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Flying qualities evaluation of a commuter aircraft with an ice-contaminated tailplane

机译:用冰污染的尾巴的飞行器的飞行素质评估

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During the NASA/FAA Tailplane Icing Program, pilot evaluations of aircraft flying qualities were conducted with various ice shapes attached to the horizontal tailplane of the NASA Twin Otter Icing Research Aircraft. Initially, only NASA pilots conducted these evaluations, assessing the differences in longitudinal flight characteristics between the baseline or clean aircraft, and the aircraft configured with an Ice-Contaminated Tailplane (ICT). Longitudinal tests included Constant Airspeed Flap Transitions, Constant Airspeed Thrust Transitions, zero-G Pushovers, Repeat Elevator Doublets, and, Simulated Approach and Go-Around tasks. Later in the program, guest pilots from government and industry were invited to fly the NASA Twin Otter configured with a single full- span artificial ice shape attached to the leading edge of the horizontal tailplane. This shape represented ice formed due to a "Failed Boot" condition, and was generated from tests in the Glenn Icing Research Tunnel on a full-scale tailplane model. Guest pilots performed longitudinal handling tests, similar to those conducted by the NASA pilots, to evaluate the ICT condition. In general, all pilots agreed that longitudinal flying qualities were degraded as flaps were lowered, and further degraded at high thrust settings. Repeat elevator doublets demonstrated reduced pitch damping effects due to ICT, which is a characteristic that results in degraded flying qualities. Pilots identified elevator control force reversals (CFR) in zero-G pushovers at a 20° flap setting, a characteristic that fails the FAR 25 no CFR certification requirement. However, when the same pilots used the Cooper-Harper rating scale to perform a simulated approach and go-around task at the 20° flap setting, they rated the airplane as having Level I and Level II flying qualities respectively. By comparison, the same task conducted at the 30° flap setting, resulted in Level II flying qualities for the approach portion, and Level III for the go-around portion. The results of this program indicate that safe and acceptable flying qualities with an ICT condition, can be effectively assessed by task-oriented pilot maneuvers. In addition, other maneuvers such as repeat elevator doublets provide good qualitative and quantitative assessments of pitch damping and elevator effectiveness, which are characteristics that correlate well with pilot task ratings. The results of this testing indicate that the FAR 25 zero-G pushover maneuver, which requires no CFR during its execution, may be an overly conservative pass/fail criteria for aircraft certification.
机译:在NASA / FAA Tailplane结冰程序期间,使用各种冰形状的飞机速度评估,附着在美国宇航局双獭冰工程研究飞机的水平尾翼上。最初,只有NASA飞行员进行了这些评估,评估了基线或清洁飞机之间的纵向飞行特性的差异,以及配置有冰污染的尾尾(ICT)的飞机。纵向测试包括恒定的空速翻转过渡,恒定的空速推力过渡,零G慢速推动,重复电梯双峰,以及模拟方法和远程任务。后来在该计划中,邀请了政府和行业的访客飞行员飞行NASA双输送系统,配置有一个完整的人工冰形,附着在水平尾翼的前缘。由于“启动失败”条件,该形状表示冰,并从全尺寸尾机模型上的Glenn结冰研究隧道中的测试生成。来宾飞行员进行了纵向处理测试,类似于美国宇航局飞行员进行的纵向处理测试,以评估ICT条件。一般而言,所有飞行员都同意,随着襟翼降低,并在高推力环境下进一步降解纵向速度速度。重复电梯双峰表明由于ICT引起的降低音调阻尼效应,这是导致劣化的燃烧品质的特征。飞行员在20°PLAP设置下识别电梯控制力逆转(CFR),以20°PLAP设置,这是一个特征,失败了远远超过CFR认证要求。然而,当相同的飞行员使用COOPOR-HARPER评级刻度来执行模拟方法并在20°翻盖设置时进行围绕任务,它们分别评定了飞机,分别具有级别I和II级等级等级。相比之下,在30°PLAP设置下进行的相同任务导致接近部分的II级飞行质量,以及用于远程部分的级别III。该计划的结果表明,可以通过面向任务导向的飞行员动作有效地评估具有ICT条件的安全和可接受的飞行品质。此外,诸如重复电梯双板的其他机动提供了对音调阻尼和电梯效力的良好定性和定量评估,这是与试点任务额定值相互作用的特性。该测试的结果表明,在执行期间不需要CFR的零型零浦的Pushover机构可能是飞机认证的过于保守的通过/失败标准。

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