METHOD AND SYSTEM FOR OPEN ROTOR ENGINE FUSELAGE PROTECTION

An aircraft 100 and method of operating the aircraft 100 are provided. The aircraft 100 includes a fuselage 102 including a nose 104, a tail 106, and a hollow, elongate body 108 extending therebetween, a wing 110 extending laterally away from the fuselage 102, the wing 110 including a leading edge 1...

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Bibliographische Detailangaben
Hauptverfasser:	RAMAKRISHNAN KISHORE, WOOD TREVOR HOWARD, BREEZE-STRINGFELLOW ANDREW, MILLER BRANDON WAYNE, GOERIG TREVOR WAYNE, PRENTICE IAN FRANCIS
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	An aircraft 100 and method of operating the aircraft 100 are provided. The aircraft 100 includes a fuselage 102 including a nose 104, a tail 106, and a hollow, elongate body 108 extending therebetween, a wing 110 extending laterally away from the fuselage 102, the wing 110 including a leading edge 114 in a direction 116 of motion of the aircraft 100 during normal flight and a trailing edge 118 on an opposing edge of the wing 110, and an engine 120 configured to drive a bladed rotatable member 122, the engine 120 coupled to at least one of the wing 110 and the fuselage 102. The aircraft 100 further includes at least one of a forward chine member 123 and an aft chine member 132 extending from the fuselage 102 at a point 124 forward of the engine 120 aftward to a point 128 aft of the bladed rotatable member 122. 提供种飞机(100)和运行飞机(100)的方法。飞机包括：机身(102)，其包括鼻部(104)、尾部(106)和在它们之间延伸的空心伸长本体(108)；沿侧向从机身延伸出的翼(110)，翼包括在正常飞行期间在飞机的运动方向(116)上的前缘(114)和在翼的相对的边缘上的后缘(118)；以及构造成驱动带叶片的可旋转部件(122)的发动机(120)，发动机联接到翼(110)和机身(102)中的至少个上。飞