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Twin-jet and trijet aircraft: a study for an optimal design of regional aircraft

机译:双喷气和三喷气飞机:支线飞机的最佳设计研究

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Aircraft with three engines, as known as trijet became a standard design among manufacturers after 1964 when the FAA’s 60-minute rule was established for these aircraft. This regulation restricted the flight path to 60 minutes’ flying time to a suitable airport, therefore affecting the operation costs and limiting the range of twin-jet aircraft. However, improvements to the engine’s reliability in the following decades allowed ETOPS certification for twin-jet aircraft. The traditional trijet designs were slowly retired, the last commercial trijet flight was in 2014.The industry abandoned the trijet design as solution for commercial aviation; however, executive jets such as the Falcon 7x and Falcon 8x, certified in 2016, show that this configuration might still be advantageous for specific markets. The certification at one engine inoperative condition presents advantage for trijet aircraft reducing take-off thrust, since when one engine is inoperative, 75% of the installed thrust is available for the trijet aircraft, while this value is only 50% for a twin-jet aircraft. An initial study conducted showed a trend of lower thrust to weight ratio for trijet aircraft when compared to twin-jet aircraft, being particularly evident for MTOW (maximum take-off weight) lower than 75,000 lb. The aim of this work is to study the viability of a trijet aircraft configuration and potential advantages for a regional aviation scenario. The trijet configuration performance was evaluated and compared to twin-jet configuration in a multidisciplinary design environment considering disciplines such as aerodynamics, noise, performance, flight mechanic, weight, and structure. An aircraft with MTOW of 48,500 lb was studied and the results show that a reduction up to 9.4% of installed thrust might be achieved with the trijet design compared to twin-jet aircraft when the balanced field length is the critical constraint. However, flyover noise and structural weight might increase slightly in trijet design.
机译:1964年,FAA为这些飞机制定了60分钟规则后,具有三引擎的飞机(即称为trijet的飞机)成为制造商的标准设计。该规定将飞行路线限制在60分钟的飞行时间内,无法到达合适的机场,因此影响了运营成本并限制了双喷气飞机的航程。但是,在接下来的几十年中,发动机可靠性的提高使双喷气飞机获得了ETOPS认证。传统的三喷气机设计逐渐淘汰,上一次商业三喷气机飞行是在2014年。但是,2016年认证的猎鹰7x和猎鹰8x等公务机显示,这种配置可能仍对特定市场有利。一台发动机不工作状态下的认证为三喷射飞机降低了起飞推力提供了优势,因为当一台发动机不工作时,三喷射飞机可获得75%的安装推力,而双发飞机只有50%的推力。飞机。进行的初步研究表明,与双翼飞机相比,三翼飞机的推力重量比有降低的趋势,特别是对于MTOW(最大起飞重量)低于75,000磅的飞机而言,这一点尤为明显。 Trijet飞机配置的可行性以及区域航空场景的潜在优势。在多学科设计环境中,考虑了空气动力学,噪声,性能,飞行机械,重量和结构等学科,评估了Trijet构型的性能并将其与双喷气构型进行了比较。对一台MTOW为48,500磅的飞机进行了研究,结果表明,在平衡场长是关键约束的情况下,与双喷飞机相比,三喷设计可将安装推力降低多达9.4%。但是,在三喷射设计中,飞越噪声和结构重量可能会略有增加。

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