| 摘要 |
A distal end portion (21) and a proximal end portion (22) of a guide vane (20) formed from a composite material are respectively supported by connecting support bodies (30, 31) formed from a metal, and the connecting support bodies (30, 31) of the distal end portion (21) and the proximal end portion (22) are connected by a conductive wire (40) while the conductive wire (40) is passed through a space between a leading edge surface (20a) of the guide vane (20) and a sheath (23). In a turbofan jet engine, a lightning current due to a lightning strike can be fended off while a controlling function of a stator vane formed from a composite material is ensured, and an inspection is also easy. |
