会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 2. 发明申请
    • COUPLING PART STRUCTURE FOR VANE AND JET ENGINE INCLUDING THE SAME
    • 包括其中的叶轮和喷气发动机的联接部件结构
    • US20150132118A1
    • 2015-05-14
    • US14398360
    • 2014-10-31
    • IHI CORPORATIONIHI AEROSPACE CO., LTD
    • Takaomi INADAShinichi TANAKA
    • F01D25/00F01D25/24F01D9/02
    • F01D25/005F01D5/282F01D9/02F01D25/24F05D2230/644F05D2240/12F05D2260/31F05D2300/44F05D2300/603Y02T50/672Y02T50/673
    • A coupling support member including a pair of divided pieces is placed in a coupling part between a vane proximal end portion of a guide vane and an attachment flange, and the pair of divided pieces are joined to the vane proximal end portion from both the sides in the vane thickness direction. A groove is formed in one end portion joint surface of the coupling support member, a linear protrusion is formed on the other end portion joint surface, the vane proximal end portion is formed into a concavo-convex shape, a linear protrusion that is engaged with the groove which is formed in the end portion joint surface is formed on a joint surface to the one end portion joint surface, a groove that is engaged with the linear protrusion formed on the end portion joint surface is formed in the joint surface to the other end portion joint surface. The vane proximal end portion is held between the pair of divided pieces of the coupling support member, by the fastening force that is applied to the coupling support member from both the sides in the vane thickness direction. It is possible to obtain a high structural strength while contributing to a reduction in weight of a jet engine.
    • 包括一对分割片的联接支撑构件被放置在导向叶片的叶片近端部分和附接凸缘之间的联接部分中,并且一对分开的片从两侧分别接合到叶片近端部分 叶片厚度方向。 在联接支撑构件的一个端部接合表面中形成有一个槽,在另一个端部接合表面上形成一个直线突起,该叶片的基端部形成为一个凹凸的形状,一个与 形成在端部接合面的槽形成在与一端部接合面的接合面上,与端部接合面上形成的线状突起配合的槽形成在接合面上 端部接合面。 通过从叶片厚度方向的两侧施加到联接支撑构件的紧固力,叶片近端部分保持在联接支撑构件的一对分割片之间。 可以获得高结构强度,同时有助于减少喷气发动机的重量。