融合式翼梢小翼由复合材料和钛金属制成，是一种翼尖气动装置，通过降低诱导阻力和翼尖涡流阻力来提高飞机的性能。机翼和翼梢小翼之间的圆滑弯曲过渡方式，被称为“融合式”过渡技术，已获得专利。 　　融合式翼梢小翼的应用，使飞机的气动效率得到改进、油耗降低、发动机维修 Made of composite materials and titanium, the fusion wingtip is a wingtip pneumatic device that increases aircraft performance by reducing induced drag and tip-wing vortex resistance. The sleek, curved transition between the wing and the wingtip, known as the “fusion” transitional technique, has been patented. The application of the integrated wingtip winglets improves the aerodynamic efficiency of the aircraft with reduced fuel consumption, engine maintenance