飞机积冰及其英文译文

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6.3 飞机积冰

6.3 飞机积冰

我国飞机积冰的气候区划
积冰对飞行的 影响
机翼积冰
使升力减少,阻力增大,导致飞机失速,严重的积冰将 使飞机操纵变得困难。
❖1989年联合捷运公司的一架喷气流飞机在 华盛顿的帕斯科发生的撞地事故是尾翼失 速的一个例子。事故发生时的飞行情况是 飞机在夜间进行ILS进近,云底高度是离地 1000英尺,低于目视飞行条件,飞机表面 温度是32F,露点温度是30F。
❖ 3.在下面几种情况下能产生低空风切变的是( ) ❖ A.高空急流里的风速差异 ❖ B.850hPa图上切变线两侧的风向风速改变 ❖ C.阵风吹过跑道附近的高大建筑物 ❖ D.产生高积云的空中波动气流
❖ 4.与锋面活动有关的低空风切变,其特征是( ) ❖ A.由于暖锋移速较慢,故不会出现低空风切变 ❖ B.锋面两侧温差越大、移速越快,则风切变越强 ❖ C.在冷锋移近机场时,低空风切变已经过去 ❖ D.锋面雾预示着有较强的逆温型风切变
❖NTSB的调查报告认为,在下降过程中, 飞机在积冰条件下飞行了9.5分钟。进近是 不稳定的,导致五边进近时速度大于正常 空速,最后导致撞地,2名飞行员和使 拉力减小,螺旋桨效率降低。
涡轮发动机进气口积冰
涡轮螺旋桨或涡桨风扇等发动机的进气道积冰,会 使进气量减小,发动机的功率或推力降低。甚至造成更 为严重的后果。
风挡、天线积冰
风挡结冰后会模糊视线甚至损坏风挡玻璃;天线积 冰造成通讯中断。
空速管、静压孔积冰
空速管结冰后,会导致速度表显示错误, 影响飞行员对飞机状态的判断。
❖1974年在美国纽约Thiels附近发生的波 音727坠毁事故就与空速管积冰有关。飞 机在爬升时遇到积冰条件,机组没有打开
空速管除冰设备,得到了错误的仪表读数。 当飞机爬升到22000英尺时出现失速,最 后落地坠毁。

飞机积冰与冬季飞行

飞机积冰与冬季飞行

生。当时飞机在芝加哥上空盘旋等待着陆 许可, 半个小时后机翼形成结冰, 导致飞机 失控。 2004年11 月28日, 一架庞巴迪挑战者
冻雨和毛毛雨。 雨滴保持在过冷状态, 一旦 与地面物体接触便会结冰。 —— 冻结的降水, 如雪、 雨夹雪或冰 雹。 湿雪通常出现于温度和露点之差在1℃ 以内, 外界温度大约在-4℃~1℃之间;干 雪出现于温度 / 露点相差5℃以上。 —— 过冷的地面雾和低云。 在寒冷天 气条件下,带过冷水滴的云雾会在物体上
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航 空 安 全 SA FE T Y & S EC UR IT Y
结冰 / 霜。 —— 相对湿度很高、 温度在冰点以下 的情况, 飞机表面会形成霜。 飞机停场过夜 以及飞机从巡航高度下降着陆后,飞机表 面和燃油温度仍保持在冰点以下时,霜的 积聚是很常见的。 —— 在降雨条件下, 且机翼温度达到 结冰温度时, 机翼上表面就容易结冰。 在机 翼寒冷的地方也可能积冰。 此外, 机翼下表 面也可能有相当多的霜或结冰。这时的机 翼外表上给人的印象可能有点潮湿而已, 结成的冰也很难被发现。 —— 飞机在地面遇到疾风和高吹雪时, 机身上不受空气动力干扰的地方会受到吹 雪的污染。 —— TAT 为 10℃或低于此温度,以及 出现目视可见湿气(云,能见度少于1英里的 雾、 雪、 雨、 冻雨、 冰晶等), 或停机坪、 滑 行道或跑道上有积水、 冰或雪时, 存在结冰 条件。 着陆高度不准确, 可能影响着陆安全, 严重 时会出现危险。
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Байду номын сангаас
Nov. 2007 (Vol. 83)
SA FE T Y & S EC UR IT Y
度低于- 40℃SAT 时都必须接通发动机防 冰。 避免长时间在中度到严重结冰条件下 飞行。通常可以用改变高度和/或空速的 方法避开严重结冰, 如果可能的话, 尽量绕 开严重结冰区。 4. 机翼防冰的使用——空中 机翼防冰系统可用作除冰器或防冰器, 但用作除冰只能在空中使用。使用该系统 的主要方法是接通机翼防冰之前,先让冰 形成, 然后用其除冰。 此程序可使机翼表面 最光洁, 重新结冰的可能性最小, 推力和燃 油的损耗最小。 第二种方法是在结冰之前使用机翼防 冰。将机翼防冰系统用作防冰器仅在遇到 中度至重度结冰条件而进行延伸操作时才 使用,如:等待。 驾驶舱风档框架、风档中柱或风档雨 刷臂上出现结冰现象时,表明存在结构结 冰, 此时需要接通机翼防冰。 通常,除非延伸飞行需要通过结冰区 (等待), 否则无需定期溶冰。

飞机积冰及其英文译文

飞机积冰及其英文译文

飞机积冰在飞行中冰是个坏消息。

它破坏了空气的畅通,增加阻力,同时减少了机翼所产生的升力。

结冰对飞机重量的影响与它对气流的干扰相比是微不足道的。

随着油门增加,抬高机头弥补阻力带来的升力损失,攻角增加,造成机翼和机身底部积累更多的冰。

结冰会发生在飞机的所有暴露面,不仅仅是对翅膀,螺旋桨和挡风玻璃,而且天线,通风口,进水口和整流罩都会受到影响。

它通常产生于在飞行中如无发热的地方。

它能够引起天线震动,造成断裂。

在中度至重度的结冰条件下,小型飞机结冰将变得非常容易,因此继续飞行是不可能的。

飞机可能会在比平常更高的速度或者更低的攻角失速。

它使飞机在俯仰和滚动上面失控,并可能无法恢复。

结冰也肯能使汽化器冻结致使发动机停止,或在一个燃油喷射发动机的情况下,挡住了发动机的气源。

冰种和飞行及其影响结构冰这种东西,会凝固在飞机外面。

它被描述为霜,明冰(有时称为釉冰),和混合冰。

雾凇粗糙,外观呈乳白色,一般附着在表面的轮廓。

大部分可除去除冰或防冰设备都可预防。

明(或釉)冰有时是清晰流畅,但通常含有一些气泡,或块状,半透明的外观效果。

积冰越大,越符合机翼形状,其形状往往是由上,下为特点清除冰密集,更难,比雾凇冰更加透明,并且像“牛角”。

一般很难打破。

(冲击力越大的地方,机翼上的结冰就越少;这种形状像是上下两端凸起中间下凹的角。

明冰密度更大,更坚硬比雾凇更透明,通常也很难去除。

)混合冰是雾凇和明冰的组合。

冰可以在机翼表面空气流动扭曲,减少机翼的最大升力,降低了最大升力攻角,影响飞机的操纵品质,在风洞测试中表明,霜,雪,冰(在前沿或机翼上表面),厚度不超过一粗砂纸片可减少百分之三十升力和增加阻力高达百分之四十。

较大的附着,更会减少升力,可以增加百分之八十以上的阻力。

即使飞机进入结冰条件下飞行配备除冰系统,未受保护区域依然会有冰的积累。

美国航天局研究显示,近百分之三十的阻力依然存在即使已经对飞机的主要表面进行清理。

非保护表面可能包括天线,襟翼铰链,控制喇叭,机身前部区域,挡风玻璃刮水器,机翼支柱,固定起落架等。

飞行气象学:12-1 航空天气报告

飞行气象学:12-1 航空天气报告
▪ 用经纬度或四字地名代码 ▪ 如“ZULS” ▪ 表示拉萨
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(7)气温
▪ 气温以整摄氏度编报,负值前用“MS”。 ▪ “MS31”表示“气温-31C”
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(8)风向风速
▪ 风向用整度数表示,风速以km/h的整数表示。 ▪ “220/100”表示“风向220,风速100 km/h”。
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(9)飞机颠簸
(阴天,云量8)
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云的说明
▪ (1)“SKC”表示“碧空”。 ▪ (2)当天空不明时报告垂直能见度,如“VER
VIS300”表示“垂直能见度300 m”。
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云的说明
▪ (3)当观测到机场上空及附近有积雨云或浓积 云时,应说明云状
▪ (4)描述云底状况用三个简语 “RAG”表示“破碎”, “DIF”表示“散乱”, “FLUC”表示“有起伏”。
▪ “HVY TSRA”(强雷雨) ▪ 或“VCFG”(机场附近有雾),
▪ “HVY DZ FG”(大的毛毛雨和雾)
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现在天气
▪ 天气现象最多报告三种。如“HVY TSRA SN” 意为“强雷暴伴雨夹雪”,或“FBLSN RA FG” 表示“小雨雪伴雾”。
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(8)云
云量的说明
▪ “FEW”(少云,1~2个八分量), ▪ “SCT”(疏云,3~4个八分量), ▪ “BKN”(多云,5~7个八分量),“OVC”
(4) (5) (6) 现在天气 云 气温和露点 气压
(7) (8) (9) (10) 补充信息 (11)
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(1)报告名称
“MET REPORT” 为日常航空天气报告的开头 翻译为“日常航空天气报告”
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地名 东京 名古屋 汉城 台北 马尼拉 墨尔本 悉尼

航空气象情报释读

航空气象情报释读

模式SN 用于飞行文件的符号1.重要天气符号雷暴毛毛雨热带气旋雨严重飑线* 雪中度颠簸阵雨雹严重颠簸大片吹雪山地波严重沙或尘霾中度飞机积冰大片沙(尘)暴严重飞机积冰大片霾大片雾大片轻雾大气中的放射性物质**大片烟火山喷发*** 冻雨***山地状况不明可见火山灰云****** 在为飞行高度层100以下飞行的飞行文件中,这个符号指“飑线”。

** 下列情报涉及的符号应该在图边标明:放射物符号;意外事故点的经/纬度;意外事故发生的日期和时间;进一步情报的核对航行通告。

*** 下列情报应该在图边标明:火山喷发符号;火山名字和国际编号(如果知道);经/纬度;首次喷发的日期和时间(如果知道);关于火山灰的核对重要气象情报和航行通告或火山通告。

**** 这个符号不涉及在很低温度下由于降水而引起的飞机积冰。

*****可见的火山云符号仅仅适用于VAG模式,对SIGWX图不适用。

注:每幅图例的预期现象的底顶间高度指示。

2.锋面、辐合带和其他的符号地面冷锋最大风的位置、速度和高度层地面暖锋幅合线地面锢囚锋零度等温度层高度地面准静止锋热带辐合带对流层顶高点海面状况对流层顶低点海面温度对流层顶高度大范围的强地面风风矢表明急流的最大风和所在的飞行高度层。

用双横线标明大于或等于20海里/小时的风速变化和3000英尺(或更小,如果可行)的飞行高度层的显著变化。

在此例中,双横线处风速是225公里/小时(120公里/小时)。

粗线描绘预报风速为150公里/小时(80公里/小时)的急流轴的起始点和终止点。

* 该符号指出大范围地面风速超过60公里/小时(30海里/小时)。

3.用于描述云的缩写3.1 云状CI一卷云CS一卷层云AS一高层云SC一层积云CU一积云CC一卷积云AC一高积云NS一雨层云ST一层云CB一积雨云3.2 云量除CB以外的云:SKC = 碧空(0/8) FEW =少云(1/8-2/8) SCT = 疏云(3/8-4/8)BKN = 多云(5/8-7/8) 0VC = 阴天(8/8)只限CB:ISOL = 个别(孤立的)CBOCNL = 完全分离的CBFRQ = 很少或不分离的CBEMBD = 隐嵌在其他云层中或隐嵌在霾里的CB3.3 高度在SWH和SWM图上的高度都用飞行高度层表示,当用XXX表示底或顶的高度时,底高或顶高都在SWL图的气层以外。

翻译(颠簸激流和积冰)

翻译(颠簸激流和积冰)

翻译1 英文原文TURBULENCEEveryone who flies encounters turbulence at some time or other . A turbulent atmosphere as one in which air currents range from rather mild eddies to strong currents of relatively large dimensions. As an aircraft moves through these currents, it undergoes changing accelerations which jostle it from its smooth flight path. This jostling is turbulence. Turbulence ranges from bumpiness which can annoy crew and passengers to severe jolts which can structurally damage the aircraft or injure its passengers.Aircraft reaction to turbulence varies with the difference in wind speed in adjacent currents, size of the aircraft, wing loading, airspeed, and aircraft attitude. When an aircraft travels rapidly from one current to another, it undergoes abrupt changes in acceleration. Obviously , if the aircraft moves more slowly, the changes in acceleration would be more gradual. The first rule in flying turbulence is to reduce airspeed. Your aircraft manual most likely lists recommended airspeed for penetrating turbulence.Knowing where to expect turbulence helps a pilot avoid or minimize turbulence discomfort and hazards. The main causes of turbulence are (1) convective currents, (2) mountain wave, and (3) wind shear. Turbulence also occurs in the wake of moving aircraft whenever the airfoils exert lift—wake turbulence. Any combination of causes may occur at one time.CONVECTIVE CURRENTSConvective currents are a common cause of turbulence, especially at low altitudes. These currents are localized vertical air movements, both ascending and descending. For every rising current, there is a compensating downward current. The downward currents frequently occur over broader areas than do the upward currents, and therefore, they have a slower vertical speed than dothe rising currents.Convective currents are most active on warm summer afternoons when winds are light. Heated air at the surface creates a shallow, unstable layer, and the warm air is forced upward. Convection increases in strength and to greater heights as surface heating increases. Barren surfaces such as sandy or rocky wastelands and plowed fields become hotter than open water or ground covered by vegetation. Thus, air at and near the surface strength of convective currents can vary considerably within short distances.When cold air moves over a warm surface, it becomes unstable in lower levels. Convective currents extend several thousand feet above the surface resulting in rough, choppy turbulence when flying in the cold air. This condition often occurs in any season after the passage of a cold front.Turbulence on approach can cause abrupt changes in airspeed and may even result in a stall at a dangerously low altitude. To prevent the danger, increase airspeed slightly over normal approach speed. This procedure may appear to conflict with the rule of reducing airspeed for turbulence penetration; but remember, the approach speed for your aircraft is well below the recommended turbulence penetration speed.As air moves upward, it cools by expansion. A convective current continues upward until it reaches a level where its temperature cools to the same as that of the surrounding air. If it cools to saturation, a cloud forms. Billowy fair weather cumulus clouds, usually seen on sunny afternoons, are signposts in the sky indicating convective turbulence. The cloud top usually marks the approximate upper limit of the convective current. A pilot can expect to encounter turbulence beneath or in the clouds, while above the clouds, air generally is smooth.MOUNTAIN WAVEWhen stable air crosses a mountain barrier, the turbulent situation is somewhat reversed. Air flowing up the windward side is relatively smooth. Wind flow across the barrier is laminar—that is, it tends to flow in layers. The barrier may set up waves in these layers much as waves develop on a disturbed water surface. The waves remain nearly stationary while the wind blows rapidly throughthem. The wave pattern is a “standing” or “mountain” wave, so named because it remains essentially stationary and is associated with the mountain. The wave pattern may extend 100 miles or more downwind from the barrier.Wave crests extend well above the highest mountains, sometimes into the lower stratosphere. Under each wave crest is a rotary circulation, the “rotor” forms below the elevation of the mountain peaks. Turbulence can be violent in the overturning rotor. Updrafts and downdrafts in the waves can also create violent turbulence.When planning a flight over mountainous terrain, gather as much preflight information as possible on cloud reports, wind direction, wind speed, and stability of air. Satellites often help locate mountain waves, but adequate information may not always be available, so remain alert for signposts in the sky. What should you look for both during preflight planning and during your in flight observations?Wind at mountain top level in excess of 25 knots suggests some turbulence. Wind in excess of 40 knots across a mountain barrier dictates caution. Stratified clouds mean stable air. Standing lenticular and rotor clouds suggest a mountain wave; expect turbulence many miles to the lee of mountains and relative smooth flight on the windward side. Convective clouds on the windward the mountain.When approaching mountains from the leeward side during strong winds, you’d better begin your climb well away from the mountain—100 miles in mountain wave .Climb to an altitude 3,000 to 5,000 feet above mountain tops before attempting to cross. The best procedure is to approach a ridge at a 45°angle to enable a rapid retreat to calmer air. If unable to make good on your first attempt and you have higher altitude capabilities, you may back off and make another attempt at higher altitude. Sometimes you may have to choose between turning back or detouring the area.Flying mountain passes and valleys is not a safe procedure during high winds. The mountains funnel the wind into passes and valleys thus increasing wind speed and intensifying turbulence. If winds at mountain top level are strong, go high, or go around. Surface wind may be relatively calm in a valley surrounded by mountains when wind aloft is strong.. If taking off in the valley, climb above mountain clearance from the mountains sufficient to allow recovery if caught in a downdraft.WIND SHEARWind shear generates eddies between two wind currents of differing velocities. The differences may be in wind speed, wind direction, or in both. Wind shear may be associated with either a wind shift or a wind speed gradient at any level in the atmosphere. Three conditions are of special interest—(1) wind shear with a low-level temperature inversion, (2) wind shear in a frontal zone, and (3) clear air turbulence at high levels associated with a jet stream or strong circulation.WIND SHEAR WITH A LOW-LEVEL TEMPERATURE INVERSIONWhen surface wind is calm or very light, takeoff or landing can be in any direction. Takeoff may be in the direction of the wind above the inversion. If so, the aircraft encounters a sudden tailwind and a corresponding loss of airspeed when climbing through the inversion. Stall is possible. If approach is into the wind above the inversion, the headwind is suddenly lost when descending through the inversion. Again, a sudden loss in airspeed may induce a stall.A temperature inversion forms near the surface on a clear night with calm or light surface wind. When taking off or landing in calm wind under clear skies within a few hours before or after sunrise, be prepared for a temperature inversion near the ground. You can be relatively certain of a shear zone in the inversion if you know the wind as 2000 to 4000 feet is 25 knots or more. Allow a margin of airspeed above normal climb or approach speed to alleviate danger of stall in event of turbulence or sudden change in wind velocity.WIND SHEAR IN A FRONTAL ZONEA front can contain many hazards. However, a front can be between two dry stable airmasses and can be devoid of clouds. Even so, wind changes abruptly in the frontal zone and can inducewind shear turbulence. The degree of turbulence depends on the magnitude of the wind shear. When turbulence in expected in a frontal zone, follow turbulence penetration procedures recommended in your aircraft manual.CLEAR AIR TURBULENCEClear air turbulence implies turbulence devoid of clouds. However, we commonly reserve the term for high level wind shear turbulence, even when in cirrus clouds. A preferred location of CAT is in an upper trough on the cold side of the jet stream. Another frequent CAT location is along the jet stream north and northeast of a rapidly deepening surface low. Even clear air turbulence can destroyed the aircraft so easily, it is every pilots’ obligation to report the CAT when encountered, and pilot when preflight must check the weather forecast, and report to make sure there is no CAT in the flight path.WAKE TURBULENCEAn aircraft receives its lift by accelerating a mass of air downward. Thus, whenever the wings are providing lift, air is forced downward under the wings generating rotary motions or vortices off the wing tips. When the landing gear bears the entire weight of the aircraft, no wing tip vortices develop. But the instant the pilot “hauls back” on the controls, these vortices begin and spread downward and outward from the flight path. They also drift with the wind. Strength of the vortices is proportional to the weight of the aircraft as well as other factors. Therefore, wake turbulence is more intense behind large, transport category aircraft than behind small aircraft. Generally, it is a problem only when following the larger aircraft.The turbulence persists several minutes and may linger after the aircraft is out of sight. At controlled airports, the controller generally warns pilots in the vicinity of possible wake turbulence. When left to your own resources, you could use a few pointers. Most jets when taking off lift the nose wheel about midpoint in the takeoff roll; therefore, vortices begin about the middle of the takeoff roll. Vortices behind propeller aircraft begin only a short distance behind lift-off. Followinga landing of either type of aircraft, vortices end at about the point where the nose wheel touches down. Avoid flying through these vortices. More specifically, when using the same runway as a heavier aircraft:(1)if landing behind another aircraft, keep your approach above his approach and keep youtouchdown beyond the point where his nose wheel touched the runway;(2)if landing behind a departing aircraft, land only if you can complete your landing roll beforereaching the midpoint of his takeoff roll;(3)if departing behind another departing aircraft, take off only if you can become airbornebefore reaching the midpoint of his takeoff roll and only if you can climb fast enough to stay above his flight path;(4)If departing behind a landing aircraft, don’t un less you can taxi onto the runway beyond theat which his nose wheel touched down and have sufficient runway left for safe takeoff. The foregoing procedures are elementary. The problem of wake turbulence is more operational than meteorological. The FAA issues periodic advisory circulars of operational problems. If you plan to operate out of airports used routinely by air carriers, we highly recommend you read the latest advisory circulars on wake turbulence. Titles of there circulars are listed in the FAA “Advisory Circular Checkl ist and Status of Regulations.”ICINGAircraft icing is one of the major weather hazards to aviation. Icing is a cumulative hazard. It reduces aircraft efficiency by increasing weight, reducing lift, decreasing thrust, and increasing drag. As shown in figure 1, each effect tends to either slow the aircraft or force it downward. Icing also seriously impairs aircraft engine performance. Other icing effects include false indications on flight instruments, loss of radio communications, and loss of operation of control surfaces, brakes, and landing gear.Figure 1. Effects of structural icing.In this article we discuss the principles of structural, induction system, and instrument icing, and other factors on icing. Although ground icing and frost are structural icing, we discuss them separately because of their different effect on an aircraft. And we wind up the chapter with a few operational pointers.STRUCTURAL ICINGTwo conditions are necessary for structural icing in flight: (1) the aircraft must be flying through visible water such as rain or cloud droplets, and (2) temperature at the point where the moisture strikes the aircraft must be 0° ; C or colder. Aerodynamic cooling can lower temperature of an airfoil to 0° C even though the ambient temperature is a few degrees warmer.Supercooled water increases the rate of icing and is essential to rapid accretion. Supercooled water is in an unstable liquid state; when an aircraft strikes a supercooled drop, part of the drop freezes instantaneously. The latent heat of fusion released by the freezing portion raises the temperature of the remaining portion to the melting point. Aerodynamic effects may cause theremaining portion to freeze. The way in which the remaining portion freezes determines the type of icing. The types of structural icing are clear, rime, and a mixture of the two. Each type has its identifying features.CLEAR ICEClear ice forms when after initial impact, the remaining liquid portion of the drop flows out over the aircraft surface gradually freezing as a smooth sheet of solid ice. This type forms when drops are large as in rain or in cumuliform clouds. Figure 2 illustrates ice on the cross section of an airfoil, clear ice shown at the top.Figure 2. Clear, rime, and mixed icing on airfoilsRIME ICERime ice forms when drops are small, such as those in stratified clouds or light drizzle. The liquid portion remaining after initial impact freezes rapidly before the drop has time to spread over the aircraft surface. The small frozen droplets trap air between them giving the ice a white appearance as shown at the center of figure 2.Rime ice is lighter in weight than clear ice and its weight is of little significance. However, its irregular shape and rough surface make it very effective in decreasing aerodynamic efficiency of airfoils, thus reducing lift and increasing drag. Rime ice is brittle and more easily removed than clear ice.MIXED CLEAR AND RIME ICINGMixed ice forms when drops vary in size or when liquid drops are intermingled with snow or ice particles. It can form rapidly. Ice particles become imbedded in clear ice, building a very rough accumulation sometimes in a mushroom shape on leading edges as shown at the bottom of figure 2.INDUCTION ICINGIce frequently forms in the air intake of an engine robbing the engine of air to support combustion. This type icing occurs with both piston and jet engines, and almost everyone in the aviation community is familiar with carburetor icing. The downward moving piston in a piston engine or the compressor in a jet engine forms a partial vacuum in the intake. Adiabatic expansion in the partial vacuum cools the air. Ice forms when the temperature drops below freezing and sufficient moisture is present for sublimation. In piston engines, fuel evaporation produces additional cooling. Induction icing always lowers engine performance and can even reduce intake flow below that necessary for the engine to operate. Figure 3 illustrates carburetor icing.Figure 3. Carburetor icing. Expansional cooling of air and vaporization of fuel can induce freezing and cause ice to clog the carburetor intake.Induction icing potential varies greatly among different aircraft and occurs under a wide range of meteorological conditions. It is primarily an engineering and operating problem rather than meteorological.INSTRUMENT ICINGIcing of the pitot tube as seen in figure 4 reduces ram air pressure on the airspeed indicator and renders the instrument unreliable. Most modern aircraft also have outside static pressure port as part of the pitot-static system. Icing of the static pressure port reduces reliability of all instruments on the system - the airspeed, rate-of-climb, and altimeter.Figure 4. Internal pitot tube icing. It renders airspeed indicator unreliable.Ice forming on the radio antenna distorts its shape, increases drag, and imposes vibrations that may result in failure in the communications system of the aircraft. The severity of this icing depends upon the shape, location, and orientation of the antenna.OTHER FACTORS IN ICINGIn addition to the above, other factors also enter into icing. Some of the more important ones are discussed below.FRONTSAtmospheric circulation is the movement of air around the surface of the Earth. It is caused by uneven heating of the Earth’s surface and upsets the equilibrium of the atmosphere, creating changes in air movement and atmospheric pressure. Because the Earth has a curved surface that rotates on a tilted axis while orbiting the sun, the equatorial regions of the Earth receive a greater amount of heat from the sun than the polar regions. The amount of sun that heats the Earth depends upon the time of day, time of year, and the latitude of the specific region. All of these factors affect the length of time and the angle at which sunlight strikes the surface. In general circulation theory, areas of low pressure exist over the equatorial regions, and areas of high pressure exist over the polar regions due to a difference in temperature. Solar heating causes air to become less dense and rise in equatorial areas. The resulting low pressure allows the high-pressure air at the poles to flow along the planet’s surface toward the equator. As the warm air flows toward the poles, it cools, becoming more dense, and sinks back toward the surface. This pattern of air circulation is correct in theory; however, the circulation of air is modified by several forces, most importantly the rotation of the Earth. The force created by the rotation of the Earth is known as Coriolis force. This force is not perceptible to us as we walk around because we move so slowly and travel relatively short distances compared to the size and rotation rate of the Earth. However, it does significantly affect bodies that move over great distances, such as anair mass or body of water. The Coriolis force deflects air to the right in the Northern Hemisphere, causing it to follow a curved path instead of a straight line. The amount of deflection differs depending on the latitude. It is greatest at the poles, and diminishes to zero at the equator. The magnitude of Coriolis force also differs with the speed of the moving body—the faster the speed, the greater the deviation. In the Northern Hemisphere, the rotation of the Earth deflects moving air to the right and changes the general circulation pattern of the air. The speed of the Earth’s rotation causes the general flow to break up into three distinct cells in each hemisphere. [Figure 10-9] In the Northern Hemisphere, the warm air at the equator rises upward from the surface, travels northward, and is deflected eastward by the rotation of the Earth. By the time it has traveled one-third of the distance from the equator to the North Pole, it is no longer moving northward, but eastward. This air cools and sinks in a belt-like area at about 30°latitude, creating an area of high pressure as it sinks toward the surface. Then it flows southward along the surface back toward the equator. Coriolis force bends the flow to the right, thus creating the northeasterly trade winds that prevail from 30°latitude to the equator. Similar forces create circulation cells that encircle the Earth between 30° and 60° latitude, and between 60° and the poles. This circulation pattern results in the prevailing westerly winds in the conterminous United States. Circulation patterns are further complicated by seasonal changes, differences between the surfaces of continents and oceans, and other factors. Frictional forces caused by the topography of the Earth’s surface modify the movement of the air in the atmosphere. Within 2,000 feet of the ground, the friction between the surface and the atmosphere slows the moving air. The wind is diverted from its path because the frictional force reduces the Coriolis force. This is why the wind direction at the surface varies somewhat from the wind direction just a few thousand feet above the Earth.Air flows from areas of high pressure into those of low pressure because air always seeks out lower pressure. In the Northern Hemisphere, this flow of air from areas of high to low pressure is deflected to the right; producing a clockwise circulation around an area of high pressure. This is also known as anti-cyclonic circulation. The opposite is true of low-pressure areas; the air flows toward a low and is deflected to create a counter-clockwise or cyclonic circulation. High-pressure systems are generally areas of dry, stable, descending air. Good weather is typically associated with high-pressure systems for this reason. Conversely, air flows into a low-pressure area to replace rising air. This air tends to be unstable, and usually brings increasing cloudiness and precipitation. Thus, bad weather is commonly associated with areas of low pressure.A condition favorable for rapid accumulation of clear icing is freezing rain below a frontal surface. Rain forms above the frontal surface at temperatures warmer than freezing. Subsequently, it falls through air at temperatures below freezing and becomes supercooled. The supercooled drops freeze on impact with an aircraft surface. Figure 5 diagrams this type of icing. It may occur with either a warm front (top) or a cold front. The icing can be critical because of the large amount of supercooled water. Icing can also become serious in cumulonimbus clouds along a surface cold front, along a squall line, or embedded in the cloud shield of a warm front.Figure 5. Freezing rain with a warm front (top) and a cold front (bottom). Rainfall through warm air aloft into subfreezing cold air near the ground. The rain becomes supercooled and freezes on impact.TERRAINAir blowing upslope is cooled adiabatically. When the air is cooled below the freezing point, the water becomes supercooled. In stable air blowing up a gradual slope, the cloud drops generally remain comparatively small since larger drops fall out as rain. Ice accumulation is rather slow and you should have ample time to get out of it before the accumulation becomes extremely dangerous. When air is unstable, convective clouds develop a more serious hazard as described in "Icing and Cloud Types."Icing is more probable and more hazardous in mountainous regions than over other terrain. Mountain ranges cause rapid upward air motions on the windward side, and these vertical currentssupport large water drops. The movement of a frontal system across a mountain range often combines the normal frontal lift with the upslope effect of the mountains to create extremely hazardous icing zones.Each mountainous region has preferred areas of icing depending upon the orientation of mountain ranges to the wind flow. The most dangerous icing takes place above the crests and to the windward side of the ridges. This zone usually extends about 5,000 feet above the tops of the mountains; but when clouds are cumuliform, the zone may extend much higher.SEASONSIcing may occur during any season of the year; but in temperate climates such as cover most of the contiguous United States, icing is more frequent in winter. The freezing level is nearer the ground in winter than in summer leaving a smaller low level layer of airspace free of icing conditions. Cyclonic storms also are more frequent in winter, and the resulting cloud systems are more extensive. Polar regions have the most dangerous icing conditions in spring and fall. During the winter the air is normally too cold in the polar regions to contain heavy concentrations of moisture necessary for icing, and most cloud systems are stratiform and are composed of ice crystals.GROUND ICINGFrost, ice pellets, frozen rain, or snow may accumulate on parked aircraft. You should remove all ice prior to takeoff, for it reduces flying efficiency of the aircraft. Water blown by propellers or splashed by wheels of an airplane as it taxis or runs through pools of water or mud may result in serious aircraft icing. Ice may form in wheel wells, brake mechanisms, flap hinges, etc, and prevent proper operation of these parts. Ice on runways and taxiways create traction and braking problems.中文翻译颠簸激流每一个飞行员都有可能遇到颠簸,当一个颠簸的气流运动(包括涡旋和大的相对气流),飞机飞过这些气流时,它改变了飞机的速度,从而使飞机偏离了它平滑的航道。

飞机积冰

飞机积冰

主要的积冰类型为:明冰、毛冰、雾淞和 霜。
1.明冰( Clear Ice ):光滑透明、结 构坚实。在0~-10℃的过冷雨中或大水 滴组成的云中形成
明冰(Clear Ice)
明冰凝 结时只有少 部分水滴是 立即凝结的, 大多数水滴 是有一个流 动的过程逐 渐凝结的, 因此明冰没 有气泡,密 度大,透明, 并且质地坚 硬。
过冷水滴温度接近0℃:冻结~蒸发~再冻结 过冷水滴较小,温度接近-20℃:直接冻结 气温低于0℃,• 机表面的温度低于0℃,和有温度低于 飞 0℃的水滴存在。
2、积冰过程

3、基本条件
二、积冰的种类 无论对于预报员或飞行员来说,认识 积冰的不同类型都是很重要的,因为不同 的积冰类型对飞行的危害程度是不一样的。
注:霜是在晴空中飞行时出现的一 种积冰,它是未饱和空气与温度低 于0℃的飞机接触时,如果机身温度 低于露点,水汽在机体表面直接凝 华而成
各种积冰的发生率
Clear Mixed 0° C to -10° C -10° C to -15° C
Rime
-15° C to - 40° C
雾淞最常见
这只是大概的规律
微量积冰
微量积冰指冰层的生成速度略大于其升华速 度,这种积冰没有明显危害,无需启动防冰除冰 设备,也无需改变飞行高度或航径,除非这种积 冰达到1小时以上。
轻度积冰
轻度积冰 指如果这种积 冰持续1小时以 上,则对飞行 将构成威胁, 因此间断使用 防冰除冰设备 成为必要,如 果需要在这种 环境中长时间 飞行,则必须 改变高度或改 变航径。轻度 积冰是最常见 的。
3.影响仪表和通讯,甚至使之失灵
如空速管积冰影响空速表工作;天线积 冰影响通讯质量甚至使通讯中断;风挡 积冰影响视线等。

6.3-飞机积冰

6.3-飞机积冰
❖过冷水滴温度接近-20℃:直接冻结~释放 的潜热不足以减缓冻结速度。
飞机积冰的基本条件
❖气温低于0℃ ❖飞机表面的温度低于0℃ ❖有温度低于0℃的水滴存在(过冷水滴)
飞机积冰的种类
❖ 明冰 光滑透明、结构坚实。在0~-10℃的过冷雨中或 大水滴组成的云中形成;水滴与机身相碰后一部分冻结, 一部分沿着气流向后面的位置上冻结,冻结速度比较慢。 明冰较坚固,危害较大。
我国飞机积冰的气候区划
积冰对飞行的 影响
机翼积冰
使升力减少,阻力增大,导致飞机失速,严重的积冰将 使飞机操纵变得困难。
❖1989年联合捷运公司的一架喷气流飞机在 华盛顿的帕斯科发生的撞地事故是尾翼失 速的一个例子。事故发生时的飞行情况是 飞机在夜间进行ILS进近,云底高度是离地 1000英尺,低于目视飞行条件,飞机表面 温度是32F,露点温度是30F。
明冰
❖ 雾凇:不透明,表面粗糙。多形成在温度为-20℃左右 的云中;过冷水滴较小,冻结速度快,在水滴和机身相 碰时就能冻结。容易除去。
雾凇
飞机上的雾凇
雾凇
雾凇
❖毛冰:表面粗糙不平,冻结得比较坚固, 像白瓷,形成在温度为-5 ~ -15℃的云 中;由大的过冷水滴和小的过冷水滴同时 冻结形成。毛冰表面粗糙、 比较坚固,
❖ 9.较强的低空风切变多产生于下列何种天气系统中 ()
❖ A.海陆风和热低压 B.气旋和低涡 ❖ C.槽线和切变线 D.锋面和雷暴
❖ 10.飞机从逆风进入顺风时所遇到的风切变是( )
❖ A.顺风切变
B.逆风切变
❖ C.侧风切变
D.垂直风切变
❖ 11.飞机在着陆时突然遇到逆风切变,会出现下述何种现象( ) ❖ A.飞机空速突然增大,升力增加,飞机上仰并上升到下滑线之上 ❖ B.飞机高度下降,空速减小,未到正常着陆点即提前着陆 ❖ C.飞机空速突然减小,升力减小,飞机将掉至正常下滑线之下 ❖ D.空速表读数急剧变化,飞机颠簸严重
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飞机积冰在飞行中冰是个坏消息。

它破坏了空气的畅通,增加阻力,同时减少了机翼所产生的升力。

结冰对飞机重量的影响与它对气流的干扰相比是微不足道的。

随着油门增加,抬高机头弥补阻力带来的升力损失,攻角增加,造成机翼和机身底部积累更多的冰。

结冰会发生在飞机的所有暴露面,不仅仅是对翅膀,螺旋桨和挡风玻璃,而且天线,通风口,进水口和整流罩都会受到影响。

它通常产生于在飞行中如无发热的地方。

它能够引起天线震动,造成断裂。

在中度至重度的结冰条件下,小型飞机结冰将变得非常容易,因此继续飞行是不可能的。

飞机可能会在比平常更高的速度或者更低的攻角失速。

它使飞机在俯仰和滚动上面失控,并可能无法恢复。

结冰也肯能使汽化器冻结致使发动机停止,或在一个燃油喷射发动机的情况下,挡住了发动机的气源。

冰种和飞行及其影响结构冰这种东西,会凝固在飞机外面。

它被描述为霜,明冰(有时称为釉冰),和混合冰。

雾凇粗糙,外观呈乳白色,一般附着在表面的轮廓。

大部分可除去除冰或防冰设备都可预防。

明(或釉)冰有时是清晰流畅,但通常含有一些气泡,或块状,半透明的外观效果。

积冰越大,越符合机翼形状,其形状往往是由上,下为特点清除冰密集,更难,比雾凇冰更加透明,并且像“牛角”。

一般很难打破。

(冲击力越大的地方,机翼上的结冰就越少;这种形状像是上下两端凸起中间下凹的角。

明冰密度更大,更坚硬比雾凇更透明,通常也很难去除。

)混合冰是雾凇和明冰的组合。

冰可以在机翼表面空气流动扭曲,减少机翼的最大升力,降低了最大升力攻角,影响飞机的操纵品质,在风洞测试中表明,霜,雪,冰(在前沿或机翼上表面),厚度不超过一粗砂纸片可减少百分之三十升力和增加阻力高达百分之四十。

较大的附着,更会减少升力,可以增加百分之八十以上的阻力。

即使飞机进入结冰条件下飞行配备除冰系统,未受保护区域依然会有冰的积累。

美国航天局研究显示,近百分之三十的阻力依然存在即使已经对飞机的主要表面进行清理。

非保护表面可能包括天线,襟翼铰链,控制喇叭,机身前部区域,挡风玻璃刮水器,机翼支柱,固定起落架等。

不幸的是,一些粗心的飞行员们,遇到严重结冰的时候措手不及,并且没有相应的计划。

许多飞行员只从天气简报中的信息来确定哪些地方不容易结冰,哪些地方可能会出现结冰。

然而,飞行员可以学到足够的基本气象了解那里的冰可能会得到他们的等待。

飞行员可以在离开地面之前制定一些防冰除冰的飞行计划。

结冰飞机表面可以形成在0摄氏度(华氏32度)或更冷时液态水存在。

即使是最好的飞行计划也有一些变数。

虽然这是相当容易预测的地方结冰潜力的大面积存在,具体结冰地区和高度准确的预测会带来更多的困惑。

山,水,风,温度,湿度和大气压力在对这些决策方面都充当着重要的角色。

所有的云都不尽相同。

有干,湿云。

云干水分,相对较少,因此,对飞机结冰潜力低。

北达科他州,因为它非常寒冷的冬天,往往是干云。

然而,在宾夕法尼亚州和纽约的冬天往往会带来阿巴拉契亚山脉与冷空气和大量的湿云及大量水分,当温度冻结或以下,与冰加载。

大湖是一个非常大的水汽来源。

一个寒冷的空气质量的起源是多少过冷云水将进行的关键。

如果盛行风携带超过水云,他们可能会被淋湿了。

以上图表显示了潜在的高冰的一些领域。

结冰状况有时可能会出现在地图上显示的上述低风险地区。

锋面和低气压的地区是主要结冰的区域,但隔离空气充足的水分质量不稳定可以产生足够的结冰云,使轻型飞机无法通过。

冻雨和小雨是飞行中最大的敌人,可以大大粗糙飞机机翼表面积大的区域或扭曲机翼形状,这是对飞行非常危险的,即使在短短的几分钟内。

冻雨发生时,从高空暖空气降水通过将低于冷空气逆温层下面。

较大的水滴可能会在没有除冰加热的后方部位冻结。

随着一道冷锋,冷空气下温暖的空气,解除在潮湿的积云形成更加迅速和由此产生的。

沿着暖锋,温暖的空气往往滑过较冷的空气,有利于形成层云结冰。

当你接近前,云层建立非常迅速,层与层之间纯净的空气也会迅速消失。

冻雨和冰冻毛毛雨,包括冻结小雨升空,有时出现在锋面附近。

如果您选择它通过前,请确保它不包含冻雨或冻结小雨和其他有害,如天气条件嵌入式(隐藏)雷暴。

你应该计划飞行通过前最短的路线,而不是在锋面附近久留。

结构冰如何迅速采集冰表面上取决于其形状的一部分。

薄冰现代化的机翼将更加比厚的冰还要影响大,旧飞机的机翼尾部表面通常会结冰速度远远超过了翅膀。

如果尾部失速是由于冰和它引起的气流干扰,在低海拔处改出的可能性不大。

有许多运货飞机由于尾部失速而失事。

同时也发生在很多轻型飞机,但通常是没有很好的记载。

对于尾失速不太熟悉的许多飞行员,需要强调的是,机翼失速威胁更大,这是非常重要的正确区分这两个,因为所需采取的行动大致相反。

机翼失速机翼失速通常会在较低的攻角,从而较高速时,当冰累积。

即使是少量的冰会产生效果,如果冰粗糙,它会造成非常大的影响。

因此,我们建议若是遇到结冰情况,应该在进近的时候适当增大速度。

如何增加在很大程度上取决于机型和冰量。

请参考AFM或POH与冰相关会使飞机机翼失速特性变得不明显,而严重的滚转控制问题,也并不罕见。

积冰可能在两翼之间是不对称的。

隐藏,一边机翼,通常结冰较薄,从而更好地收集的冰,外面的部分可能会首先失速,比另外一边机翼更加迅速。

结冰对滚转控制的影响在副翼的翅膀上结冰可以影响滚转控制。

通用航空(GA)的飞机机翼的设计是使机翼先从跟部开始失速然后向外延伸开来,因此不会干扰副翼控制。

然而,翼尖通常要比后面的地方要薄,所以它们的机翼部分,更容易集冰。

这可能导致翼尖失速,可能会影响副翼,从而对滚转控制造成影响。

如果冰在副翼和边缘的链接部位积累,这可能会影响气流,干扰与副翼的正常运作。

如果副翼功能受损,如果遭遇这样的情况,上轻微向前压盘可能有助于使气流重新附着在副翼上。

Aircraft icingIce in flight is bad news. It destroys the smooth flow of air, increasing drag while decreasing the ability of the airfoil to create lift. The actual weight of ice on an airplane is insignificant when compared to the airflow disruption it causes. As power is added to compensate for the additional drag and the nose is lifted to maintain altitude, the angle of attack is increased, allowing the underside of the wings and fuselage to accumulate additional ice. Ice accumulates on every exposed frontal surface of the airplane—not just on the wings, propeller, and windshield, but also on the antennas, vents, intakes, and cowlings. It builds in flight where no heat or boots can reach it. It can cause antennas to vibrate so severely that they break. In moderate to severe conditions, a light aircraft can become so iced up that continued flight is impossible. The airplane may stall at much higher speeds and lower angles of attack than normal. It can roll or pitch uncontrollably, and recovery might be impossible.Ice can also cause engine stoppage by either icing up the carburetor or, in the case of a fuel-injected engine, blocking the engine’s air source.Kinds of Ice and Their Effects on FlightStructural ice is the stuff that sticks to the outside of the airplane. It is described as rime, clear (sometimes called glaze), or mixed.Rime ice has a rough, milky white appearance, and generally follows the contours of the surface. Much of it can be removed by deice systems or prevented by anti-ice.Clear (or glaze) ice is sometimes clear and smooth, but usually contains some air pockets that result in a lumpy, translucent appearance. The larger the accretion, the less glaze ice conforms to the shape of the wing; the shape is often characterized by the presence of upper and lower “horns.” Clear ice is denser, harder, and more transparent than rime ice, and is generally hard to break.Mixed ice is a combination of rime and clear ice.Ice can distort the flow of air over the wing, diminishing the wing’s maximum lift, reducing the angle of attack for maximum lift, adversely affecting airplane handling qualities, and significantly increasing drag. Wind tunnel and flight tests have shown that frost, snow, and ice accumulations (on the leading edge or upper surface of the wing) no thicker or rougher than a piece of coarse sandpaper can reduce lift by 30 percent and increase drag up to 40 percent. Larger accretions can reduce lift even more and can increase drag by 80 percent or more. Even aircraft equipped for flight into icing conditions are significantly affected by ice accumulation on the unprotected areas. A NASA study (NASA TM83564) showed that close to 30 percent of the total drag associated with an ice encounter remained after all the protected surfaces are cleared. No protected surfaces may include antennas, flap hinges, control horns, fuselage frontal area, windshield wipers, wing struts, fixed landing gear, etc.Some unwary pilots have, unfortunately, been caught by surprise with a heavy coating of ice and no plan of action. Many pilots get a weather briefing and have little or no idea how to determine where icing may occur. However, pilots can learn enough basicmeteorology to understand where ice will probably be waiting after they get their weather briefing. The pilot can then formulate an ice-avoidance flight plan before ever leaving the ground.Ice can form on aircraft surfaces at 0 degrees Celsius (32 degrees Fahrenheit) or colder when liquid water is present. Even the best plans have some variables. Although it is fairly easy to predict where the large areas of icing potential exist, the accurate prediction of specific icing areas and altitudes poses more of a quandary. Mountains, bodies of water, wind, temperature, moisture, and atmospheric pressure all play ever changing roles in weather-making. All clouds are not alike. There are dry clouds and wet clouds. Dry clouds have relatively little moisture and, as a result, the potential for aircraft icing is low. North Dakota, because of its very cold winters, is often home to dry clouds. However, winter in the Appalachians in Pennsylvania and New York often brings a tremendous amount of moisture with the cold air and lots of wet clouds that, when temperatures are freezing or below, are loaded with ice. The Great Lakes are a great moisture source. The origin of a cold air mass is a key to how much super cooled water the clouds will carry. If the prevailing winds carry clouds over water, they will probably be wet. The chart above shows some of the areas of high icing potential. Heavy icing conditions may sometimes occur in the low-risk areas shown on the map above.Fronts and low-pressure areas are the biggest ice producers, but isolated air mass instability with plenty of moisture can generate enough ice in clouds to make light aircraft flight inadvisable.Freezing rain and drizzle are the ultimate enemy that can drastically roughen large surface areas or distort airfoil shapes and make flight extremely dangerous or impossible in a matter of a few minutes. Freezing rain occurs when precipitation from warmer air aloft fallsthrough a temperature inversion into below-freezing air underneath. The larger droplets may impact and freeze behind the area protected by surface deicers.Along a cold front, the cold air plows under the warm air, lifting it more rapidly and resulting in the formation of moist cumulus. Along a warm front, the warmer air tends to slide over the colder air, forming stratus clouds conducive to icing. As you approach the front, the clouds build quickly and the clear air between layers rapidly disappears.Freezing rain and freezing drizzle, including freezing drizzle aloft, are sometimes found in the vicinity of fronts. If you choose to fly through the front, be sure that it does not contain freezing rain or freezing drizzle and other hazardous weather conditions such as embedded thunderstorms. You should plan on flying the shortest route through the front instead of flying the length of the front.Structural IceHow quickly a surface collects ice depends in part on its shape. Thin, modern wings will be more critical with ice on them than thick, older wing sections. The tail surfaces of an airplane will normally ice up much faster than the wing. If the tail stalls due to ice and the airflow disruption it causes, recovery is unlikely at low altitudes. Several air carrier aircraft have been lost due to tail stalls. It also happens to ligh t aircraft but usually isn’t well documented.Since a tail stall is less familiar to many pilots, it is emphasized in this advisor, but a wing stall is the much more common threat, and it is very important to correctly distinguish between the two, since the required actions are roughly oppositeWing StallThe wing will ordinarily stall at a lower angle of attack, and thus a higher airspeed, when contaminated with ice. Even small amounts of ice will have an effect, and if the ice is rough, it can be a large effect. Thus an increase in approach speed is advisable if ice remains on the wings. How much of an increase depends on both the aircraft type and amount of ice. Consult your AFM or POH.Stall characteristics of an aircraft with ice-contaminated wings will be degraded, and serious roll control problems are not unusual. The ice accretion may be asymmetric between the two wings. Also, the outer part of a wing, which is ordinarily thinner and thus a better collector of ice, may stall first rather than last.Effects of Icing on Roll ControlIce on the wings forward of the ailerons can affect roll control. Wings on general aviation (GA) aircraft are designed so that stall starts near the root of the wing and progresses outward, so the stall does not interfere with roll control of the ailerons. However, the tips are usually thinner than the rest of the wing, so they are the part of the wing that most efficiently collects ice. This can lead to a partial stall of the wings at the tips which can affect the ailerons and thus roll control.If ice accumulates in a ridge aft of the deice boots but forward of the ailerons, this can affect the airflow and interfere with proper functioning of the ailerons. If aileron function is impaired due to ice, slight forward pressure on the elevator may help to reattach airflow to the aileron.。

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