotation of the
long hand represents 1000 meters and one full rotation of the shorter hand
represents 10000 meters.
气压高度表指示海拨高度(ASL),两个指针,长的用于指示1000米,短的用于指示10,000米
.
-the vertical velocity indicator (VVI) measures the aircraft's rate of climb
or descent and is also used to help maintain level flight.
垂直速率指示(VVI)用于指示飞行中的瞬间的上升或下降率.
-the rotor RPM indicator displays the tachometer measurement of the rotor's
revolutions per minute(RPM) as a percentagt of its maximum value.
螺旋桨转速批示用于指示螺旋桨每分钟最大的转速.
-the air speed indicator displays the aircraft's indicated airspeed
空速表用来指示空速.
-the accelerometer(or "G-meter") indicates the current maneuver loading on
the helicopter,represented by the white needle.the red needles indicate the
highest and lowest G attained during a sortie.
加速度计(或称为G指示),白色指针,红色指针用于指示机动时所达最高和最低G值.
-the radar altimeter displays the helicopter's altitude above ground level
(AGL) to a maxinum altitude of 300 meters altitude is measured with a
small,downwardfacing FM radar.
雷达高度计指示直升机的距地高度(AGL),最小高度为300米.使用一个向下的FM雷达.
-the mechanical clock displays the current time of day in hours,minutes,and
seconds.it can also be used to measure misson time in hours and minutes,and
as stop watch to measure short time penods(up to an hour) in minutes and
seconds.
飞行时针用于显示小时,分钟及秒.除此也可用于显示任务的时间.亦可短时用于精确计
时(一小时内)
-the EKRAN-32-03 built-in test(BIT) display is part of the integrated
cockpit information system.EKRAN functions include diagnostics of all
aircraft systems and components that inform the pilot of any failures,and
when in the system tracing mode,provides indications of any in-flight
equipment operation abnormalities.the EKRAN also provides equipment
diagnostics using built-in sensors and documents test results during pre-
flight checks and ground maintenance.
EKRAN-32-03 显座舱内整合的内置测试系统.功能包括诊断飞机所有的系统和部件,在系
统追踪模式中若出现任何设备的异常以提醒飞行员所有的可能的失败.EKRAN也能够提供
设备诊断使用内置的感应器和文档的测试结果在飞行前的检查和地面维修.
-the backup artificial horizon indicates the bank and pitch attitude of the
helicopter,sideslip,and also provides attitude data to the flight data
recorder.
备用的人工地平线也能体现飞机俯仰的坡度姿态,侧滑,能够提供飞行数据的记录.
-the exhaust gas temperature(EGT) indicator displays the exhaust gas
temperature for each engine.
排气温度指示显示每个引擎的排气温度.
-the tachometer indicates the RPM of each engine turbine.The scale is
calibrated to display RPM as a percentage of maximum.
转速表显示每个引擎涡轮的转速.此表是校准后的引擎的最大转速.
-the fuel-quantity indicator measures the remaining fuel in the front and
rear tanks.the display is demarcated from 0 to 800 kilograms.
燃油表显示前后主油箱的燃油数,数量为0至800 KG.
-the caution light panels are used to display advisory and caution lights to
the pilot.
警示面板用于显示为飞行员进行警告提示和声音警告.
-the landing gear control panel is used to raise and lower the landing gear
as well as display the position of the landing gear.
起落架控制面板显示起落架的收出或放下状态.
-the left side of the overhead panel includes the navigation lights
brightness switch the windshield wiper switch,the windshield washer fluid
switch the pitot static port and AOA/sideslip sensors heat switches,the
pitot ram air and clock heat switches,the windshield heater setting
switch,and the magnetic compass.
左侧的顶面板包含导航灯开关及亮度切换,挡风风刷开关,挡风玻璃清洗液开关,飞行员
静态端口,攻角侧滑传感器以及热交换机.充压空气皮托时针热交换机,风挡的热交换设
定及磁罗盘.
-the right side of the overhead includes the rotor de-icing system
switch,the engine de-icing/dust-protection systems switch the left/right
pitot heat indicator lamps,the pitot heat test button,and the cockpit
ventilation fan switch.
右侧面板包括螺旋桨防冻结系统开关,引擎的过热保护开关,左/右皮托指示灯,皮托热测
试自检开关,通风机开关.
-the data link control panel is located on the left side of the overhead
panel.it is integrated with the weapons control system and its purpose is to
send and receive target information to and from other flight members.
数据链面板被装在左侧抬头面板处.被集成到武器控制系统,其目的是从其他飞行成员
处发送和接收信息的目标.
-the L-140 laser warming receiver(LWR)is designed to display the direction
and type of incoming laser energy.it indicates four horizontal quadrants and
two vertical hemispheres above and below the helicopter.
L-140激光警告接收系统,被设计用于显示来自激光照射的方向和类型.其表明四个水平
象限,垂直的两个半球.
-the uv-26 countermeasures controls panel is located to the right of the
overhead panel and is used to configure the release of infrared flare
countermeasures.
UV-26 用于红外控制面板用于控制弹外干扰弹的释放
-the magnetic compass is an autonomous,self-contained,direction-indicating
instrument that does not require a power source.it serves as a backup to
other navigation instruments.
the magnetic compass is an autonomous,self-contained,direction-indicating
instrument that does not require a power source.it serves as a backup to
other navigation instruments.
有磁性的指南针自身包含定位指示,它是一个备用的导航器。
-the PUI-800 weapon status and control panel is used to prepare weapons for
employment,view weapon inventory and status,and control numerous parameters
of weapon delivery.
PUI-800 武器状态控制面板用于武器的准备,查看控制武器状态及传递多种参数.
-the weapons control panel has the follwing functions selected weapon
type.master arm switch,stores jettison button,HE-API cannon ammunition
select switch,short-medium-long burst switch,automatic and manual weapon
control system mode switch,weapon readiness indicator,weapon/fuel tank
presence indicator,selected weapons remaining indicator,cannon rounds
remaining indicator,emergency ATGM launch button,arm and disarm switch for
emergency,weapon jettison/launch,and high or low cannon rate of fire switch.
武器控制面板有以下功能,选择武器类型,挂架切换,释放按钮,机炮选择开关,短中长选
择开关,自动手动武器控制模式,武器就绪指示,武器燃油箱仪表指示.选择武器余量,机
炮弹药余量指示,反坦克导弹紧急释放按钮,紧急情况装备和解除装备按钮,武器紧急投
放,机炮射速调整.
-the landing light and voice warming control panel is located in the lower
part of the center dash.it controls landing lights,navigation channels,and
the automatic voice message unit(VMU)
首陆信号灯及语音告警控制面板被设置在中间稍底点的位置,控制着陆灯,导航频道和自
动主意信息单元.
-the panel contains the following functions main and backup landing light
switch on/off switch for the landing light,inner-outer-automatic NDB
switch,VMU cease message button,VMU repeat button,and emergency switch for
activating voice messages for all warning in emergency mode.
这个面板包含主备用着陆信号灯切换开关,内部-外部-自动NDB(无向信标台)开关VMU语
音按钮,VMU重复按钮,所有紧急情况活动语音信息开关.
-the PVI-800 navigation control panel is used to select the operating mode
of the flight navigation system and support its interaction with other
systems.
PVI-800 导航控制面板可以同其他的系统一起用于飞行导航.
-the Autopilot panel is used to set the flight control augmentation channels
and several autopilot functions.
自动驾驶面板用于飞行增稳控制及几个自动驾驶的功能.
-The ARK-22 ADF control panel is used to configure the Automatic Direction
finder.
ARK-22 ADF(自动定向)控制面板用于配置自动定向
-The R-828 control panel is used to select the channel and control the
volume and noise reduction of the R-828 VHF radio.
R-828控制面板用于选择频道及音量及R-828 VHF噪声的抑制
-The signal flares panel is used to control power to the signal flare system
and fire the flares.The flares come in four colors red,green white and
yellow.and yellow.A cassette with four flares is located on the left
wingtip.
火警信号面板用于控制火警信息系统的控制.用四色表示火警信息,红绿白黄.灭火弹挂
载于左翼尖上.
-the electrical power control panel that is used to provide electrical power
to the aircraft's systems
电原控制面板用于给飞机提供电力系统.
-The radio and data link power control panel is used to enable and disable
power to the radios,intercom,and data link systems.
无线电和数据链电源控制面板用于开启和关闭无线电的电源,内部通话系统及数据链的
电源.
-the fuel boost pump control panel is used to control the fuel boost pumps
of both the internal and external fuel tanks.it also provides power the fuel
gauge.
增压燃油泵控制面板用于内外部油箱燃油的增压.也能为测量仪表提供能力.
-the fire extinguisher control panel includes fire warning indicators and
the system controls.
灭火器控制面板包括火警指示和系统的控制.
-The fuel shut-off valve control panel is used to open and close the fuel
valves to the enginess and APU.
燃油阀控制面板用于控制引擎和APU燃油的通断
-the transmission/oil pressure and temperature gauges.
油压与油温
-The onboard equipment control panel includes switches for the back-up
ADI,main bydraulics systems,weapons control system,stobe beacon,and others.
飞机装备控制面板包括备用ADI,主液压系统,武器控制系统,灯光及其他.
-The lighting control panel includes switches for the rotor tip
lights,formation lights,cockpit instrumentation lights,and NVG-compatible
cockpit lights.
照明控制面板包括旋翼尖灯开关,编队灯开关,座舱灯开关,仪表照明开关.
-The electronic engine governors(EEG) control panel is used to control the
fuel flow at high gas-generator(GG) RPM and to shut down an engine in case
of powerturbine over-speed.
电子调速器(EEG)控制面板控制燃油流的转速,以防止引擎超速.
-The engine power indicator is used to control the engine compressor outlet
pressure relative to the red index marks for take-off("B")maximum
continuous("H")and cruise("K").
引擎功率指示器被用来控制引擎压缩机出口与红色的索引相关的压力标志为起飞 ("
B") 最大连续 (" H") 和巡航 (" K").
-The rear auxiliary panel is located behind the pilot's right side and
includes the following controls:de-icing control panel,engine indicators
control panel,ejection system Built-In-Test panel,voice message unit BIT.
-后面的附加面板位于飞行员的右边之后而且包括下列的控制:除冰控制面板、引擎指
示器控制嵌板,弹射系统内建-测试嵌板,声音信息组件BIT。
EKRAN warning system BIT controls,hydraulic system temperature and pressure
indicators,laser warning system and infrared countermeasure system
controls,equipment bay lighting switch,and lighting brightness control
panel.
EKRAN 警告系统BIT控制,液压系统温度和压力指示器,激光警告系统和红外线的对策
系统控制,设备电灯开关、和照明光亮控制面板。
-The left panel includes the R-800L1 VHF radio control panel,targeting mode
control panel,engine and APU start-up controls,radio intercom control
panel,and the auxiliary power unit control panel.
-左边的嵌板包括 R-800 L1 特高频无线电操纵嵌板,目标准模态控制嵌板,引擎和
APU 启动控制,收音机对讲器控制嵌板,和APU控制嵌板。
-In conclusion,you should be able to find any of the cockpit controls blind
-folded.
-在结论中,任何一个驾驶员座舱控制既使带着眼罩也应该能够找所需要的。
-This concludes the lesson about cockpit instrumentation.
-这总结关于驾驶员座舱使用仪器的课。
-You may take over now by pressing the "ESC" key.
-你可以按 " ESC" 键接管现在。
Have a good flight.
祝飞行愉快。